The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 01, 2022

Filed:

May. 11, 2021
Applicant:

Airbus Operations (S.a.s.), Toulouse, FR;

Inventors:

Patrick Zaccaria, Toulouse, FR;

David Boyer, Toulouse, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/44 (2006.01); F02C 7/232 (2006.01); F01D 21/00 (2006.01); B64D 31/04 (2006.01); B64D 31/06 (2006.01);
U.S. Cl.
CPC ...
F02C 9/44 (2013.01); B64D 31/04 (2013.01); B64D 31/06 (2013.01); F01D 21/00 (2013.01); F02C 7/232 (2013.01); F05D 2220/323 (2013.01); F05D 2270/304 (2013.01); F05D 2270/52 (2013.01);
Abstract

To control an engine shutdown in an aircraft, a control system includes a fuel supply shut-off member, a control member with a set of switches, a first switch on an electrical power supply link of the fuel supply shut-off member and second switches connected to avionics of the aircraft, the set of switches switching position on an engine shutdown command. An engine shutdown confirmation unit includes a third switch on the electrical power supply link, the third switch in open position by default. The engine shutdown confirmation unit includes electronic circuitry configured to switch the third switch over to closed position when a predefined quantity Q of switches of the control member switches position within a sliding window of predefined duration and, otherwise, keeps the third switch in open position. Thus, it is ensured that the engine shutdown is intentional.


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