[특허]Method for continuously manufacturing composite hollow structure

Method for continuously manufacturing composite hollow structure 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B29C-070/38 B29C-047/12 B29C-070/52 B29C-047/10 B29C-047/26 B29C-047/02 B29C-047/00 B29C-070/54 B29C-035/02 B29C-035/08 B29C-070/00 B29C-070/20 B29C-070/22
출원번호	US-0130412 (2016-04-15)
등록번호	US-10105910 (2018-10-23)
발명자 / 주소	Tyler, Kenneth Lyle
출원인 / 주소	CC3D LLC
대리인 / 주소	Stockett, Ryan C.
인용정보	피인용 횟수 : 0 인용 특허 : 41

초록 ▼

A method is disclosed for continuously manufacturing a composite hollow structure. The method may include continuously coating fibers with a matrix, and revolving matrix-coated fibers about a non-fiber axis. The method may also include diverting the matrix-coated fibers radially outward away from th

대표청구항 ▼

1. A method of continuously manufacturing a composite hollow structure, comprising: continuously coating fibers with a matrix to form matrix-coated fibers;revolving the matrix-coated fibers about a non-fiber axis;diverting the matrix-coated fibers radially outward away from the non-fiber axis;dynamically adjusting a trajectory of the non-fiber axis of the composite hollow structure; andcuring the matrix-coated fibers to maintain the adjusted trajectory of the composite hollow structure. 2. The method of claim 1, wherein revolving matrix-coated fibers includes: revolving a first subset of the matrix-coated fibers in a first direction; andrevolving a second subset of the matrix-coated fibers in a second direction opposite the first direction. 3. The method of claim 2, wherein revolving the first and second subsets of matrix-coated fibers includes synchronously oscillating between the first and second directions. 4. The method of claim 2, wherein revolving the first and second subsets of matrix-coated fibers includes revolving the first and second subsets of matrix-coated fibers through a range of up to 180°. 5. The method of claim 4, wherein revolving the first and second subsets of matrix-coated fibers includes revolving the first and second subsets of matrix-coated fibers through a range of about 15° to about 30°. 6. The method of claim 2, wherein revolving the first and second subsets of the matrix-coated fibers includes revolving the first subset of the matrix-coated fibers through a range different than a revolving range of the second subset of the matrix-coated fibers. 7. The method of claim 2, wherein revolving the first and second subsets of the matrix-coated fibers includes continuously revolving the first subset of the matrix-coated fibers in the first direction and selectively revolving the second subset of the matrix coated fibers in the first direction. 8. The method of claim 2, wherein revolving the first and second subsets of the matrix-coated fibers includes revolving the first subset of the matrix-coated fibers at a first rate and revolving the second subset of the matrix-coated fibers at a second rate. 9. The method of claim 8, further including dynamically adjusting the first and second rates during manufacturing of the composite hollow structure. 10. The method of claim 2, further including dynamically adjusting a pattern of weave created by revolving the first and second subsets of matrix-coated fibers during manufacturing of the composite hollow structure. 11. The method of claim 2, further including pressing the first subset of the matrix-coated fibers against the second subset of the matrix-coated fibers. 12. The method of claim 11, further including varying the pressing to thereby adjust a wall thickness of the composite hollow structure. 13. The method of claim 2, wherein the first subset of the matrix-coated fibers has at least one of a different diameter and a different material type than the second subset of the matrix-coated fibers. 14. The method of claim 2, wherein the first subset of the matrix-coated fibers has a different type of matrix than the second subset of the matrix-coated fibers. 15. The method of claim 1, wherein curing the matrix-coated fibers includes curing the matrix-coated fibers from inside the composite hollow structure. 16. The method of claim 1, wherein curing the matrix-coated fibers includes directing at least one of UV light and ultrasonic vibrations toward the matrix-coated fibers. 17. The method of claim 16, further including controlling an environment of the matrix-coated fibers for a period of time during and after the at least one of the UV light and the ultrasonic vibrations are directed toward the matrix-coated fibers. 18. The method of claim 1, further including mechanically pinching the matrix-coated fibers prior to curing the matrix-coated fibers in order to fix a length of the composite hollow structure. 19. The method of claim 1, further including filling an interior of the composite hollow structure as the hollow structure is curing. 20. A method of continuously manufacturing a composite hollow structure, comprising: continuously coating fibers with a matrix to form matrix-coated fibers;revolving a first subset of the matrix-coated fibers in a first direction; andrevolving a second subset of the matrix-coated fibers in a second direction opposite the first;diverting the first and second subsets of the matrix-coated fibers radially outward away from a non-fiber axis;pressing the first subset of the matrix-coated fibers against the second subset of the matrix-coated fibers;dynamically adjusting revolving of the first and second subsets of the matrix-coated fibers during manufacturing of the composite hollow structure;curing the first and second subsets of the matrix-coated fibers to retain the adjusted first and second subsets of the matrix coated fibers; andmechanically pinching the first and second subsets of the matrix-coated fibers prior to curing the first and second subsets of the matrix-coated fibers in order to fix a length of the composite hollow structure.

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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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Method for continuously manufacturing composite hollow structure 원문보기

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Method for continuously manufacturing composite hollow structure 원문보기

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