Method and system for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter

Method and system for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter

  • CN 101,784,964 A
  • Filed: 07/07/2008
  • Published: 07/21/2010
  • Est. Priority Date: 08/20/2007
  • Status: Active Application
First Claim
Patent Images

1. the system of at least one actuator of the trhrust-reversal device radome fairing of control one turbojet comprises one group and activates and/or Control Component, comprises at least:

  • -at least one radome fairing (2) actuator (6) of driven by at least one motor (7),The control device (9) of described actuator of-control and described motor (7),-communicating devices (10) between a described control device (9) and a flight control system is characterised in thatDescribed control device (9) is in order to detect the fault of an actuating and/or Control Component (7,16,13), judgement is for system operation, fault is obstructive or nonobstructive, if described fault is a nonobstructive, just from a normal operation mode switch to a fault accommodation operation mode (M1, M2, M3), the fault of wherein said actuating and/or Control Component (7,16,13) is compensated by a revision directive of other actuating and/or Control Component (7,16,13) at least in part.

View all claims
    ×
    ×

    Thank you for your feedback

    ×
    ×