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특허 상세정보

System and method for optimizing performance of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/38    B64C-013/16    B64C-009/16    B64C-013/04   
출원번호 US-0034920 (2013-09-24)
등록번호 US-9359065 (2016-06-07)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 22

A system for optimizing performance of an aircraft may include a flight control computer for computing an optimum flap setting based on aircraft data. The system may further include a flap control system having a flap control device. The system may additionally include a flap actuation system coupled to the flap control system for positioning the trailing edge device at the optimum flap setting.


1. A system for optimizing performance of an aircraft, comprising: a flight control computer configured to compute an optimum flap setting based on aircraft data;a flap control system having a flap control device for selecting one of multiple flap lever positions comprising non-designated flap lever positions and at least one designated flap lever position, the non-designated flap lever positions and the designated flap lever position each corresponding to a standard flap setting, the flap control device having a variable-trailing-edge-position switch be...

이 특허에 인용된 특허 (22)

  1. Yamasaki, Koichi. Aerodynamic coefficient estimation device and control surface failure/damage detection device. USP2015028954208.
  2. Borzachillo Angelo (San Marcos CA). Aeroelastic control flap. USP1988034729528.
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  9. Richter, Martin; Fleddermann, Andreas. Fault-tolerant actuating system for adjusting flaps of an aircraft, comprising adjustment kinematics with a fixed pivot, and a method for monitoring an actuating system. USP2014088814085.
  10. Bliesner Wayne T.. Leading edge slat/wing combination. USP1998115839699.
  11. Muller Dietmar,DEX. Lift body having a variable camber. USP2000116152405.
  12. Shmilovich, Arvin; Yadlin, Yoram. Low noise wing slat system with rigid cove-filled slat. USP2013048424810.
  13. Gangsaas Dagfinn (Bellevue WA) Norman Daniel C. (Renton WA). Maneuver enchancement and gust alleviation system. USP1989044821981.
  14. Williams George H. (Bristol GBX). Mechanism for supporting and extending a high lift device for aircraft wings. USP1989064838503.
  15. Fleddermann, Andreas; Hartwig, Wolfgang; Darbois, Alexandre; Richter, Martin. Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft. USP2012098256718.
  16. Luckner, Robert; Lauterbach, Matthias; Dorr, Björn. Method for planning a landing approach of an aircraft, computer program product with a landing approach plan stored thereon, as well as device for planning a landing approach. USP2014118880247.
  17. Sakurai,Seiya; Fox,Stephen J.; Beyer,Kevin W.; Lacy,Douglas S.; Johnson,Paul L.; Wells,Stephen L.; Noble,Jack S.; Meredith,Paul T.; Huynh,Neal V.; Christianson,Russell R.; Vijgen,Paul M.; Fitzpatrick. Multi-function trailing edge devices and associated methods. USP2007077243881.
  18. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger W.; Manley, David J.. System for aerodynamic flows and associated method. USP2009127635107.
  19. Delaplace,Franck; Buisson,Dominique. System for automatically controlling lift-enhancing devices of an aircraft, in particular wing leading edge slats. USP2008047366592.
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