IP Library Granted Patent US 9,194,302
Granted Patent B2
US 9,194,302 · App. 13/880,997 · Granted Nov 24, 2015

Control of a fuel metering device for turbomachine

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Quick Facts
Patent No.
US 9,194,302
App. No.
13/880,997
Granted
Nov 24, 2015
Kind
B2
Abstract

A control of a fuel metering device for a turbine engine as a function of a weight flow rate setpoint includes responding to at least one validity criterion to select a weight flow rate from among: a weight flow rate calculated as a function of a position signal; a weight flow rate calculated as a function of the position signal and of at least one temperature measurement signal; a weight flow rate calculated as a function of the position signal and of at least one permittivity measurement signal; a weight flow rate calculated as a function of the position signal, of at least one temperature measurement signal, and of at least one permittivity measurement signal; and a weight flow rate calculated as a function of a temperature measurement signal, of a permittivity measurement signal, and of a volume flow rate measurement signal.

Claims (22)

1. A method of controlling a position of a slide of a fuel metering device for a turbine engine as a function of a weight flow rate setpoint, the method comprising:

obtaining a position signal coming from a sensor configured to measure a position of the slide;

obtaining at least one measurement signal coming from a flow meter configured to measure a fuel flow rate in the flow meter;

estimating at least one validity criterion for the at least one measurement signal;

determining a fuel weight flow rate through the flow meter; and

controlling the position of the slide as a function of the determined weight flow rate and of the weight flow rate setpoint;

the at least one measurement signal comprises first and second fuel temperature measurement signals, first and second fuel permittivity measurement signals, and first and second fuel volume flow rate measurement signals; and

the determining comprises acting as a function of the at least one validity criterion to select a weight flow rate from among:

a weight flow rate calculated as a function of the position signal;

a weight flow rate calculated as a function of the position signal and of at least one of the temperature measurement signals;

a weight flow rate calculated as a function of the position signal and of at least one of the permittivity measurement signals;

a weight flow rate calculated as a function of the position signal, of at least one of the temperature measurement signals, and of at least one of the permittivity measurement signals; and

a weight flow rate calculated as a function of at least one of the temperature measurement signals, of at least one of the permittivity measurement signals, and of at least one of the volume flow rate measurement signals.

2. A control method according to claim 1 , wherein the at least one validity criterion comprises a validity criterion for a temperature measurement, a validity criterion for a permittivity measurement, and a validity criterion for a volume flow rate measurement.

3. A control method according to claim 2 , wherein the at least one validity criterion further comprises a secondary validity criterion for a volume flow rate measurement, estimated by comparing firstly the weight flow rate calculated as a function of at least one of the temperature measurement signals, of at least one of the permittivity measurement signals, and of at least one of the volume flow rate measurement signals, and secondly the weight flow rate calculated as a function of the position signal, of at least one of the temperature measurement signals, and of at least one of the permittivity measurement signals.

4. A control method according to claim 2 , wherein the validity criterion for a temperature measurement is determined by comparing the first and second temperature measurement signals with a temperature measurement range, and the validity criterion for a permittivity measurement is determined by comparing the first and second permittivity measurement signals with a permittivity measurement range.

5. A control method according to claim 4 , wherein the validity criterion for a temperature measurement and the validity criterion for a permittivity measurement are also determined as a function of a data set representing density of a fuel as a function of temperature and of permittivity.

6. A control method according to claim 5 , wherein, when the temperature or permittivity measurement range and the data set do not indicate that the first and second temperature or permittivity measurement signals are invalid, then the validity criterion for a temperature or permittivity measurement is also determined as a function of the difference between the first and second temperature or permittivity measurement signals.

7. A control method according to claim 2 , wherein the validity criterion for a volume flow rate measurement is determined by comparing the first and second volume flow rate measurement signals with a volume flow rate measurement range.

8. A non-transitory computer readable medium including computer executable instructions for executing a method according to claim 1 when executed by a computer.

9. An electronic unit for controlling a turbine engine, comprising a non-transitory computer readable medium according to claim 8 .

10. An aeroengine comprising a gas turbine and an electronic unit according to claim 9 .

Assignments (2)
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 →