Autonomous engine health management system

• US 9,885,250 B2
• Filed: 10/23/2015
• Issued: 02/06/2018
• Est. Priority Date: 10/23/2015
• Status: Active Grant

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: James, Denman H.
• Primary Examiner(s): To, Tuan C
• Application Number:
  US14/921,429
• Publication Number:
  US 20170114660A1
• Time in Patent Office: 837 Days
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: F02C 3/04 having a turbine driving a compressor power transmission arrangements F02C7/36; control of working fluid flow F02C9/16
• CPC Class Codes: F02C 7/06 Arrangements of bearings bearings F16C; Lubricating of turbo machines F01D25/18; of machines or engines in general F01M
• CPC Class Codes: F02C 7/26 Starting; Ignition
• CPC Class Codes: F02D 41/26 using computer, e.g. microprocessor
• CPC Class Codes: F05D 2260/80 Diagnostics
• CPC Class Codes: F05D 2260/85 Starting
• CPC Class Codes: F05D 2270/301 Pressure
• CPC Class Codes: F05D 2270/304 Spool rotational speed

Abstract

An engine health monitoring system includes an engine component having a sensor system configured to monitor at least one parameter of the component. An autonomous monitoring system is coupled to the sensor system and is configured to receive and store the at least one monitored parameter while an engine controller is unpowered. The engine controller is communicatively coupled to the autonomous monitoring system.

Claims

1. A method of monitoring the health of a gas turbine engine comprising:

sensing at least one of an inlet oil pressure and a shaft speed while a gas turbine engine is off;

storing the sensed values of the at least one of an inlet oil pressure and a shaft speed in a local memory of an autonomous monitoring system; and

reporting the stored sensed values of the at least one of said inlet oil pressure and said shaft speed to an engine controller during an engine initialization.

2. The method of claim 1, further comprising analyzing the reported stored sensed values using the engine controller during an initialization of the engine, and halting the initialization of the engine in response to a determination that at least one component operated in a potentially damaging condition based on the sensed values.

3. The method of claim 2, further comprising the engine controller determining that a shaft operated in a potentially damaging condition in response to a sensed rotational shaft speed exceeding a maximum threshold while the engine is off.

4. The method of claim 2, further comprising the engine controller determining that a shaft operated in a potentially damaging condition in response to a sensed inlet oil pressure falling below a minimum threshold while the engine is off.

5. The method of claim 1, further comprising charging a local power storage device of the autonomous monitoring system while said engine is operating.

6. The method of claim 1, further comprising correlating the stored sensed values of the at least one of an inlet oil pressure and a shaft speed with a time at which the value was sensed using a local processor of the autonomous monitoring system, and storing the time correlation in the local memory.

7. The method of claim 6, wherein reporting the stored sensed values of the at least one of said inlet oil pressure and said shaft speed to the engine controller during an engine initialization further includes reporting the time correlated to the engine controller.

8. The method of claim 1, wherein sensing at least one of the inlet oil pressure and the shaft speed while a gas turbine engine is off comprises sensing both the inlet oil pressure and the shaft speed while the gas turbine engine is off.

9. The method of claim 1, wherein sensing at least one of the inlet oil pressure and the shaft speed while a gas turbine engine is off comprises sensing both the inlet oil pressure and the shaft speed while the gas turbine engine is off.