Method of acceleration control during APU starting

Patent metadata

Field	Value
Publication number	US-10094292-B2
Application number	US-201213410752-A
Country	US
Kind code	B2
Filing date	Mar 2, 2012
Priority date	Mar 2, 2012
Publication date	Oct 9, 2018
Grant date	Oct 9, 2018

Abstract

A method for controlling fuel flow to a gas turbine engine during starting includes monitoring acceleration of the gas turbine engine to determine actual acceleration value, and calculating a fuel flow rate for a setpoint acceleration using the actual acceleration value as a factor. The method further includes commanding the calculated fuel flow for the setpoint acceleration to the gas turbine engine.

First claim

The invention claimed is:

1. A method for controlling fuel flow to a gas turbine engine during starting, the method comprising:
monitoring acceleration of the gas turbine engine unit to determine an actual acceleration value;
populating an acceleration based fuel command look-up table with the actual acceleration of the gas turbine engine unit during starting;
calculating a fuel flow rate for a setpoint acceleration using the actual acceleration value as a factor; and
commanding the calculated fuel flow rate to the gas turbine engine.

2. The method of claim 1 , wherein monitoring the acceleration of the gas turbine engine comprises:
monitoring a speed of the gas turbine engine to determine when the gas turbine engine reaches a set speed;
recording time elapsed for the gas turbine engine to reach the set speed; and
dividing the monitored speed by the recorded time to calculate the actual acceleration.

3. The method of claim 2 , wherein the set speed is between about 1% and about 20% of maximum rated speed for the gas turbine engine.

4. The method of claim 2 , wherein the set speed is about 5% of maximum rated speed for the gas turbine engine.

5. The method of claim 1 , further comprising:
comparing a fuel flow rate from a temperature based fuel command look up table with a fuel flow rate from the acceleration based fuel command look up table.

6. The method of claim 1 , wherein an electronic engine control performs the method of claim 1 .

7. A method for controlling fuel flow to an auxiliary power unit during starting, the method comprising:
activating a starter for the auxiliary power unit;
monitoring a speed of the auxiliary power unit;
measuring an amount of time elapsed to reach a set speed to determine an actual acceleration of the auxiliary power unit;
populating an acceleration look up table with the actual acceleration of the auxiliary power unit during starting; and
controlling a rate of fuel flow to the auxiliary power unit during starting.

8. The method of claim 7 , further comprising:
comparing a first fuel flow rate from the acceleration look up table to a second fuel flow rate from an exhaust gas temperature (“EGT”) look up table;
selecting one of the first fuel flow rate and the second fuel flow rate as a desired fuel flow rate; and
commanding the desired fuel flow rate to a fuel metering valve.

9. The method of claim 8 , wherein selecting one of the first fuel flow rate and the second fuel flow rate includes choosing whichever fuel flow rate is lower.

10. The method of claim 8 , wherein comparing the first fuel rate to the second fuel flow rate occurs continuously during starting of the auxiliary power unit.

11. The method of claim 7 , wherein the set speed is between about 1% and about 10% of maximum rated speed.

12. The method of claim 7 , wherein the set speed is about 5% of maximum rated speed.

13. The method of claim 9 , wherein the starter is part of a hydraulic starting system.

14. An auxiliary power unit comprising:
a starter for starting rotation of an engine;
a speed sensor for sensing engine speed;
a fuel metering valve for metering fuel flow to the engine; and
a controller connected to the starter, the speed sensor, and the fuel metering valve, the controller receiving the sensed engine speed and calculating acceleration of the engine, the controller commanding a fuel flow rate to the fuel metering valve, wherein the fuel flow rate is determined in part by the calculated acceleration of the engine;
wherein the calculated acceleration of the engine is used as a multiplying factor in determining the fuel flow rate; and
wherein the controller populates an acceleration based fuel command look up table with the calculated acceleration of the engine during starting of the engine.

15. The auxiliary power unit of claim 14 , wherein the controller compares a first fuel flow rate from the acceleration based fuel command look up table with a second fuel flow rate from temperature based look up table.

Assignees

• Ainslie Walter Ernest
• Ajami Andre M
• Saifuddin Mujtaba T
• Hamilton Sundstrand Corp

Inventors

• Ainslie Walter Ernest
• Ajami Andre M
• Saifuddin Mujtaba T

Classifications

• F05D2220/50

  for auxiliary power units (APU's) · CPC title

• F02C9/26

  Control of fuel supply (F02C9/48 takes precedence; fuel valves F02C7/232) · CPC title

• F02C7/26 Primary

  Starting; Ignition · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title