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Apparatus and method for reducing aircraft loads resulting from atmospheric turbulence and gusts 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-013/16
출원번호 US-0884581 (1992-05-18)
발명자 / 주소
  • Bleeg Robert J. (Mercer Island WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 47  인용 특허 : 0

초록 ▼

A controller for reducing unwanted sideways motion of an aircraft by reducing lateral side loads, resulting from air mass, turbulence and gusts. The controller functions in a manner that in the presence of higher frequency side loads, the rudder is caused to move in a relieving direction so that the

대표청구항 ▼

A control system for reducing aft body sideways loads on an aircraft by operation of an aircraft rudder, the control system comprising: a. means for sensing, prior to a yawing movement of the aircraft, side forces on a vertical stabilizer on the aircraft; b. means for generating a signal as a functi

이 특허를 인용한 특허 (47)

  1. Kari Appa, Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression.
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  2. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
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  3. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
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  4. Cotton Bryan S. ; Thornberg Christopher A. ; Walsh David M. ; Corning ; III Sherman, Aircraft course correction for wind and fuzzy logic course intercept profile based upon accuracy and efficiency.
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  5. Tran Chuong B. (Lynnwood WA) White Stephen (Bothell WA), Aircraft frequency adaptive modal suppression system.
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  6. Tran Chuong B. ; White Stephen, Aircraft frequency adaptive modal suppression system.
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  7. Tran Chuong B. ; White Stephen, Aircraft frequency adaptive modal suppression system.
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  8. Najmabadi, Kioumars; Tran, Chuong B.; Ho, John Koon-Hung, Aircraft multi-axis modal suppression system.
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  9. Najmabadi,Kioumars; Tran,Chuong B.; Ho,John Koon Hung, Aircraft multi-axis modal suppression system.
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  10. Gölling, Burkhard, Aircraft with wings and a system for minimizing the influence of unsteady flow states.
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  11. Pachikara, Abraham J.; Moser, Matthew A.; Carpenter, Paul H.; Finn, Michael R.; Koch, Thomas S.; Bieniawski, Stefan R.; Whitehead, Brian T., Closed loop control of aircraft control surfaces.
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  12. Altieri, Russell E.; Jolly, Mark R., Computer system and program product for controlling vibrations.
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  13. Enzinger,Michael; Kordt,Michael, Device and method for damping at least one of a rigid body mode and elastic mode of an aircraft.
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  14. Jolly, Mark R.; Badre-Alam, Askari; Altieri, Russell E.; Meyers, Andrew D., Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations.
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  15. Jolly, Mark R.; Badre-Alam, Askari; Altieri, Russell E.; Meyers, Andrew D., Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations.
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  16. Kubica, Fran.cedilla.ois; Cazy, Daniel; Marquier, Sylvie, Electrical fly-by-wire system for operating an aircraft rudder.
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  17. Whitehead, Brian T.; Bieniawski, Stefan R.; Halaas, David; Lavretsky, Eugene, Formation flight control.
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  18. Jolly, Mark R.; Black, Paul, Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations.
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  19. Jolly, Mark R.; Meyers, Andrew D.; Mellinger, Daniel; Ivers, Douglas E.; Badre-Alam, Askari; Swanson, Douglas A.; Altieri, Russell E., Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations.
    상세보기
  20. Jolly, Mark R.; Altieri, Russell E.; Badre-Alam, Askari; Ivers, Douglas E.; Swanson, Doug A.; Mellinger, Daniel; Meyers, Andrew D., Helicopter vibration control system and circular force generation systems for canceling vibrations.
    상세보기
  21. Jolly, Mark R.; Meyers, Andrew D.; Mellinger, Daniel; Ivers, Douglas E.; Badre-Alam, Askari; Swanson, Douglas A.; Altieri, Russell E., Helicopter vibration control system and circular force generation systems for canceling vibrations.
    상세보기
  22. Jolly, Mark; Hildebrand, Stephen; Altieri, Russell; Ferguson, Matthew; Ivers, Douglas, Helicopter vibration control system and rotary force generator for canceling vibrations.
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  23. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W., Horizontal tail load alleviation system.
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  24. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W., Horizontal tail load alleviation system.
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  25. Nadkarni Arun A. (Kirkland WA) Bryant William F. (Bellevue WA), Method and apparatus for detecting oscillatory phenomena indicative of airflow separation.
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  26. Wildschek, Andreas, Method and apparatus for minimizing dynamic structural loads of an aircraft.
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  27. Wildschek, Andreas; Hanis, Tomas, Method and apparatus for minimizing dynamic structural loads of an aircraft.
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  28. Jenaro Rabadan, Guillermo; Puig, Stephane, Method and device for attenuating the effects of turbulence on an aircraft.
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  29. Livet, Tania, Method and device for lightening loads on the wing system of an aircraft in roll motion.
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  30. Puig, Stephane; Byzery, Romeo, Method and device for reducing on an aircraft lateral effects of a turbulence.
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  31. Puig, Stéphane, Method and device for reducing on an aircraft lateral effects of a turbulence.
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  32. Van De Kreeke, Marc; Cassein, Guillaume, Method and system for controlling an aircraft control surface.
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  33. Pautsch, Christian; Wohlers, Wolfgang, Method and system for monitoring of the temperature of the surface of an aircraft.
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  34. Tanguy, Alain, Method for enhancing the aerodynamic efficiency of the vertical tail of an aircraft.
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  35. Tanguy, Alain, Method for improving the aerodynamic efficiency of the vertical tail of an aircraft.
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  36. Hahn, Klaus-Uwe, Method for reducing the turbulence and gust influences on the flying characteristics of aircraft, and a control device for this purpose.
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  37. Eglin,Paul, Method for using a steerable tall fin to reduce the vibration generated on the fuselage of a helicopter.
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  38. Eglin,Paul, Method for using a tiltable stabilizer to reduce vibration generated on the fuselage of a helicopter.
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  39. Pauly,Bernard, Method making it possible to prevent vibration of a rudder of an aircraft and aircraft using this method.
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  40. Singer, Donald James; Wilkens, Dean Richard, Methods and apparatus suitable for facilitating control of an aircraft rudder.
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  41. Van De Kreeke, Marc; Cassein, Guillaume, Process and system for moving a control surface of an aircraft.
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  42. Kubica,Fran챌ois; Briere,Dominique, Process for countering the vibrations induced in an aircraft by the windmilling of a fan and system of electric flight controls implementing this process.
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  43. McFarland R. E. ; Dulsenberg Ken, System and method for finite element simulation of helicopter turbulence.
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  44. Walton, Vincent M.; Borland, Christopher J.; Siu, Tze L.; Najmabadi, Kioumars; Coleman, Edward E.; Marquis, David P.; McMullin, Dianne L.; Milligan, Kevin H., Vertical gust suppression system for transport aircraft.
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  45. Najmabadi, Kioumars; Shivitz, William F.; Coleman, Edward Ernest; Ho, John Koon-hung; Johnson, Richard D.; Carver, William F.; Grubb, David W.; McIntosh, Robert James, Wing-body load alleviation for aircraft.
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  46. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E., Yaw damping system and method for aircraft.
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  47. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E., Yaw damping system and method for aircraft.
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