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특허 상세정보

Control surface continuous seal

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/06   
미국특허분류(USC) 244/217 ; 244/075R ; 244/215 ; 244/219 ; 244/214
출원번호 US-0958717 (1997-10-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Anderson
인용정보 피인용 횟수 : 46  인용 특허 : 0
초록

A continuous skin and seal airfoil comprises a rigid structural wing box located centrally chordwise and extending spanwise and including a spanwise extending spar, an upper skin surface and a lower skin surface. Upper and lower control surfaces are pivotally mounted on the spar for movement about a spanwise extending axis between an elevated position and a lowered position and includes an upper skin surface. In similar fashion, a lower control surface is pivotally mounted on the wing box for movement about a spanwise extending axis between an elevated p...

대표
청구항

[ What is claimed is:] [10.] A continuous skin and seal airfoil comprising:a rigid structural wing box located centrally chordwise and extending spanwise and including a spanwise extending spar, an upper skin surface and a lower skin surface;an upper control surface pivotally mounted on said spar for movement about a spanwise extending axis between an elevated position and a lowered position, said upper control surface including an upper skin surface;a lower control surface pivotally mounted on said wing box for movement about a spanwise extending axis b...

이 특허를 인용한 특허 피인용횟수: 46

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