Variable stiffness joint mechanism |
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申请号 | US11949029 | 申请日 | 2007-12-01 | 公开(公告)号 | US08475074B1 | 公开(公告)日 | 2013-07-02 |
申请人 | Christopher P Henry; | 发明人 | Christopher P Henry; | ||||
摘要 | In some embodiments, a variable stiffness joint is provided which has a plurality of structural members with a variable stiffness material coupled between the plurality of structural members. The variable stiffness material may be selectively activated/inactivated to control the stiffness of the joint. Additional embodiments and implementations are disclosed. | ||||||
权利要求 | What is claimed is: |
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说明书全文 | This application is a continuation in part of U.S. application Ser. No. 11/713,560, filed Mar. 1, 2007, now U.S. Pat. No. 7,678,440 by McKnight et al. entitled DEFORMABLE VARIABLE-STIFFNESS CELLULAR STRUCTURES, which is a continuation in part application that claims the benefit of priority of U.S. Provisional Application No. 60/778,245, filed Mar. 1, 2006 entitled DEFORMABLE VARIABLE-STIFFNESS CELLULAR STRUCTURES. The topology and spatial connectivity of a structure determine how loads and displacements are transmitted from their source to reaction locations. Some structures where topology and connectivity are especially important are in a variety of truss structures, 2D and 3D cellular structures, compliant mechanisms, composites, and the like. The locations where two or more structural/mechanism members join are joints or structural nodes. In the structure of some mechanisms, it is sometimes advantageous to control the extent of engagement between certain members, such as along the load path between the source and reaction. As such, the present inventor has discovered that what is needed is a means to selectively control which members of a structural node are permitted to become kinematically free in rotation, and/or which members of a structural node can transmit loads. Moreover, the present inventor has discovered what is needed is customized levels of mechanical resistance, or “load tailoring” within a structure. Further, the present inventor has discovered what is needed is a joint that allows the angle of members coming out of the spherical joint to be varied and then fixed or locked into place. In some embodiments, a variable stiffness joint is provided which has a plurality of structural members with a variable stiffness material coupled between the plurality of structural members. The variable stiffness material may be selectively activated/inactivated to control the stiffness of the joint. Additional embodiments and implementations are disclosed. The features and advantages of the present invention will be better understood with regard to the following description, appended claims, and accompanying drawings where: This application is related to U.S. patent application Ser. Nos. 11/347,505, by McKnight et al., filed Feb. 3, 2006, entitled ACTUATION CONCEPTS FOR VARIABLE STIFFNESS MATERIALS, and 11/713,560, by McKnight et al., entitled DEFORMABLE VARIABLE STIFFNESS VARIABLE CELLULAR STRUCTURES, filed Mar. 1, 2007, both herein incorporated by reference in their entireties. When these specific sections 130 of the variable stiffness material change stiffness (to a soft state) the desired kinematic degree of freedom is expressed. Otherwise, when the variable stiffness material is rigid, the degree of freedom cannot be expressed and joint is static and can transmit load along the degree of freedom. For a spherical joint 100 with many structural members 120, the variable stiffness material between these structural members 120 could selectively permit kinematic degrees of freedom in desired directions, while maintaining static joint connections in other selective directions. As shown in The sections 130 may be selectively activated. For example, in one embodiment, the variable stiffness material may be a heat sensitive shape memory polymer. In such an embodiment, heaters may be embedded in, adjacent to, or on the surface of the variable stiffness material. Or, a structural member 120 or its connector 140 could be heated. Separate control (illustrated in The structural members 120 may include connectors 140 which are a different geometry than the structural members 120, or they may be same geometry and size. The structural members 120 may be connected directly to the variable stiffness material 130, or the variable stiffness material 130 may have a geometry similar to the connector 140 which surrounds or partially surrounds the end or a portion of the structural members 120. For example, the variable stiffness material may be cubic, spherical, etc., or sections thereof, in which the structural member is embedded. As used herein, a “structural member” of the variable stiffness joint may be simply a connector, to which a truss or another structural member is connected, joined, inserted, bonded, secured, fixed, etc. In some embodiments, the connectors 140 are not structural, but rather are formed in whole or in part of variable stiffness material. In such embodiments, the structural members 120 may extend and mechanically connect to each other (not shown) within the joint 100. Thus, the variable stiffness material may partially or completely surround the structural members 120 and/or the linkage (not shown) within the joint 100. In this embodiment, the variable stiffness material sections 230 form an umbrella like webbing between the structural connectors 240. In some embodiments, the sections 230 may be segmented, or be continuous material, capable of being stretched, folded, accordioned, or the like. The variable stiffness material may form the entire material of the sections 230, select portions of the sections 230, or only the connection between the sections 230 and/or structural connectors 240 to allow deflection of the sections 230. In other embodiments (not shown), the sections 230 form a continuous web, not separated by the structural connectors 240. In other embodiments, the variable stiffness material may be associated with connecting linkages connecting the structural members 220 to restrain the movement of the connecting linkages, connectors 240, and/or structural members 220. In one embodiment (not shown), a mechanical interconnection, such as a helical spring or other flexure member could be coated with a variable stiffness material to control the action of such a linkage. The sections 230, or portions of the sections 230, may be selectively activated/inactivated, such as by heating/cooling in the case of a shape memory polymer. In some embodiments, all or a portion of the hole 270 in the middle of the spherical joint 200 may be filled with variable stiffness material to create a direct connection between non-adjacent structural members 240. This would make it possible to fix non-adjacent structural members 240 to one another, to allow transfer of loads between non-adjacent members 240. The above embodiments are not limited to the number of structural members illustrated. In some embodiments, the entire spherical joint 400 may be place within a field, such as a thermal field to act upon the entire spherical joint 400, for example to heat/cool the entire spherical joint 400, instead of separate activators/inactivators for each portion 430a, 430b, and 430c. Some methods to enable a thermal field are: fluid or air flow, resistively or inductively heated material, etc. In this embodiment, it is possible to locate the variable stiffness material 730 not only between the outer guide portions 715a, 715b, and 715c and the structural members 716, 717, and 718, but also extending along the length of the structural members 716, 717, and 718. Further, variable stiffness material 730 may be located along the exterior of the guide portions 715a, 715b, and 715c. This can provide additional support for the joint 710. It is not necessary in all embodiments, to have the joints 710 and 720 connected by a unitary structural member 717, or that the joint 710 be connected to another joint 720 as shown. The joint 710 may be used alone, or connected other joints 720 as needed. As with the above embodiments, the variable stiffness material 930 (shown in Embodiments of the variable stiffness spherical joint may permit virtual mechanical mechanisms without determining the topology a priori, or allow changing the topology during operation. Some embodiments can allow another design variable, tailored stiffness and joint connectivity. Depending on the configuration of the variable stiffness spherical joint and of the variable stiffness elements, 1, 2, or 3 degrees of freedom may be freed for individual structural members that converge at a joint. Various embodiments allow the number of intersecting structural members to be greater than two, the number and location of structural member node connections that are selectively controllable to be greater than 1, and the number of rotational degrees of freedom that are selectable to be 1, 2, or 3. In some embodiments, the variable stiffness material may allow controllable restraint of the structural members, either by completely or partially releasing and securing the structural members, providing complete, partial, or substantially no resistance to motion, depending on the embodiment. In various embodiments, the placement of variable stiffness materials, for example shape memory polymers or their composites, within or between structural members at a node in a truss structure allows selective control of members of a structural node. As such, in some embodiments, it is possible to select which members are permitted to undergo large angular displacements (because of a mechanically underspecified/underconstrained linkage), and which members of a structural node are permitted to transmit loads. This can allow for customized levels of mechanical resistance, or “load tailoring” within a structure. Depending on the embodiment, the range and ease of motion of the structural members will be limited by the deformability of the variable stiffness material. For example, this will occur where the variable stiffness material directly connects the structural members. Thus, while allowing motion, the variable stiffness material can also restrict the range of motion, as well as control the ease with which the structural members may be moved. The range of motion can also be restricted by the addition of hard stops attached to the structural members and/or structural connectors. In other embodiments, the range of motion may be limited by mechanical linkages or interconnections, for example where the variable stiffness material couples/controls coupling of the structural members along with a mechanical linkage or other mechanical interconnection. The variable stiffness material may directly or indirectly couple the structural members together. The variable stiffness material may control the coupling between structural members if it directly or indirectly couples the structural members together, or if it inhibits a mechanical linkage which couples the structural members. Various embodiments, potentially provide the advantages of a controllable mechanical load switch at the joints and nodes of a truss-like structure. This could permit increases or decreases of deformation, switching of mechanical components into the load path, transferring strain energy to a different portion of the structure, preventing damage to or isolate a portion of a structure, reducing vibrations, creating hinges, moving structural portions for stowing and deploying, and affecting performance sensitive geometries such as reflectors and aerofoil surfaces. The structural members, connectors, and guides may be rigid, semi rigid, or even compliant in various embodiments. Various embodiments could be used in applications such as morphing aircraft wings or other structures, reconfigurable reflectors for space or other applications, tunable damping and crash structures for automobiles or other vehicles or crafts, and/or deployable structures. Many other applications and uses are possible. Although the term spherical joint is used herein, each of the structural members may have 1, 2, or 3 degrees of freedom. As such, the degrees of freedom of the joint may be termed planar, conical, and spherical, respectively. Selectively active variable stiffness materials may include materials controlled thermally, electrically, magnetically, chemically, and/or electromagnetically. Non-limiting examples of thermally controlled materials include shape memory polymers and shape memory alloys. A related class of thermal materials which change stiffness in association with a change in the phase of the material include solid-liquid phase change materials. Non-limiting examples of this type of phase change materials include metals and metal alloys, polymers, wax, water, etc. Non-limiting examples of materials which undergo a change in stiffness associated with the application of an electrical field include ferroelectric materials, electrostrictive polymers, liquid crystal elastomers, and electrorheological fluids. Non-limiting examples of materials which undergo a change in stiffness associated with the application of a magnetic field include magnetostrictive materials, ferromagnetic shape memory alloys, and magnetorheological materials. Variable stiffness materials such as baroplastics, solvable polymers, reversible adhesive polymers or structures may be utilized. Such materials, as well as other known materials, can provide a variable stiffness coupling means, which allow the stiffness of a connection to be changed, softened or stiffened, and then returned to, or close to, its original stiffness. The example embodiments herein are not intended to be limiting, various configurations and combinations of features are possible. Having described this invention in connection with a number of embodiments, modification will now certainly suggest itself to those skilled in the art. As such, the invention is not limited to the disclosed embodiments, except as required by the appended claims. |