SPHERISTRUCTURE METHOD, SYSTEM, AND APPARATUS
A structural system and a method for joining a launch vehicle and with satellites are disclosed. The method includes generating centerlines of objects requiring a connection for a structure, generating hemispheres about the centerlines, shelling of the hemispheres; performing a finite element analysis (FEA) for verifying the strength of the structure; and increasing or decreasing the thickness of the hemispheres for providing both optimal strength and minimum mass for the structure. The novel design and construction of interconnected hemispheres provide nearly the maximum physical strength for a given amount of material that could otherwise not be accomplished by utilization of a single spherical structure. In addition, the structure permits the construction of modular elements that are readily constructed using generally low-cost, simple, reliable and verifiable methods.
1 . A method of providing a structure, said method comprising the steps of:
generating centerlines of objects requiring a connection for a structure;
generating hemispheres about said centerlines;
shelling of said hemispheres;
performing a finite element analysis (FEA) for verifying the strength of said structure; and
increasing or decreasing the thickness of said hemispheres for providing both optimal strength and minimum mass for said structure.
2 . The method of claim 1 , wherein said hemispheres generated intersect at a set of planes that are circular in shape.
3 . The method of claim 2 , wherein the diameter of at least one of said hemispheres generated is made large such that the intersection of said hemispheres provides a circular plane whose diameter is at least half the diameter of the smallest hemisphere in the connecting path.
4 . The method of claim 1 , wherein said hemispheres are generated from each plane of said objects as the axis of rotation for each hemisphere and the diameter of the maximum structure attach circle equaling the diameter of said hemisphere.
5 . The method of claim 1 , further comprising, prior to performing the FEA, slicing each of said hemispheres in symmetric fashion, about the axis of rotation and connecting flanges generated by projecting small joining planes away from the slicing planes.
6 . The method of claim 5 , further comprising joining the sliced hemispheres.
7 . A structural system, comprising:
objects; and
hemispherical membrane structures,
wherein said objects connect by intersections of said hemispherical membrane structures.
8 . The structural system of claim 7 , wherein said objects comprise a launch vehicle and satellites.
9 . The structural system of claim 7 , wherein each of said objects projects a centerline from its plane.
10 . The structural system of claim 8 , wherein said launch vehicle projects a centerline in the direction of planes of said satellites.
7 . structural system of claim 7 , wherein said objects comprise a launch vehicle interface ring and at least two satellite interface rings.
12 . The structural system of claim 7 , wherein said hemispherical membrane structures intersect at a set of planes that are circular in shape.
13 . The structural system of claim 7 , wherein each of said hemispherical membrane structures are sliced in symmetric fashion, about the axis of rotation and connecting flanges generated by projecting small joining planes away from the slicing planes.
14 . The structural system of claim 13 , wherein said sliced hemispherical membrane structures are joined.
15 . The structural system of claim 14 , wherein said sliced hemispherical membrane structures are joined using one of fasteners, rivets, and adhesives.
16 . The structural system of claim 13 , wherein the thickness of said hemispherical membrane structures is increased to provide optimal strength and minimum mass for said structural system.
17 . The structural system of claim 13 , wherein the thickness of said hemispherical membrane structures is decreased to provide optimal strength and minimum mass for said structural system.