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특허 상세정보

Monolithic composite wing manufacturing process

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B31C-013/00    B65H-081/00    B64C-003/00   
미국특허분류(USC) 156/189 ; 156/169 ; 156/172 ; 156/182 ; 156/184 ; 156/195 ; 156/425 ; 244/123
출원번호 US-0252750 (1999-02-19)
발명자 / 주소
인용정보 피인용 횟수 : 72  인용 특허 : 5
초록

A method of manufacturing a monolithic composite wing without using mechanical fasteners is described. The process begins with the formation of a center wing box in combination with a pair of spars, riblets and a pair of skin-molds including the wrapping and binding of the box by means of resin impregnated composite tapes. Next, additional cells are adjoined contiguously on either side of the current framework and an overlap wrapping and bonding process is continued around the current framework. The overlap wrapping and binding procedure provides increas...

대표
청구항

[ I claim:] [1.] A method of manufacturing a monolithic composite wing comprising the steps of:(a) fabricating a center wing box cell having a pair of longitudinally disposed U-shaped pre-formed spars, laterally disposed plurality of rib-lets between said spars, and a pair of resin impregnated wing skin-molds glued to upper and lower surfaces of said spars wherein said box cell is wrapped, compacted, and bonded by means of locally heated resin impregnated composite tapes in a plurality of layers along spanwise and helical directions; and(b) adjoining add...

이 특허를 인용한 특허 피인용횟수: 72

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