Title:
航空機のフラップおよびスポイラを制御するためのシステムならびに方法
Document Type and Number:
Japanese Patent JP5201997
Kind Code:
B2
Abstract:
Systems and methods for controlling aircraft flaps and spoilers are disclosed. Systems in accordance with some embodiments include a wing having a trailing edge, and a flap positioned at least partially aft of the wing trailing edge and being deployable relative to the wing between a first flap position and a second flap position by operation of a first actuator. A spoiler can be positioned at least proximate to the trailing edge and can be movable among at least three positions, including a first spoiler position in which the spoiler forms a generally continuous contour with an upper surface of the wing, a second spoiler position deflected downwardly from the first, and a third spoiler position deflected upwardly from the first. A second actuator can be operatively coupled to the spoiler to move the spoiler among the first, second and third spoiler positions in a manner that is mechanically independent of the motion of the flap.
Inventors:
Brig, robert jay
Win, Neil Buoy
Standley, John A
Scott, Pepper
Bock El, Bock El
Win, Neil Buoy
Standley, John A
Scott, Pepper
Bock El, Bock El
Application Number:
JP2007554252A
Publication Date:
June 05, 2013
Filing Date:
February 03, 2006
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64C9/12; B64C9/06; B64C9/20; B64C13/50
Foreign References:
| US4120470 | ||||
| US2117607 | ||||
| US4530271 | ||||
| GB1304194A | ||||
| FR2756540A1 | ||||
| US4720066 | ||||
| EP0216033A1 | ||||
| EP1516813A1 | ||||
| US5957798 |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori
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