Invention Grant
- Patent Title: Gas turbine engine uncontrolled high thrust detection system and method
-
Application No.: US14863140Application Date: 2015-09-23
-
Publication No.: US09932906B2Publication Date: 2018-04-03
- Inventor: Yufei Xiong , Dave Faymon , Scot Coffey
- Applicant: HONEYWELL INTERNATIONAL INC.
- Applicant Address: US NJ Morris Plains
- Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee Address: US NJ Morris Plains
- Agency: Lorenz & Kopf, LLP
- Main IPC: F02C9/28
- IPC: F02C9/28 ; F02C9/46 ; F02C9/54

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.
Public/Granted literature
- US20170081974A1 GAS TURBINE ENGINE UNCONTROLLED HIGH THRUST DETECTION SYSTEM AND METHOD Public/Granted day:2017-03-23
Information query
IPC分类: