Method and apparatus for processing open three-dimensional core structures such as folded honeycomb structures
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B28B-007/30
B28B-001/14
B29C-049/00
D03D-003/08
B32B-001/00
E04C-002/34
출원번호
UP-0083391
(2005-03-17)
등록번호
US-7749420
(2010-07-26)
우선권정보
DE-10 2004 013 144(2004-03-17)
발명자
/ 주소
Endres, Gregor Christian
Weber, Hans-Juergen
출원인 / 주소
Airbus Deutschland GmbH
대리인 / 주소
Fasse, W. F.
인용정보
피인용 횟수 :
0인용 특허 :
19
초록▼
A method and an apparatus facilitate the processing of a core structure for a composite sandwich structure. The core has an open three-dimensional structure and is not self-supporting due to an insufficient strength or stiffness. The method involves temporarily providing a support arrangement on the
A method and an apparatus facilitate the processing of a core structure for a composite sandwich structure. The core has an open three-dimensional structure and is not self-supporting due to an insufficient strength or stiffness. The method involves temporarily providing a support arrangement on the core structure to mechanically support and stabilize it, then subjecting the supported core structure to the desired processing, and then separating and removing the core structure and the support arrangement from one another. The processing can involve immersion into a processing liquid such as a curable resin, or mechanical machining operations. The support arrangement preferably includes a core impression that is surfacially form-fitting on a structured surface of the core structure. The apparatus includes a support arrangement including a core impression to be disposed on a surface of the core structure. The core impression may be formed of a polymer, a metal, or a casting material.
대표청구항▼
What is claimed is: 1. A method of processing a core structure for a composite structure, comprising the steps: a) providing a folded valley core structure that has opposite first and second major surfaces having a structured shape configured with an open three-dimensionally contoured configuration
What is claimed is: 1. A method of processing a core structure for a composite structure, comprising the steps: a) providing a folded valley core structure that has opposite first and second major surfaces having a structured shape configured with an open three-dimensionally contoured configuration with continuous transverse fold valley channels extending respectively along each of said major surfaces of said core structure, and that is not a honeycomb core having open cells extending perpendicularly to a major plane of the core, and that alone is not self-supporting due to an insufficient strength and/or stiffness; b) temporarily providing a first support arrangement including at least a first core support arranged form-fittingly on at least a first partial area of said first major surface of said core structure to mechanically support and stabilize said core structure having said three-dimensionally contoured configuration, wherein said first core support form-fittingly fills said fold valley channels at least in said first partial area on only said first major surface and not on said second major surface, wherein said first core support comprises a form-fitting first core impression, and wherein said step b) comprises disposing said first core impression form-fittingly on at least said first partial area of said first major surface of said core structure; c) while said core structure is supported and stabilized by said first support arrangement, subjecting said core structure to a first processing; d) after said first processing, then separating and removing said core structure and said first support arrangement from one another; e) temporarily providing a second support arrangement comprising a form-fitting second core impression on said core structure to mechanically support and stabilize said core structure, by disposing said second core impression form-fittingly on at least a second partial area of said second major surface of said core structure, wherein said second core impression form-fittingly fills said fold valley channels at least in said second partial area on only said second major surface and not on said first major surface; f) while said core structure is supported and stabilized by said second support arrangement, subjecting said core structure to a second processing; and g) after said second processing, separating and removing said core structure and said second support arrangement from one another; and h) after said step d), sandwiching said core structure between two cover layers. 2. The method according to claim 1, wherein said step b) further comprises fixing said first core impression on said core structure after said disposing. 3. The method according to claim 2, wherein said fixing comprises applying a reduced pressure or vacuum between said first core impression and said first major surface of said core structure. 4. The method according to claim 2, wherein said fixing comprises clamping said first core impression onto said core structure with clamp elements. 5. The method according to claim 1, further comprising forming said first core impression by casting or molding an impression material to form-fittingly match said fold valley channels of said structured shape of said first major surface of said core structure. 6. The method according to claim 5, wherein said casting or molding comprises temporarily supporting said core structure and casting or molding said impression material using said first major surface of said core structure as a form or mold while said core structure is temporarily supported. 7. The method according to claim 1, wherein said disposing of said first core impression on said first major surface comprises temporarily supporting said core structure and applying a curable or hardenable impression material onto said first major surface and then curing or hardening said impression material so as to stiffen said impression material and form thereof said first core impression while said core structure is temporarily supported. 8. The method according to claim 1, wherein said first processing and said second processing comprise carrying out a same process for said first processing in said step c) and for said second processing in said step f). 9. The method according to claim 1, wherein said step c) comprises subjecting said second major surface of said core structure to said first processing, and said step f) comprises subjecting said first major surface of said core structure to said second processing. 10. The method according to claim 1, wherein said first support arrangement and said core structure together form a processing unit in said steps b) and c), and said first processing in said step c) comprises introducing said processing unit at least partially into a processing bath. 11. The method according to claim 10, wherein said processing bath contains a processing liquid, and wherein said introducing of said processing unit into said processing bath comprises dipping said processing unit partially into said processing liquid, or submerging said processing unit entirely in said processing liquid, or moving said processing unit through said processing liquid, so that said core structure becomes coated and/or impregnated with said processing liquid. 12. The method according to claim 11, wherein said processing liquid comprises a curable or hardenable polymer material. 13. The method according to claim 1, wherein said step b) further comprises fixing said core structure on said first support arrangement, and said first processing in said step c) comprises a mechanical machining of said core structure. 14. A method of processing a core structure for a composite structure, comprising the steps: a) providing a folded valley core structure that has an open three-dimensionally contoured configuration with a three-dimensionally contoured first major surface and a three-dimensionally contoured second major surface with continuous transverse fold valley channels extending respectively along each of said major surfaces, wherein said core structure alone is not self-supporting due to an insufficient strength and/or stiffness; b) temporarily providing a first core support on only said first major surface of said core structure to mechanically support and stabilize said core structure, wherein said first core support has a contoured shape that form-fittingly mates with said fold valley channels on said first major surface; c) while said core structure is supported and stabilized by said first core support, leaving said fold valley channels on said second major surface open and exposed, and subjecting said second major surface of said core structure to a first processing; d) after said first processing, separating and removing said core structure and said first core support from one another; e) after said first processing, temporarily providing a second core support on only said second major surface of said core structure to mechanically support and stabilize said core structure, wherein said second core support has a contoured shape that form-fittingly mates with said fold valley channels on said second major surface; f) while said core structure is supported and stabilized by said second core support, leaving said fold valley channels on said first major surface open and exposed, and subjecting said first major surface of said core structure to a second processing; and g) after said second processing, separating and removing said core structure and said second core support from one another. 15. The method according to claim 1, wherein said first partial area is a lattice-shaped area and said first core support has a lattice shape with openings therein corresponding to said lattice-shaped area. 16. The method according to claim 1, wherein said first core support is formed of a flexurally stiff polymer material. 17. The method according to claim 1, wherein said first core support is formed of a flexurally stiff metal material. 18. The method according to claim 17, further comprising applying a release coating on said metal material. 19. The method according to claim 7, wherein said impression material is a silicone elastomer. 20. The method according to claim 1, wherein said first support arrangement further includes a mechanically rigid supporting understructure that carries and supports said first core support thereon. 21. The method according to claim 1, wherein an impression surface of said first core support is a continuous solid surface that is form-fitting on said first partial area of said first major surface of said core structure. 22. The method according to claim 1, wherein an impression surface of said first core support is a perforate mesh or grid surface that is form-fitting on said first partial area of said first major surface of said core structure. 23. The method according to claim 3, wherein said reduced pressure or vacuum is applied through at least one suction hole in said first core impression, by a suction source connected to said suction hole.
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이 특허에 인용된 특허 (19)
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Ichikawa Hiroo (18-9 ; Nishi-Waseda 3-chome Shinjuku-ku ; Tokyo 160 JPX), Method of production of reinforced composite corrugated body and method of formation of corrugating rollers for use ther.
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