Pyramid waffle core structure and method of fabrication
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F02K-001/82
B32B-003/12
E04B-001/84
B32B-003/26
B32B-005/02
B32B-007/04
B32B-037/00
B32B-037/14
B32B-037/18
B32B-037/20
B32B-005/24
B32B-003/30
G10K-011/172
F02K-001/78
B32B-003/10
B32B-037/12
B64D-033/02
출원번호
US-0245418
(2014-04-04)
등록번호
US-9284726
(2016-03-15)
발명자
/ 주소
Tien, Allan
출원인 / 주소
The Boeing Company
대리인 / 주소
Economou, John S.
인용정보
피인용 횟수 :
1인용 특허 :
16
초록▼
A structural core and associated method of forming such structure is disclosed. The structure includes a single layer of at least two rows of hollow pyramid-like structures. The hollow pyramid-like structures dampen acoustic noise and provide a truss-like structure that provides a high level of stif
A structural core and associated method of forming such structure is disclosed. The structure includes a single layer of at least two rows of hollow pyramid-like structures. The hollow pyramid-like structures dampen acoustic noise and provide a truss-like structure that provides a high level of stiffness against transverse loads, shear stresses and side-loading. The hollow pyramid-like structures preferably have upward facing and downward facing open bases, and are formed in rows and columns. To aid in sound attenuation, the single layer is formed from a partially porous material, a woven thermoplastic, woven carbon fiber, fiberglass and paper. To provide additional structural integrity, the single layer is formed from a solid non-porous material such as a metal. The structural core may be included within outer panels to form acoustical or structural panels.
대표청구항▼
1. A structural core comprising: a single layer of adjacent hollow pyramid-like structures, wherein the single layer is comprised of at least two rows of the adjacent hollow pyramid-like structures, each pyramid-like structure formed from four faces having substantially straight edges and having an
1. A structural core comprising: a single layer of adjacent hollow pyramid-like structures, wherein the single layer is comprised of at least two rows of the adjacent hollow pyramid-like structures, each pyramid-like structure formed from four faces having substantially straight edges and having an open base, each open base in one of the at least two rows offset with respect to each open base in an adjacent another of the at least two rows, the edges of each adjacent pyramid-like structure combining to form a truss-like structure for providing support against transverse loads applied to the structural core. 2. The structural core of claim 1, wherein the hollow pyramid-like structures have upward facing open bases. 3. The structural core of claim 1, wherein the hollow pyramid-like structures have downward facing open bases. 4. The structural core of claim 1, wherein the hollow pyramid-like structures have alternate upward facing and downward facing open bases. 5. The structural core of claim 1, wherein the single layer of hollow pyramid-like structures is formed in rows and columns of adjacent hollow pyramid-like structures. 6. The structural core of claim 1, wherein the single layer of hollow pyramid-like structures is formed from a partially porous material. 7. The structural core of claim 6, wherein the partially porous material is one of a woven thermoplastic, woven carbon fiber, fiberglass and paper. 8. The structural core of claim 1, wherein the single layer of hollow pyramid-like structures is formed from a solid non-porous material. 9. The structural core of claim 8, wherein the solid non-porous material is a metal. 10. A structural core, comprising: a plurality of rows bonded together laterally, each row formed from two ribbons, each ribbon having upper and lower edges forming a zig-zag pattern having an upper point and a lower point, each upper point of the zig-zag pattern on the upper edge directly above an adjacent upper point of the zig-zag pattern on the lower edge and each lower point of the zig-zag pattern on the upper edge directly above an adjacent lower point on the lower edge, the two ribbons bonded together along bonding lines running from each lower point of the zig-zag pattern on the upper edge to the two adjacent upper points of the zig-zag pattern on the lower edge, each ribbon having bend lines running from each upper and lower points of the zig-zag pattern on the upper edge to the adjacent respective upper and lower points of the zig-zag pattern on the lower edge, wherein the upper points of the zig-zag pattern on the upper edge and the lower points of the zig-zag pattern on the lower edge expand laterally as the two ends of the row are moved together, forming adjacent hollow pyramid-like structures having alternate upward-facing and downward-facing open bases, each hollow pyramid-like structure formed from four faces having substantially straight edges, each open base in one of the plurality of rows offset with respect to each open base in an adjacent another of plurality of rows, the edges of each adjacent pyramid-like structure combining to form a truss-like structure for providing support against transverse loads applied to the structural core. 11. The structural core of claim 10, wherein the plurality of rows are bonded together by bonding vertices of each upward-facing and downward-facing hollow pyramid-like structures in each row to the adjacent row. 12. The structural core of claim 10, wherein the ribbons are formed from a partially porous material. 13. The structural core of claim 12, wherein the partially porous material is one of a woven thermoplastic, woven carbon fiber, fiberglass and paper. 14. The structural core of claim 10, wherein the ribbons are formed from a solid non-porous material. 15. The structural core of claim 14, wherein the solid non-porous material is a metal. 16. A method of forming a structure, comprising the steps of: forming a plurality of ribbons, each ribbon having upper and lower edges forming a zig-zag pattern having an upper point and a lower point, each upper point of the zig-zag pattern on the upper edge directly above an adjacent upper point of the zig-zag pattern on the lower edge and each lower point of the zig-zag pattern on the upper edge directly above an adjacent lower point on the lower edge;forming a plurality of rows, each row formed from two ribbons bonded together along bonding lines running from each lower point of the zig-zag pattern on the upper edge to the two adjacent upper points of the zig-zag pattern on the lower edge, each ribbon having bend lines running from each upper and lower points of the zig-zag pattern on the upper edge to the adjacent respective upper and lower points of the zig-zag pattern on the lower edge, wherein the upper points of the zig-zag pattern on the upper edge and the lower points of the zig-zag pattern on the lower edge expand laterally as the two ends of the row are moved together, forming adjacent hollow pyramid-like structures having alternate upward-facing and downward-facing open bases, each hollow pyramid-like structure formed from four faces having substantially straight edges, each open base in one of the plurality of rows offset with respect to each open base in an adjacent another of the plurality of rows, the edges of each adjacent pyramid-like structure combining to form a truss-like structure for providing support against transverse loads applied to the structure; andbonding the plurality of rows together laterally to create a structural core having a plurality of rows and columns of adjacent hollow pyramid-like structures. 17. The method of claim 16, wherein the bonding step is performed by bonding vertices of each hollow pyramid-like structure in each row to the adjacent row. 18. The method of claim 16, further comprising the step of forming the structural core into a predetermined contoured shape. 19. The method of claim 16, further comprising the step of forming the structural core into a predetermined angled shape. 20. The method of claim 16, further comprising the step of bonding panels to a respective upper and lower surface of the structural core to create a panel structure including the structural core sandwiched between the two panels.
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이 특허에 인용된 특허 (16)
Peiffer, Alexander; Maier, Rudolf, Acoustic absorber for aircraft engines.
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