Title:
航空機の翼のフラップ動作を制御するためのシステム及び方法
Document Type and Number:
Japanese Patent JP6924603
Kind Code:
B2
Abstract:
A system and method of controlling one or more flaps (102, 108) of an aircraft (106) may include receiving first and second sensor signals from respective first and second sensors (120, 122) coupled to respective first and second actuators (112, 114) that are moveably secured to a first flap (102) of a first wing (104) of the aircraft (106). The first and second sensor signals relate to one or both of the position or the speed of the respective first and second actuators (112, 114). The system and method may also include comparing the first and second sensor signals to determine a difference between the first and second sensor signals, and adjusting the speed of one or both of the first or second actuators (112, 114) based on the difference between the first and second sensor signals. A system and method may include determining a difference between one or both of speed or position of the first and second flaps (102, 108), and adjusting the speed of one or both of the first and second flaps (102, 108) based on the difference between one or both of the speed or the position of the first and second flaps (102, 108).
Inventors:
Michael raymond fin
Patrick McCormick
George Moy
Rene Toen Nguyen
Patrick McCormick
George Moy
Rene Toen Nguyen
Application Number:
JP2017081856A
Publication Date:
August 25, 2021
Filing Date:
April 18, 2017
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64C13/00
Foreign References:
| US20160028332 | ||||
| US20130334372 |
Attorney, Agent or Firm:
Minoru Yoshida
Tatsuya Tanaka
Yasumitsu Suzuki
Nao Usui
Fumiaki Doi
Keita Kobuchi
Shintaro Suzuki
Tatsuya Tanaka
Yasumitsu Suzuki
Nao Usui
Fumiaki Doi
Keita Kobuchi
Shintaro Suzuki