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특허 상세정보

Laminar supersonic transport aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/10    B64D-027/02   
미국특허분류(USC) 244/015 ; 244/045R ; 244/045A ; 244/214 ; 244/055 ; 244/204 ; D12/332 ; D12/341
출원번호 US-0805034 (1997-02-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Anderson
인용정보 피인용 횟수 : 43  인용 특허 : 0
초록

The present invention is a laminar supersonic transport aircraft having a reverse delta wing located between a forward section and a distal end of the aircraft, a set of jet engines superposed on another set of jet engines, a stabilizing vertical tail located near the distal end of the aircraft, a stabilizing canard surface located near the forward section of said aircraft. Also, a laminar flow control device can be incorporated within the wing. The reverse delta aerodynamic wing has a basic reverse delta wing portion bounded by a leading edge and by a p...

대표
청구항

[ What is claimed is:] [1.] A laminar supersonic transport aircraft having a forward section and a distal end, comprising:a reverse delta wing located between said forward section and said distal end of said aircraft;a first set of at least two jet engines located on a top surface of said reverse delta wing;a second set of at least two jet engines superposed to said first set of at least two jet engines on a bottom surface of said reverse delta wing;a stabilizing vertical tail located near said distal end of said aircraft; anda stabilizing canard surface...

이 특허를 인용한 특허 피인용횟수: 43

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  39. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
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