Gas turbine engine uncontrolled high thrust detection system and method

Patent metadata

Field	Value
Publication number	US-9932906-B2
Application number	US-201514863140-A
Country	US
Kind code	B2
Filing date	Sep 23, 2015
Priority date	Sep 23, 2015
Publication date	Apr 3, 2018
Grant date	Apr 3, 2018

Abstract

A system and method of detecting an uncontrolled high thrust (UHT) condition in a turbofan gas turbine engine includes processing data to determine when a current commanded fan speed value is greater than a predetermined speed value. A current UHT commanded fan speed value is processed to determine if it will cause a target fan speed value to increase, remain steady, or decrease. The target fan speed value is set equal to the current UHT commanded fan speed value when the current UHT commanded fan speed value will cause the target fan speed value to increase or remain steady, and to a deceleration threshold value when the current UHT commanded fan speed value will cause the target fan speed value to decrease. An uncontrolled high thrust alert signal is generated when actual engine fan speed exceeds the target fan speed value by a predetermined amount for a preset time period.

First claim

What is claimed is:

1. A method of detecting an uncontrolled high thrust (UHT) condition in a turbofan gas turbine engine, the method comprising:
processing data to determine when a current commanded fan speed value is greater than a predetermined speed value;
setting, by a processor, a current UHT commanded fan speed value to the greater of the current commanded fan speed value and the predetermined speed value,
processing the current UHT commanded fan speed value, to determine when the current UHT commanded fan speed value will cause a target fan speed value to increase, remain steady, or decrease;
setting the target fan speed value equal to (i) the current UHT commanded fan speed value when the current UHT commanded fan speed value will cause the target fan speed value to increase or remain steady, or (ii) a deceleration threshold value when the current UHT commanded fan speed value will cause the target fan speed value to decrease;
generating an uncontrolled high thrust alert signal when actual engine fan speed exceeds the target fan speed value by a predetermined amount for a preset time period; and
controlling, with an engine control, the actual engine fan speed by adjusting fuel flow to the turbofan gas turbine engine via a fuel metering valve.

2. The method of claim 1 , further comprising:
processing the current UHT commanded fan speed value through a delay when the current UHT commanded fan speed value will cause the target fan speed value to decrease to thereby generate a delayed fan speed command;
processing the delayed fan speed command through a filter to thereby generate a filtered fan speed command; and
processing the filtered fan speed command through a rate limiter to limit a rate of change of the filtered fan speed command, to thereby generate the deceleration threshold value.

3. The method of claim 2 , wherein the predetermined amount is a predetermined threshold value, and wherein the method further comprises:
adding the predetermined threshold value to the target fan speed value to thereby generate an uncontrolled high thrust trip limit;
comparing the actual engine fan speed to the uncontrolled high thrust trip limit; and
generating the uncontrolled high thrust alert signal when the actual engine fan speed exceeds the uncontrolled high thrust trip limit for the preset time period.

4. The method of claim 2 , further comprising:
limiting the rate of change of the filtered fan speed command to a deceleration minimum rate limit value.

5. The method of claim 4 , further comprising:
generating the deceleration minimum rate limit value as a function of the deceleration threshold value.

6. The method of claim 5 , further comprising:
limiting a rate of change of the deceleration minimum rate limit value to a predetermined deceleration limit value.

7. The method of claim 4 , further comprising:
processing data to determine when a degraded engine mode command is received; and
when the degraded engine mode command is received, reducing the deceleration minimum rate limit value by a predetermined amount.

8. The method of claim 2 , further comprising:
resetting the delay, the filter, and the rate limiter upon determining that the current UHT commanded fan speed value will cause the target fan speed value to increase, whereby the UHT commanded fan speed value is not delayed, filtered, and rate limited.

9. The method of claim 8 , further comprising:
adding the predetermined threshold value to the target fan speed value to thereby generate an uncontrolled high thrust trip limit;
comparing the actual engine fan speed to the uncontrolled high thrust trip limit; and
generating the uncontrolled high thrust alert signal when the actual engine fan speed exceeds the uncontrolled high thrust trip limit for the preset time period.

10. The method of claim 1 , further comprising:
comparing the current UHT commanded fan speed value to the deceleration threshold value;
determining that the current UHT commanded fan speed value will cause the target fan speed value to increase when the current UHT commanded fan speed value is greater than the deceleration threshold value; and
determining that the current UHT commanded fan speed value will cause the target fan speed value to decrease when the current UHT commanded fan speed value is less than the deceleration threshold value.

11. A turbofan gas turbine engine uncontrolled high thrust (UHT) condition detection system, comprising:
a plurality of sensors configured to supply data; and
an engine control, implemented with a processor, coupled to receive at least a portion of the data supplied by the plurality of sensors and configured, upon receipt of the data, to:
determine a current commanded fan speed value,
determine when the current commanded fan speed value is greater than a predetermined speed value,
set a UHT commanded fan speed value to the greater of the current commanded fan speed value and the predetermined speed value,
determine when the current UHT commanded fan speed value will cause a target fan speed value to increase, remain steady, or decrease,
set the target fan speed value equal to (i) the current UHT commanded fan speed value when the current UHT commanded fan speed value will cause the target fan speed value to increase or remain steady, or (ii) a deceleration threshold value when the current UHT commanded fan speed value will cause the target fan speed value to decrease,
generate an uncontrolled high thrust alert signal when actual engine fan speed exceeds the target fan speed value by a predetermined amount for a preset time period; and
control the actual engine fan speed by adjusting fuel flow to the turbofan gas turbine engine via a fuel metering valve.

12. The system of claim 11 , wherein the engine control is further configured to:
process the current UHT commanded fan speed value through a delay when the current UHT commanded fan speed value will cause the target fan speed value to decrease to thereby generate a delayed fan speed command;
process the delayed fan speed command through a filter to thereby generate a filtered fan speed command; and
process the filtered fan speed command through a rate limiter to limit a rate of change of the filtered fan speed command, to thereby generate the deceleration threshold value.

13. The system of claim 12 , wherein the predetermined amount is a predetermined threshold value, and wherein the engine control is further configured to:
add the predetermined threshold value to the target fan speed value to thereby generate an uncontrolled high thrust trip limit;
compare the actual engine fan speed to the uncontrolled high thrust trip limit; and
generate the uncontrolled high thrust alert signal when the actual engine fan speed exceeds the uncontrolled high thrust trip limit for the preset time period.

14. The system of claim 12 , wherein the engine control is further configured to:
generate a deceleration minimum rate limit value as a function of the deceleration threshold value;
limit the rate of change of the filtered fan speed command to the deceleration minimum rate limit value; and
limit the rate of change of the deceleration minimum rate limit value to a predetermined deceleration limit value.

15. The system of claim 14 , wherein the engine control is further configured to:
determine when a degraded engine mode command is received; and
when the degraded engine mode command is received, reduce the deceleration minimum rate limit value by a predetermined amount.

16. The system of claim 12 , wherein the engine control is fu

Assignees

• Honeywell Int Inc

Inventors

• Xiong Yufei
• Faymon Dave
• Coffey Scot

Classifications

• F05D2270/095

  by temporary overriding set control limits · CPC title

• F05D2260/80

  Diagnostics · CPC title

• F02C9/54

  by throttling the working fluid, by adjusting vanes · CPC title

• F02C9/46

  Emergency fuel control · CPC title

• F02C9/28 Primary

  Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title