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Rotorcraft autopilot system, components and methods

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-027/68
  • B64C-013/18
  • B64C-027/57
  • B64C-013/30
출원번호 US-0415469 (2017-01-25)
등록번호 US-10059441 (2018-08-28)
발명자 / 주소
  • Mercer, John E.
  • Feifel, Marc
  • Marvin, Mark
  • Albion, Nicolas
출원인 / 주소
  • MERLIN TECHNOLOGY, INC.
대리인 / 주소
    Pritzkau Patent Group LLC
인용정보 피인용 횟수 : 0  인용 특허 : 41

초록

An autopilot actuator includes first and second motors each including a rotatable motor output shaft such that either one or both of the motors can drive an actuator output shaft. An autopilot main unit enclosure is removably mounted to the helicopter proximate to a cyclic control and commonly house

대표청구항

1. An autopilot system for a helicopter, comprising: an autopilot display unit that is mounted in an instrument console of the helicopter at least for displaying autopilot flight data to a pilot of the helicopter;an autopilot main unit enclosure that is removably mounted to the helicopter proximate

이 특허에 인용된 특허 (41)

  1. Hegg Jeffrey W. (N. Reddington Beach FL) Yount Larry J. (Scottsdale AZ) Potter William F. (Glendale AZ), Active hand controller redundancy and architecture.
  2. Hanlon, Casey; Ezran, Shmuel; Christensen, Don, Active pilot inceptor with self warm-up.
  3. Adams Don L. ; Provenzano Thomas J. ; Novis Ari M. ; Crowley Ann, Aircraft flight mode selector system.
  4. Briffe Michel,FRX ; Mitaux-Maurouard Guy,FRX, Apparatus and mehod for aircraft monitoring and control including electronic check-list management.
  5. Murphy Richard D. (Monroe CT) Cotton Lou S. (Monroe CT), Automatic approach to hover system.
  6. Gerstine Milton I. (Wilmington DE) Goldberg Joshua I. (Ridgefield CT) Futatsugi Setsuo (Kogamigahara JA) Ueda Kazuo (Kogamigahara JA) Seo Ryozo (Kogamigahara JA) Iwasaki Koji (Kogamigahara JA) Uemura, Automatic flight control means for rotary wing aircraft having attitude-air speed control.
  7. Bachelder, Edward N.; Lee, Dong-Chan; Aponso, Bimal L., Autorotation flight control system.
  8. Skutecki Edmund (Glendale AZ), Cross axis torque limiter for helicopter autopilot.
  9. Adams Don L. (Fairfield CT) Murphy Richard D. (Monroe CT) Fischer William C. (Monroe CT), Desensitizing helicopter control response to inadvertent pilot inputs.
  10. Black Homer D. (Phoenix AZ) Stribley Charles R. (Scottsdale AZ), Differential linkage apparatus for an aircraft series servoactuator apparatus.
  11. Mercer, John E., Drive mechanism and method.
  12. Mercer, John E.; Marvin, Mark H., Emergency collective actuator and method for a helicopter.
  13. Conner, James P., Emergency flight control system.
  14. Duerksen, Noel J.; Johnson, John C.; Williams, Justin S., Envelope protection for mechanically-controlled aircraft.
  15. Christensen, Kevin Thomas; Shue, Shyhpyng Jack; Caudill, Troy Sheldon, Flight control laws for vertical flight path.
  16. Shue, Shyhpyng Jack; Shillings, John J., Flight control system having a three control loop design.
  17. Adams ; Sr. Don L. (Fairfield CT) Johnson ; Jr. Raymond G. (Milford CT), Heading hold logic.
  18. Moore M. Samuel (Northridge CA) Paluka Charles F. (Northridge CA), Helicopter low-g monitor, recorder and warning system.
  19. Sherman Porter D. (Fairfield CT) Hetzler David H. (Media PA) Weisser ; Jr. Paul (South Windsor CT) Wright Stuart C. (Woodbridge CT), Helicopter turn coordination and heading hold mode control.
  20. Wright Stuart C. (Woodbridge CT) Murphy Richard D. (Trumbull CT) Adams Don L. (Fairfield CT), Incorporation of pitch bias actuator function into an existing AFCS.
  21. Fogler ; Jr. Donald L. (Milford) Richard James L. (Stratford) Gold Phillip J. (Shelton CT) Glusman Steven L. (Springfield PA), Low speed model following velocity command system for rotary wing aircraft.
  22. Green David Lee (Potomac MD), Maneuver margin presenting.
  23. Allieta, Jean-Marie; Chaduc, Bruno; Lafisse, Jean-Francois; Honnorat, Olivier, Method of assisting piloting, piloting assistance means, and a piloting assistance device for a rotorcraft using said piloting assistance means to implement said piloting assistance method.
  24. Cerchie, Dino A.; Dockter, Gregory E.; Hardesty, William Mark, Multi-mode unmanned and manned vehicle systems and methods.
  25. Chu ; Pak-Jong ; Audette ; Jacques Marcel, Multiple contact switch.
  26. Kamen Dean L. (Bedford NH) Miller Bradley D. (Londonderry NH), Position stick with automatic trim control.
  27. Delattre Jacques (Valpuiseaux FRX) Gouze Philippe (Villemoisson FRX), Position-controlled actuator.
  28. McCall, Hiram; Lin, Ching-Fang, Processing method for motion measurement.
  29. Adams Don L. (Fairfield CT) Fischer William C. (Monroe CT) Wright Stuart C. (Milford CT) Verzella David J. (Guilford CT), Retaining airspeed hold engagement in low speed maneuver.
  30. Carlavan, Cédric; Leguay, Pascal, Simplified flight control system including a declutchable friction device.
  31. Calise Anthony J. ; Kim Byoung-Soo,KRX, System and method for adaptive control of uncertain nonlinear processes.
  32. Younkin,James R.; Bilbe,Charles R., System and method for gyro enhanced vertical flight information.
  33. Svancarek Mark K. ; Adan Manolito E. ; Van Flandern Michael W. ; Pierce John G. ; Suzuki Hajime,JPX ; Kash Richard B., System and method for the software emulation of a computer joystick.
  34. Griffith Carl D. (Phoenix AZ) Skutecki Edmund R. (Glendale AZ), Three cue flight director system for helicopters.
  35. Grome, Donald C.; Nielsen, Kurt T., Three degree of freedom mechanism for input devices.
  36. Hollow Richard H. (Sunnyvale CA), Thumb-actuated two-axis controller.
  37. Grisham Michael G. (New York NY), Thumb-controlled, hand-held joystick.
  38. McKeown William L., Trim actuator.
  39. Shue, Shyhpyng Jack; Shillings, John J., Vehicle management system using finite state machines.
  40. Lee Richard J., Vibration damping device.
  41. Fischer ; Jr. William C. (Monroe CT), X-wing fly-by-wire vehicle management system.
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