Monitoring the fuel supply cutoff valve for an engine

Patent metadata

Field	Value
Publication number	US-9470604-B2
Application number	US-201414299392-A
Country	US
Kind code	B2
Filing date	Jun 9, 2014
Priority date	Jun 10, 2013
Publication date	Oct 18, 2016
Grant date	Oct 18, 2016

Abstract

A method of testing an engine fuel supply cutoff valve includes: detecting a fuel supply cutoff command; commanding to close the fuel supply cutoff valve; commanding to hold the fuel metering valve in the open position for a predetermined time; commanding to close the fuel metering valve after the predetermined time; measuring an engine operating parameter during performance of the previous steps; and comparing the measured parameter with a predetermined threshold, so as to determine whether or not the engine operating parameter corresponds to an engine fuel supply cutoff by normal operation of the fuel supply cutoff valve.

First claim

The invention claimed is:

1. A method of testing a fuel supply cutoff valve in a fuel circuit for supplying fuel to an aircraft engine, said fuel circuit further comprising a fuel metering valve having an open position and a closed position in order to meter fuel being injected into a combustion chamber of the engine, said method comprising:
detecting a fuel supply cutoff command;
commanding to close the fuel supply cutoff valve;
commanding to hold the fuel metering valve in the open position for a predetermined time;
commanding to close the fuel metering valve after the predetermined time;
measuring an engine operating parameter while the commanding to close the fuel supply cutoff valve, the commanding to hold the fuel metering valve in the open position for the predetermined time, and the commanding to close the fuel metering valve after the predetermined time are carried out; and
comparing the measured engine operating parameter with a predetermined threshold, so as to determine whether or not the engine operating parameter corresponds to an engine fuel supply cutoff by normal operation of the fuel supply cutoff valve.

2. A testing method according to claim 1 , wherein the engine operating parameter is an engine speed gradient.

3. The testing method according to claim 1 , wherein the engine operating parameter is a pressure gradient.

4. A non-transitory computer readable recording medium including computer executable instructions for executing the method according to claim 1 .

5. A testing method according to claim 1 , wherein the predetermined threshold corresponds to a maximum value in a case in which the fuel supply cutoff valve is not closed.

6. The testing method according to claim 1 , further comprising a preliminary step of checking that prerequisites are verified.

7. The testing method according to claim 6 , wherein the engine is an aircraft engine, and said prerequisites include detection that the aircraft is on the ground.

8. The testing method according to claim 1 , further comprising a preliminary step of checking that validity conditions are satisfied.

9. The testing method according to claim 8 , wherein the validity conditions include verification that the engine speed is above a predetermined threshold.

10. A device to test an engine fuel supply cutoff valve in a fuel circuit for supplying fuel to an aircraft engine, said fuel circuit further comprising a fuel metering valve having an open position and a closed position in order to meter fuel being injected into a combustion chamber of the engine, said device comprising:
means of detecting a fuel supply cutoff command;
means of giving a command to close the fuel supply cutoff valve;
means of giving a command to hold the fuel metering valve in the open position for a predetermined time;
means of giving a command to close the fuel metering valve after the predetermined time;
means of measuring an engine operating parameter while the command to close the fuel supply cutoff valve, the command to hold the fuel metering valve in the open position for the predetermined time, and the command to close the fuel metering valve after the predetermined time are carried out and
means of comparing the measured engine operating parameter with a predetermined threshold so as to determine whether or not the engine operating parameter corresponds to an engine fuel supply cutoff due to normal operation of the fuel supply cutoff valve.

Assignees

• Snecma

Inventors

• Javelot Christophe
• Boutaleb Mohamed
• Djelassi Cedrik
• Henry Victor

Classifications

• F02C9/46

  Emergency fuel control · CPC title

• F02D41/22

  Safety or indicating devices for abnormal conditions {(in air/fuel ratio feedback systems F02D41/1495, in electric control linkage F02D11/107, in purge control systems F02M25/0809)} · CPC title

• F02D2041/226

  Fail safe control for fuel injection pump · CPC title

• G01M15/042 Primary

  by monitoring a single specific parameter not covered by groups G01M15/06 - G01M15/12 · CPC title

• F01D21/20 Primary

  Checking operation of shut-down devices · CPC title