# US 5,333,003 A · Laminated composite shell structure having improved thermoplastic properties and method for its fabrication > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 5,333,003 A - Document ID: US5333003A - Status: Granted - Kind: A - Application number: 07/823,419 - Filed: 1992-01-21 - Granted: 1994-07-26 - Earliest claimed: 1992-01-21 - Assignees: TRW Inc. - Inventors: John S. Archer - Web page: https://patentgrep.com/patent/US5333003A ## CPC - H01Q 15/144: {with a honeycomb, cellular or foamed sandwich structure} - H01Q: ANTENNAS, i.e. RADIO AERIALS (radiators or antennas for microwave heating H05B6/72) ## Abstract A laminated composite shell structure having quasi-isotropic thermal expansion and contraction characteristics and a method for its fabrication. The laminated composite shell structure includes multiple layers of overlapping strips of composite material conforming to an axisymmetric doubly-curved surface. The fibers in the multiple layers are arranged at different relative angular orientations, with the composite strips being shaped to maintain the fibers at a constant relative angular orientation throughout the shell structure. ## Claims ### Claim 1 A laminated composite shell structure having improved thermoelastic properties, comprising: multiple layers of overlapping strips of composite material conforming to an axisymmetric doubly-curved surface, the fibers in the multiple layers being arranged at different relative angular orientations; wherein the composite strips are shaped to maintain the fibers at a constant relative angular orientation throughout the shell structure, thus providing a shell structure having quasi-isotropic thermal expansion and contraction characteristics. ### Claim 2 (depends on 1) The laminated composite shell structure as set forth in claim 1, wherein each composite strip includes multiple piecewise straight segments of composite material. ### Claim 3 (depends on 1) The laminated composite shell structure as set forth in claim 1, wherein the strips of composite material are strips of unidirectional graphite fiber reinforced epoxy tape. ### Claim 4 A method for fabricating a laminated composite shell structure having improved thermoelastic properties, comprising the steps of: generating a three-dimensional strip pattern that conforms to an axisymmetric doubly-curved surface and can be rotated any angle about the vertex of the curved surface relative to an identical fixed strip pattern with centerlines of the strips in the rotated pattern intercepting centerlines of the strips in the fixed pattern at the same angle and at the angle of rotation; generating a planar strip pattern from the the three-dimensional strip pattern; cutting multiple layers of composite strips using the planar strip pattern; laying the composite strips in place on a three-dimensional mold to form multiple layers of overlapping composite strips, the fibers in the multiple layers being arranged at different relative angular orientations; and curing the composite strips; wherein the composite strips are shaped to maintain the fibers at a constant relative angular orientation throughout the shell structure, thus providing a shell structure having quasi-isotropic thermal expansion and contraction characteristics. ### Claim 5 (depends on 4) The fabrication method as set forth in claim 4, wherein the step of generating a planar strip pattern includes the step of developing the three-dimensional strip pattern onto a planar surface. ### Claim 6 (depends on 4) The fabrication method as set forth in claim 4, wherein the step of generating a planar strip pattern includes the step of cutting the planar strip pattern directly on a three-dimensional mold of the shell structure having the three-dimensional strip pattern inscribed on its surface. ### Claim 7 (depends on 4) The fabrication method as set forth in claim 4, wherein the step of generating a three-dimensional strip pattern includes the step of generating a strip pattern on the curved surface such that the local angle of intersection between a plane at any angle .THETA. and each of a set of lines defining the strips is equal to the angle .THETA. that the plane makes with the X-axis of the strip pattern, the local angle of intersection being defined as the angle measured in the plane of tangency to the curved surface between a normal to the plane and the tangent to the line at the point of intersection, the plane including the vertex of the curved surface. ### Claim 8 (depends on 7) The fabrication method as set forth in claim 7, wherein the step of generating a three-dimensional strip pattern includes the step of varying .THETA. from 0.degree. to 90 .degree. and constructing a set of lines on the doubly-curved surface that extend from initial positions on the surface in the XZ plane, each line being extended from its initial position by incrementally adding infinitesimal segments on the curved surface such that these segments intersect the plane at the angle .THETA.. ### Claim 9 (depends on 5) The fabrication method as set forth in claim 5, wherein the step of developing the three-dimensional strip pattern onto a planar surface includes the steps of: generating successive line segments in a developed line corresponding to successive line segments in an original line in the curved surface; maintaining the cumulative length of the developed line equal to the cumulative length of the original line; and ensuring that the angle between each segment of the original line and a local segment of a meridian curve drawn at a constant distance from the planar surface face is equal to the angle between the corresponding segment of the developed line and a line in the planar surface drawn parallel to the local segment of the meridian curve. ### Claim 10 A method for developing a line in a curved surface onto a planar surface for fabricating a laminated composite shell structure having improved thermoelastic properties, comprising the steps of: generating successive line segments in a developed line corresponding to successive line segments in an original line in the curved surface; maintaining the cumulative length of the developed line equal to the cumulative length of the original line; and ensuring that the angle between each segment of the original line and a local segment of a meridian curve drawn at a constant distance from the planar surface is equal to the angle between the corresponding segment of the developed line and a line in the planar surface drawn parallel to the local segment of the meridian curve; wherein the line in the planar surface is used for generating a planar strip pattern from a three-dimensional strip pattern that conforms to an axisymmetric doubly-curved surface and can be rotated any angle about the vertex of the curved surface relative to an identical fixed strip pattern, with centerlines of the strips in the rotated pattern intercepting centerlines of the strips in the fixed pattern at the same angle and at the angle of rotation.