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특허 상세정보

Hamilton H.N2 laminar flow diskette wing

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06   
미국특허분류(USC) 244/199.1; 244/198; 244/199.4; 244/201; 244/204; D12/319; D12/325; D12/333; D12/334; D12/314
출원번호 US-0932032 (2011-02-16)
등록번호 US-8382040 (2013-02-26)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 20
초록

A wing assembly has a wing and one or more no-bias laminar flow oval diskettes that are fixed on a support structure along the C/L (center of lift) of an airfoil, of an aircraft wing. The benefit of an oval diskette with laminar flow is that it has no speed limitations and it allows an aircraft to clime at a speed that matches its Ground Effect Lift speed which is a 25% performance increase and a 40% reduction in vortex drag with a increase stability that eliminates inertia coupling of high-speed airfoils.

대표
청구항

1. A laminar flow oval diskette flight assembly comprising: an oval diskette with a top surface bonded to a bottom surface that when suspended over the top of an aircraft wing along the center of gravity of an aircraft, having the said aircraft lifting surface, said oval diskette is suspended in a length wise direction with the apex of the oval diskette facing the direction of flight of the aircraft and overhang on the leading edge of the aircraft wing and with the long sides of the oval diskette parallel to direction of flight of the aircraft and the ta...

이 특허에 인용된 특허 (20)

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