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특허 상세정보

Elastomeric transition for aircraft control surface

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/52   
미국특허분류(USC) 244/215 ; 244/219 ; 244/130
출원번호 US-0059725 (1998-01-09)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Anderson
인용정보 피인용 횟수 : 43  인용 특허 : 12
초록

Elastomeric transition sections (118, 124) are mounted between the upper and lower portions of a wing (100) and a control surface (102) hinged thereto. The elastomeric transition sections include elastomeric material (126) having a plurality of holes (128) formed therethrough. Flexible rods (134, 136) are secured to either the wing or the control surface and extend through the holes (128) in the elastomeric material (126). The elastomeric transition sections provide a smooth aerodynamic transition between the wing and the control surface while permitting...

대표
청구항

[ What is claimed is:] [1.] An aircraft wing assembly, comprising:a main wing portion;a control surface having a forward end, an inboard edge and an outboard edge, the forward end being attached to the main wing portion for movement of the control surface relative to the main wing portion; anda single elastomeric transition section joining the main wing portion to the forward end, the inboard edge and the outboard edge of the control surface, for mitigating aerodynamic discontinuities occurring therebetween.

이 특허를 인용한 특허 피인용횟수: 43

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