method of forming a joint joined by injection and structural set

专利摘要:
METHOD OF FORMING A JOINT UNITED BY INJECTION, AND, STRUCTURAL ASSEMBLY Method of forming a joint joined by injection (106) forming a chamber wall (212) within a region of joint line (300) between mating surfaces ( 192, 198) of a first part (190) and a second part (196), the chamber wall (212) dividing a length of the joining line (306) and defining at least one adhesive chamber (210), injecting a structural adhesive (370) into the adhesive chamber (210) through an injection port (312), and discharge excess adhesive (336) from the adhesive chamber (210) through a bleed hole (330).
公开号:BR112015019975B1
申请号:R112015019975-5
申请日:2014-02-04
公开日:2021-01-19
发明作者:John A. Woleader；Andrew R. Street
申请人:The Boeing Company；
IPC主号:

专利说明:

FIELD
[001] The present description generally refers to structural joints and, more particularly, to adhesively joined joints of relatively long length. FUNDAMENTALS
[002] Joined joints are typically formed by applying a layer of adhesive to the joining surfaces of one or more parts to be joined. The parts are then put together and held in position with respect to each other, while allowing the adhesive on the joining line to cure. For example, when attaching an end ring having a C-shaped cross section to an edge of a cylinder, the end ring can be oriented so that the C channel faces upwards. A concentration of adhesive can be installed inside the C channel and the cylinder edge can be lowered into the C channel. The adhesive can drain out of the C channel until the cylinder edge contacts the base of the C channel. The cylinder and end ring can be held in place while the adhesive cures.
[003] Unfortunately, the process noted above can produce less than desirable results on the final joint joined between the end ring and the cylinder. In this regard, the relatively long length of the joining line extending around the cylinder circumference can result in unpredictability with respect to the flow of adhesive in the C-channel when the cylinder is lowered into the end ring. For example, the long-length joining line can affect the ability of the adhesive to flow from the bottom of the C-channel to the top edge of the C-channel at all locations around the cylinder circumference when the cylinder edge is lowered in. of the channel in C.
[004] Such unpredictability in relation to the adhesive flow can result in reworking the jointed joint to bring the jointed joint within design tolerances. In cases where repair of the joint is not possible, it may be necessary to scrape the joined parts and assemble a replacement part, which can have a detrimental impact on cost and planning. The unpredictability associated with the flow of adhesive may also require the installation of anti-peeling fasteners along the joint line to prevent peeling of the joint joined at the edges of the joint line. Unfortunately, the installation of anti-stripping fasteners can add to the cost, complexity, and weight of the structural set.
[005] As can be seen, there is a need in the art for a system and method of forming a joined joint that provides a means to control the flow of adhesive within the joining line during the joining process. In this regard, there is a need in the art for a system and method of forming a joined joint that provides predictability with respect to the adhesive flow in long-length joining lines. SUMMARY
[006] The needs noted above, associated with joined joints, are specifically addressed and mitigated by the present description, which provides a method of forming a joint joined by injection. The method may include forming a chamber wall within a region of joining line between mating surfaces of a first part and a second part. The chamber wall can divide a length of joining line and defining at least one adhesive chamber. The method may additionally include injecting a structural adhesive into the adhesive chamber through an injection port, and discharging excess adhesive from the adhesive chamber through a bleed hole.
[007] In another embodiment, a method of forming a joint joined by injection is described, including the step of forming a series of chamber walls within a region of joint line between mating surfaces of a first and a second part part. The chamber walls can divide the length of the joining line in a plurality of adhesive chambers. The method may additionally include forming line dams along a part edge of at least one between the first part and the second part. Chamber walls, bonding dams, and mating surfaces can collectively enclose the adhesive chambers. The method may also include injecting a structural adhesive into the adhesive chambers through an injection orifice formed in one between the first part and the second part, discharging excess adhesive from the adhesive chambers through at least one bleed hole. , and collect the excess adhesive in adhesive reservoirs, fluidly coupled to the bleed holes.
[008] A structural set consisting of a first part and a second part is also described. The first part and the second part can have mating surfaces, which can be adhesively joined together over a joint line region having a joint line length. The structural assembly may include a series of chamber walls, formed along the length of the joining line and dividing the length of the joining line into a plurality of adhesive chambers. The structural assembly can include a structural adhesive injected into the adhesive chambers through at least one injection orifice to join the first part to the second part.
[009] In short, according to one aspect of the invention, a method (400) of forming a joint joined by injection (106) is provided, comprising the steps of: forming a chamber wall (212) within a region of bonding line (300) between mating surfaces (192, 198) of a first part (190) and a second part (196), the chamber wall (212) dividing a length of bonding line (306) and defining at least one adhesive chamber (210); injecting a structural adhesive (370) into the adhesive chamber (210) through an injection port (312); and discharge excess adhesive (336) from the adhesive chamber (210) through a bleed hole (330).
[0010] Advantageously, the method (400), wherein the step of forming the chamber wall (212) comprises: forming the chamber wall (212) from adhesive (214).
[0011] Advantageously, the method (400), wherein the step of forming the chamber wall (212) comprises: including a connecting wire (230) in the chamber wall (212).
[0012] Advantageously, the method (400), further comprising the step of: forming a dam of union line (314) along a part edge (194, 200) of at least one of the first part (190) and the second part (196); and the chamber wall (212), the union line dam (314), and the mating surfaces (192, 198) collectively enclosing the adhesive chamber (210).
[0013] Advantageously, the method (400), which additionally comprises the steps of: collecting the excess adhesive (336) in an adhesive reservoir (350), fluidly coupled to the bleed hole (330).
[0014] Advantageously, the method (400), which further comprises the step of: forming the adhesive reservoir (350) as one among a shelf (354) and a vertical column (352).
[0015] Advantageously, the method (400), wherein the length of the joining line (306) is at least twice the width of the joining line (308).
[0016] Advantageously, the method (400), in which the injection port (312) is formed in at least one of the first part (190) and the second part (196).
[0017] Advantageously, the method (400), in which the injection orifice (312) is positioned close to a chamber wall (212).
[0018] Advantageously, the method (400), in which the injection orifice (312) is positioned close to a lower edge (222) of the adhesive chamber (210).
[0019] Advantageously, the method (400), in which the bleed hole (330) is positioned close to an upper edge (220) of the adhesive chamber (210).
[0020] Advantageously, the method (400), in which the bleed hole (330) and the injection hole (312) are positioned at opposite ends of the chamber (218) of the adhesive chamber (210).
[0021] Advantageously, the method (400), in which: a large bleed hole (334) and a small bleed hole (332) are positioned at opposite ends of the chamber (218) of the adhesive chamber (210); and the injection port (312) being positioned close to a chamber end (218) having the small bleed hole (332).
[0022] Advantageously, the method (400), wherein the first part (190) comprises a cylinder (110), the second part (196) comprising an end ring (130) having a cross section (132) configured as a C-channel (134), the step of forming the chamber wall (212) comprising: affixing a series of connecting wires (230) along a cylinder edge (120) so that the connecting wires (230) divide the length of the joining line (306); covering the connecting threads (230) with adhesive (214); and inserting a cylinder edge (120) into the C-channel (134).
[0023] Advantageously, the method (400), wherein the first part (190) comprises a cylinder (110), the second part (196) comprising at least one of an inner ring (170) and an outer ring (172) , the step of forming the chamber wall (212) comprising: affixing a series of connecting wires (230) along a cylinder surface (114, 116); coat the connecting wire (230) with adhesive (214); and positioning at least one of the inner ring (170) and the outer ring (170, 172) in relation to the cylinder (110).
[0024] In accordance with another aspect of the invention, a method (400) of forming a joint joined by injection (106) is provided, comprising the steps of: forming a series of chamber walls (212) between mating surfaces (192 , 198) of a first part (190) and a second part (196), the chamber walls (212) dividing a length of joining line (306) in a plurality of adhesive chambers (210); form union line dams (314) along a part edge (194, 200) of at least one of the first part (190) and the second part (196), the chamber walls (212), the dams of joining line (314), and the mating surfaces (192, 198) collectively enclosing the adhesive chambers (210); injecting a structural adhesive (370) into the adhesive chambers (210) through an injection port (312) formed in at least one of the first part (190) and the second part (196); discharge excess adhesive (336) from the adhesive chambers (210) through at least one bleed hole (330); and collecting the excess adhesive (336) in adhesive reservoirs (350), fluidly coupled to the bleed holes (330).
[0025] In accordance with yet another aspect of the invention, a structural assembly (104) is provided, comprising: a first part (190) and a second part (196) having mating surfaces (192, 198) adhesively joined together along a seam line region (300) having a seam line length (306); a series of chamber walls (212) formed along the length of the bonding line (306) and dividing the length of the bonding line (306) into a plurality of adhesive chambers (210); and a structural adhesive (370) injected into the adhesive chambers (210) through at least one injection port (312).
[0026] Advantageously, the structural assembly (104), in which: the injection orifice (312) is formed in at least one of the first part (190) and the second part (196).
[0027] Advantageously, the structural assembly (104), in which: the chamber walls (212) are oriented generally transversal to the length of the connecting line (306).
[0028] Advantageously, the structural assembly (104) additionally comprises: a connecting wire (230) included with at least one of the chamber walls (212).
[0029] Advantageously, the structural assembly (104), in which: the joining thread (230) defines a joining line thickness (310) between the joining surfaces (192, 198).
[0030] Advantageously, the structural assembly (104), wherein: the structural adhesive (370) comprises an epoxy adhesive.
[0031] Advantageously, the structural assembly (104) additionally comprises: at least one mechanical fastener (388) which extends through the first part (190) and the second part (196) in the region of the joining line (300).
[0032] Advantageously, the structural assembly (104), in which: the first part (190) and the second part (196) define a region of flat, substantially rectilinear, line (300).
[0033] Advantageously, the structural assembly (104), wherein: the first part (190) comprises a cylinder (110) having a cylinder edge (120); the second part (196) comprising an end ring (130) having a cross section (132) configured as a C-channel (134); and the series of chamber walls (212) being distributed around a cylinder circumference (112) to form the plurality of adhesive chambers (210) joining the cylinder edge (120) to the C-channel (134).
[0034] Advantageously, the structural assembly (104), wherein: the first part (190) comprises a cylinder (110); the second part (196) comprising at least one of an inner ring (170) and an outer ring (172); and the series of chamber walls (212) being distributed around a cylinder circumference (112) to form the plurality of adhesive chambers (210) joining the cylinder (110) to at least one of the inner ring (170) and the outer ring (172).
[0035] Advantageously, the structural assembly (104), in which: the first part (190) is formed of fiber matrix material, reinforced with fiber, (124); and the second part (196) is formed of metallic material (162).
[0036] Advantageously, the structural assembly (104), wherein the length of the joining line (306) is at least twice the width of the joining line (308).
[0037] The characteristics, functions and advantages that have been discussed can be obtained independently in several modalities of the present description or can be combined in still other modalities, other details of which can be seen with reference to the following description and drawings below. BRIEF DESCRIPTION OF THE DRAWINGS
[0038] These and other characteristics of the present description will become more apparent in the reference to the drawings, in which the same numbers refer to the same parts throughout the description, and in which: Figure 1 is a cross-sectional illustration of a spacecraft encapsulated within a launch vehicle; figure 2 is a perspective illustration of an embodiment of a structural assembly to support the spacecraft of figure 1 and comprising a structural cylinder having an inner ring, an outer ring, and a pair of end rings with channel-shaped cross sections in C, joined to a structural cylinder; figure 3 is an illustration of the cross section of the end ring taken along the line 3 of figure 2 and illustrating the joint joined between the C-shaped cross section and the cylinder edge of the cylinder; Figure 4 is a schematic of a flat pattern of the joint joined between the mating surfaces of the end ring and the cylinder and illustrating the relatively long length of the joining line in the joining line region; Figure 5 is a schematic illustration in exploded perspective of a portion of a joined joint embodiment and illustrating a pair of joining wires that can be mounted against the cylinder edge, prior to insertion of the cylinder edge into the C-channel; figure 6 is a schematic perspective view of the joined joint of figure 5 showing a pair of shims temporarily installed on opposite sides of the joining wires to assist in the formation of the chamber walls dividing the length of the joining line; figure 7 is a schematic perspective view of the joint joint of figure 6 showing a joint line dam, installed along a channel edge of the C channel and further illustrating bleeding holes formed as openings in the union line dam ; figure 8 is a schematic perspective view of the joined joint of figure 7 showing an embodiment of an adhesive reservoir configured as a shelf and positioned along the channel edge; figure 9 is a schematic perspective view of the joined joint of figure 7 showing adhesive reservoirs configured as vertical columns, fluidly coupled to the bleed holes; figure 10 is a schematic side illustration of the joined joint of figure 9 in one embodiment having a large bleed hole and a small bleed hole, positioned on opposite sides of the chamber walls; figure 11 is a schematic side illustration of the joint joined in figure 10 and showing the injection of structural adhesive into the adhesive chamber defined by the chamber walls and illustrating the flow direction of the structural adhesive and air bubbles within the adhesive chamber; figure 12 is a schematic side illustration of the joint joint in figure 11 and showing the flow of structural adhesive and air bubbles in the direction to the large bleed hole and the discharge of excess adhesive resin through the small bleed hole and to inside the adhesive reservoir; figure 13 is a cross-sectional illustration of the joined joint, taken along line 13 of figure 12 and showing the direction of flow of structural adhesive through interstices between the cylinder edge and the C-channel; figure 14 is a schematic side illustration of the joint joined in figure 11 and showing the adhesive chamber in a state filled with excess adhesive, contained in the adhesive reservoirs on opposite sides of the central adhesive chamber; figure 15 is a schematic side illustration of the joint joined in figure 14 and showing the injection of the structural adhesive in the plurality of adhesive chambers; figure 16 is a cross-sectional illustration of the joined joint, taken along line 16 of figure 15 and illustrating a plug to plug the injection orifice after filling the adhesive chamber with structural adhesive; figure 17 is a schematic side illustration of the joint joined in figure 15 and showing each of the adhesive chambers filled with structural adhesive and still showing excess adhesive contained within the adhesive reservoirs; figure 18 is a schematic side illustration of the joined joint of figure 17 in a final state, following the removal of the adhesive reservoirs and bonding line dams, and further illustrating the optional installation of mechanical fasteners through each of the chambers adhesive; figure 19 is a cross-sectional illustration of the structural cylinder, taken along line 19 of figure 2 and illustrating an embodiment of a joint joined between an outer ring and the cylinder; figure 20 is a schematic of a flat pattern of the joint joint of figure 19 illustrating the injection of structural adhesive into an injection orifice positioned in an approximate geometric center of the adhesive chamber; figure 21 is a cross-sectional illustration of the joined joint, taken along line 21 of figure 20 and illustrating the injection of structural adhesive into the adhesive chamber; figure 22 is a schematic side illustration of the joined joint of figure 20 in a final state, following the removal of the adhesive reservoirs and the connecting line dams, and still illustrating the optional installation of mechanical fasteners through each of the chambers adhesive; figure 23 is an illustration of a flow chart of a method of forming a joint joined by injection; figure 24 is a block diagram of a joined joint; figure 25 is a flow chart illustrating an aircraft manufacturing and service methodology; and figure 26 is a block diagram of an aircraft. DETAILED DESCRIPTION
[0039] Referring now to the drawings, in which those shown are for purposes of illustrating preferred embodiments and various description modalities, shown in figure 1 is a sectional illustration of spacecraft 102, encapsulated within a launch vehicle 100. Spacecraft 102 can be supported on a central core structural assembly 104 having a cylindrical configuration and extending vertically through the center of spacecraft 102.
[0040] Figure 2 illustrates a modality of cylindrical structural assembly 104. Structural assembly 104 may include a cylinder 110 which may be formed of fiber-reinforced polymer matrix material 124, although cylinder 110 may be formed of material metallic (not shown) or a combination of composite material and metallic material and / or other materials. Structural assembly 104 may additionally include one or more rings 130, 170, 172, which can be joined to cylinder 110 to increase the resistance of cylinder 110 and / or accommodate localized loads and / or interface loads in locations where cylinder 110 it is attached to conjugation components (not shown), such as an interface (not shown) between launch vehicle 100 (figure 1) and spacecraft 102 (figure 1). In the embodiment shown, the rings may include an inner ring 170, an outer ring 172, and a pair of end rings 130.
[0041] Advantageously, in figure 2, rings 130, 170, 172 are adhesively joined to cylinder 110 using an injection joining method, described here, which provides a means for joining rings 130, 170, 172 to cylinder 110 with a significant increase in the quality and consistency of joined joints 106 over conventionally joined joints. The injection joining method, described herein, advantageously includes adhesive chambers 210, formed in a region of joining line 300 between the mating surfaces 192, 194 of the mating parts. Adhesive chambers 210 can be provided by constructing a series of chamber walls 212 within the joining line region 300. Chamber walls 212 can be spaced from each other along the length of joining line 306 to fragment the junction line length 306 in defined small adhesive chambers 210. Chamber walls 212 can be spaced from each other at substantially equal spacing 224 from each other, or chamber walls 212 can be spaced from each other in uneven spaces (not shown). Structural adhesive 370 can be injected into each of the adhesive chambers 210 in a controlled manner and structural adhesive 370 can be allowed to cure.
[0042] As described in greater detail below, in Figure 2, by fragmenting the length of the joining line 306 and controlling the flow of structural adhesive 370 within the small defined segment of each adhesive chamber 210, structural adhesive 370 can fill each adhesive chamber 210 by rising to the top (not shown) of adhesive chamber 210 and remaining there until a substantial totality of adhesive chamber 210 is filled with structural adhesive 370. In this way, the potential for empty spaces to occur (not shown) or air bubbles (not shown) along the perimeter of bond line 302, such as along the upper edge (not shown) of the adhesive chamber 210, can be significantly reduced or eliminated. Reduction or elimination of empty spaces (not shown) and air bubbles (not shown) in high voltage locations (not shown) along the perimeter of the 302 seam line (figure 3) can result in an increase in total strength and durability of the joint joint 106 in relation to the conventionally joined joints.
[0043] In figure 2, the joining method is specifically advantageous for geometric features of relatively long length 108, which can be characterized as regions of the joining line 300 having a long joining line length 306 in relation to the joining line width. joint 308. For example, in the context of cylindrical structural assembly 104, shown in figure 2, the feature of relatively long geometry 108 can be represented by the long distance around cylinder circumference 112 in relation to the small width of the joint line 308. Advantageously, a joining method, currently described, allows the elimination of screws (not shown) or other mechanical fasteners in cylindrical joint joints 106, which provides significant advantages over conventionally joined joints (not shown) in cylindrical structures that require fasteners mechanical (not shown) to obtain the required strength and durability in such conventional joints internationally united. In this regard, the method currently described provides a means for forming joint joints 106, of high strength, of high durability, in cylindrical structural assemblies 104 without mechanical fasteners and resulting in significant weight savings compared to conventional mechanically fixed / joined cylindrical joints .
[0044] In figure 2, the adhesive chambers 210 can provide additionally high flexibility with respect to the amount of time available to complete the joint seal 106 within the time of use after preparation of the structural adhesive 370. For example, in one embodiment, a portion of the adhesive chambers 210 in a joint line region 300 can be filled with structural adhesive 370 and allowed to cure. The remaining portions of the adhesive chambers 210 of the splicing line can then be filled and allowed to cure during one or more subsequent splicing operations. In the context of cylindrical structural assembly 104, shown in figure 2, the effect of the injection joint method, described here, is an elimination of the mass penalty otherwise associated with affixing rings 130, 170, 172 to cylinder 110 using mechanical fasteners (not shown). The elimination of the mass penalty translates into a reduction in the structural mass of the spacecraft 102. The reduction in the structural mass in the aircraft 102 may allow an increase in the amount of fuel (not shown) carried by the spacecraft to the attitude control system (no shown), which can result in an increase in spacecraft 102 operational life.
[0045] Although the joining method, described here, is described in the context of a cylindrical structural assembly 104 (figure 2) for spacecraft 102 (figure 1), the joining method can be implemented in any of a variety of applications different and in any of a variety of different industries. For example, the joining method can be implemented in commercial, civil and military applications. In addition, the joining method can be incorporated into a wide variety of platforms including, but not limited to marine, automotive, aeronautical and / or space platforms. In this regard, the joining method can be incorporated into any vehicle system or non-vehicle system, without limitation.
[0046] In figure 3, there is shown a cross-sectional illustration of an embodiment of a joint 106 between a first part 190 and a second part 196 having joining surfaces 192, 198 adhesively joined together. In figure 3, the first part 190 comprises a cylinder 110 and the second part 196 comprises an end ring 130 having a cross section 132 configured as a C-channel 134. The cylinder 110 has an outer surface of cylinder 116 and an inner surface cylinder 114 defining a cylinder thickness 118. In addition, cylinder 110 has a cylinder edge 120, which can be adhesively joined within the C-channel 134. End ring 130 may include base 136 and a pair of flanges 138 defining the channel cross section at C 134 132. One or both channel edges 144 may include a beveled edge 146 to minimize stress concentrations in cylinder 110 at the location of channel edges 144. End ring 130 may have a channel depth 142 corresponding to the joining line width 308 and extending from the lower channel surface 152 to the channel edge 144. The distance between the lateral channel surfaces (i.e., the su channel side inner surface 148 and channel side outer surface 150) can define a channel width 140.
[0047] In figure 3, cylinder 110 can be positioned within the C 134 channel so that the interstice 160 between the outer surface of cylinder 116 and the outer lateral surface of channel 148 is substantially equalized with the interstice 158 between the surface. inner cylinder 114 and inner side channel surface 148. In addition, cylinder 110 can be positioned vertically with respect to end ring 130 so that the interstice 156 between the lower channel surface 152 and the cylinder edge surface 122 is substantially equalized with the interstices 158, 160 between the cylinder 110 and the flanges 138. The joining process can include a means for maintaining the position of the cylinder 110 with respect to the end ring 130 so that the desired interstices 156, 158 , 160 are fixed (i.e., do not change) during injection of structural adhesive 370 into adhesive chambers 210 (figure 2) and during curing of structural adhesive 370.
[0048] In figure 4, a schematic of the flat pattern of the joint gasket 106 between the end ring 130 and the cylinder 110 of figure 3 is shown. Figure 4 illustrates the relatively long joining line length 306 of the region of junction line 300 between end ring 130 and cylinder edge 120. In one embodiment, the long-length geometry feature 108 can be defined as a junction line length 306, which is at least approximately twice the width of seam line 308 of joint seam 106. However, the length of seam line 306 may be less than the width of seam line 308.
[0049] In Figure 4, the joint gasket 106 advantageously includes a series of chamber walls 212, spaced from each other along the length of the joining line 306 and dividing the length of the joining line 306 in a plurality of adhesive chambers 210. In the embodiment shown, the chamber walls 212 are generally oriented transversely to the length of the joining line 306. In this respect, the chamber walls 212 can extend across the width of the joining line 308 between opposite edges of the joining line. 304 of the junction line region 300. The chamber walls 212 can be oriented in a non-parallel relationship to the junction line length 306. For example, one or more of the chamber walls 212 can be oriented generally perpendicular to the junction line length. connection 306, although the chamber walls 212 can be oriented in any direction in relation to the length of connection line 306 and are not limited to a perpendicular orientation. In addition, although each of the chamber walls 212 is shown to be generally rectilinear in shape, the chamber walls 212 can be formed in any size, shape, and configuration, without limitation. For example, chamber walls 212 can be curved or provided in other shapes or configurations.
[0050] As described in more detail below, in figure 4, each of the adhesive chambers 210 can be filled with structural adhesive 370 to join the mating surfaces 192, 198 of the first part 190 (e.g. cylinder 110) and of the second part 196 (for example, the end ring 130). A structural adhesive can be selected, which is compatible with the material of the first part 190 and the material of the second part 196. As indicated above, the first part 190 can be formed of a material, which is different from the material of the second part 196. For example, the first part 190 may comprise cylinder 110, which may be formed of fiber-reinforced polymer matrix material 124, such as a carbon fiber / epoxy matrix material. The second part 196 can comprise the end ring 130, which can be formed of metallic material 162, such as aluminum. However, the first part 190 and the second part 196 can be formed from any material, and can be of any shape, size, and configuration, without limitation.
[0051] In figure 4, structural adhesive 370 can be injected into each of the adhesive chambers 210 through at least one injection hole 312. In one embodiment, one or more injection holes 312 can be formed in the first part 190 and / or in the second part 196. However, injection holes 312 can be formed at any location that allows the injection of structural adhesive 370 into the adhesive chambers 210. For example, although not shown, one or more injection holes 312 can be positioned close to, or formed on, the edges of part 194, 200.
[0052] With reference to the flowchart of figure 23, with additional reference to figures 5-22, the method 400 of forming a joined joint 106 (figure 4) will now be described. In the context of joining the rear end ring 130 (figure 5) to the cylinder 110 (figure 5), the end ring 130 can initially be dry adjusted to the cylinder 110, without structural adhesive 370 (figure 4) before starting the process of union. The dry fit may comprise positioning the end ring 130 so that the C 134 channel (figure 5) faces upwards, and then lower the cylinder 110 into the C 134 channel to check and equalize the interstices 158, 160 ( figure 3) between the internal and external lateral surfaces of channel 148, 150 (figure 3) and the internal and external surfaces of cylinder 114,116 (figure 3) around the circumference of cylinder 112 (figure 2), and adjust the interstices 156 ( figure 3) between the lower channel surface 152 (figure 3) and the cylinder edge surface 122 (figure 3). Pins (not shown) can be installed to fix the relative position of the cylinder 110 and end ring 130. The interstices 156, 158, 160 can be measured and recorded to establish the thickness of the joining line 310 (figure 3) between the mating surfaces of cylinder 110 and end ring 130. Once the interstices 156, 158, 160 are equalized or adjusted, the pins (not shown) can be removed and cylinder 110 can be separated from end ring 130 to allow the mating surfaces to be cleaned, such as by cleaning with a solvent swab in preparation for joining. Unattached surfaces (not shown) of cylinder 110 and / or end ring 130 can be covered with adhesive tape (not shown) or other material to protect against contact with structural adhesive 370 (figure 3) during the process of union.
[0053] With reference to figure 5, step 402 of method 400 (figure 23) may include forming chamber walls 212 at predetermined spacing 224 (figure 4) from one another along the length of the joining line 306 (figure 4) . In one embodiment, the chamber walls 212 can be positioned so that each adhesive chamber 210 has a chamber length 216 (figure 4), which is greater than the chamber width 217 (figure 4). Chamber walls 212 can be formed using an adhesive 214, which can be applied to a bonding wire 230. The bonding wire coated with adhesive 230 can then be mounted on the first part 190 (for example, cylinder 110) before connecting the first part 190 (for example, the cylinder 110) to the second part 196 (for example, the end ring 130). However, the present description contemplates applying adhesive 214 to the first part (for example, the cylinder 110) without a connecting wire 230. Alternatively, the adhesive 214 can be applied to the second part 196 (for example, the end ring 130) in place of the first part 190 to form the chamber walls 212. The method may include forming the chamber walls 212 generally transverse to the length of the joining line 306 (figure 4). The chamber walls 212 can be oriented in a non-parallel relation to the connecting line length 306, just as in the perpendicular orientation to the connecting line length 306. However, the chamber walls 212 can be formed in any configuration or format that divides the length of the connecting line 306, as indicated above.
[0054] In figure 5, step 404 of method 400 (figure 23) may comprise including a connecting thread 230 in one or more of the chamber walls 212. The connecting threads 230 can adjust the interstice 154 (figure 3) or the thickness of the joining line 310 (figure 3) between the mating surfaces 192, 198 and can assist as a barrier to the adhesive chamber 210. The method may include selecting a wire diameter 234 based on the desired interstice 154 or thickness line 310 between the mating surfaces. If the connecting wires 230 are not available in a wire diameter 234 that corresponds to the gap size 154, then a wire diameter 234 can be selected, which is slightly smaller than the gap size 154, and shims 238 (figure 6 ) can be used to assist in the formation of the desired interstice 154 (figure 3) between the mating surfaces 192, 198, as described below. In addition, the shim 238 can facilitate sealing the adhesive wall chamber 212 214 to the mating surfaces 192, 198, and forming the sides of the chamber walls 212.
[0055] In figure 5, each of the connecting wires 230 can be preformed in a desired shape, such as in a U shape, to adapt to the cylinder edge 120 and so that the connecting wire 230 has free ends 232, which will extend upward beyond the channel edge 144, when cylinder 110 is installed in the C 134 channel. Bonding wires 230 can be cleaned, such as by solvent cleaning, and adhesive 214 can be cleaned applied to the connecting wires 230, such as by using a syringe (not shown). The method may include coating the bonding wires 230 with adhesive 214, without preferably showing bare wire. The adhesive 214 can be provided in a relatively high viscosity, such as a paste-like viscosity, so that the adhesive 214 is held on the joining threads 230. The joining threads 230 can be positioned against the surface of the first part 190 (i.e., the cylinder 110) at predetermined spacings 224 (figure 4) from one another so that the connecting threads 230 divide the length of the connecting line 306 (figure 4). The method may include taping the free ends 232 of the connecting wires 230 to the inner and outer surfaces of cylinder 114, 116 with tape 236.
[0056] In Figure 6, the method may include installing cylinder 110 (ie, first part 190) with end ring 130 (i.e., second part 196) by inserting cylinder edge 120 into the C channel 134. The process of installing the connecting wires 230, installing the adhesive 214, and assembling the cylinder 110 with the end ring 130, and forming or finishing the chamber walls 214 is preferably completed within the time of use after preparing the adhesive 214. The free ends 232 of each tie wire 230 can be held in position using tape 236, as shown. The cylinder 110 can be secured in position using pins (not shown) to secure the cylinder 110 and the end ring 130 in the same position determined during the dry adjustment process.
[0057] In figure 6, the method may include temporarily inserting a pair of shims 238 into the region of the joining line 300 between the cylinder 110 and the flanges 138 of the end ring 130. The shims 238 can be manufactured in a thickness of chock, which corresponds to the size of the interstice 154 (figure 3) or the measurements of the thickness of the joining line 310 (figure 3) from the dry adjustment process. The bonding wires 230 can be provided in a wire diameter 234, which substantially corresponds to the desired interstice 154 between the bonding surfaces 192, 198, so that the bonding wires adjust the thickness of the bonding line 310 (figure 3) between the mating surfaces 192, 198. If the connecting wires 230 are not available in a wire diameter 234 that corresponds to the interstice size 154, then the nearest smaller wire diameter can be used on the chamber walls and the shims 238 can be used to adjust the interstice size 154 between the mating surfaces 192, 198. Shims 238 can be formed of any material including any metallic or non-metallic material and can be covered or wrapped with a silicone material (not shown) ), such as TeflonTM tape (not shown) or other material that facilitates the separation of the shims 238 from the chamber walls 212 after the adhesive 214 has cured.
[0058] As shown in figure 6, the shims 238 can be positioned on opposite sides of each joining wire 230 at an initial spacing from each other. The method may include moving the shims 238 towards each other for a final spacing, where the shim edges 240 can compact the adhesive 214 of the chamber wall 212 to seal the adhesive 214 to the mating surfaces 192, 198 and remove the empty spaces from the adhesive 214. In addition, the shims 238 can provide a defined edge (for example, straight) to the chamber wall 212. The shims 238 can be moved towards each other so that the edges shims 240 are generally parallel to each other and spaced from each other by a distance corresponding to the desired width of the chamber walls 212. For example, the shims 238 can be moved towards each other in the spacing of approximately 0.64 cm ( 0.25 inch) or other spacing distances. In an alternative embodiment, the chamber walls 212 can be formed without joining threads 230 by inserting shims 238 in the joint line region 300 and then injecting adhesive 214 into a mold space (not shown), defined by the spacing between the shim edges 240. Regardless of the way in which the chamber walls 212 are formed, the adhesive 214 on the chamber walls 212 may be allowed to cure before the removal of the shims 238 and before the injection of structural adhesive 370 (figure 3 ) inside the adhesive chamber 210.
[0059] In figure 6, the connecting wires 230 can be formed of any material and are not limited to being formed of metallic wire. In addition, a chamber wall 212 can be formed without the use of adhesive 214. For example, a chamber wall 212 can be configured as a mechanical device (not shown), which can be fixedly positioned across the width of the joining line. 308 in a manner that provides substantial sealing with respect to an adhesive chamber 210. In another embodiment, as indicated above, the connecting wires 230 can be omitted from the chamber walls 212 and adhesive 214 can be applied directly to the outer edge of cylinder 120 before lowering cylinder 110 into the C-channel 134. Shims 238 can be positioned on opposite sides of adhesive 214 and moved towards each other to form adhesive 214 on chamber walls 212. The shims 238 can be removed prior to joining by injecting structural adhesive 370 (figure 3) into the adhesive chambers 210.
[0060] In figure 7, step 406 of method 400 (figure 23) may comprise forming one or more junction line dams 314 along one or more junction line edges 304 of the junction line region 300. One or more of bond line dams 314 can be formed of a relatively high viscosity adhesive 316 or other material that has the ability to adhere to cylinder 110 and end ring 130 and remains in position during the bonding process and resists pressure of structural adhesive 370 (figure 3) during its injection into adhesive chamber 210. In one embodiment, bonding line dams 314 can be formed from adhesive 316 having a higher viscosity than the viscosity of structural adhesive 370 , which is injected into the adhesive chamber 210. The junction line dams 314 can be formed along an edge of part 194, 200 of the first part 190 (for example, the cylinder 110) and / or the second part 196 (e.g., ext ring 130) being joined together.
[0061] In figure 7, the union line dams 314 can be formed along the upper channel edges144 of the end ring 130 on both sides of the cylinder 110. One or more of the union line dams 314 can terminate the a spaced distance from the chamber walls 212 to form a bleed hole 330 for the discharge of excess adhesive 336 (figure 12) from the adhesive chamber 210. In one embodiment, each bleed hole 330 can be positioned close by to an upper edge 220 of the adhesive chamber 210. In addition, each bleed hole 330 can be positioned close to a chamber wall 212. The positioning of the bleed holes 330 along the upper edge 220 of the adhesive chamber 210 and near the chamber walls 212 can facilitate the evacuation of air bubbles 382 (figure 11) from the adhesive chamber 210 during the injection of structural adhesive 370 (figure 11). However, the bleed holes 330 can be positioned in any position in the adhesive chamber 210. In one embodiment, one or more of the adhesive chambers 210 may include a large bleed hole 334 and a small bleed hole 332, positioned at the ends. opposite chamber 218 from adhesive chamber 210. The large bleed hole 334 and the small bleed hole 332 can be formed in any size without limitation. As described in more detail below, the arrangement of the large bleed hole 334 and the small bleed hole 332 can facilitate the evacuation of air bubbles 382 from the adhesive chamber 210.
[0062] In figure 7, the configuration of the union line dam 314 and the bleed holes 330 on the inner cylinder surface (not shown) can be similar to the configuration of the union line dam 314 and the bleed holes 330 on the inner surface. outer surface of cylinder 116. However, the configuration of the union line dam 314 and the bleed holes 330 on each side of the cylinder 110 may be different. Bond line dams 314 and chamber walls 212 can define at least a portion of bond line perimeter 302. Chamber walls 212, bond line dams 314, and bond surfaces 192, 198 can collectively enclose adhesive chambers 210. Bond line dams 314 can be formed from adhesive 316, such as by using a syringe (not shown). The method may include allowing adhesive 316 from bond line dam 314 to cure prior to injection of structural adhesive 370 (figure 11) into adhesive chamber 210. Although bond line dams 314 are described as being formed from adhesive 316, it is contemplated that the connecting line dams 314 may comprise a mechanical device (not shown), such as a rigid element, which can be mechanically coupled or otherwise affixed to the first part 190 and / or the second part 196 to the along the perimeter of junction line 302.
[0063] In figure 8, the method may include forming one or more reservoirs of adhesive 350 to collect excess adhesive 336 (figure 12), which can be discharged from the bleed holes 330 during injection of structural adhesive 370 (figure 12) inside the adhesive chambers 210. In one embodiment, one or more of the adhesive reservoirs 350 can be formed as a shelf 354, which extends laterally out of the cylinder 110 and / or from the end ring 130. The adhesive reservoirs 350 can collect excess adhesive (not shown), which can seep out as a concentration on shelf 354 during the discharge of excess adhesive 336 from bleed holes 330. shelf 354 can be configured to collect excess adhesive 336 and / or to prevent excess adhesive 336 from flowing over the exterior of structural assembly 104. Shelf 354 may be formed of non-silicone material, such as tape or polymeric veneer and / or chromate tape or other material, which can be applied to end ring 130 and / or cylinder 110. In one embodiment, each adhesive chamber 210 can include a dedicated shelf 354, which can be physically separated from the dedicated shelf 354 of the adjacent adhesive chamber 210, so that each shelf 354 contains excess adhesive 336 discharged from the corresponding adhesive chamber 210.
[0064] In figure 9, one or more of the adhesive reservoirs 350 can be formed as a vertical tube or vertical column 352, which can be fluidly coupled to a bleed hole 330. In one embodiment, each of the vertical columns 352 can be securely affixed to the cylinder 110, such as by using adhesive tape (not shown). In one embodiment, vertical columns 352 can be formed of polymeric material, not silicone, (not shown), to avoid contamination of structural adhesive 370 (figure 12). The material to form the vertical columns 352 can be at least transparent material 356, partially transparent, to facilitate the observation of the excess adhesive flow 336 (figure 12) into the vertical columns 352 during the discharge of the same from the borehole. bleed 330.
[0065] Figure 10 illustrates a large bleed hole 334 and a small bleed hole 332, positioned at opposite ends of chamber 218 of each adhesive chamber 210. In one embodiment, the large bleed hole 334 can have a width in range from approximately 0.30 to 2.54 cm (0.12 to 1.0 inch) or greater. For example, the large bleed hole can be approximately 1.27 cm (0.50 inch) in length. The small bleed hole 332 can have a width in the range of approximately 1.57 to 127 cm (0.12 to 50 inches) in length or longer. For example, the small bleed hole 332 can be approximately 0.64 cm (0.25 inch) in length. Each bleed hole 332, 334 can be positioned close to a chamber wall 212. In addition, each bleed hole 332, 334 can be formed along a junction dam 314 or at a terminal end of a dam. joining line 314 along the upper channel edge 144 of end ring 130.
[0066] In the embodiment shown in figure 10, an injection orifice 312 can be positioned close to the end of chamber 218, where the small bleed hole 332 can be positioned. The injection port 312 can be positioned close to the lower edge 222 of the adhesive chamber 210, as well as along the lower surface of the channel 152 (figure 9). As described below, by positioning the injection hole 312 at the chamber end 218 having the small bleed hole 332, air bubbles 382 within the adhesive chamber 210 can initially evacuate through the small bleed hole 332 and the large bleed hole. 334 when structural adhesive 370 (figure 11) is initially injected into the adhesive chamber 210. After structural adhesive 370 begins to be discharged through the small bleed hole 332, air bubbles 382 (figure 11) can continue to be evacuated from the large bleed hole 334. In this respect, by positioning the injection hole 312 close to the chamber end 218 having the small bleed hole 332, air bubbles 382 can be evacuated over a substantial total length of chamber 216 from one end of chamber 218 to an opposite end of chamber 218 and which may result in a reduced propensity to prevent the formation or entrapment of bol ha of air 382 (figure 11) along the perimeter of the upper union line 302.
[0067] With reference to figure 11, step 408 of method 400 (figure 23) may include injecting structural adhesive 370 into the adhesive chamber 210. Figure 11 illustrates the flow direction 380 of structural adhesive 370 and the bubbles of air 382 inside the adhesive chamber 210. The structural adhesive 370 can be injected by means of an injection pressure 372 using an injection device 374, such as a sealing cannon or adhesive cannon or similar device coupled to a pressure source air 378, as with an air hose 376. Structural adhesive 370 can be injected into adhesive chamber 210 at an injection pressure 372 of approximately 0.344 to 68.95 N / cm2 (0.5 to 100 pounds) per square inch (psi)) or higher. For example, structural adhesive 370 can be injected at an injection pressure 372 of between approximately 13.79 to 68.95 N / cm2 (20 to 100 pounds per square inch (psi)), such as approximately 34.47 N / cm2 (50 psi). The selection of the injection pressure 372 can be dependent on several parameters including, but not limited to, the thickness of the joining line 310 (figure 3), the cross-section configuration of the joint joint 106, as well as the cross-section configuration of the channel in C 134 (figure 13) versus a straight-line cross-section configuration (figure 21), viscosity and temperature of structural adhesive 370, geometry and dimensions of adhesive chamber 210, including chamber length 216, chamber width 217, thickness of joining line 310, and other parameters.
[0068] In figure 11, in one embodiment, the structural adhesive 370 may initially comprise a liquid or semi-liquid material, configured to be injected into the adhesive chambers 210. The structural adhesive 370 may comprise a one-part adhesive or an adhesive. multiple parts. In one embodiment, structural adhesive 370 may comprise epoxy adhesive. The adhesive composition can be selected based on the material composition of the conjugation parts. Structural adhesive 370 can have a viscosity that facilitates injection into the adhesive chambers 210. Viscosity can be selected based on the thickness of the joining line 310 (figure 3) so that structural adhesive 370 flows through the interstices 156, 158, 160 (figure 3) between the mating surfaces 192, 198 (figure 3) to substantially fill the adhesive chamber 210 in a manner that promotes the evacuation of air bubbles 382 and that minimizes or eliminates the formation of voids. In one embodiment, structural adhesive 370 may comprise a thixotropic material having an initially low viscosity to facilitate the flow of structural adhesive 370 into the adhesive chamber 210 and through the relatively narrow thickness of the line 310 of the adhesive chamber 210. Then Upon injection, structural adhesive 370 may increase in viscosity or thickening over time, such as after adhesive chambers 210 are filled and capped and / or during curing of structural adhesive 370.
[0069] In figure 12, step 410 of method 400 (figure 23) may include evacuating air bubbles 382 from the adhesive chamber 210 through one or more of the bleed holes 330, which can be fluidly coupled to the chamber adhesive 210. In figure 12, adhesive chamber 210 is shown approaching a filled state 384 (figure 17) and illustrating the flow of structural adhesive 370 and air bubbles 382 in the direction of the large bleed hole 334. In Figure 12, by positioning the injection hole 312 close to a lower edge 222 of the adhesive chamber 210, air bubbles 382 will advantageously migrate upwards towards the bleed holes 330. For the modalities that have a small bleed hole 332 and a large bleed hole 334, the injection hole 312 can advantageously be positioned under the small bleed hole 332, which can promote the evacuation of air bubbles 382 along the flow direction 380 from an end of camera 218 for one and opposite end of chamber 218 due to the tendency for air bubbles 382 to move along the path of least resistance presented by the large bleed hole 334.
[0070] In figure 12, step 412 of method 400 (figure 23) may include unloading excess adhesive 336 through one or more of the bleed holes 330. Figure 12 shows the discharge of excess adhesive 336 through the small hole bleed 332 and into the adhesive reservoir 350 during injection of structural adhesive 370 into the adhesive chamber 210. Excess adhesive discharge 336 can occur simultaneously with the evacuation of air bubbles 382 from the adhesive chamber 210 As noted above, bleed holes 330 can be formed at a perimeter of bond line 302, such as along the bond line dam 314. Although not shown, one or more bleed holes 330 can also be formed at the the first part 190 and / or the second part 196 of a structural assembly 104, as an alternative for the formation of the bleed holes 330 along a union line dam 314.
[0071] In figure 13, a cross-sectional view showing the injection of structural adhesive 370 into the adhesive chamber 210 through an injection port 312 is shown. The injection port 312 can be lowered to seat a nozzle ( injection device 374. For the C 134 channel configuration, shown in figure 13, structural adhesive 370 can be injected into an injection hole 312 positioned on one side of the C 134 channel so that the structural adhesive 370 flows along the indicated flow direction 380, upwards along the outer surface of cylinder 116 in the direction of the union line dam 314 at channel edge 144. Structural adhesive 370 can also flow through the interstice 154 between the bottom surface of channel 152 and the edge of cylinder 120 and then upward along the direction of flow 380 into the interstice 154 between the side surface of channel 148 and the inner surface of cylinder 114 in one side of the C 134 channel, opposite the injection port 312, and towards the union line dam 314, in which excess adhesive 336 can be discharged into one or more reservoirs of adhesive, positioned along the inner cylinder surface 114.
[0072] In figure 14, step 414 of method 400 (figure 23) may include collecting excess adhesive 336 with the adhesive reservoirs 350 that are fluidly coupled to the bleed holes 330. In figure 14, an adhesive chamber is shown 210 in a filled state 384, with excess adhesive 336 collected inside the adhesive reservoirs 350. On an opposite side (not shown) of the cylinder 110, a similar set of bleed holes 330 and adhesive reservoirs 350 can be provided to collect excess adhesive 336. At the joint joint 106 of figure 14, the bleed holes 330 and the injection hole 312 can be positioned so that the structural adhesive 370 flows upwards towards the joining line dam 314 at the edge of upper channel 144. Structural adhesive 370 remains on the upper channel edge 144 while adhesive chamber 210 is filled, allowing structural adhesive 370 to flow along the upper channel edge 144 in the direction of the bleed holes. ia 330 and into the adhesive reservoirs 350 fluidly coupled to the adhesive chamber 210. The injection of structural adhesive 370 into the adhesive chamber 210 can continue until a predetermined amount of excess adhesive 336 is collected in each of the adhesive reservoirs 350. During injection of structural adhesive 370, a technician can be located on each side (ie, inside and outside) of cylinder 110 to visually check that each reservoir of adhesive 350 contains excess adhesive 336, which can indicate that the adhesive chamber 210 is completely filled.
[0073] In figure 15, the injection of structural adhesive 370 is shown in another adhesive chamber 210 positioned next to a recently filled adhesive chamber 210. In figure 15, the joint gasket 106 includes a series of the adhesive chambers 210, which are arranged along the length of the joining line 306. The adhesive chambers 210 of the series of adhesive chambers can be filled in succession, or the adhesive chambers 210 can be filled in an alternative filling sequence. Structural adhesive 370 can be injected into each adhesive chamber 210 until the adhesive reservoirs 350 for each adhesive chamber 210 are filled. By filling the adhesive reservoirs 350 to a level, which is above the level of the bleed holes 330, the adhesive reservoirs 350 can provide positive pressure to the adhesive chambers 210 to prevent air from entering the adhesive chamber 210.
[0074] In figure 16, step 416 of method 400 (figure 23) may include plugging each injection port 312 with a plug 386 after filling the adhesive chamber 210 and removing an injection device 374 from the injection port 312. Adhesive residue (not shown) can be cleaned from outside injection port 312 prior to installation of plug 386. Plug 386 can trap structural adhesive 370 within adhesive chamber 210 and to prevent adhesive leakage structural 370. The plug 386 can be sized and configured to provide a relatively close fit with the injection port 312. The plug 386 can be formed of a metallic material or any other material that can be separated from the structural adhesive 370 and removed injection port 312 after structural adhesive 370 is cured.
[0075] In figure 17, a portion of the joint gasket 106 between the cylinder 110 and the end ring 130 is shown and illustrating each of the adhesive chambers 210 filled with structural adhesive 370. Excess adhesive 336 is contained in each of the adhesive reservoirs 350. Plugs 386 are shown installed in each of the injection ports 312. As indicated earlier, adhesive reservoirs 350 can be constructed of substantially optically transparent material to allow visual observation of the excess adhesive level 336, as confirmation that the adhesive chambers 210 are filled.
[0076] In figure 18, step 418 of method 400 (figure 23) may include allowing structural adhesive 370 within adhesive chamber 210 to cure for a predetermined period of time. Heat (not shown) can optionally be applied to joint gasket 106 to facilitate curing of structural adhesive 370. After curing of structural adhesive 370, bonding line dams 314 (figure 17) and adhesive reservoirs 350 (figure 17) can be removed from the joint joint 106. Protruding joining wires 230 can be trimmed. Adhesive residue (not shown) can be removed from the joint gasket 106. Optionally, one or more 388 mechanical fasteners can be installed, as shown. For example, a mechanical fastener 388 can be installed through the adhesive chambers 210 to increase the strength of the joint gasket 106 and / or to prevent peeling forces between the cylinder 110 and the flanges 138 of the end ring 130.
[0077] In figure 19, an embodiment of a joint joint 106 between an outer ring 172 and cylinder 110 of structural assembly 104 of figure 2 is shown. As indicated above, cylinder 110 can be formed of a polymer matrix material , fiber-reinforced, 124, such as an epoxy material and carbon fibers or other composite material. The outer ring 172 can be formed of a metallic material 162, such as aluminum. The outer ring 172 can have an upper ring edge 174 and a lower ring edge 176. The outer ring 172 can be fixed in position with respect to cylinder 110 to provide a predetermined thickness of joining line 310 around a circumference of cylinder 112 (figure 2). The thickness of the joining line 310 can be established during a dry adjustment operation similar to the dry adjustment operation described above for the joint joint 106 shown in figure 3.
[0078] In figure 19, the thickness of the joining line 310 between the outer ring 172 and the cylinder 110 can be established using a series of connecting wires 230 (figure 6) positioned around the circumference of cylinder 112. The wires of junction 230 can be positioned at predetermined spacing 224 (figure 2) with each other. Although not shown, such tie wires can have a generally straight configuration and can be installed in a similar manner to the installation of tie wire 230 (figure 5) described above with respect to end ring 130 of the C 134 channel (figure 5 ), shown in figure 5. In figure 19, cylinder 110 can be installed inside outer ring 172 and outer ring 172 can be secured in position relative to cylinder 110. Shims (not shown) can be inserted in the line region joining 300 to form each chamber wall 212 (figure 20) in a manner described above. Shims can be removed after the formation of the chamber walls 212 and before the injection of structural adhesive 370 into the adhesive chambers 210 (figure 20).
[0079] In an alternative embodiment, in figure 19, the chamber walls 212 can be formed without the use of connecting wires 230 (figure 20). For example, a pair of shims 238 (figure 6) can be inserted into the junction region 300 to establish the interstice 154 (figure 3) between the mating surfaces 192, 198. Adhesive 214 (figure 20) can be injected within the space between the shims 238 to form the chamber walls 214. The shims 238 can be moved towards each other in a manner, as shown in figure 6, to form the edges of the chamber walls 212 and to define a width of the chamber walls 212 and to seal the adhesive 214 against the mating surfaces 192, 198. Shims 238 can be removed from the joint line region 300 following curing of the adhesive 214 of the chamber walls 212.
[0080] In figure 20, a flat pattern scheme of the joint joint 106 of figure 19 is shown during a joining process, in which structural adhesive 370 can be injected into an injection hole 312 of one of the adhesive chambers 210. The adhesive chambers 210 are separated from each other by chamber walls 212. One or more adhesive reservoirs 350 can be formed to collect excess adhesive 336 from adhesive chambers 210. adhesive reservoirs 350 can be configured as vertical columns 352, as described above, and can be formed of at least transparent, partially transparent, polymeric, non-silicone material, 356 or other material that facilitates the observation of the discharge of excess adhesive 336 from the adhesive chambers 210. However, the adhesive reservoirs 350 can be provided with any of a variety of alternative configurations for collecting excess adhesive 336 discharged from the bleed holes 330. For For example, adhesive reservoirs 350 can be formed as shelves 354 (figure 8).
[0081] In figure 21, a sectional view of the outer ring 172 and cylinder 110 is shown and illustrating the union line dams 314, which can be formed along the upper edge of ring 174 and / or the lower edge of ring 176 Bond line dams 314 can define the bond line perimeter 302 by enclosing the adhesive chamber 210. Bleeding holes 330 (figure 20) can be formed along the upper ring edge 174 and / or the lower ring edge 176, in a manner described above. An injection device 374 can be seated in the injection port 312 for the injection of structural adhesive 370 into the adhesive chamber 210.
[0082] In figures 20 to 21, injection holes 312 can be positioned approximately at a geometric center 318 (for example, vertical center and / or horizontal center) of the adhesive chamber 210 to facilitate uniform distribution and flow of the structural adhesive 370 from the injection port 312 in the direction to the junction line perimeters 302. During the injection process, air bubbles 382 (figure 20) can evacuate from the adhesive chamber 210 through the bleed holes 330. Although the bleed holes 330 in figure 20 are shown to be positioned along the upper edge of ring 174 for the vertically oriented joint line region 300, it is contemplated that for arrangements in which the joint line region 300 is generally oriented horizontally (not shown), bleed holes 330 can be included at the opposite edges of the outer ring 172, as well as along the same edges as the union line dams 314 in figure 21.
[0083] In figure 22, the joint gasket 106 of figure 20 is shown in a final state, following the curing of structural adhesive 370 in adhesive chambers 210 and the removal of adhesive reservoirs 350 (figure 20), from dams. union line 314, and plugs (not shown). Also shown is the optional installation of 388 mechanical fasteners, such as threaded fasteners (eg screws, Hi-loksTM, rivets, etc.) through each of the adhesive chambers 210 to increase the strength of the joint gasket 106 and / or to minimize stripping forces. The process of joining an inner ring 170 (figure 2) to the cylinder 110 can be carried out in a similar manner to the above described process of joining the outer ring 172 to the cylinder 110.
[0084] Figure 24 is a block diagram of a joint joint 106 illustrating the mating surface 192 of a first part 190 joined to the mating surface 198 of a second part 196. The first part 190 and the second part 196 can collectively form the structural assembly 104. The mating surfaces 192, 198 can be joined together over a region of joint line 300 having a length of joint line 306 and a width of joint line 308. In one embodiment, the joint joint 106 may comprise a long-length geometry feature 108 (figure 2). For example, the length of the splicing line 306 can be at least twice the width of the splicing line 308.
[0085] In figure 24, in one embodiment, the first part 190 and the second part 196 can define a region of flat joining line 300, substantially rectilinear, as is schematically shown in figure 5, and are not limited to a curved panel or a cylinder 110 joined to a ring, such as an end ring 130 or inner or outer ring 170, 172, as shown in figure 2. In this regard, the first part 190 and the second part 196 can define a line region union 300, relatively long, rectilinear, generally flat, having a cross-sectional configuration generally in a straight line (for example, figure 21). The length of the splicing line 306 can be twice the width of the splicing line 308 or greater. For example, the length of the seam line 306 of such a straight seam line region 3600, flat can be three (3) or more times the width of the seam line 308 or longer.
[0086] In figure 24, the length of the joining line 306 can be divided by a series of chamber walls 212, which can be formed within the region of the joining line 300 between the joining surface 192 of the first part 190 and the mating surface 198 of the second part 196. In one embodiment, the chamber walls 212 can be oriented generally transverse to the length of the joining line 306, although other orientations of the chamber walls 212 are contemplated. One or more of the chamber walls 212 may include a tie wire 230 to fit an interstice (not shown) between the mating surfaces 192, 198. At least one tie line dam 314 (figure 17) can be formed along of an edge of part 194, 200 (figure 13) of at least one of the first part 190 and the second part 196 to define at least a portion of the joining line perimeter 302 (figure 17). Chamber wall (s) 212, bond line dam (s) 314, and mating surfaces 192, 198 can collectively enclose adhesive chamber (s) 210.
[0087] In figure 24, one or more bleed holes 330 can be formed along the union line dam 314 (figure 17) or along other locations in the union line region 300. The hole (s) ( s) bleed 330 can (m) allow excess adhesive 336 to be discharged (figure 12) from adhesive chambers 210. One or more adhesive reservoirs 350 can be fluidly coupled to bleed holes 330 to collect excess adhesive 336 discharged from the adhesive chambers 210 during the injection of structural adhesive 370 into the adhesive chambers 210. The structural adhesive 370 can be injected into the adhesive chamber 210 through an injection port 312 after the adhesive chamber 210 be sealed and / or closed along the chamber walls 212 and the union line dams 314.
[0088] With reference to figures 25-26, modalities of the description can be described in the context of an aircraft manufacturing and service method 500, as shown in figure 25 and an aircraft 502, as shown in figure 26. During the pre- example 500 method may include specification and design 504 of aircraft 502 and material acquisition 506. During production, the manufacture of components and subassemblies 508 and systems integration 510 of aircraft 502 take place. Thereafter, aircraft 502 can go through certification and delivery 512 in order to be put into service 514. While in service by a customer, aircraft 502 is scheduled for routine maintenance and service 516 (which may also include modification, reconfiguration , remodeling and others).
[0089] Each of the 500 method processes can be performed or executed by a system integrator, a third party, and / or an operator (for example, a customer). For the purposes of this description, a system integrator may include, without limitation, any number of aircraft manufacturers and subcontractors to the main systems; a third party may include, without limitation, any number of vendors, subcontractors and suppliers; and an operator can be an airline, leasing company, military organization, service organization, and others.
[0090] As shown in figure 26, aircraft 502 produced by example method 500 may include a fuselage 518 with a plurality of systems 520 and an interior 522. Examples of high level systems 520 include one or more of a propulsion system 524, an electrical system 526, a hydraulic system 528, and an environmental system 530. Any number of other systems can be included. Although an aerospace example is shown, the principles of the invention can be applied to other industries, such as the automotive industry.
[0091] The apparatus and methods incorporated here may be employed during any one or more of the stages of the production method and method 500 service. For example, the components or subassemblies corresponding to the 508 production process may be manufactured or manufactured in a similar to the components or subassemblies produced while the 502 aircraft is in service. Also, one or more apparatus modalities, method modalities, or a combination thereof can be used during the 508 and 510 production stages, for example, by substantially speeding up the assembly of, or reducing the cost of, a 502 aircraft. Similarly , one or more of the apparatus modalities, method modalities, or a combination thereof may be used while the aircraft 502 is in service, for example and without limitation, for maintenance and service 516.
[0092] Modifications and improvements to the present description may be apparent to those of ordinary skill in the art. Thus, the particular combination of parts described and illustrated here is intended to represent only certain modalities of the present description and is not intended to serve as limitations on alternative modalities or devices within the spirit and scope of the description.

权利要求:
Claims (20)
[0001]
1. Method (400) of forming a joint joined by injection (106), characterized by the fact that it comprises the steps of: providing a first part (190) having opposite internal and external surfaces, and a second part (196) having a cross section comprising a C channel (134); inserting a circumferential or planar end of the first part (190) into the C-channel (134); forming a chamber wall (212) within a region of joining line (300) between opposing mating surfaces (192, 198) of the first part (190) and the C-channel (134) of the second part (196), the chamber wall (212) dividing a length of joining line (306) and defining at least one adhesive chamber (210); form a union line dam (314) along an upper end of the C-channel (134) on each of the opposite inner and outer surfaces of the first part (190), the chamber wall (212), the dam of joining line (314), and the mating surfaces (192, 198) collectively enclosing the adhesive chamber (210) injecting a structural adhesive (370) into each adhesive chamber (210) through an injection orifice (312 ) formed in the second part (196); discharge the excess structural adhesive (370) from each adhesive chamber (210) through a bleed hole (330) located between the first and second parts (190, 196) and formed inside the joining line dam (314) the adhesive chamber (210); and collecting excess structural adhesive (370) into an adhesive reservoir (350) fluidly coupled to each bleed hole (330), each adhesive reservoir (350) being formed as one of a column comprising a longitudinally extended channel fixed to external surface of the first part (190) and an outwardly projecting shelf (354) attached to an external surface of the second part (196).
[0002]
Method (400) according to claim 1, characterized in that the step of forming the chamber wall (212) comprises: forming the chamber wall (212) from adhesive (214).
[0003]
Method (400) according to claim 1, characterized in that the step of forming the chamber wall (212) comprises: including a connecting wire (230) in the chamber wall (212).
[0004]
Method (400) according to claim 1, characterized in that the length of the joining line is twice the width of the joining line.
[0005]
5. Method (400) according to claim 1, characterized by the fact that the injection port (312) is located close to the chamber wall (212).
[0006]
6. Method (400) according to claim 1, characterized in that the injection port (312) is located near the lower end of the adhesive chamber (210).
[0007]
Method (400) according to claim 1, characterized in that the bleed port (330) and the injection port (312) are located at opposite chamber ends of the adhesive chamber (210).
[0008]
8. Method (400) according to claim 1, characterized in that: a large bleed hole (330) and a small bleed hole (330) are located at opposite chamber ends of the adhesive chamber (210) ; and the injection port (312) is located near a chamber end having a small bleed port (330).
[0009]
Method (400) according to claim 1, characterized in that the first part (190) comprises a cylinder (110), the second part (196) comprising an end ring (130) having a cross section ( 132) configured as a C-channel (134), the step of forming the chamber wall (212) comprising: affixing a series of connecting wires (230) along a cylinder edge (120) so that the wires tie (230) divide the tie line length (306); coating the connecting threads (230) with camera wall adhesive (214); and inserting a cylinder edge (120) into the C-channel (134).
[0010]
10. Method (400) of forming a joint joined by injection (106), characterized by the fact that it comprises the steps of: providing a first part (190) having opposite internal and external surfaces, and a second part (196) having a cross section comprising a C channel (134); inserting a circular or flat end of the first part (190) into the C-channel (134); forming a series of chamber walls (212) within a region of joining line (300) between opposing mating surfaces (192, 198) of the first part (190) and of the C channel (134) of the second part (196) ), the chamber walls (212) dividing a length of joining line (306) into a plurality of adhesive chambers (210); form a union line dam (314) along an upper end of the C-channel (134) on each of the opposite inner and outer surfaces of the first part (190), the chamber wall (212), the dam of joining line (314), and the mating surfaces (192, 198) collectively enclosing the adhesive chamber (210); injecting a structural adhesive (370) into each adhesive chamber (210) through an injection port (312) formed in the second part (196); discharge the excess structural adhesive (370) from each adhesive chamber (210) through at least one bleed hole (330) located in the connecting line dams (314) between the first and second parts (190, 196) in an adhesive line perimeter of the adhesive chamber (210); and collecting the excess structural adhesive (370) in an adhesive reservoir (350) fluidly coupled to the bleed holes (330), each adhesive reservoir (350) being formed as one of a vertical column comprising a longitudinally extended channel fixed to external surface of the first part (190) and an outwardly projecting shelf (354) attached to an external surface of the second part (196).
[0011]
11. Structural assembly (104), characterized by the fact that it comprises: a first part (190), having opposite internal and external surfaces, and a second part (196) having a cross section comprising a C channel (134), a circumferential or planar end of the first part (190) being inserted into the C channel (134), and opposite mating surfaces (192, 198) of the first part (190) and the C channel (134) being adhesively joined together along a seam line region (300) having a seam line length (306); a series of chamber walls (212) formed along the length of the bonding line (306) and dividing the length of the bonding line (306) into a plurality of adhesive chambers (210); a union line dam (314) formed along an upper end of the C-channel (134) on each of the opposite inner and outer surfaces of the first part (190), the chamber wall (212), the dam of joining line (314), and the mating surfaces (192, 198) collectively enclosing the adhesive chamber (210); a structural adhesive (370) injected into the adhesive chambers (210) through at least one injection orifice (312) formed in the second part (196), and excess structural adhesive (370) being discharged from an orifice bleed (330) located between the first and second parts (190,196) and formed within the union line dam (314) of each of the adhesive chambers (210); and a plurality of adhesive reservoirs (350), each attached to an external surface of one of the first and second parts (190, 196) and fluidly coupled to a respective one of the bleed holes (330) to collect excess adhesive structural (370), each reservoir of adhesive (350) being formed as one of a vertical column comprising a longitudinally extended channel fixed to the external surface of the first part (190) and an outwardly projecting shelf (354) fixed to a surface external part (196).
[0012]
Structural assembly (104) according to claim 11, characterized in that: the chamber walls (212) are generally oriented transversely to the length of the joining line.
[0013]
Structural assembly (104) according to claim 11, characterized in that it additionally comprises: a connecting wire (230) included with at least one of the chamber walls (212).
[0014]
Structural assembly (104) according to claim 13, characterized in that: the joining thread (230) defines a joining line thickness between the mating surfaces (192, 198).
[0015]
Structural assembly (104) according to claim 11, characterized in that: the structural adhesive (370) comprises an expoxi adhesive.
[0016]
Structural assembly (104) according to claim 11, characterized in that it additionally comprises: at least one mechanical fastener (388) that extends through the first part (190) and the second part (196) in the region of joining line (300).
[0017]
17. Structural assembly (104) according to claim 11, characterized by the fact that: the first part (190) and the second part (196) define a region of straight and flat joining line.
[0018]
Structural assembly (104) according to claim 11, characterized in that: the first part (190) comprises a cylinder (110) having a cylinder edge (120); the second part (196) comprising an end ring (130) having a cross section (132) configured as a C-channel (134); and the series of chamber walls (212) being distributed around a cylinder circumference (112) to form the plurality of adhesive chambers (210) joining the cylinder edge (120) to the C-channel (134).
[0019]
19. Structural assembly (104) according to claim 11, characterized in that: the first part (190) is formed of fiber-reinforced polymer matrix material (124); and the second part (196) is formed of metallic material (162).
[0020]
Structural assembly (104) according to claim 11, characterized in that the length of the joining line is at least twice the width of the joining line.

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同族专利:

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公开号 | 公开日

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AU2014219398A1|2015-08-06|

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US9555608B2|2017-01-31|

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KR102207471B1|2021-01-27|

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US20170097031A1|2017-04-06|

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WO2014130234A1|2014-08-28|

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US10458454B2|2019-10-29|

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US20140241790A1|2014-08-28|

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BR112015019975B8|2021-03-30|

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RU2015127436A|2017-03-30|

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KR20150120365A|2015-10-27|

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AU2014219398B2|2017-07-06|

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RU2652554C2|2018-04-26|

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BR112015019975A2|2017-07-18|

引用文献:

---

公开号 | 申请日 | 公开日 | 申请人 | 专利标题

---

---

GB966772A|1961-08-16|1964-08-19|Montaplast G M B H|Pipe joint|

---

BE794882A|1972-02-15|1973-05-29|Stewing Albert|CHANNEL SHEATH FOR CABLES AND METHOD FOR ITS REALIZATION|

---

US4715162A|1986-01-06|1987-12-29|Trus Joist Corporation|Wooden joist with web members having cut tapered edges and vent slots|

---

SU1434144A1|1986-12-22|1988-10-30|Предприятие П/Я А-1882|Adhesive joint|

---

EP0627988A4|1992-02-28|1995-02-08|Armorvision Plastics & Glass|Bullet-resistant transparent panel, and method and press for making same.|

---

FR2681003B1|1991-09-10|1995-05-05|Aerospatiale|PROCESS FOR ASSEMBLING A PART FROM SANDWICH MATERIAL AND A METAL PART, TOOLS FOR IMPLEMENTING THE PROCESS, AND ASSEMBLY OBTAINED.|

---

US5851036A|1995-12-14|1998-12-22|Vanesky; Frank W.|Permanent fitting for fluid-tight connections|

---

DE19844411C3|1998-09-28|2003-08-07|Hochspannungsgeraete Porz Gmbh|Arrangement with a flange and method for producing a pressure connection in a flange|

---

US6749155B2|2002-09-13|2004-06-15|The Boeing Company|Composite assembly with integrated composite joints|

---

JP4227045B2|2004-03-10|2009-02-18|三菱電機株式会社|Tubular member joining method and tubular member joining structure|

---

US7341285B2|2004-03-24|2008-03-11|Ips Corporation Weld-On Division|Chemical fusion of non-metallic pipe joints|

---

US20060115320A1|2004-11-30|2006-06-01|The Boeing Company|Determinant assembly features for vehicle structures|

---

US7645406B2|2005-04-21|2010-01-12|The Boeing Company|Adhesive injection process for Pi-joint assemblies|

---

US7393488B2|2005-05-25|2008-07-01|The Boeing Company|Methods of joining structures and joints formed thereby|

---

US7670527B2|2006-05-09|2010-03-02|Lockheed Martin Corporation|Failsafe injected adhesive joint|

---

US8241450B2|2007-12-17|2012-08-14|Nike, Inc.|Method for inflating a fluid-filled chamber|

---

US8409381B2|2011-05-24|2013-04-02|General Electric Company|Method and system for bonding wind turbine blades|US9987025B2|2006-05-26|2018-06-05|Bruce B. Becker|Increased axial load carrying sheathed irrigating balloon catheter|

---

DE102012205814B3|2012-04-10|2013-07-04|Continental Automotive Gmbh|Method and device for aligning an actuator of an exhaust gas turbocharger|

---

JP5700186B1|2013-07-08|2015-04-15|ソニー株式会社|Curing condition determination method, circuit device manufacturing method, and circuit device|

---

KR20170019366A|2014-05-16|2017-02-21|디버전트 테크놀로지스, 인크.|Modular formed nodes for vehicle chassis and their methods of use|

---

US10960929B2|2014-07-02|2021-03-30|Divergent Technologies, Inc.|Systems and methods for vehicle subassembly and fabrication|

---

CN106794634A|2014-07-02|2017-05-31|迪根特技术公司|System and method for manufacturing joint member|

---

JP6109271B2|2015-02-06|2017-04-05|株式会社神戸製鋼所|Junction structure and manufacturing method of junction structure|

---

US10502250B2|2016-01-19|2019-12-10|The Boeing Company|Methods and systems for slot joining using slot cases|

---

US20180345599A1|2017-06-02|2018-12-06|Divergent Technologies, Inc.|Node with co-printed locating features and methods for producing same|

---

US20190061835A1|2017-08-25|2019-02-28|Divergent Technologies, Inc.|Apparatus and methods for connecting nodes to panels in transport structures|

---

US11110514B2|2017-12-14|2021-09-07|Divergent Technologies, Inc.|Apparatus and methods for connecting nodes to tubes in transport structures|

---

US11085473B2|2017-12-22|2021-08-10|Divergent Technologies, Inc.|Methods and apparatus for forming node to panel joints|

---

US20190193163A1|2017-12-27|2019-06-27|Divergent Technologies, Inc.|Assembling structures comprising 3d printed components and standardized components utilizing adhesive circuits|

---

EP3527356A1|2018-02-15|2019-08-21|Carbon Truck & Trailer GmbH|Load introduction device and method for bonding same|

---

US20190344299A1|2018-05-09|2019-11-14|Divergent Technologies, Inc.|Multi-circuit single port design in additively manufactured node|

法律状态:
2018-11-13| B06F| Objections, documents and/or translations needed after an examination request according art. 34 industrial property law|

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2019-11-19| B06U| Preliminary requirement: requests with searches performed by other patent offices: suspension of the patent application procedure|

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2020-12-01| B09A| Decision: intention to grant|

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2021-01-19| B16A| Patent or certificate of addition of invention granted|Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 04/02/2014, OBSERVADAS AS CONDICOES LEGAIS. |

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2021-03-30| B16C| Correction of notification of the grant|Free format text: REF. RPI 2611 DE 19/01/2021 QUANTO AO TITULO. |

优先权:

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申请号 | 申请日 | 专利标题

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US13/774,246|2013-02-22|

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US13/774,246|US9555608B2|2013-02-22|2013-02-22|System and method of forming an injection-bonded joint|

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PCT/US2014/014701|WO2014130234A1|2013-02-22|2014-02-04|System and method of forming an injection-bonded joint|

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