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특허 상세정보

Pivoted flap mechanism for adjusting an aerodynamic pivoted flap associated with a wing

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50    B64C-003/00   
미국특허분류(USC) 244/215
출원번호 UP-0400509 (2006-04-10)
등록번호 US-7600718 (2009-10-28)
우선권정보 DE-10 2005 016 638(2005-04-11)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Greenblum & Bernstein, P.L.C.
인용정보 피인용 횟수 : 22  인용 특허 : 1
초록

A pivoted flap mechanism for adjusting an aerodynamic pivotable flap associated with a wing, including: an actuating device including a gear device; a drive device including a drive arm that rotates about an axis, and which is structured and arranged to load the actuating device; and a flap support composed of a leading flap support portion and a trailing flap support portion. The aerodynamic pivotable flap is arranged on the flap support, and a steering arm of the gear device is swivellably coupled by a link to a part of the trailing flap support portio...

대표
청구항

What is claimed: 1. A pivoted flap mechanism for adjusting an aerodynamic pivotable flap associated with a wing, comprising: an actuating device including a gear device; a drive device including a drive arm that rotates about an axis, and which is structured and arranged to load the actuating device; and a flap support composed of a leading flap support portion and a trailing flap support portion, wherein the aerodynamic pivotable flap is arranged on the flap support, and wherein a steering arm of the gear device is swivellably coupled by a link to a pa...

이 특허를 인용한 특허 피인용횟수: 22

  1. Schlipf, Bernhard; Missbach, Mirko. Adjustment mechanism of an adjustment device for coupling an adjustment flap to a main wing, and such an adjustment device. USP2013118584992.
  2. Schlipf, Bernhard; Gibbert, Markus; Schulze, Daniel; Danne, Timo. Aerofoil comprising a high lift flap. USP2015018939411.
  3. Schlipf, Bernhard; Hue, Xavier. Aerofoil comprising a high lift flap. USP2015038967550.
  4. McDonald, Lynn. Aileron actuator bracket. USP2012128328142.
  5. Sakurai, Seiya; Wheaton, James M.; Fox, Stephen J.; Che, Sharon Xiangdong. Aircraft flap mechanism having compact large fowler motion providing multiple cruise positions. USP2014048684316.
  6. Soenarjo, Mochamad-Agoes. Flap support. USP2016019227722.
  7. Soenarjo, Mochamad-Agoes. Flap support. USP2018029889922.
  8. Dorr, Björn; Ulmer, Tobias; Neuhaus, Philip. Function-monitored guidance system for adjusting at least one system component and method for monitoring the function of such a guidance system. USP2016119483057.
  9. Voss, Timo; Loerke, Joachim. High lift system for an aircraft. USP2014098844878.
  10. Sobolewski, Pawel A.; Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Szulyk, Zenon P.. Rotary piston actuator anti-rotation configurations. USP2017049631645.
  11. Kim, Joseph H.; O Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator. USP2016019234535.
  12. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator. USP20180710030679.
  13. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2017079709078.
  14. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2017119816537.
  15. Kim, Joseph H; O'Hara, Robert P; Hydari, Shahbaz H; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2015109163648.
  16. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.; Szulyk, Zenon P.. Rotary piston type actuator with hydraulic supply. USP2017039593696.
  17. Sobolewski, Pawel A.; Kim, Joseph H.; Szulyk, Zenon P.. Rotary piston type actuator with modular housing. USP2016109476434.
  18. Sobolewski, Pawel A.; Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.. Rotary piston type actuator with pin retention features. USP2015028955425.
  19. De Conto, Sébastien; Rival, Fabrice; Bernes, Romain; Coll, Frédéric. Supporting set for a wing flap system of an aircraft. USP2017059637220.
  20. Morris, Stuart. Trailing edge flap. USP2013098534612.
  21. Morris, Stuart. Trailing edge flap. USP2014058714493.
  22. Morris, Stuart. Trailing edge flap. USP2013108567727.