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특허 상세정보

Canard type aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-005/04    B64C-005/10   
미국특허분류(USC) 244/45A ; 244/46 ; 244/214 ; 244/90R
출원번호 US-0859685 (1977-12-12)
우선권정보 DE-2656692 (1976-12-15)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 16  인용 특허 : 0
초록

The present canard type of aircraft comprises steering rudder elements which are tiltable substantially about the leading edge of each wing of the aircraft, whereby the respective edge of the rudder element extends alongside said leading edge of the respective wing. Another edge of the rudder element extends alongside a surface portion of the fuselage or body of the aircraft in close conformity with said surface portion, but movable relative thereto. A sealing may be inserted between the rudder element and the fuselage in such a manner that said movement...

대표
청구항

A canard type aircraft comprising fuselage means (6) having a longitudinal axis, wing means (4) operatively secured to said fuselage means, steering means (1′, 1″) operatively secured to said wing means so that said steering means are tiltable about a tilting axis extending at an acute angle relative to said longitudinal axis of said fuselage means (6), said steering means (1′, 1″) each comprising a first edge (5) facing the aircraft fuselage means (6), and a second edge (2, 3) facing the respective wing means (4), said first and second edges (2, 5; 3, 5...

이 특허를 인용한 특허 피인용횟수: 16

  1. Morgenstern, John M.; Arslan, Alan. Aircraft lift device for low sonic boom. USP2005086935592.
  2. Franklin, III, Walter M.; Morgenstern, John M.; Lee, Howard; Quayle, Brian; Hajic, Ken; Scarcello, John; Arslan, Alan E.. Aircraft tail configuration for sonic boom reduction. USP2004116824092.
  3. Arata,Allen A.; Graham,David H.. Aircraft with articulated leading edge of fuselage and wings. USP2007047204454.
  4. Arata,Allen A.. Aircraft with extendable leading edge of fuselage and wings. USP2007057216835.
  5. Arata,Allen A.. Aircraft with rotatable leading edge of fuselage and wings. USP2007077246770.
  6. Lockheed John A. (7925 Dead Indian Rd. Ashland OR 97520). Canard control system for aircraft. USP1989074848700.
  7. Martorella Romeo P. (Dix Hills NY) Chin Jimmie (Flushing NY). Flight control optimization system for multi-control surface aircraft. USP1989014797829.
  8. Klein Robert W. (Rancho Palos Verdes CA). Flight control system employing complementary filter. USP1987104697768.
  9. Bowcutt, Kevin G.. Hypersonic waverider variable leading edge flaps. USP2003106634594.
  10. Rao Dhanvada M. (Hampton VA). Leading edge flap system for aircraft control augmentation. USP1984124485992.
  11. Gleine Wolfgang,DEX ; Hilbig Reinhard,DEX ; Wendt Hans-Joachim,DEX. Method and apparatus for optimizing the aerodynamic effect of an airfoil. USP1999035875998.
  12. Staudacher Werner (Zorneding DEX). Method for steering an aircraft. USP1981054267990.
  13. Sakata Sumio T. (Seattle WA). Pitch control of swept wing aircraft. USP1986024569494.
  14. Smith Brian E.. Secondary wing system for use on an aircraft. USP1999115992796.
  15. Chang, Ming; Meza, Victor; Morgenstern, John M.; Arslan, Alan E.. Supersonic aircraft with channel relief control. USP2005076921045.
  16. Rao Dhanvada M. (Hampton VA) Murri Daniel G. (Grafton VA). Yaw and pitch control of air vehicles at high angles of attack. USP1988114786009.