• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    sealing system for fasteners. The present invention relates to a method and apparatus for sealing a fastener that extends across a surface. the apparatus comprises a housing having a base and a cover, wherein the cover is configured to cover a portion of a fastener extending across a surface, and wherein the housing is configured to apply suction to the surface.
    公开号:BR102016017838B1
    申请号:R102016017838-0
    申请日:2016-08-01
    公开日:2022-01-11
    发明作者:Weidong Song；Daniel Joseph Perron
    申请人:The Boeing Company；
    IPC主号:
    专利说明:

    KEY INFORMATION FIELD
    [0001] The present description generally refers to protection for fasteners. Specifically, the present description relates to a method and apparatus for sealing fasteners. BACKGROUND
    [0002] In composite structures, sealing metal surfaces and holes that penetrate the structure can have a number of purposes, including reducing fuel leakage, with respect to fuel leaking from the tank, reducing other fluids entering or come out of the fuel tank, covering metallic components that may have a propensity to accumulate electrical charge, or preventing galvanic corrosion.
    [0003] Components, such as metal fasteners, can be sealed. A sealant in the form of sealing caps can cover these fasteners. A "seal cap" is a structure that covers one end of a metallic component. The metallic component may be a fastener. The end can be the head fastener or the threaded end of the fastener with a nut. The fastener can be, for example, a tenon, a screw, or some other type of fastener.
    [0004] For example, a sealing cap can be attached to the end of a fastener that extends into the fuel tank. This sealing cap is configured to provide a seal against the flow of fuel out of the fuel tank. The sealing cap can also reduce or eliminate electrical charge build-up on the exposed fastener surface.
    [0005] Sealing caps are often comprised of materials that retain sealing properties when submerged in fuel and/or when left dry for different periods of time. For example, molded polymeric seal caps can be used on jet fuel tanks. These types of seal caps can mount over the protruding end of a fastener inside the fuel tank. Sealants can be placed inside the seal caps before the seal caps are placed over the fastener. The seal may be in the form of a plastic forming material.
    [0006] For example, a sealing cap may have an interior that is partially filled with an uncured sealant. This sealing cap with the sealant is then pressed into place over the fastener. When in this position, excess sealant extrudes around the bottom of the cap. This sealant can be mixed around and over the outside of the cover. The sealant is then allowed to cure to form the final sealant material.
    [0007] However, installing molded seal caps can take an undesirable amount of time. For example, molded sealing caps can be placed over fasteners by hand. Manual installation can take an undesirable amount of time. In addition, molded seal caps can be manually inspected for voids prior to installation over fasteners. Furthermore, extruded sealant mixing can be performed manually and require training to achieve desired tolerances.
    [0008] Therefore, it would be desirable to have a method and apparatus that takes into account at least some of the problems discussed above, as well as possibly other problems. SUMMARY
    [0009] In an illustrative embodiment, an apparatus is provided. The apparatus comprises a housing. The housing has a base and a cover. The cover is configured to cover a portion of a fastener that extends across a surface. The housing is configured to apply suction to the surface.
    [0010] A further illustrative embodiment of the present description provides an apparatus. The apparatus comprises a surface, a fastener, and a housing. The fastener has an end that extends from the surface. Housing covers end of fastener. The housing is formed of a flexible material selected to apply suction to the surface after pressing the housing against the fastener. The housing includes a base and a cover.
    [0011] A still further illustrative embodiment of the present disclosure provides a method for sealing a fastener that extends across a surface. A housing is pressed onto one end of the fastener so that a portion of the housing conforms to a portion of the fastener. The housing includes a base and a cover. The housing is held over the fastener with suction applied by the housing to the surface.
    [0012] The features and functions can be achieved independently in various embodiments of the present description or can be combined in still other embodiments in which additional details can be seen with reference to the following description and drawings.
    [0013] Further, the description comprises embodiments in accordance with the following clauses: Clause 1. An apparatus comprising: a surface; a fastener having an end that extends from the surface; and a housing covering the end of the fastener, wherein the housing is formed of a flexible material selected to apply suction to the surface after pressing the housing against the fastener, the housing including a base and a cap. Clause 2. The apparatus of clause 1, wherein a space between the housing and the surface has a lower air pressure than an air pressure outside the housing. Clause 3. The apparatus of clause 1-2, wherein a first cover cross section is greater than a second cover cross section. Clause 4. The apparatus of clause 1-3, wherein the first cross section is closer to the base of the housing than the second cross section. Clause 5. The apparatus of clause 1-4 further comprising: an adhesive between the housing base and the surface. BRIEF DESCRIPTION OF THE DRAWINGS
    [0014] The new believed features characteristic of the illustrative modalities are presented in the appended claims. Illustrative embodiments, however, as well as a preferred mode of use, additional objects, and their features will be better understood by reference to the following detailed description of an illustrative embodiment of the present description when read in conjunction with the accompanying drawings, wherein:
    [0015] Figure 1 is an illustration of an airplane according to an illustrative embodiment;
    [0016] Figure 2 is an illustration of a block diagram of a manufacturing environment according to an illustrative embodiment;
    [0017] Figure 3 is an illustration of a cross-sectional view of a seal assembly according to an illustrative embodiment;
    [0018] Figure 4 is an illustration of a cross-sectional view of a seal assembly according to an illustrative embodiment;
    [0019] Figure 5 is an illustration of a cross-sectional view of a seal assembly according to an illustrative embodiment;
    [0020] Figure 6 is an illustration of a cross-sectional view of a seal assembly according to an illustrative embodiment;
    [0021] Figure 7 is an isometric view illustration of a seal assembly installed in accordance with an illustrative embodiment;
    [0022] Figure 8 is an illustration of a cross-sectional view of a seal assembly installed in accordance with an illustrative embodiment;
    [0023] Figure 9 is a flowchart illustration of a method for sealing a fastener that extends across a surface in accordance with an illustrative embodiment;
    [0024] Figure 10 is an illustration of an airplane manufacturing and service method in the form of a block diagram according to an illustrative embodiment; and
    [0025] Figure 11 is an illustration of an airplane in the form of a block diagram in which an illustrative embodiment can be implemented. DETAILED DESCRIPTION
    [0026] The different illustrative modalities recognize and take into account one or more considerations. For example, the illustrative embodiments recognize and take into account that the fuel tanks in an airplane are often integral structures of the airplane. For example, the wing structure of an airplane can be sealed. The internal cavities of the sealed wing structure can be used as a fuel tank. These types of wings are also referred to as "wet wings".
    [0027] Illustrative embodiments recognize and take into account that with a wet wing, components, such as fasteners, hoses, piping, or other components that extend into the wing, may be sealed to exclude the exterior from the interior, or covered. to reduce or eliminate the buildup of electrical charge on conductive surfaces. These components can extend through structures within the fuel tank, such as crossmembers, or between fuel tank bays through holes in the structure that form the fuel tank, such as ribs or other supporting structures. In conventional fuel tanks made of metal, the components and the holes through which they extend can be sealed to reduce leakage or seepage from the fuel tank formed inside the wing.
    [0028] The illustrative embodiments also recognize and take into account that currently used sealing systems may employ sealing caps that are configured to reduce energy transfer into a fuel tank system caused by an electromagnetic event. The energy transfer may involve a spark, a static discharge, a gas under pressure, a heated gas, a mechanical force, or some other transfer of energy that may be undesirable within a fuel tank system.
    [0029] The illustrative embodiments also recognize and take into account that sealing caps can add an undesirable amount of time to fabrication of the structure. Further, the illustrative embodiments recognize and take into account that a fuel tank system may be space-restricted. Movement within the fuel tank system may be limited by the size of the fuel tank system. Also, the distances between a number of fasteners in the fuel tank system can be small. The illustrative embodiments recognize and take into account that an apparatus for applying a seal to a fuel tank system must be compact enough to move within the fuel tank system. Thus, the illustrative embodiments provide a method and apparatus for reducing manufacturing time for sealing fasteners in a fuel tank system, reducing energy transfer in a fuel tank system, or a combination of the two.
    [0030] An illustrative embodiment of the present description may provide a fuel tank system. The fuel tank system may comprise a fuel tank, a number of fasteners, and a number of housings. The number of fasteners may have a number of ends that extend into an interior of the fuel tank. The number of pockets is set to cover the number of ends of the number of fasteners. A pocket in the number of pockets is configured to cover one end of a fastener in the number of ends. The housing has a base and a cover. The housing is formed of a flexible material selected to apply suction to the fuel tank after the housing has been pressed against the fastener.
    [0031] With reference now to the figures, and specifically with reference to Figure 1, an illustration of an airplane is presented in accordance with an illustrative embodiment. In this illustrative example, the airplane 100 has a wing 102 and a wing 104 attached to the body 106. The airplane 100 includes an engine 108 attached to the wing 102 and an engine 110 attached to the wing 104.
    [0032] The body 106 has a tail section 112. A horizontal stabilizer 114, a horizontal stabilizer 116, and a vertical stabilizer 118 are attached to the tail section 112 of the body 106. As shown, the airplane 100 also includes a system of fuel tank 120. As shown, the fuel tank system 120 includes a fuel tank 122 and a fuel tank 124.
    [0033] Fuel tank 122 is located inside wing 102, and fuel tank 124 is located inside wing 104 in fuel tank system 120. In these illustrative examples, fuel tank 122 and fuel tank 124 are formed by sealing the structures within the wing 102 and the wing 104, respectively. A sealing system for fasteners in the fuel tank system 120 may be implemented in accordance with an illustrative embodiment.
    [0034] With reference below to Figure 2, an illustration of a block diagram of a manufacturing environment is presented according to an illustrative embodiment. In this illustrative example, manufacturing environment 200 can be used to seal fasteners to platform 201. Airplane 100 of Figure 1 is an example of a physical implementation of platform 201 in Figure 2.
    [0035] The platform 201 may include the fuel tank system 202. The fuel tank system 120 in Figure 1 is an example of an implementation for the fuel tank system 202 in Figure 2. fuel 202 includes a number of fuel tanks 203. As used herein, a "number of", when used with reference to items, means one or more items. For example, "number of fuel tanks 203" is one or more fuel tanks. Fuel tank 122 and fuel tank 124 in Figure 1 are examples of fuel tanks which may be a number of fuel tanks 203. A fuel tank in the number of fuel tanks 203 may also be in locations other than in the wing 102 and wing 104 of airplane 100. For example, a fuel tank may be located within body 106 of airplane 100.
    [0036] In some illustrative examples, a number of fasteners 204 may be installed within the fuel tank 205 in the number of fuel tanks 203. Specifically, a number of fasteners 204 may be installed in a number of holes 206 formed in the structures 207 The structures 207 can be structures that form or support the fuel tank 205. The structures 207 can include at least one of a number of ribs, a number of beams, a number of skins, or other structures. The number of fasteners 204 can have a large number of fasteners. For example, the number of fasteners 204 may include between 20,000 and 80,000 fasteners. When the number of fasteners 204 includes a large number of fasteners, even small increases in time for an individual fastener relative to fabrication, sealing, or inspection can increase the total fabrication time by a large amount of time.
    [0037] The number of fasteners 204 has a number of first ends 208 and a number of second ends 209. The number of first ends 208 may extend into the interior 210 of the fuel tank 205. In these illustrative examples, the number of second ends 209 is on the outside 211 of the fuel tank 205.
    [0038] In this illustrative example, seal assembly 212 may be used within fuel tank 205 in the number of fuel tanks 203. Seal assembly 212 may be one of a plurality of seal assemblies 213.
    [0039] The plurality of seal assemblies 213 may be used to seal the number of fasteners 204 installed within the fuel tank 205. More specifically, the plurality of seal assemblies 213 may be used to seal the number of holes 206 in the structures 207 of the fuel tank 205 with the number of fasteners 204 installed inside the number of holes 206.
    [0040] Specifically, the seal assembly 212 can be used to seal a fastener in the number of fasteners 204 installed inside the fuel tank 205. More specifically, the seal assembly 212 can be used to seal a hole in the number of holes 206 in the structures 207 of the fuel tank 205 with the number of fasteners 204 installed in the number of holes 206.
    [0041] Seal assembly 212 may be designed to cover first end 214 of fastener 215. In some illustrative examples, seal assembly 212 may be the same as other seal assemblies of the plurality of seal assemblies 213. In others illustrative examples, seal assembly 212 may be different from other seal assemblies of the plurality of seal assemblies 213.
    [0042] For example, the plurality of seal assemblies 213 may be designed to seal a number of first ends 208 of the number of fasteners 204. In some illustrative examples, number of fasteners 204 may be of a variety of sizes. For example, the number of fasteners 204 can have a variety of diameters. The plurality of seal assemblies 213 can have a variety of at least one of shapes or sizes to desirably seal a number of fasteners 204 having a variety of diameters.
    [0043] As another example, the number of first ends 208 can have a variety of lengths. The plurality of seal assemblies 213 may have a variety of at least one of shapes or sizes to desirably cover and seal the number of first ends 208 of the number of fasteners 204.
    [0044] As shown, the seal assembly 212 may be configured to cover the first end 214 of the fastener 215 in the number of fasteners 204. The seal assembly 212 may form a barrier between the first end 214 of the fastener 215 and the interior 210 of the fuel tank 205.
    [0045] The first end 214 of the fastener 215 is an end within the number of first ends 208 that extends into the interior 210 of the fuel tank 205 of the structures 207. In these illustrative examples, the fastener 215 is installed in the hole 216 inside the number of holes 206 in fuel tank 205.
    [0046] In the illustrative examples, seal assembly 212 is configured to reduce effects resulting from an electromagnetic event 217. Specifically, seal assembly 212 may be configured to reduce energy transfer 218 into or within 210 of the fuel tank 205. The energy transfer 218 may be to the interior 210 of the fuel tank 205 of the current caused by the electromagnetic event 217. The energy transfer 218 may be to the interior 210 of the fuel tank 205 of the electrostatic charge that accumulates on the metallic components inside 210 of the fuel tank 205.
    [0047] In the illustrative examples, electromagnetic event 217 can be, for example, without limitation, a lightning strike, electrostatic discharge, or other types of discharge to platform 201. Electromagnetic event 217 can transfer energy 218 to platform 201 .
    [0048] In these illustrative examples, energy 218 can take a number of different forms. For example, the energy 218 may be at least one of a spark, an electrostatic discharge, heat, a mechanical force, a moving particle, or some other form of energy that may be undesirable within 210 of the fuel tank 205. As here used, the phrase "at least one of", when used with a list of items, means that different combinations of one or more of the listed items may be used, and only one of each item in the list may be required. For example, "at least one of item A, item B, and item C" may include, without limitation, item A, or item A and item B. This example may also include item A, item B, and item C, or item B and item C.
    [0049] In an illustrative example, energetic particles may originate from one or more of the number of first ends 208 of the number of fasteners 204 in response to the electromagnetic event 217. In the illustrative examples, the seal assembly 212 is configured to reduce and/or preventing energy 218 from being transferred into or within 210 of fuel tank 205. Seal assembly 212 is configured to contain energy 218, absorb energy 218, or a combination of the two. Containing energy 218, absorbing energy 218, or a combination of the two, the amount of energy 218 reaching the interior 210 of fuel tank 205 can be reduced, impeded, or both. In these illustrative examples, containing energy 218 means that the amount of energy 218 reaching interior 210 of fuel tank 205 is reduced, impeded, or both.
    [0050] Material 220 of seal assembly 212 may be selected to provide desirable characteristics. In the illustrative examples, the material 220 of the seal assembly 212 may be selected as one that does not retain unwanted amounts of electrical charge. The material 220 of the seal assembly 212 may be selected as one that is electrostatically conductive. In some illustrative examples, the material 220 may be a polymeric material 222. In some illustrative examples, when the material 220 is a polymeric material 222, the seal assembly 212 may be a thermoset 224 or a thermoplastic elastomeric material 226.
    [0051] A thermostable material can become hard when heated. A thermoplastic material can become soft under heating and harden under cooling. A thermoplastic material may be capable of being repeatedly heated and cooled.
    [0052] As another example, the material 220 of the seal assembly 212 may be selected as having properties configured to contain energy 218 in the form of thermal energy. Thermal energy can be, for example, in the form of a spark or heated gas.
    [0053] Material 220 of seal assembly 212 may be selected for desirable inspection or application properties. For example, the material 220 of the seal assembly 212 may be selected so that the seal assembly 212 is substantially transparent 228 after curing. When the seal assembly 212 is substantially transparent 228 after curing, the seal assembly 212 can be visually inspected for voids.
    [0054] The number of fasteners 204 may extend across the surface 229 of the platform 201. When the number of fasteners 204 is present in the fuel tank system 202, the fastener 215 may extend across the surface 229 in the fuel tank system. 202.
    [0055] While the number of fasteners 204 has been discussed as being present on the fuel tank system 202, the number of fasteners 204 may be used in locations other than the fuel tank system 202. In these other illustrative examples, the surface 229 may be any desirable surface other than within the fuel tank system 202. For example, surface 229 may be an outer surface of platform 201. In another illustrative example, surface 229 may be an inner surface of platform 201.
    [0056] Seal assembly 212 takes the form of housing 230. Housing 230 is formed prior to installation over a fastener. Housing 230 may be formed using injection molding, thermoforming, or any other desirable form of fabrication.
    [0057] Housing 230 may be positioned so housing 230 covers first end 214 of fastener 215 extending from surface 229. Housing 230 is configured to apply suction 232 to surface 229. Housing 230 has a base 233 and a cap 234. Base 233 may take the form of a flange 236. When seal assembly 212 is mounted on fastener 215, base 233 contacts surface 229 of platform 201.
    [0058] Cover 234 is configured to cover a portion of fastener 215 that extends across surface 229. More specifically, cover 234 may cover first end 214 of fastener 215. Cover 234 has a first cross section 240 and a second cross section 242. First cross section 240 is closer to base 233 of housing 230 than second cross section 242. First cross section 240 is larger than second cross section 242.
    [0059] In some illustrative examples, cap 234 may be referred to as dome 244. In some illustrative examples, dome 244 may have a generally rounded end. In other illustrative examples, dome 244 may have a substantially flat end. In some illustrative examples, dome 244 may be substantially conical.
    [0060] Cover 234 has an internal cavity 246. The internal cavity 246 may be designed to cover the first end 214 of the fastener 215. The shape 248 of the internal cavity 246 may be designed based on the fastener 215. The shape 248 of the fastener 248 The internal cavity may be designed based on at least one of the size, shape, or length of the first end 214 of the fastener 215.
    [0061] Inner cavity 246 may be designed so that a portion of inner cavity 246 contacts fastener 215 when seal assembly 212 is mounted on fastener 215. Inner cavity 246 may be designed so that a space 250 between internal cavity 246 and fastener 215 is desirable. Space 250 may be a total amount of volume between inner cavity 246 of cap 234 and fastener 215. For example, it may be desirable to minimize space 250 within inner cavity 246 when seal assembly 212 is installed over fastener 215 .
    [0062] Seal assembly 212 may be positioned over fastener 215. After positioning of seal assembly 212 over fastener 215, pressure may be applied to cap 234 to press housing 230 over first end 214 of fastener 215 so that a housing portion 230 conforms to a fastener portion 215.
    [0063] When housing 230 is pressed onto first end 214 of fastener 215, housing 230 is secured over fastener 215 by suction 232 applied by housing 230 to surface 229. Housing 230 can be described as acting as a cup of suction.
    [0064] The material 220 of the housing 230 may be flexible 252 so that the housing 230 acts as a suction cup. When the material 220 of housing 230 is flexible 252, a portion of the cap 234 may conform to a portion of the fastener 215.
    [0065] When housing 230 is held against surface 229 by suction 232, air pressure 254 inside space 250 is lower than air pressure 256 outside housing 230. When air pressure 254 is lower than air pressure 256, air pressure 254 can be referred to as negative pressure. Air pressure 256 outside housing 230 may be approximately atmospheric pressure. In some illustrative examples, space 250 may be referred to as a space within housing 230. In other illustrative examples, space 250 may be referred to as a space between housing 230 and surface 229.
    [0066] When the air pressure 254 is lower than the air pressure 256 outside the housing 230, the housing 230 may have desirable characteristics during operation of the platform 201. For example, when the platform 201 is an aircraft such as the airplane 100 of Figure 1, the air pressure 256 may be lower when the airplane is flying than when the airplane is on the ground. As air pressure 256 drops below atmospheric pressure, housing 230 may still have suction 232. If air pressure 254 and air pressure 256 are both approximately atmospheric pressure, housing 230 may exit fastener 215 as air pressure 256 decreases during flight.
    [0067] When platform 201 is an aircraft, the air within housing 230 will expand when the aircraft is at cruising altitude. If the air pressure 254 was atmospheric pressure, the air inside the housing 230 could expand during flight and push against the housing 230. By pushing against the housing 230, the air inside the housing 230 could break the seal of the housing 230. air pressure 254 being lower than air pressure 256, the air within housing 230 may not provide an undesirable amount of pressure against housing 230.
    [0068] In some illustrative examples, suction 232 alone may secure housing 230 over fastener 215. In some other illustrative examples, additional retention components may secure housing 230 over fastener 215. For example, a water sensitive adhesive pressure 258 can be present within the internal cavity 246. When pressure sensitive adhesive 258 is present, both pressure sensitive adhesive 258 and suction 232 can hold housing 230 in place over fastener 215.
    [0069] Pressure sensitive adhesive 258 can be a permanent or temporary adhesive. For example, pressure-sensitive adhesive 258 may continue to hold housing 230 in place over fastener 215 through the entire use of platform 201. In other illustrative examples, pressure-sensitive adhesive 258 may temporarily hold housing 230 in place. over fastener 215. In one example, adhesive 260 may be present between base 233 and surface 229. In this example, pressure-sensitive adhesive 258 may hold housing 230 in place as adhesive 260 cures. After the adhesive 260 is cured, at least one of the adhesive 260 and the suction 232 can hold the housing 230 in place over the fastener 215. For example, the adhesive 260 can be the primary component that holds the housing 230 in place over the fastener. 215. Adhesive 260 may be optional.
    [0070] In some illustrative examples, the seal assembly 212 may further include a number of self-locking flanges 262. The number of self-locking flanges 262 may also be formed from material 220. The number of self-locking flanges 262 may extend from housing 230 to the interior 264 of housing 230. Pressing housing 230 over first end 214 of fastener 215 may include applying housing 230 so that the number of self-locking flanges 262 engage fastener 215.
    [0071] In some illustrative examples, the number of self-locking flanges 262 may provide additional retention for housing 230. In some illustrative examples, the number of self-locking flanges 262 may provide primary retention for housing 230. In some illustrative examples, the number of self-locking flanges 262 may provide primary retention for housing 230. In some illustrative examples, the number of self-locking flanges 262 can be used in conjunction with other retention components such as at least one suction 232, pressure sensitive adhesive 258, or adhesive 260.
    [0072] The number of self-locking flanges 262 can center the housing 230 with respect to the fastener 215. By centering the housing 230 with respect to the fastener 215, the number of self-locking flanges 262 can minimize the space 250.
    [0073] In other illustrative examples, material 220 may provide retention for housing 230. For example, when base 233 is formed of thermoplastic elastomeric material 226, base 233 may be heated. Upon heating the base 233, the thermoplastic elastomeric material 226 can become flexible and tacky. By heating the base 233, the thermoplastic elastomeric material 226 can adhere to the surface 229.
    [0074] Seal assembly 212 may be installed over fastener 215 in any desirable manner. In some illustrative examples, seal assembly 212 may be pressed onto fastener 215 manually. In another illustrative example, a robotic arm 266 can move the seal assembly 212 within the fuel tank system 202. The robotic arm 266 can install the seal assembly 212 over a fastener in a number of fasteners 204, such as fastener 215 .
    [0075] The illustration of the manufacturing environment 200 in Figure 2 is not intended to imply physical or architectural limitations on the way in which an illustrative embodiment may be implemented. Other components in addition to or in place of those illustrated may be used. Some components may be unnecessary. Also, blocks are presented to illustrate some functional components. One or more of these blocks may be combined, divided, or combined and divided into different blocks when implemented in an illustrative embodiment.
    [0076] For example, each of the number of self-locking flanges 262, adhesive 260, and pressure sensitive adhesive 258 can be optional. In some illustrative examples, seal assembly 212 may include at least one of heated thermoplastic elastomeric material 226 of base 233, number of self-locking flanges 262, adhesive 260, or pressure sensitive adhesive 258. Further, in some illustrative examples, the assembly Seal 212 may include none of heated thermoplastic elastomeric material 226 of base 233, number of self-locking flanges 262, adhesive 260, or pressure sensitive adhesive 258.
    [0077] Looking now at Figure 3, an illustration of a cross-sectional view of a seal assembly is presented according to an illustrative embodiment. Seal assembly 300 may be a physical implementation of seal assembly 212 of Figure 2. Seal assembly 300 includes a housing 302 disposed over fastener 304. First end 306 of fastener 304 extends across surface 308. As shown, housing 302 is in an uninstalled position. To seal fastener 304 using housing 302, housing 302 may be pressed in direction 310 over fastener 304. When housing 302 is pressed in direction 310, housing 302 may be placed in an installed position.
    [0078] The housing 302 includes a cover 312 and a base 314. As shown, a number of self-locking flanges 315 extend from the housing 302 into the interior 316 of the housing 302. In addition, an adhesive 318 is positioned between the base 314 and the surface 308.
    [0079] When housing 302 is pressed in direction 310, the suction created by housing 302 can hold housing 302 in place relative to surface 308 and fastener 304 while adhesive 318 cures. When housing 302 is installed over fastener 304, at least one of the number of self-locking flanges 315, adhesive 318, or suction can hold housing 302 in place relative to surface 308 and fastener 304.
    [0080] Looking now at Figure 4, an illustration of a cross-sectional view of a seal assembly is presented according to an illustrative embodiment. Seal assembly 400 may be a physical implementation of seal assembly 212 of Figure 2. Seal assembly 400 includes a housing 402 disposed over fastener 404. First end 406 of fastener 404 extends across surface 408. As shown, housing 402 is in an uninstalled position. To seal fastener 404 using housing 402, housing 402 can be pressed in direction 410 onto fastener 404.
    [0081] Housing 402 includes cover 412 and base 414. As shown, adhesive 416 is positioned between base 414 and surface 408.
    [0082] When housing 402 is pressed in direction 410, suction created by housing 402 can hold housing 402 in place relative to surface 408 and fastener 404 while adhesive 416 cures. When housing 402 is installed over fastener 404, at least one of adhesive 416 or suction can hold housing 402 in place relative to surface 408 and fastener 404.
    [0083] Looking now at Figure 5, an illustration of a cross-sectional view of a seal assembly is presented according to an illustrative embodiment. Seal assembly 500 may be a physical implementation of seal assembly 212 of Figure 2. Seal assembly 500 includes a housing 502 disposed over fastener 504. First end 506 of fastener 504 extends across surface 508. As shown, housing 502 is in an uninstalled position. To seal fastener 504 using housing 502, housing 502 can be pressed in direction 510 onto fastener 504.
    [0084] Housing 502 includes a cap 512 and a base 514. As shown, a number of self-locking flanges 515 extend from housing 502 into the interior 516 of housing 502. When housing 502 is installed over fastener 504, at least one of the number of self-locking flanges 515 or suction can hold housing 502 in place relative to surface 508 and fastener 504.
    [0085] Looking now at Figure 6, an illustration of a cross-sectional view of a seal assembly is presented according to an illustrative embodiment. Seal assembly 600 may be a physical implementation of seal assembly 212 of Figure 2. Seal assembly 600 includes a housing 602 disposed over fastener 604. First end 606 of fastener 604 extends across surface 608. As shown, housing 602 is in an uninstalled position. To seal fastener 604 using housing 602, housing 602 can be pressed in direction 610 onto fastener 604.
    [0086] Housing 602 includes a cap 612 and a base 614. When housing 602 is pressed in direction 610, suction created by housing 602 can hold housing 602 in place relative to surface 608 and fastener 604.
    [0087] Referring to Figure 7, an illustration of an isometric view of an installed seal assembly is presented according to an illustrative embodiment. Installed seal assembly 700 may be a physical implementation of seal assembly 212 of Figure 2. Installed seal assembly 700 may be an example of seal assembly 400 of Figure 4 or seal assembly 600 of Figure 6 in a state. installed.
    [0088] Installed seal assembly 700 includes a housing 702, which has a cap 704 and a base 706. In this installed state, base 706 is substantially flat against surface 708.
    [0089] Installed seal assembly 700 may be held in place over fastener 714 by at least one suction or adhesive positioned between base 706 and surface 708. As shown, fastener 716 is not yet sealed. In some illustrative examples, the seal assembly substantially the same as the installed seal assembly 700 may be used to seal the fastener 716. In other illustrative examples, the fastener 714 and the fastener 716 may be different. For example, a length of fastener 716 extending from surface 708 may be greater than a length of fastener 714 extending from surface 708. In another illustrative example, fastener 714 and fastener 716 may have different diameters. When fastener 714 and fastener 716 are different, a seal assembly for sealing fastener 716 may be different than seal assembly 700. For example, at least one of base size, cap shape, internal cavity shape , or another desirable feature of the seal assembly may be different from the seal assembly 700.
    [0090] As shown, housing 702 of seal assembly 700 is transparent 718. When housing 702 is transparent 718, inspection of housing 702 can be faster than if housing 702 were not transparent 718. For example, Out-of-tolerance conditions may be visible through housing 702 when housing 702 is transparent 718.
    [0091] Looking now at Figure 8, an illustration of a cross-sectional view of an installed seal assembly is presented according to an illustrative embodiment. View 800 may be a cross-sectional view of seal assembly 700 along 8 of Figure 7.
    [0092] As shown, portion 802 of housing 702 contacts portion 804 of fastener 714. The space 806 between housing 702 and surface 708 is desirably small. Minimizing the space 806 can also minimize the amount of air within the inner cavity 808 of the cap 704. The space 806 within the inner cavity 808 of the cap 704 also desirably has a pressure of below atmospheric pressure.
    [0093] The different components shown in Figures 1 and 3-8 can be combined with the components in Figure 2, used with the components in Figure 2, or a combination of the two. In addition, some of the components in Figures 1 and 3-8 may be illustrative examples of how the components shown in block form in Figure 2 can be implemented as physical structures.
    [0094] Looking now at Figure 9, a flow chart illustration of a method for sealing a fastener that extends across a surface is shown in accordance with an illustrative embodiment. Process 900 may be a process for sealing the fastener 215 of Figure 2. Process 900 may be a process for sealing a fastener on the plane 100 of Figure 1.
    [0095] Process 900 may press a housing over one end of the fastener so that a portion of the housing conforms to a portion of the fastener, the housing including a base and a cap (operation 902). In some illustrative examples, pressing the housing over the end of the fastener comprises applying the housing over the end of the fastener so that a space between the housing and the surface has a lower air pressure than an air pressure outside the housing.
    [0096] In some illustrative examples, a number of self-locking flanges extend from the housing into an interior of the housing, and pressing the housing over the end of the fastener comprises applying the housing so that the number of self-locking flanges engage the fastener. In some illustrative examples, the number of self-locking flanges that engage the fastener secure the housing relative to the fastener while an adhesive between the housing and the surface cures.
    [0097] Process 900 can then hold the housing over the fastener with suction applied by the housing to the surface (operation 904). Afterwards the process ends. In some illustrative examples, the suction holds the housing relative to the fastener while an adhesive between the housing and the surface cures.
    [0098] The flowcharts and block diagrams in the different modalities presented illustrate an architecture, functionality, and operation of some possible implementations of devices and methods in an illustrative modality. In this regard, each block in flowcharts or block diagrams may represent a module, a segment, a function, and/or a portion of an operation or step.
    [0099] In some alternative implementations of an illustrative modality, the function or functions noted in the blocks may occur out of the order noted in the figures. For example, in some cases, two blocks shown in succession may be executed substantially concurrently, or the blocks may sometimes be executed in reverse order, depending on the functionality involved. Also, other blocks can be added in addition to the blocks illustrated in a flowchart or block diagram. Also, some blocks may not be implemented. For example, process 900 may further comprise applying an adhesive to the base of the housing.
    [0100] Illustrative embodiments of the description may be described in the context of a method of manufacturing and servicing airplane 1000 as shown in Figure 10 and airplane 1100 as shown in Figure 11. Looking first at Figure 10, an illustration of a diagram of blocks of an airplane manufacturing and service method is shown in accordance with an illustrative embodiment. During pre-production, the method of manufacturing and servicing airplane 1000 may include specification and design 1002 of airplane 1100 in Figure 11 and material procurement 1004.
    [0101] During production, of components and subassemblies 1006 and system integration 1008 of the plane 1100 in Figure 11 takes place. Thereafter, the airplane 1100 in Figure 11 may pass through certification and delivery 1010 in order to be placed in service 1012. While in service 1012 by a customer, the airplane 1100 in Figure 11 is scheduled for routine maintenance and service 1014, the which may include modification, reconfiguration, renewal, and other maintenance or service.
    [0102] Each of the processes of the Airplane Manufacturing and Service Method 1000 may be done or performed by a system integrator, a third party, and/or an operator. In these examples, the operator can be a customer. For purposes of this description, a system integrator may include, without limitation, any number of aircraft manufacturers and major system subcontractors; a third party may include, without limitation, any number of vendors, subcontractors, and suppliers; and an operator can be an airline, a leasing company, a military entity, a service organization, and so on.
    [0103] Referring now to Figure 11, an illustration of a block diagram of an airplane is presented in which an illustrative embodiment can be implemented. In this example, airplane 1100 is produced by the method of manufacturing and servicing airplane 1000 in Figure 10 and may include airplane structure 1102 with a plurality of systems 1104 and interior 1106. Examples of systems 1104 include one or more of propulsion system 1108 , 1110 electrical system, 1112 hydraulic system, and 1114 environmental system. Any number of other systems can be included. Although an aerospace example is shown, different illustrative modalities can be applied to other industries, such as the automotive industry.
    [0104] The method and apparatus incorporated herein may be employed during at least one of the stages of the aircraft manufacturing and service method 1000 in Figure 10. One or more illustrative embodiments may be used during the fabrication of components and subassemblies 1006. For example, seal assembly 212 of Figure 2 may be used to seal a fastener during the manufacture of components and sub-assemblies 1006. Further, seal assembly 212 may also be used to seal a fastener during maintenance and service 1014.
    [0105] The method and apparatus presented can reduce the amount of time required to seal a fastener. Further, the seal set shown may reduce the training or experience to seal a fastener. A seal assembly can seal a fastener by being pressed onto the fastener. Pressing a seal assembly onto a fastener can be performed manually or by a robotic system in less than a minute. In some illustrative examples, a seal assembly can be pressed onto a fastener in ten seconds or less.
    [0106] Using a preformed housing, a sealant overflow may not occur. As a result, the seal assembly shown may lack sealant formation, mixing, or sealant removal steps. By eliminating the steps of sealant formation, mixing, or sealant removal, sealing a fastener can have a shorter seal time.
    [0107] The method and apparatus presented can also reduce the amount of time to manufacture a fuel tank system. A seal assembly can be applied over one end of a fastener. Using a seal assembly such as a pre-molded housing, a fastener can be sealed in less time than manually applying conventional seal caps. Manual application of conventional sealing caps can take up to twenty minutes each. The time required to apply a conventional sealing cap may be related to at least one of the location within the fuel tank system, the size of the end to be covered, the desired surface treatments, or other factors.
    [0108] Using a seal set, application processes can be reduced to less than one minute for each fastener. Thus, the sealing time for the fasteners can also be reduced. By reducing the sealing time, the manufacturing time of the fuel tank system can be reduced. By reducing sealing time, fuel tank system manufacturing time can be reduced by hundreds of hours. In some illustrative examples, fuel tank system manufacturing time can be reduced by over 1,000 hours.
    [0109] Furthermore, by providing transparent seal assemblies, inspection time can be reduced. By reducing inspection time, manufacturing time can be further reduced.
    [0110] The description of the different illustrative modalities has been presented for purposes of illustration and description and is not intended to be exhaustive or limited to the modalities as described. Many modifications and variations will be apparent to those skilled in the art. Also, different illustrative embodiments may provide different features compared to other illustrative embodiments. The modality or modalities selected are chosen and described in order to better explain the principles of the modalities, the practical application, and to allow others skilled in the art to understand the description for various modalities with various modifications as are suitable for the specific use contemplated. .
    权利要求:
    Claims (13)
    [0001]
    1. Apparatus comprising: a housing (302) having a base (314) and a cap (312), wherein the cap (312) is configured to cover a portion (306) of a fastener (304) extending through of a surface (308), and wherein the housing (302) is configured to apply a suction to the surface (308), characterized in that the apparatus further comprises an adhesive (318), the adhesive configured to be located between the base (312) of housing (302) and surface (308) when the apparatus is installed.
    [0002]
    2. Apparatus according to claim 1, characterized in that the housing (302) is formed of a thermoplastic elastomeric material.
    [0003]
    Apparatus as claimed in claim 1 or 2 further comprising: the fastener (304), wherein the housing (302) is configured to be positioned such that the housing (302) covers one end of the fastener (306) extending from the surface (308).
    [0004]
    Apparatus according to claim 3, characterized in that the apparatus is configured to provide a space (316) between the housing (302) and the surface (308) that has an air pressure lower than an air pressure. of air outside the housing (302).
    [0005]
    Apparatus according to claim 3 or 4 characterized in that it further comprises: a number of self-locking flanges (315) extending from the housing (302) to an interior (316) of the housing (302).
    [0006]
    Apparatus according to claim 5, characterized in that the number of self-locking flanges (315) engage the fastener (304) to hold the housing (302) in place with respect to the fastener (304).
    [0007]
    7. Apparatus according to claim 5 or 6, characterized in that the number of self-locking flanges (315) couples the fastener (304) and centers the housing (302) in relation to the fastener (304).
    [0008]
    8. Apparatus according to any one of claims 1 to 7, characterized in that the housing (302) is formed of a polymeric material selected to protect the fastener (304) from energy caused by an electromagnetic event.
    [0009]
    9. A method of sealing a fastener (304) that extends across a surface (308), the method comprising: pressing a housing (302) over an end (306) of the fastener (304) so that a portion of the housing (304) 302) conforming to a portion of the fastener (304), the housing (302) including a base (314) and a cover (312); and securing the housing (302) onto the fastener (304) with a suction applied by the housing (302) to the surface (308), characterized in that the method further comprises: applying an adhesive (318) to the base (314) of the accommodation (302).
    [0010]
    10. Method according to claim 9, characterized in that the suction holds the housing (302) in relation to the fastener (304) while the adhesive (318) between the housing (302) and the surface (304) cures.
    [0011]
    A method as claimed in claim 9 or 10, characterized in that a number of self-locking flanges (315) extend from the housing (302) into the interior (316) of the housing (302), and in which to press the housing (302). 302) over the end of the fastener (304) comprises applying the housing (302) so that the number of self-locking flanges (316) engage the fastener (304).
    [0012]
    12. Method according to claim 11, characterized in that the number of self-locking flanges (316) that couple the fastener (304) holds the housing (302) in relation to the fastener (304) while the adhesive (318) between housing (302) and surface (304) cure.
    [0013]
    A method as claimed in any one of claims 9 to 12 further comprising: heating the base (314) so that a thermoplastic elastomeric material of the base (304) adheres to the surface (308).
    类似技术:
    公开号 | 公开日 | 专利标题
    BR102016017838B1|2022-01-11|APPLIANCE AND METHOD FOR SEALING A FIXER
    JP2019055778A|2019-04-11|Method and apparatus for covering fastener system
    BR102017018085A2|2018-05-02|WING AND MANUFACTURING METHOD
    BR102014021753B1|2021-02-23|apparatus and method for applying sealant
    BR102014020484B1|2021-04-27|SYSTEM FOR USE IN THE COVERAGE OF A PORTION OF A HARNESS, AND, METHOD FOR COVERING A PORTION OF A HARNESS
    CN105599217B|2019-07-02|Use the injection molding fastener cap sealing element in thermoplastic elastic material scene
    US10301033B2|2019-05-28|Foamed energy absorptive fastener seal cap
    RU2606419C2|2017-01-10|Electric charge dissipation system for aircraft
    US10051767B2|2018-08-14|Method and apparatus for covering a fastener system
    JP2015174144A|2015-10-05|Method and system for installing fasteners with electromagnetic effect protection function
    US20090123745A1|2009-05-14|Fabrication and installation of preformed dielectric inserts for lightning strike protection
    US11074839B2|2021-07-27|Method for conforming a display panel
    ES2813571T3|2021-03-24|Expandable resin filled fastener, fastener system and method for composite structures
    CN107231760A|2017-10-03|A kind of high-precision mold encapsulating method of circuit board assemblies
    US9415853B2|2016-08-16|Surface sealing system
    ES2486016T3|2014-08-14|Protection of composite elements
    JP2015507566A|2015-03-12|Aircraft charge dissipation system
    KR102368245B1|2022-02-25|Method and apparatus for covering a fastener system
    BR102015019237A2|2018-03-06|WAY TO SUPPORT A VOLUME OF A BOLD SUBSTANCE
    US20030228448A1|2003-12-11|Foamed chiller insulative assemblies
    同族专利:
    公开号 | 公开日
    KR20170054235A|2017-05-17|
    EP3156670A1|2017-04-19|
    BR102016017838A2|2017-05-30|
    EP3156670B1|2020-07-22|
    CA2936594A1|2017-04-14|
    CN106641253A|2017-05-10|
    AU2016204078B2|2020-09-17|
    RU2016123451A|2017-12-20|
    RU2660096C2|2018-07-04|
    US9939006B2|2018-04-10|
    AU2016204078A1|2017-05-04|
    JP7001338B2|2022-01-19|
    JP2017106619A|2017-06-15|
    US20170108029A1|2017-04-20|
    ES2824152T3|2021-05-11|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US2417262A|1945-06-25|1947-03-11|Adel Prec Products Corp|Sealing nut|
    US5044852B1|1978-08-24|1995-04-04|Sweeney Theodore Co|Vacuum fixed adhesively secured fastener|
    US4830558A|1978-08-24|1989-05-16|Theodore J. Sweeney & Co.|Adhesively securable fastener|
    US4756654A|1984-06-13|1988-07-12|Trw Inc.|Fastening device|
    US5048898A|1990-07-06|1991-09-17|Del-Met Corporation|Wheel cover twist fastener system|
    US5129770A|1991-07-15|1992-07-14|Coleman Kirby D|Armadillo tamper resistant bolt and head protector|
    JP3021104U|1995-07-28|1996-02-16|大東電材株式会社|Anti-rust cap for bolts and nuts|
    US5642973A|1995-12-26|1997-07-01|Pretty; Daniel Glenn|Plumbing cleanout cover|
    MY135737A|1996-02-09|2008-06-30|Petronas Res & Scient Services Sdn Bhd|Protective caps for bolts with nuts|
    US5810532A|1997-05-09|1998-09-22|Grand General Accessories Manufacturing Inc.|Vehicle lug nut covers|
    DE19823624C1|1998-05-27|2000-02-10|Radolid Thiel Gmbh|Protective cap for wheel nut has internal spring grip to secure to wheel nut and to enable cover to be pulled off|
    CA2565469C|2004-05-03|2013-04-16|Poetters, Gert|Suction-type holding device|
    CN2703166Y|2004-05-24|2005-06-01|陈军权|Sealing ring|
    DE602004017035D1|2004-12-30|2008-11-20|Sony Ericsson Mobile Comm Ab|Sealed housing, gasket and procedures for mounting and dismounting the sealed housing|
    US7665941B2|2005-07-27|2010-02-23|The Dyson Corporation|Method and structure for an anchor rod cap|
    US20100140437A1|2007-08-28|2010-06-10|John Orban|Suction cup|
    US8002508B2|2008-09-26|2011-08-23|Griptight Bolt Cover Co.|Protective cover for fasteners|
    JP5619446B2|2010-03-23|2014-11-05|三菱重工業株式会社|Cap, fastening structure using the cap, and aircraft having the fastening structure|
    CA2707556A1|2010-06-10|2011-12-10|Bud-Eze Systems Inc.|Protective cover adapted for a visual aid|
    JP2012102808A|2010-11-10|2012-05-31|Kitagawa Ind Co Ltd|Sealing cap|
    JP5931458B2|2012-01-17|2016-06-08|三菱航空機株式会社|How to install lightning-resistant fasteners and lightning-resistant fasteners|
    US10301033B2|2012-02-01|2019-05-28|The Boeing Company|Foamed energy absorptive fastener seal cap|
    CN102678927A|2012-05-22|2012-09-19|西安飞机工业（集团）有限责任公司|Sealing method of fastener|
    AU2014257277A1|2013-04-22|2015-11-12|Prc-Desoto International, Inc.|Sealant caps including internal barrier rings|
    US9188226B2|2013-07-15|2015-11-17|The Boeing Company|Apparatus for installing a seal cap|
    US9618029B2|2013-09-23|2017-04-11|The Boeing Company|Systems and methods for use in covering a portion of a fastener protruding from a surface|
    CN203784283U|2014-03-04|2014-08-20|鼎向科研股份有限公司|Sealing strip structure|
    GB2535518A|2015-02-20|2016-08-24|Airbus Operations Ltd|Cap with injected sealant|
    US9939006B2|2015-10-14|2018-04-10|The Boeing Company|Sealing system for fasteners|US11260945B1|2015-03-06|2022-03-01|Robert S Patterson|Propeller nut|
    US9939006B2|2015-10-14|2018-04-10|The Boeing Company|Sealing system for fasteners|
    US10556665B2|2016-06-20|2020-02-11|The Boeing Company|Apparatuses and methods for improved sealing|
    GB2557962A|2016-12-20|2018-07-04|Airbus Operations Ltd|Cap for a fastener|
    US20180339788A1|2017-05-26|2018-11-29|Joe A. Garcia|Protective cap and nut gauge for an aircraft fuel tank fastener system|
    US10501202B2|2017-08-23|2019-12-10|The Boeing Company|Ignition-quenching systems, apparatuses, and methods|
    EP3466808A1|2017-10-03|2019-04-10|Airbus Operations S.L.|Fitting for the transport of an industrial part|
    GB2568890A|2017-11-29|2019-06-05|Airbus Operations Ltd|Spark containment cap|
    JP6487586B1|2018-04-25|2019-03-20|株式会社Ｉｈｉインフラ建設|Transparent bolt nut cap|
    CN109578411A|2018-12-07|2019-04-05|西安飞机工业（集团）有限责任公司|A kind of metal cap monaural seal traveling self-locking nut|
    RU2709632C1|2019-05-24|2019-12-19|Публичное акционерное общество"Туполев"|Anchor floating nut with cap for tight containers assembly|
    WO2021055391A1|2019-09-17|2021-03-25|Clarcorp Industrial Sales, Inc.|Reinforced cap head screws|
    CN112259972A|2020-09-25|2021-01-22|中国直升机设计研究所|Composite material and aluminum structural member lap joint anti-corrosion conductive structure and processing method|
    法律状态:
    2017-05-30| B03A| Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]|
    2020-03-24| B06U| Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]|
    2021-11-09| B09A| Decision: intention to grant [chapter 9.1 patent gazette]|
    2022-01-11| B16A| Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]|Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 01/08/2016, OBSERVADAS AS CONDICOES LEGAIS. |
    优先权:
    申请号 | 申请日 | 专利标题
    US14/882,645|US9939006B2|2015-10-14|2015-10-14|Sealing system for fasteners|
    US14/882,645|2015-10-14|
    [返回顶部]