Method and apparatus for controlling fuel flow into an aircraft engine

Patent metadata

Field	Value
Publication number	US-11920522-B2
Application number	US-202217882268-A
Country	US
Kind code	B2
Filing date	Aug 5, 2022
Priority date	Mar 7, 2022
Publication date	Mar 5, 2024
Grant date	Mar 5, 2024

Abstract

Based upon a measured first resistance, a first delta curve is selected. Based upon a measured second resistance, a second delta curve is selected. A first fuel valve position (FVP) is received from a first position sensor, and the first FVP is applied to the first delta curve to obtain a first offset. A second FVP is received from a second position sensor, and the second FVP is applied to the second delta curve to obtain a second offset. The first offset is applied to the first measured FVP to obtain the first compensated FVP and the second offset is applied to the second measured FVP to obtain the second compensated FVP. The first compensated FVP and the second compensated FVP are correlated to obtain a final compensated FVP, which is applied to a desired fuel valve position to obtain a final fuel valve position.

First claim

What is claimed is:

1. A non-transitory, machine-accessible storage medium having computer instructions and wherein the instructions are configured, when executed by a controller, to cause the controller to:
measure a first resistance of a first resistor associated with a first position sensor;
based upon the measured first resistance, select a first delta curve, the first delta curve describing differences between a nominal fuel valve position and a first measured fuel valve position associated with the first position sensor;
measure a second resistance of a second resistor associated with a second position sensor;
based upon the measured second resistance, select a second delta curve, the second delta curve describing differences between the nominal fuel valve position and a second measured fuel valve position associated with the second position sensor;
receive a first fuel valve position (FVP) from the first position sensor, and apply the first FVP to the first delta curve to obtain a first compensated FVP;
receive a second FVP from the second position sensor, and apply the second FVP to the second delta curve to obtain a second compensated FVP;
correlate the first compensated FVP and the second compensated FVP to obtain a final compensated FVP;
apply the final compensated FVP to a desired fuel valve position to obtain a final fuel valve position and apply the final fuel valve position to a fuel valve to control an operation of the fuel valve.

2. The non-transitory, machine-accessible storage medium of claim 1 , wherein the first delta curve and the second delta curve are represented as a table.

3. The non-transitory, machine-accessible storage medium of claim 1 , wherein the desired fuel valve position is obtained via an apparatus in a cockpit of an aircraft.

4. The non-transitory, machine-accessible storage medium of claim 1 , wherein the fuel valve controls an amount of fuel provided to an engine of an aircraft.

5. The non-transitory, machine-accessible storage medium of claim 1 , wherein the first delta curve and the second delta curve are derived from curves obtained by a manufacturer.

6. The non-transitory, machine-accessible storage medium of claim 1 , wherein the first FVP and the second FVP indicate an amount of an opening of the fuel valve.

7. The non-transitory, machine-accessible storage medium of claim 1 , wherein at least some of the steps are performed in a continuous loop.

8. The non-transitory, machine-accessible storage medium of claim 1 , wherein the first compensated FVP and the second compensated FVP are similar in value.

9. The non-transitory, machine-accessible storage medium of claim 1 , wherein correlating the first compensated FVP and the second compensated FVP averages the first compensated FVP and the second compensated FVP.

10. A system, the system comprising:
a first position sensor;
a second position sensor;
a fuel valve;
a controller coupled to the first position sensor, the second position sensor, and the fuel valve;
wherein a first resistance of a first resistor associated with the first position sensor is measured and based upon the measured first resistance, a first delta curve is selected, the first delta curve describing differences between a nominal fuel valve position and a first measured fuel valve position associated with the first position sensor;
wherein a second resistance of a second resistor associated with the second position sensor is measured and based upon the measured second resistance, a second delta curve is selected, the second delta curve describing differences between the nominal fuel valve position and a second measured fuel valve position associated with the second position sensor;
wherein the controller is configured to:
receive a first fuel valve position (FVP) from the first position sensor, and apply the first FVP to the first delta curve to obtain a first compensated FVP;
receive a second FVP from the second position sensor, and apply the second FVP to the second delta curve to obtain a second compensated FVP;
correlate the first compensated FVP and the second compensated FVP to obtain a final compensated FVP;
apply the final compensated FVP to a desired fuel valve position to obtain a final fuel valve position and apply the final fuel valve position to the fuel valve to control an operation of the fuel valve.

11. The system of claim 10 , wherein the first delta curve and second delta curve are represented as a table.

12. The system of claim 10 , wherein the desired fuel valve position is obtained via an apparatus in a cockpit of an aircraft.

13. The system of claim 10 , wherein the fuel valve controls an amount of fuel provided to an engine of an aircraft.

14. The system of claim 10 , wherein the first delta curve and the second delta curve are derived from curves obtained by a manufacturer.

15. The system of claim 10 , wherein the first FVP and the second FVP indicate an amount of an opening of the fuel valve.

16. The system of claim 10 , wherein at least some of the steps executed by the controller are performed in a continuous loop.

17. The system of claim 10 , wherein the first compensated FVP and the second compensated FVP are similar in value.

18. The system of claim 10 , wherein correlating the first compensated FVP and the second compensated FVP averages the first compensated FVP and the second compensated FVP.

19. A method, comprising:
measuring a first resistance of a first resistor associated with a first position sensor;
based upon the measured first resistance, selecting a first delta curve, the first delta curve describing differences between a nominal fuel valve position and a first measured fuel valve position associated with the first position sensor;
measuring a second resistance of a second resistor associated with a second position sensor;
based upon the measured second resistance, selecting a second delta curve, the second delta curve describing differences between the nominal fuel valve position and a second measured fuel valve position associated with the second position sensor;
receiving a first fuel valve position (FVP) from the first position sensor, and applying the first FVP to the first delta curve to obtain a first compensated FVP;
receiving a second FVP from the second position sensor, and applying the second FVP to the second delta curve to obtain a second compensated FVP;
correlating the first compensated FVP and the second compensated FVP to obtain a final compensated FVP;
applying the final compensated FVP to a desired fuel valve position to obtain a final fuel valve position and applying the final fuel valve position to a fuel valve to control an operation of the fuel valve.

20. The method of claim 19 , wherein the first delta curve and the second delta curve are represented as a table.

Assignees

• Ge Avio Srl

Inventors

• Di Leo Diego
• Cipolla Lorenzo
• Recchia Simone
• Lai Cristian

Classifications

• F02C9/263 Primary

  by means of fuel metering valves · CPC title

• F02C7/232 Primary

  Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title

• F16K37/0041

  for measuring valve parameters (F16K37/0033 takes precedence) · CPC title

• G01R27/02

  Measuring real or complex resistance, reactance, impedance, or other two-pole characteristics derived therefrom, e.g. time constant (by measuring phase angle only G01R25/00) · CPC title

• B64D37/00

  Arrangements in connection with fuel supply for power plant (refuelling during flight B64D39/00) · CPC title