This invention relates to collapsible structural members or beams and more particularly to collapsible structural members which use substantially identical modules to form beam which are rigid in three dimensions.
Various collapsible members have been used to form beams for collapsible structures such as temporary buildings and tents and also for work arms to position working tools in awkward locations. The collapsible structural members typically employ cables as tensioning members to bring separate segments or modules together to form a rigid structure. Such prior art structures usually rely on the cable itself to provide rigidity to the member or to separate pins or fasteners which must be installed to obtain rigidity and must be removed to permit collapse of the structure. Usually collapsible structural members require multiple parts and also require substantial time to form a structure and to collapse that structure.
There is a need for a collapsible structural member which is simple to erect and to collapse and uses a minimum number of parts. It appears also that there is a need for a collapsible structural member which uses a tensioning member to bring the parts together but which locks them in a position so that they are not reliant on the tensioning member for rigidity or strength.
An object of the invention is to provide a collapsible structural member which is simple and eliminates the need for many removable parts.
Another object of the invention is to provide a collapsible structure member where a tensioning member is used to bring components, segments or modules of the structure together and into a position in which the components lock together frictionally and are maintained in the locked position without undue loading required on the tensioning member.
A further object of the invention is to provide a collapsible beam structure which uses frictional locking principles similar to that used in Morse tapers for locking tapered drill bits and complementary tapered rotatable chucks to provide frictional locking between the drill and the chuck to transmit rotational torque.
Still another object of the invention is to provide a collapsible beam structure having the ability of locking adjacent modules relative to each other using complementary spherical locking surfaces to provide a frictional lock required to hold the modules in a rigid position relative to each other whether the modules are aligned axially or at an angle to each and independently of the cable or tensioning member.
The objects of the invention are attained by a collapsible structural member utilizing a plurality of substantially identical adjacent modules with each of the modules including an elongated body with a pair of oppositely facing walls forming a head at one end and a skirt forming a socket at the other end to receive the head of an adjacent module. Each of the heads forms a pair of outwardly facing spherical concave locking surfaces facing away from each other and the skirts of each of the modules form concave complementary spherical locking surfaces facing each other. A passage is formed within the modules to extend longitudinally from the head and through the skirt to receive a tensioning member in the form of a cable. Upon application of the tension to the cable at the skirt of an end module of a number of modules on the cable to bring the pair of convex spherical locking surface of the head portions of each module into frictional locking engagement with a pair of concave locking surfaces of an adjacent one of the modules to form a lock between the adjacent modules of all of the modules. Stops are formed on each module to determine the angular relation of the modules so that the collapsible beam can be curved or straight and to form a rigid but collapsible structural member. The cable is used to maintain the position of the modules and upon release permits the cable to be collapsed.
The present invention utilizes a concept of spherical frictional locking surfaces.
A common example of a frictional locking surface is the conical form found in the Morse taper invented by Steven A. Morse about 1864 and still in wide commercial use in drill presses and lathes. In such a locking arrangement the conical end of a shaft of a tool or drill bit has an included angle at the apex of about seven degrees (7°) or less. When the tool is inserted in a chuck having a complementary conical socket with the same included angle, friction alone maintains the tool in the socket. A small axial force applied to the tool to bring the tapered locking surfaces into engagement with each other is sufficient to frictionally lock the shank of the tool in torque transmitting relationship to the socket. A similar axial force in the opposite direction is applied to disconnect the tapered locking surfaces from each other.
The locking surfaces employed in the present invention uses opposed complementary spherical locking surfaces to form a frictional locking angle of about seven degrees (7°) or less. The spherical surfaces are used to accommodate angled positions of modules relative to each other.
A collapsible beam 10 of the present invention is made up of a plurality of modules or beads 12. The modules 12 are substantially identical to each other when the beam 10 is to be straight and vary only slightly from each other if any portion of the beam is to be curved. The modules required for straight beams or those curved in a single plane will be discussed first.
Each module 12 of the plurality of modules forming a collapsible beam 10 has a generally flat and elongated body portion 14 with a head 16 at one end and a skirt 18 at the other end forming a receiving socket 20 for the head 16 of an adjacent module 12.
Each module 12 is generally flat with front and back walls 22 which are identical to each other but facing in opposite directions from an imaginary longitudinal plane indicated at 24 in
The side walls 26 of the head 16 are portions of the circumference of a circle with the center of radius 33 being located at the point 34 as seen in
Front and back walls 22 of head 16 have identical convex surfaces 38 which are formed by opposed segments of a sphere having a radius 39 centered at point 40 in
By making the radius approximately the length of the illustrated modules as illustrated in the drawings, the appropriate seven-degree (7°) or less included angle for frictional locking will be obtained. In the present case, if the overall length of the module is about three inches, the radius 39 could be approximately three inches and centered at 40 as seen in
The sockets 20 in the skirts 18 of each of the modulesl2 are provided with a pair of concave spherical locking surfaces 46 which face each other and are complementary to the spherical convex locking surfaces 38 on the head 16 of an adjacent module.
The concave locking surface 46 in socket 20 are generated with a radius 45 substantially equal to radius 42 used to form the complementary spherical locking surface 38 with the convex shape. Referring to
The passages 32 formed longitudinally of each module 12 serve to receive a cable or tensioning member 48 in which the modules or beads 12 are strung as best seen in
The plurality of adjacent modules 12 in a collapsible beam 10 are maintained in line with each other by the cable or other tensioning member 48 extending in axial passage 32 in each of the modules 12 as best seen in FIG. 8. The cable has been omitted in most of the other figures to simplify the drawings. The passages 32 and the cable 48 are so arranged that the modules 12 are in substantial alignment with each other in the collapsed condition of the structural members 10 with a portion of the head 16 in the socket 20 of an adjacent module as illustrated by the two modules in
The straight or angled position of adjacent modules 12 in their interlocked relation is determined by a pair of stop elements 50 formed on each of the front and back walls 22 of the head 16 of each of the modules 12 as seen in
The four stop elements 50 are adapted to engage four stop recesses or notches 52 formed in the end wall 37 of the skirt 18 of an adjacent module 12. The end walls 37 on skirts 18 coincide with the transverse plane 42 so that as seen in
In the preferred embodiment of the invention shown in
The modules for any given size are molded of plastic material and the only differences between modules for straight beams and for curved beams is the position of the stop elements 50. To create a collapsible structural member 10 only a few different modules are required namely those for straight beam portions and those for curved beam portions. Even here the inventory is simplified because modules for angled connection form an angle either to the left or to the right by simply turning the module one hundred eighty degrees (180°) about its longitudinal axis 26.
Thus far the modules 12 had been described as substantially identical except for the positioning of stop elements 50 to make curves in the collapsible structural member 10. However, in
A further modification can be made to the modules 12 in the event a collapsible structural beam is to be curved in more than a single plane, that is a three-dimensional curve or for example such as that that would occur in a spiral on helix as illustrated diagrammatically in
Still another variation of modules 12 can be made by bending the head 16 relative to skirt 18 out of the longitudinal plane 24 as seen in
In all of the modifications of the basic module 12 seen in
A three-dimension beam 60 is shown in
A two dimensional beam 64 is illustrated in
A collapsible beam structure has been providing a variety of straight or curved structural members of various sizes utilizing a basic module to be molded of plastic material. The basic module 12 is used to form straight beam structures and is modified slightly by repositioning stop elements 50, which determine the angular position of adjacent modules relative to each other. The basic module 12 is further modified to twist the head 16 relative to the head receiving socket 20 as in module 12B or to bend the head portion 16 relative to the socket portion 20 relative to the longitudinal transverse plane 28 of the modules 12 or to elongate the module as in module 12A by separating the head 16 and socket 20 and stretching the skirt portion 18 of the module 12 with a greater distance than the basic module 12. By selecting and arranging the basic module 12 and modified modules 12A, 12B and 12C, regular and irregular configurations of structural beams can be constructed using only a few different modified modules to accomplish the end result.
The beam structure of the present invention are rigid not only in a single plane or three planes but are rigid radially relative to the central axis of all of the modules. The structural strength comes from the frictional locking surfaces and the tensioning cable is required only to maintain the position of the modules.
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Number | Date | Country | |
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20070261320 A1 | Nov 2007 | US |