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특허 상세정보

Aircraft multi-axis modal suppression system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/16    B64C-013/00   
미국특허분류(USC) 244/195; 244/177; 244/075.1
출원번호 US-0180309 (2005-07-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 7  인용 특허 : 27
초록이 없습니다.
대표청구항이 없습니다

이 특허에 인용된 특허 (27)

  1. Reed ; III Wilmer H. (Hampton VA). Active control device for aircraft tail buffet alleviation. USP1996085549260.
  2. Tulinius Jan (Huntington Beach CA). Active flexible wing aircraft control system. USP1992015082207.
  3. Destuynder Roger (Noisy le Sec FRX) Bouttes Jacques (Paris FRX) Poisson-Quinton Philippe (Paris FRX). Active method and installation for the reduction of buffeting of the wings of an aircraft. USP1987114706902.
  4. Tran Chuong B. (Lynnwood WA) White Stephen (Bothell WA). Aircraft frequency adaptive modal suppression system. USP1995095452865.
  5. Tran Chuong B. (Lynnwood WA) White Stephen (Bothell WA). Aircraft frequency adaptive modal suppression system. USP1997095667166.
  6. Tran Chuong B. ; White Stephen. Aircraft frequency adaptive modal suppression system. USP1998115833173.
  7. Tran Chuong B. ; White Stephen. Aircraft frequency adaptive modal suppression system. USP1999015860625.
  8. Chakravarty Abhijit J. M. (Renton WA) Cooper Steven R. (Seattle WA) Ho John K. H. (Renton WA) Tran Chuong B. (Everett WA). Aircraft modal suppression system. USP1991125072893.
  9. Bilange Thierry,FRX ; Divoux-Plantaz Marie-Laure,FRX. Aircraft with reduced wing structure loading. USP2000056064923.
  10. Bleeg Robert J. (Mercer Island WA). Apparatus and method for reducing aircraft loads resulting from atmospheric turbulence and gusts. USP1994125375794.
  11. Bteille Roger H. (Blagnac FRX). Fixed-wing aircraft with tandem supporting surfaces. USP1986074598888.
  12. Whitaker ; Sr. Robert H. (Atlanta GA). Flight control device for airplanes. USP1984064455004.
  13. Shinagawa Takashi,JPX. Flight control system for airplane. USP2001016168117.
  14. Ako Hidenobu (Redmond WA). Flutter control system for aircraft wings. USP1992085135186.
  15. Gilyard Glenn B.. In-flight adaptive performance optimization (APO) control using redundant control effectors of an aircraft. USP1999065908176.
  16. Gangsaas Dagfinn (Bellevue WA) Norman Daniel C. (Renton WA). Maneuver enchancement and gust alleviation system. USP1989044821981.
  17. Lewis George E. (Renton WA). Maneuver load alleviation system. USP1989014796192.
  18. Nadkarni Arun A. (Kirkland WA) Bryant William F. (Bellevue WA). Method and apparatus for detecting oscillatory phenomena indicative of airflow separation. USP1997025598991.
  19. Deck Timothy D. (Renton WA) Lochtie David W. (Bellevue WA). Method and apparatus for providing a dynamic thrust asymmetry rudder compensation command with no direct thrust measurem. USP1997085657949.
  20. Bryant William F. (Bellevue WA) Nadkarni Arun A. (Kirkland WA) Salo Paul (Seattle WA). Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to at. USP1997095669582.
  21. Kelm Roland,DEX ; Grabietz Michael,DEX. Method of reducing wind gust loads acting on an aircraft. USP2000126161801.
  22. Wykes, John H.; Miller, Gerald D.. Stability augmentation system for a forward swept wing aircraft. USP1985124562546.
  23. Juergen Becker DE. System and method for compensating structural vibrations of an aircraft caused by outside disturbances. USP2002076416017.
  24. Lacabanne Michel (Saint-Orens FRX). System enabling the flutter behavior of an aircraft to be improved. USP1993075224667.
  25. Fabre Pierre (Toulouse FRX) Le Tron Xavier (Toulouse FRX) Lacoste Philippe (Toulouse FRX). System for reducing the forces applied to the wings and particularly to the root of the wings of an aircraft in flight. USP1993025186416.
  26. Schnelz James R. ; Powell Donald T.. Tuned engine mounting system for jet aircraft. USP2001026189830.
  27. Rogers John T. (Bellevue WA) Manning Kenneth J. R. (Bellevue WA). Wing load alleviation system using tabbed allerons. USP1984104479620.