• 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:
    A device (10) for deploying an elongated hollow body (14), comprising: at least one elongated hollow body (14) having a closed cross-sectional profile, and a deployment mechanism (11), comprising a winding core (12) on which the elongated hollow body (14) is wound and compressed on itself in a first state, and which rotates the elongate hollow body (14) from the first state to a second unwrapped and unfolded state, the deployment mechanism (11) comprising a holding device (20), which has a holding member located therein, arranged in a cavity inside the elongate hollow body (14), and at least partially pressing against the inner wall of the elongate hollow body (14), and an outer fastening member arranged outside the elongate hollow body (14) in the region of the holding member located at the interior, so to be able to pass the elongate hollow body (14) between the outer fixing element and the holding element situated inside, and for fixing the axial position of the holding element situated inside, the latter interacts by locking and / or by force in the axial direction with the external fixing element, without being mechanically connected directly thereto. Figure for the abstract: Fig.1
    公开号:FR3081535A1
    申请号:FR1905525
    申请日:2019-05-24
    公开日:2019-11-29
    发明作者:Martin Hillebrandt；Martin ZANDER；Christian Hühne
    申请人:Deutsches Zentrum fuer Luft und Raumfahrt eV；
    IPC主号:
    专利说明:

    Description
    Title of the invention: Device for deploying a mast [0001] The invention relates to a device for deploying an elongated hollow body, wound, in particular a deployable mast.
    [0002] Since the beginnings of aerospace, masts have been used as support for sensors and instruments, as support structure for solar panels, antennas and solar sails, as well as for others. applications. But as even today, the transport of objects, such as satellites, is subject to drastic weight and space restrictions, masts protruding from the object to be transported is a significant problem. Therefore, deployable masts are very often used which are initially prepared in a wound state and compressed on themselves and therefore flattened for their transport in space, then are unrolled and deployed at their place of destination, which their provides their appropriate stability by allowing them to properly support the corresponding instruments, collectors or solar sails.
    In general, such a deployable mast is in this case constituted by an elongated hollow body, the cross section of which is configured so that the elongated hollow body can be deformed into a flat strip. Depending on the construction method, this flat strip has a tendency to deploy, thereby forming the corresponding cavity inside the elongated hollow body.
    Within the meaning of the present invention, an elongated hollow body is therefore a part which can be present both in the deployed state than in the wound state, and having no interior cavity in the wound state. The designation elongated hollow body defines here, in the broadest sense, the possibility of forming such a cavity inside the elongated hollow body, namely when the elongated hollow body is unrolled and deployed.
    Such an elongated hollow body, intended to serve as a deployable mast, in particular in the aerospace field, is then wound on a winding core, therefore necessarily being in the form of a flattened strip suitably wound on the winding core . If the winding core is now rotated about its axis, the rolled up elongated hollow body passes from its first rolled up state to a second unrolled and rolled out state. As it is being unwound from the winding core, the elongated hollow body returns to its original cross-sectional shape or takes on a transitional cross-sectional shape, and expands thereby forming the cavity therein of the elongated hollow body.
    Such deployable masts are most often made by shells with thin walls of metal or of fiber-reinforced composite materials. Due to their small wall thickness, the individual shells can be elastically deformed into a flattened strip, and can therefore be wound on the winding core in a small space. According to the principle, a distinction is made here between two types of deployable masts also called hull masts, namely those with an open cross-section profile and those with a closed cross-section profile. In the case of an open cross-section profile, the deployable mast has a discontinuous cross-section profile, for example in the form of an opening or a longitudinal slot in the cross-section profile, which allows the mast to be easier to roll up and deploy. Such deployable masts with an open cross-section profile can then be unfolded in a single-layer strip, which allows them to be wound up considerably less cumbersome on the winding core.
    By cons, deployable masts with closed cross section do not have such an axial slot, which in principle leads to the deployment of a structure of greater stability, but these masts can no longer be rolled up in the form of single layer on the winding core. The space available radially around the winding core consequently limits the length of the coiled shell mast with closed cross section, significantly greater than in the case of a deployable mast with an open cross section profile.
    In the case of such elongated hollow bodies, intended to serve as deployable hull masts, the transition zone between the part of the hollow body still wound and compressed on itself, and the section already fully deployed, is critical on the structural plan. In this transition zone, the cross section of the elongated hollow body is not yet fully developed, which considerably reduces both rigidity and stability. This is why in practice the transition zone is stabilized from the outside with the help of additional retaining elements, such as external shaped shells or external guide rollers, in order to be able to take up generally higher loads. in the transition zone during deployment.
    The shell masts with an open cross-section profile allow them to be held, from the outside, by shaped shells and, from the inside, by a core connected to the outer shaped shells, since the core can be fixed to the outside through the lateral opening of the mast. The mast profile is thus very well protected against deformation under load, such as the formation of bumps, and this risk is limited in the transition zone. This results in high rigidity and stability as desired. Open profile masts, however, have the disadvantage of low torsional rigidity, especially during the deployment operation. This type of mast is consequently sensitive to buckling by bending-torsion, in particular in the case of slender masts of great length.
    Deployable masts with a closed cross section profile do not have this in3 [0011] [0013] [0014] [0015] [0016] is suitable, which makes them significantly more efficient structurally for high degrees of slenderness and great lengths. However, they have the disadvantage that the maintenance of the transition zone is much more difficult to achieve, since a maintenance by shaped shells can only be carried out from the outside, due to the closed cross-section profile. . Consequently, deformations occurring under the effect of the stresses can propagate without hindrance inwards, which has so far led to a massive reduction in rigidity but also in the stability of the mast in the area of transition.
    With regard to this background, the object of the present invention is to indicate an improved device for deploying an elongated hollow body, wound, in particular a mast in deployable shell, using which elongated hollow bodies with cross-sectional profile. closed, can be properly held to prevent a lowering of stability when deploying the mast, especially in the transition zone.
    The desired objective is achieved by a device for deploying an elongated wound hollow body, comprising:
    • at least one elongated hollow body having a closed cross-sectional profile, and • a deployment mechanism comprising a winding core on which the elongated hollow body is wound and compressed on itself, in a first state, and which by rotation, changes the elongated hollow body from the first state to a second unrolled and deployed state, characterized in that the deployment mechanism comprises a holding device, which has • a holding element located inside, arranged in a cavity inside the elongated hollow body, and pressing at least partially against the inner wall of the elongated hollow body, and • an external fastening element, arranged outside the elongated hollow body in the region of the element holding located inside, so that the elongated hollow body can pass between the external fixing element and the holding element located inside, • and to fix the axial position of the holding element located inside, it interacts by locking and / or by force in the axial direction, with the external fixing element, without being connected directly, mechanically, to it.
    According to the invention, there is provided a device for deploying an elongated hollow body, wound, the device comprising, in known manner, at least one elongated hollow body having a closed cross-section profile. Furthermore, the device comprises a deployment mechanism, which has a winding core on which the elongated hollow body is wound and compressed on itself, in a first state, and which by rotation, causes the elongated hollow body to pass from the first state to a second unrolled and deployed state.
    For the purposes of the present invention, it is therefore meant under the designation of elongated hollow body, a part which may as well be compressed on itself in the form of a flat strip, as having a stabilizing cross section with a interior cavity. As a result, the elongated hollow body can be wound on a winding core, which produces compression of the elongated hollow body into a flat band. If the elongated hollow body is then unwound from this compressed and flattened state, it deploys and consequently forms a cavity inside the elongated hollow body. Consequently, the body wound and compressed on itself on the winding core is also considered to be a hollow body in the optics of the present invention, since it has at least in the second state, the interior cavity considered.
    According to the invention, the deployment mechanism comprises a holding device having a holding element located inside, arranged in a cavity inside the elongated hollow body, and pressing at least partially against the inner wall of the elongated hollow body. The holding device also has an external fixing element, arranged outside the elongated hollow body in the area of the holding element located inside. The whole so as to allow the elongated hollow body to pass between the external fixing element and the holding element located inside, while to fix the axial position of the holding element located inside , it interacts by locking and / or by force with the external fixing element, without being directly connected, mechanically, to it.
    Consequently, the holding element and the fixing element are designed so as to form together a locking and / or immobilization by force, so that the holding element situated inside is fixed axially. in its position in the cavity of the elongated hollow body, thanks to the fixing element located outside and producing a locking and / or immobilization by force. Locking and / or immobilization by force makes it possible, when passing from the first state to the second state of the elongated hollow body, to pass the latter between the holding element and the fixing element, thereby executing a relative movement between the retaining element and the fixing element, the retaining element and the fixing element being precisely not directly connected mechanically, since the elongated hollow body has a closed cross-section profile which prevents direct connection of the retaining core or the retaining element situated inside, with the fixing element situated outside. On the contrary, the retaining element located inside is held by a locking and / or a forced immobilization, at the fixing element, so that the retaining element can be fixed in its axial position to the inside the elongated hollow body, without direct mechanical connection between the holding element and the fixing element.
    This allows, during the deployment of the elongated hollow body, which can for example be a deployable mast for aerospace applications, to properly stabilize in particular the transition zone, thereby improving the stability of the mast and in particular opposing inward deformations. It is precisely in the transition zone, in which the mast does not yet have its fully deployed cross-sectional shape, that stabilization from the inside to the outside is particularly advantageous, so that the elongated hollow body can be maintained from the inside during the entire deployment period, thus offering a marked increase in rigidity, stability and overall load capacity, and thus also a significant extension of the possibilities of use.
    The external fastening element is here advantageously configured so as to completely surround the elongated hollow body in the area to be fixed, by performing here, in common with the retaining element or the retaining core arranged inside in this area, locking and / or immobilization by force, so that when the mast passes between the fastening element and the holding element, in the direction of deployment, the holding element located at the the interior remains in the prescribed axial position of the extended elongated hollow body.
    Advantageously, the deployment mechanism comprises a frame or a supporting structure, on which or which are fixedly arranged the winding core and the external fixing element, so that the external fixing element cannot precisely perform relative movement with respect to the winding core. As a result, the holding element located inside is also fixed with respect to a relative movement relative to the winding core and thus remains in the prescribed axial position. This does not mean that the fixing element of the holding device is not, if necessary, rotatably arranged on the frame, thereby possibly compensating for tangential movements during the deployment of the elongated hollow body.
    As already mentioned, it turns out to be advantageous for the device for holding the deployment mechanism to be arranged in a transition zone situated on the deployment path, inside which a section of the elongated hollow body is unwound from the winding core, but not yet fully deployed. Referring to the entire deployment path of the fully wound elongated hollow body, up to the fully unwound elongated hollow body, the transition zone is located near the winding core, on a section where the elongated hollow body forms certainly already a cavity, but has not yet reached its final cross-section profile. This transition zone is ultimately due to the fact that the elongated hollow body cannot suddenly take its shape from the rolled up and compressed state on itself until the deployed and unrolled state, but on the contrary a such modification of the shape of the elongated hollow body takes place in a uniform and continuous manner, from the compressed state on itself to the deployed state. In this transition zone, the elongated hollow body has, however during its deployment, its greatest weakness in terms of stability and rigidity, so that holding the elongated hollow body in this transition zone, using the holding element located inside is particularly advantageous.
    According to another advantageous embodiment, the holding device comprises a locking mechanism making it possible to carry out a locking between a locking element of the holding element situated inside and a locking element of the fixing element located outside, thereby fixing the holding element located inside, through the wall of the elongated hollow body. To this end, the locking mechanism comprises at least two locking elements, for example in the form of rollers, in the form of domes and / or in the form of spheres, the first locking element being arranged on the holding element located at the interior and the second locking element, on the fixing element located outside, so that during deployment the elongated hollow body can pass while being guided between the first and the second locking element. The two locking elements are here arranged on the holding device so that the first locking element achieves with the second locking element a locking in the axial direction of the elongated hollow body, thereby fixing in the axial direction the element maintenance located inside. The elongated hollow body passing while being guided between the two locking elements, is on this occasion slightly pushed inward or bumped outward in this area, since due to the arrangement of the two locking elements, it there is no continuous straight line in the axial direction, i.e. the direction of deployment (parallel to the axial direction or parallel to the direction of deployment). Thanks to this locking system established by virtue of the two rollers and their suitable arrangement with respect to each other, the holding element of the holding device, situated inside, can be positioned and fixed in the axial direction , at the position of the fixing element, without this requiring a direct mechanical connection with the holding element located inside.
    With at least two locking elements, as mentioned above, it becomes possible to fix the holding element located inside, in at least one axial direction, preferably in the direction of deployment, a fixing against the direction of deployment being done only by the shape, only because of the cross section which narrows.
    The locking elements thus produce inward narrowing or outward bossing in the cross section of the elongated hollow body, which then serves to fix the respectively opposite locking element.
    Regarding the locking elements, it may for example be rollers or rollers, the locking elements in the form of rollers or rollers having, perpendicular to the direction of deployment, a center distance smaller than the sum of spokes of the two roller-shaped locking elements. In other words, the centers of the two locking elements are not located in the same plane perpendicular to the direction of deployment, namely the axial direction of the elongated hollow body, so that they are arranged offset one relative to each other and can produce a lock in the direction of deployment.
    With regard to the locking elements, it may however also be sliding elements, which have a sliding surface or contact surface at least partially curved, by which the locking elements are in contact with the elongated hollow body respectively considered. The locking elements here have a sliding section by which they are in contact with the elongated hollow body respectively considered, thus being able to achieve the corresponding locking. Thus, such locking elements, fixed, may for example be in the form of domes, in the form of spherical heads and / or be partially curved. A spherical head shape here means that the sliding surface, namely the contact surface, corresponds at least partially to a sphere shape.
    In another advantageous embodiment, it is planned to implement a third locking element, which is either arranged on the holding element and interacts by locking with the second locking element, in the manner of first locking element, or is arranged on the fixing element and interacts by locking with the first locking element, in the manner of the second locking element. With the help of at least three such locking elements, it becomes possible to fix the holding element situated inside, both axially in the direction of deployment, and axially against the direction of deployment, so that the retaining core is always fixed in the predetermined axial position by the fixing element, and remains there.
    Consequently, provision is made in this configuration to arrange the second locking element on the fixing element and to arrange the first and third locking elements on the holding element before and after this second rusting worm element. These three locking elements are not here located in the same plane perpendicular to the direction of deployment, namely perpendicular to the axial orientation of the elongated hollow body in the second deployed state. In the case of locking elements in the form of rollers, the spacing, perpendicular to the direction of deployment, namely axially in the direction of the elongated hollow body, between the second and the first and between the second and the third element of locking in the form of a roller, is smaller than the sum of the radii of the second and first locking element and respectively of the second and third locking element.
    Consequently, there is no axial straight line between the three locking elements, so that the holding element situated inside cannot be moved in the axial direction when the fixing element exterior is fixed.
    Consequently, it is also conceivable to arrange the first locking element on the holding element situated inside, and to arrange the second and the third locking element on the external fixing element, the first locking element in the form of a roller being located, in the axial direction, between the second and the third locking element of the fixing element. In the above-mentioned embodiment, where the fastening element only has the second locking element, the second locking element is located, according to the axial orientation of the elongated hollow body, between the first and the third locking element in the form of a pebble.
    In another advantageous embodiment, the holding device has several locking mechanisms, each having at least two, preferably three locking elements. This has the advantage of preventing the phenomenon of arching of the holding element situated inside in the case of relatively large cross-sectional shapes, and thus of guaranteeing the regular sliding passage of the elongated hollow body, during the deployment.
    In this case, it is conceivable to arrange at least two of the locking mechanisms so that the plane of the contact surfaces of the locking elements of the first locking mechanism forms an angle less than 180 ° with the plane of the contact surfaces of the locking elements of the second locking mechanism, preferably an angle between 90 ° and 180 °.
    In the case of locking elements in the form of rollers, the axes of the locking elements in the form of rollers of the first locking mechanism extend at an angle less than 180 ° relative to the axes of the locking elements of the second locking mechanism.
    In this case, it is conceivable to provide a third and a fourth locking mechanism, the planes of the contact surfaces of the rusting worm elements also extend at an angle less than 180 °, but preferably greater than 90 °, so that at least four locking mechanisms are provided, which in particular relating to the holding element situated inside, prevent an arching of the holding element located inside the elongated hollow body.
    Alternatively, one can also consider providing on the holding device the first locking mechanism on a first side relative to the elongated hollow body, and said at least one second locking mechanism, on a second side opposite to said first side, referring to the elongated hollow body. It is then conceivable that the plane of the contact surfaces of the locking elements of the first locking mechanism is substantially parallel to the plane of the contact surfaces of the locking elements of the second locking mechanism. The holding element is thus supported both on the upper side and on the lower side of the elongated hollow body. In the case of an elongated hollow shell-shaped body made of two half-shells, it can be envisaged that the first locking mechanism is engaged with a first half-shell, and that the second locking mechanism is then engaged with a second half-hull.
    In the case of roller-shaped locking elements, the axes of the roller-shaped locking elements of the first locking mechanism can extend parallel to the axes of the roller-shaped locking elements of the second locking mechanism. locking.
    According to an advantageous embodiment, the holding element located inside has a sliding surface, along which for the purpose of form stabilization the inner wall of the elongated hollow body slides during the passage of the body hollow elongated from the first state to the second state.
    According to another advantageous embodiment, the holding element has, next to the possibility of locking and / or immobilization by force with the fixing element, a sliding surface along which in view form stabilization the inner wall of the elongated hollow body slides during the passage of the elongated hollow body from the first state to the second state, thus, thanks to a form of corresponding support support inside the elongated hollow body, suitably stabilize it precisely in the transition zone during deployment. By means of locking and / or forcibly immobilizing with the fastening element, the retaining element remains, with its form stabilizing sliding surface, in the position where the retaining element must suitably maintain or support the elongated hollow bodies.
    In this case, it turns out very particularly advantageous that the sliding surface is of a conical conformation in the direction of deployment, so as to correspond to the shape of cross section in the region of the holding element. , and reproduce it accordingly. In fact, during deployment, the cross section of the elongated hollow body gradually increases, from the compressed state on itself to the fully deployed state, the holding element having advantageously corresponding, in the transition zone, such a conical transition in the shape of the sliding surface.
    According to another advantageous embodiment, the holding element located inside has one or more holding rollers and / or sliding pads, which for the purpose of shape stabilization come into contact with the inner wall of the elongated hollow body, when the elongated hollow body passes from the first state to the second state. These holding rollers and / or sliding shoes must in this case not be made to lock with the fixing element located outside. In this regard, it is advantageous when, for at least one of the holding rollers and / or sliding pads, the fixing element has a conjugate roller and / or conjugated sliding pad, which are arranged so as to allow the elongated hollow body to pass between the holding roller and / or sliding shoe of the holding element, and the conjugate roller and / or conjugate sliding shoe of the fixing element, with contact but without locking in the axial direction, namely the direction of deployment. It is thus possible to achieve a controlled sliding of the elongated hollow body.
    According to another advantageous embodiment, the external fixing element comprises a shaped shell, which corresponds to the shape of the elongated hollow body at this position and through which the elongated hollow body can pass. The fixing element located outside thus surrounds, in the area of the holding element located inside, the elongated hollow body, and in particular reproduces its shape of external cross section in this area, the element holding located inside being held in this position by locking and / or force. Thanks to this, the elongated hollow body is maintained in this area by stabilizing its shape both inwards and outwards, thus avoiding deficits in stability due to a variation in shape, in this area.
    According to another advantageous embodiment, which can for example be provided as an alternative to the locking elements or in addition to these, the holding device comprises a magnetic device for fixing in the axial position, by force , of the holding element located inside, a first magnet being arranged on the holding element and at least a second magnet being arranged on the external fixing element, these magnets interacting so that the magnetic force exerted fixes the holding element located inside in said axial position inside the cavity of the elongated hollow body. This is particularly advantageous when the elongated hollow body has a material which cannot be deformed in the radial direction.
    According to another advantageous embodiment, on the winding core are wound and compressed on themselves, two, three, four elongated hollow bodies or, if necessary, more, each in a first state. By rotation of the winding core, it is possible to pass all the elongated hollow bodies each from the first state to a second unrolled and deployed state, and each elongated hollow body has, as described above, its own holding device. This is for example advantageous when using the deployment mechanism, several deployable masts must be unrolled and deployed, for example for tensioning solar sails.
    The elongated hollow body can be made of a fiber-reinforced composite material comprising a fiber-based material and a matrix material in which the fiber-based material is embedded. It is also conceivable that the elongated hollow body is made of a metallic material.
    The invention will be explained in the form of examples, with reference to the appended figures. These show:
    [Fig-1] an embodiment of the device, in the wound state;
    [Fig.2] an embodiment of the device, in the deployed state;
    [Fig.3] a perspective representation of an elongated hollow body with holding device;
    [Fig.4a] a representation of a holding device according to a first embodiment;
    [Fig.4b] a representation of a holding device according to the first embodiment;
    [Fig.4c] a representation of a holding device according to the first embodiment;
    [Fig.5] a holding device according to a second embodiment;
    [Fig.6a] a holding device according to a third embodiment;
    [Fig.6b] a holding device according to the third embodiment.
    The locking elements shown in the following figures and their description are produced in the form of rollers. In principle, however, it is possible to replace all the locking elements in the form of rollers, by locking elements of spherical shape or dome-shaped. The representations provided are therefore only examples.
    Figure 1 shows a representation of the device 10 according to the invention, allowing to exit four elongated hollow bodies in the form of deployable masts. The device 10 includes a deployment mechanism 11 having inside, a winding core 12 not shown, on which are wound and compressed on themselves, the elongated hollow bodies 14, in a first state. The elongated hollow bodies are therefore compressed in the manner of a flat strip and thus wound on the cylindrical winding core 12. In the embodiment of Figure 1, the four elongated hollow bodies are all wound simultaneously on the winding core 12, so as to be wound on each other and to be able to be unwound simultaneously. FIG. 1 shows in this case all the hollow elongated bodies in the state wound on the winding core 12 and presenting themselves consequently in a first state.
    The winding core 12 is here rotatably arranged on a support structure 13 of the deployment mechanism 11. Support arms 15 extend in a star from the winding core 12 of the deployment mechanism 11 and have corresponding guide elements 16, by means of which the wound hollow bodies 14 take place inside their respective carrying arms 15, being, on this occasion, brought to their respective holding device 20.
    Each of the carrying arms 15 of the carrying structure 13 of the deployment mechanism 11 has such a holding device 20, so that each of the wound hollow bodies 14 has its own holding device 20, with the help of which the respective hollow wound body 14 is suitably maintained in its transition zone during deployment.
    The device shown in Figure 1 is shown in Figure 2 in a second unrolled and deployed state of the hollow bodies 14. As can be seen, each of the elongated hollow bodies 14 has passed, during the unwinding, the device respective support 20, which, because of its fixed arrangement on the respective support arm 15, is fixedly linked to the support structure 13, and thus in particular can not perform relative movement relative to the winding core. This makes it possible to guarantee that, during the deployment of the elongated hollow bodies 14, these perform relative to the holding device 20, a relative movement in the axial direction of the deployment direction RA thus the holding device 20 is always arranged at the interior of the transition zone 17 where the hollow bodies 14, during deployment, do not yet have their cross-section profile fully deployed, and where consequently the stability and the rigidity of the respective hollow bodies 14 are reduced in this zone transition 17. FIGS. 1 and 2 here show a device 10 allowing a total of four elongated hollow bodies 14 to come out in the form of a deployable mast. In principle, the idea of the holding device 20 in the transition zone 17 is not limited by the number of hollow bodies 14, so it is naturally possible that such a holding device 20 finds its application in a device with a single hollow body, two hollow bodies, three hollow bodies, or even more than four hollow bodies.
    Figure 3 shows by way of example a hollow body 14 having an elongated section already fully deployed. The hollow body 14, as shown in Figure 3, was formed by two half-shells 14a) and 14b) having a cross section in the shape of an omega. In the wound state, the hollow body 14 is in the form of a flat strip 18 wound and compressed on itself, this state can be designated as the first state. When fully deployed the hollow body 14 is in a second state 19 in which it has a cross-sectional profile in the form of a double omega. In the second state 19, the hollow body 14 then has its highest stability.
    In the transition zone between the first state 18 and the second state 19, the cross-section profile of the second state 19 develops continuously, the hollow body 14 not having yet reached its corresponding final stability in this transition zone 17. In the transition zone 17, the elongated hollow body may in particular bend and damage the entire device.
    In accordance with the invention, the holding device 20 having a holding element (not shown in FIG. 3) located inside the hollow body 14, has been placed in this respect in the transition zone 17. the transition zone 17, as well as an external fixing element 21, so as to position in the axial direction the holding element situated inside, by virtue of a locking and / or immobilization by force. This ensures that the holding element located inside, responsible for ensuring additional stability of the elongated hollow body 14 in the transition zone 17, remains inside the transition zone 17, although the hollow body 14 has a closed cross-section profile. Thanks to the fixing in the axial direction, by locking and / or by force, of the holding element situated inside, by means of the fixing element 21, a direct mechanical connection of the element of fixing 21 with the holding element located inside is not necessary.
    Figure 4a) shows an embodiment of the holding device 20, for which, for better representation, part of the external fastening element 21 has been omitted. This allows to see the holding element 22 located inside, normally arranged inside the hollow body 14. For a better representation, the hollow body 14 is also not shown in the following figures. For a better understanding, it should be noted that the hollow body 14 passes while being guided between the holding element 22 located inside and the external fixing element 21 when the hollow body is passed from its first wound state to its second deployed state.
    FIG. 4a) shows a locking mechanism 30, which, in the embodiment of FIG. 4a) has a first locking element 31, a second locking element 32 and a third locking element 33. The first locking element 31 and the third locking element 33, produced in the form of small rollers or rollers, are in this case arranged on the holding element 22 located inside, while the second locking element 32 in roller-shaped is arranged on the non-visible part of the external fastening element 21.
    The elongated hollow body passing, being guided, through the holding device 20, had, therefore, to pass between the second locking element 32 of the fixing element 21 on the one hand, and the two others, namely the first locking element 31 and the third locking element 33 of the holding element 22, on the other hand.
    The three locking elements 31 to 33 are here arranged with respect to each other so that the elongated hollow body cannot pass in a straight line between the locking elements, but is, on the contrary, pressed by the second element. locking 32, in the direction of the holding element 22 located inside. The first and third locking elements 31 and 33 serve here as fixed support points, while the second locking element 32 pushes the region of the elongated hollow body between the two first and third locking elements, in the direction of the holding element 22 located inside.
    This provides a lock in the axial direction of the holding member 22 located inside with the fixing member 21, because the second locking member 32 on the fixing member, forms relative to the first and third locking elements of the holding element 22, a kind of undercut, which produces in the axial direction a locking of the holding element 22 located inside.
    In the embodiment of Figure 4a), such a locking mechanism 30 also exists on the opposite side, as shown in Figures 4b) and 4c). In this case, thanks to the second locking element 32 of the respective locking mechanism, the holding element located inside is sandwiched between these two locking mechanisms, and cannot therefore move in the axial direction.
    FIG. 4b) shows the holding element 22 located inside without the external fixing element 21, the second locking elements 32 in the form of rollers, necessary for establishing the locking, being also entirely similarly represented for a better understanding. In the direction of deployment RI, there is on the holding element situated inside a sliding surface 23, which can be provided to bear against an inner wall of the elongated hollow body by sliding along it. ci, and further to prevent folding of the elongated hollow body. The sliding surface 23 has fins 24 at its lateral ends which provide additional support for the elongated hollow body in the transition zone of the two half-shells.
    In addition, the retaining element 22 located inside comprises in the embodiment of Figures 4a) to 4c), additional retaining rollers 25, which come into contact with the elongated hollow body at the level of its inner wall, without locking interaction in the axial direction. This ensures that the holding element 22 located inside does not arc inside the elongated hollow body, making deployment impossible. These retaining rollers 25 of the retaining element 22 located inside, can here be accompanied by conjugate rollers 26 arranged on the external fixing element 21, so that the elongated hollow body passes while being guided between the retaining roller 25 of the retaining element 22 located inside and the conjugate roller 26 of the fixing element 21 outside.
    This variant shown in Figures 4a) to 4c) has the advantage that with only two locking mechanisms 30, there is an axial fixing of the holding member 22 located inside, the elongated hollow body n 'being thus deformed only in two places during deployment, due to the desired locking. The retaining rollers 25 arranged laterally and extending at a certain angle make it possible to obtain lateral support or support for the retaining element 22 situated inside, and thus to prevent an arching of the retaining element 22 located inside.
    Figure 4c) shows the holding element 22 located inside once again in a form clearly showing the first locking mechanism 30a) and the second locking mechanism 30b) opposite, of the holding device. It can also be seen that an elongated hollow body passing by being guided between the second locking element 32 of the external fixing element, and the two first and third locking elements 31 and 33 of the holding element located at the inside, is deformed towards the holding element located inside, due to the arrangement of the second locking element 32, which leads to a corresponding locking of the holding element located at the inside, with the second locking elements 32 of the external fixing element.
    FIG. 5 shows an exemplary embodiment of a holding element situated inside, which, except for the locking mechanism 30, is only produced entirely, in the form of a sliding surface 23, so that the elongated hollow body is supported by its inner wall on the entire sliding surface 23, while the holding member 22 located inside is, in the axial direction, fixed axially in its position due to the locking mechanism 30. In this embodiment, the friction of the inner wall is however significantly greater, so that it is necessary in this case to use suitable materials. On the other hand, the overall stability is significantly higher.
    Figures 6a) and 6b) show a third embodiment where there are provided, in total, four locking mechanisms 30a) to 30d). Each of these locking mechanisms is here of a construction as described at length with reference to Figures 4a) to 4c).
    A feature of this embodiment lies in the arrangement of the individual locking elements of the different locking mechanisms 30a) to 30d). The axes of the locking elements of the first locking mechanism 30a) here extend at a certain angle, less than 180 °, relative to the axes of the locking elements of neighboring locking mechanisms (for example the second locking mechanism 30b) or the fourth locking mechanism 30d)). The individual locking elements, in the form of rollers, of the various locking mechanisms are thus arranged obliquely with respect to each other, the locking elements of the opposite locking mechanisms being able to have corresponding parallel axes. It is then not necessary to have other retaining rollers inside the core, since using these four locking mechanisms 30a) to 30d), the retaining element 22 located at the interior is maintained or supported in all its directions. On the other hand, in this variant embodiment, the elongated hollow body is deformed in four places in total, in order to obtain locking, which most often results in greater stress on the material. However, such a holding element 22 has, compared to the first variant of Figures 4a) to 4c), fewer rotating parts, and is therefore possibly less susceptible to damage.
    [Table 1] List of references:
    10 device for deployment [0079] 11 deployment mechanism [0080] 12 winding core [0081] 13 support structure [0082] 14 elongated hollow body [0083] 15 support arms [0084] 16 guide elements [0085 ] 17 transition zone [18] 18 first state [0087] 19 second state [0088] 20 holding device [0089] 21 external fixing element [0090] 22 holding element located inside [0091] 23 surface of sliding [0092] 24 sliding surface fins [0093] 25 holding rollers [0094] 26 conjugate rollers [0095] 30 locking mechanism [0096] 31 first locking member in the form of a roller [0097] 32 second locking member pebble-shaped 33 third pebble-shaped locking element [0099] Ri direction of axial deployment
    权利要求:
    Claims (1)
    [1" id="c-fr-0001]
    claims [Claim 1] Device (10) for deploying an elongated hollow hollow body (14), comprising:- at least one elongated hollow body (14) having a closed cross-section profile, and- a deployment mechanism (11) comprising a winding core (12) on which the elongated hollow body (14) is wound and compressed on itself, in a first state (18), and which by rotation, passes the elongated hollow body (14) from the first state (18) to a second state (19) unwound and deployed,characterized in that the deployment mechanism (11) comprises a holding device (20), which has- a holding element (22) located inside, which is arranged in a cavity inside the elongated hollow body (14), and bearing at least partially against the inner wall of the elongated hollow body (14) , and- an external fixing element (21), arranged outside the elongated hollow body (14) in the region of the holding element (22) located inside, so as to be able to pass the elongated hollow body (14) between the external fixing element (21) and the holding element (22) located inside,- And to fix the axial position of the holding element (22) located inside, it interacts by locking and / or by force in the axial direction, with the external fixing element (21), without be connected directly, mechanically, to it. [Claim 2] Device (10) according to claim 1, characterized in that the deployment mechanism (11) comprises a frame on which are fixedly the winding core (12) and the external fixing element (21). [Claim 3] Device (10) according to claim 1 or 2, characterized in that the holding device (20) of the deployment mechanism (11) is arranged in a transition zone (17) inside which a section of the hollow body elongated (14) is unwound from the winding core (12), but is not yet fully deployed. [Claim 4] Device (10) according to one of the preceding claims, characterized in that the holding device (20) has at least one locking mechanism (30), which comprises at least two locking elements, the first locking element ( 31) being arranged on
    the holding element and the second locking element on the fixing element, so that the elongated hollow body (14) can pass, being guided, between the first and the second locking element (31, 32), the first locking element achieving with the second locking element locking in the axial direction of the elongated hollow body. [Claim 5] Device (10) according to claim 4, characterized in that a third locking element (33) is provided, which either is arranged on the holding element and interacts by locking in the manner of the first locking element ( 31) with the second locking element (32), either is arranged on the fixing element and interacts by locking in the manner of the second locking element (32) with the first locking element (31). [Claim 6] Device (10) according to claim 4 or 5, characterized in that the holding device (20) has several locking mechanisms (30), each comprising at least two locking elements respectively. [Claim 7] Device (10) according to claim 6, characterized in that at least two of the locking mechanisms (30) are arranged so that the plane of the contact surfaces of the locking elements of the first locking mechanism (30a) extends at an angle less than 180 ° relative to the plane of the contact surfaces of the locking elements of the second locking mechanism (30b). [Claim 8] Device (10) according to claim 6, characterized in that the first locking mechanism (30a) is provided on the holding device (20), on a first side relative to the elongated hollow body (14), and said at least one second locking mechanism (30b), on a second side opposite to said first side with reference to the elongated hollow body (14). [Claim 9] Device (10) according to one of the preceding claims, characterized in that the holding element (22) located inside has a sliding surface (23), along which the inner wall of the elongated hollow body slides. (14), when the elongated hollow body (14) passes from the first state (18) to the second state (19), for the purpose of shape stabilization. [Claim 10] Device (10) according to claim 9, characterized in that the sliding surface (23) has a conical conformation in the direction of deployment. [Claim 11] Device (10) according to one of the preceding claims, characterized in
    [Claim 12] [Claim 13] [Claim 14] [Claim 15] [Claim 16] that the holding element (22) located inside has one or more holding rollers (25) and / or skids of sliding, which come into contact with the inner wall of the elongated hollow body (14), when the elongated hollow body (14) passes from the first state (18) to the second state (19), for the purpose of shape stabilization.
    Device (10) according to claim 11, characterized in that for at least one of the holding rollers (25) and / or sliding pads, the fixing element has a conjugate roller (26) and / or pad of conjugate sliding, which is arranged to allow passage, between the holding roller (25) and / or sliding pad of the holding element, and the conjugate roller (26) and / or conjugate sliding pad of the fixing element, the elongated hollow body (14) being in a contact relationship imposed with it.
    Device (10) according to one of the preceding claims, characterized in that the external fixing element (21) has a shaped shell, which corresponds to the shape of the elongated hollow body (14) in this position and through which it is possible to pass the elongated hollow body (14).
    Device (10) according to one of the preceding claims, characterized in that the holding device (20) comprises a magnetic device for fixing in axial position, by force, the holding element (22) located at the inside, a first magnet being arranged on the holding element and at least a second magnet being arranged on the external fixing element (21), these magnets interacting so that the magnetic force exerted fixes the holding element (22 ) located inside in said axial position inside the cavity of the elongated hollow body (14).
    Device (10) according to one of the preceding claims, characterized in that on the winding core (12) are wound and compressed on themselves, two, three, four or more elongated hollow bodies (14), each in a first state (18), and in that by rotation of the winding core (12), it is possible to pass all the elongated hollow bodies (14) each from the first state (18) to a second unrolled state (19) and deployed, each elongated hollow body (14) having its own holding device (20).
    Device (10) according to one of the preceding claims, characterized in that the elongated hollow body (14) is made of a fiber-reinforced composite material comprising a fiber-based material and a matrix material in which the material is embedded based on fibers, or the elongated hollow body (14) is made of a metallic material.
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    同族专利:
    公开号 | 公开日
    DE102018112690A1|2019-11-28|
    US20190382231A1|2019-12-19|
    US10717628B2|2020-07-21|
    DE102018112690B4|2022-02-17|
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    法律状态:
    2020-04-21| PLFP| Fee payment|Year of fee payment: 2 |
    2021-04-20| PLFP| Fee payment|Year of fee payment: 3 |
    2021-10-01| PLSC| Publication of the preliminary search report|Effective date: 20211001 |
    优先权:
    申请号 | 申请日 | 专利标题
    DE102018112690.5|2018-05-28|
    DE102018112690.5A|DE102018112690B4|2018-05-28|2018-05-28|Device for unfolding a rolled-up elongate hollow body|
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