System and method for detecting an uncommanded or uncontrollable high thrust event in an aircraft

Patent metadata

Field	Value
Publication number	US-12078074-B2
Application number	US-201916410270-A
Country	US
Kind code	B2
Filing date	May 13, 2019
Priority date	May 13, 2019
Publication date	Sep 3, 2024
Grant date	Sep 3, 2024

Abstract

System and method for detecting an uncommanded high thrust (UHT) event in an aircraft. The method comprises enabling a UHT function associated with an engine when an enabling condition has been met. When the UHT function is enabled, the UHT event is detected when a power lever of the aircraft is at a given position, a parameter indicative of engine speed or power is above a first threshold, and a rate of change of the engine speed is above a second threshold. In response to detecting the UHT event, an alert is output to trigger accommodations to the UHT event for the engine.

First claim

The invention claimed is:

1. A method for operating a powerplant of an aircraft during an uncommanded high thrust (UHT) event of the powerplant, the powerplant including an engine and a variable-pitch propeller driven by the engine, the method comprising:
enabling a UHT detection function associated with the powerplant when an enabling condition has been met;
when the UHT detection function is enabled, detecting the UHT event when:
a power lever associated with the powerplant is at a given position;
a parameter indicative of engine speed or engine power is above a first threshold;
a rate of change of the engine speed is above a second threshold; and
the aircraft is in a final approach phase of flight; and

in response to detecting the UHT event:
outputting an alert to trigger accommodations to the UHT event for the engine;
automatically commanding the engine of the powerplant to shut down; and
automatically commanding the variable-pitch propeller of the powerplant to feather.

2. The method of claim 1 , wherein the enabling condition comprises a predetermined altitude of the aircraft.

3. The method of claim 1 , wherein the parameter indicative of engine speed or engine power is a shaft horsepower of the engine.

4. The method of claim 1 , wherein the parameter indicative of engine speed or engine power is a requested gas generator speed of the engine, and wherein the first threshold is an actual gas generator speed of the engine.

5. The method of claim 1 , further comprising detecting the UHT event for a predetermined time before outputting the alert to trigger the accommodations.

6. The method of claim 1 , wherein the second threshold is a requested rate of change of the engine speed plus a margin.

7. The method of claim 6 , wherein the rate of change of the engine speed is a rate of acceleration of the engine, and wherein the margin comprises a response time for an efficient engine.

8. The method of claim 6 , wherein the rate of change of the engine speed is a rate of deceleration of the engine, and wherein the margin comprises a response time for an inefficient engine.

9. A system for operating a powerplant of an aircraft during an uncommanded high thrust (UHT) event of the powerplant, the powerplant including an engine and a variable-pitch propeller driven by the engine, the system comprising:
at least one processing unit; and
a non-transitory computer-readable medium having stored thereon program code executable by the at least one processing unit for:
enabling a UHT detection function associated with the powerplant when an engine when an enabling condition has been met;
when the UHT detection function is enabled, detecting the UHT event when:
a power lever associated with the powerplant is at a given position;
a parameter indicative of engine speed or engine power is above a first threshold;
a rate of change of the engine speed is above a second threshold; and
the aircraft is in a final approach phase of flight; and

in response to detecting the UHT event:
outputting an alert to trigger accommodations to the UHT event for the engine;
automatically commanding the engine of the powerplant to shut down; and
automatically commanding the variable-pitch propeller of the power plant to feather.

10. The system of claim 9 , wherein the enabling condition comprises a predetermined altitude of the aircraft.

11. The system of claim 9 , wherein the parameter indicative of engine speed or engine power is a shaft horsepower of the engine.

12. The system of claim 9 , wherein the parameter indicative of engine speed or engine power is a requested gas generator speed of the engine, and wherein the first threshold is an actual gas generator speed of the engine.

13. The system of claim 9 , wherein the program code is further executable for detecting the UHT event for a predetermined time before outputting the alert to trigger the accommodations.

14. The system of claim 9 , wherein the second threshold is a requested rate of change of the engine speed plus a margin.

15. The system of claim 14 , wherein the rate of change of the engine speed is a rate of acceleration of the engine, and wherein the margin comprises a response time for an efficient engine.

16. The system of claim 14 , wherein the rate of change of the engine speed is a rate of deceleration of the engine, and wherein the margin comprises a response time for an inefficient engine.

Assignees

• Pratt & Whitney Canada

Inventors

• Chahal Jasraj
• Mounir Faty Zachary
• Lisio Carmine
• Mcgrath Darragh
• Zingaro Giancarlo

Classifications

• F01D21/14

  responsive to other specific conditions · CPC title

• F05D2270/021

  to prevent overspeed · CPC title

• F02C9/58

  with control of a variable-pitch propeller · CPC title

• F05D2270/051

  Thrust · CPC title

• F02C9/44

  responsive to the speed of aircraft, e.g. Mach number control, optimisation of fuel consumption · CPC title