IP Library Granted Patent US 9,464,595
Granted Patent B2
US 9,464,595 · App. 14/651,746 · Granted Oct 11, 2016

Optimising the availability of a thrust reverser

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Quick Facts
Patent No.
US 9,464,595
App. No.
14/651,746
Granted
Oct 11, 2016
Kind
B2
Abstract

A method of controlling a thrust reverser made up of a plurality of pieces of equipment, wherein, in the event of it being detected that one of the pieces of equipment has not activated by the end of a predetermined activation period, an error message relating to the malfunction of the thrust reverser is generated, and in spite of the error message being generated, activation of the equipment is continued, and if the equipment is finally activated before a predetermined maximum period for deployment of the thrust reverser, then deployment of the thrust reverser is continued and the error message relating to the malfunction of the thrust reverser is withdrawn.

Claims (5)

1. A method of controlling a thrust reverser made up of a plurality of pieces of equipment, comprising, in the event of it being detected that one of said pieces of equipment has not activated by the end of a predetermined activation period, generating an error message relating to the malfunction of said thrust reverser, and in spite of said error message being generated, continuing activation of said one of said pieces of equipment, and if said one of said pieces of equipment is finally activated before a predetermined maximum period for deployment of said thrust reverser, continuing deployment of said thrust reverser and withdrawing the error message relating to the malfunction of said thrust reverser.

2. A method according to claim 1 , wherein when said predetermined maximum period for deployment of said thrust reverser is exceeded, issuing once more said error message relating to the malfunction of said thrust reverser and inhibiting any use of reverse thrust.

3. A method according to claim 1 , wherein said predetermined activation period for a piece of equipment is adapted to each piece of equipment as a function of its own dynamic behavior.

4. A method according to claim 1 , wherein in parallel with generating said error message relating to the malfunction of said thrust reverser, the method comprises storing an individual fault message relating to said one of said pieces of equipment that led to the error message being issued.

5. A method according to claim 1 , wherein said one of said pieces of equipment is any one of the following pieces of equipment of a thrust reverser: a primary lock, a tertiary lock, a door actuator, a directional valve DSV, a tertiary lock valve TLSV, an isolation valve ISV, a directional control valve DCV unit, or an isolation control unit ICU.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 12, 2015
From: CHALAUD, SÉBASTIEN
To: SNECMA
Reel/Frame 035828/0914 →