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특허 상세정보

Supersonic aircraft with channel relief control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-005/02   
미국특허분류(USC) 244/015; 244/045.R; 244/087
출원번호 US-0696796 (2003-10-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Koestner Bertani LLP
인용정보 피인용 횟수 : 8  인용 특허 : 22
초록

A supersonic aircraft comprises a fuselage extending forward and aft along a longitudinal axis, the fuselage having a lower surface and an upper surface, a highly swept low aspect ratio wing coupled to the fuselage and having a forward leading edge and an aft trailing edge, an effector flap coupled to the wing trailing edge, and a tail empennage. The tail empennage is coupled to the fuselage aft of the wing on the fuselage upper surface in a position high relative to the wing. The tail empennage forms a channel region subject to complex shock patterns at...

대표
청구항

1. A supersonic aircraft comprising:a fuselage extending forward and aft along a longitudinal axis, the fuselage having a lower surface and an upper surface;a highly swept low aspect ratio wing coupled to the fuselage, the wing having a forward leading edge and an aft trailing edge;an effector flap coupled to the wing trailing edge;a tail empennage coupled to the fuselage aft of the wing on the fuselage upper surface in a position high relative to the wing, the tail empennage forming a channel region subject to complex shock patterns and having an invert...

이 특허에 인용된 특허 (22)

  1. Brighton Trevor A,GBX. Aircraft undercarriage lock mechanism. USP2001086279853.
  2. Kelley-Wickemeyer Robert H. ; Seidel Gerhard E. ; Anast Peter Z. ; McLean James Douglas. Airplane with unswept slotted cruise wing airfoil. USP2001096293497.
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  8. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2003066575406.
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  17. Frosch Robert A. Administrator of the National Aeronautics and Space Administration ; with respect to an invention of ( Setauket NY) Stevens Martin L. (Setauket NY). Surface conforming thermal/pressure seal. USP1981094290612.
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