Gas turbine engine particulate ingestion and accumulation sensor system and method

Patent metadata

Field	Value
Publication number	US-11149583-B2
Application number	US-202016834112-A
Country	US
Kind code	B2
Filing date	Mar 30, 2020
Priority date	Apr 18, 2017
Publication date	Oct 19, 2021
Grant date	Oct 19, 2021

Abstract

A system and method for determining particulate accumulation in a gas turbine engine includes sensing the number, size, and type of particulate at a first position on the gas turbine engine and supplying first data representative thereof, where the first position located at a first side of a gas turbine engine component; sensing the number, size, and type of particulate at a second position on the gas turbine engine and supplying first data representative thereof, where the second position located at a second side of the gas turbine engine component and downstream of the first position; and processing the first data and the second data to determine the mass of the particulate accumulated on the gas turbine engine component.

First claim

What is claimed is:

1. A gas turbine engine particulate ingestion detection system, comprising:
a first particulate sensor mounted at a first position on the gas turbine engine, the first position located at a first side of a gas turbine engine component, the first particulate sensor configured to sense a number of, a size of, and a type of particulate at the first position and supply first data representative thereof;
a second particulate sensor mounted at a second position on the gas turbine engine, the second position located at a second side of the gas turbine engine component and downstream of the first position, the second particulate sensor configured to sense a number of, a size of, and a type of the particulate at the second position and supply second data representative thereof; and
a processor coupled to receive the first data and the second data from the first and second particulate sensors, respectively, the processor configured, to receive the first data and the second data, to determine, based at least on the number of, the size of, and the type of the particulate at the first and second positions, a mass of the particulate accumulated on the gas turbine engine component.

2. The system of claim 1 , wherein the processor is further configured to:
compare the mass of the particulate accumulated on the gas turbine engine component to a threshold mass value; and
generate a signal when the mass of the particulate accumulated on the gas turbine engine component exceeds the threshold mass value.

3. The system of claim 2 , wherein the threshold mass value depends on one or more of: the type of particulate being sensed, and the particular gas turbine engine component.

4. The system of claim 2 , further comprising:
an alert generator coupled to receive the signal from the processor and to generate an alert after receiving the signal.

5. The system of claim 4 , wherein the alert communicates the type of particulate accumulated on the gas turbine engine component.

6. The system of claim 2 , wherein the signal initiates one or more actions to mitigate further particulate accumulation on the gas turbine engine component.

7. The system of claim 6 , wherein the one or more actions include one or more of:
increasing the rotational speed of the gas turbine engine component;
varying a position of one or more variable geometry devices in the gas turbine engine;
energizing one or more heaters in the gas turbine engine;
opening one or more compressor bypass channels in the gas turbine engine; and
displaying one or more messages to exit a source of the particulate on a display for the gas turbine engine.

8. The system of claim 1 , wherein the particulate comprises one or more of water droplets, ice crystals, dust, and volcanic ash.

9. The system of claim 1 , further comprising:
a third particulate sensor mounted at the second position on the gas turbine engine, the third particulate sensor configured to sense a number of, a size of, and a type of the particulate at the second position and supply third data representative thereof to the processor.

10. The system of claim 1 , further comprising:
a plurality of additional particulate sensors, each additional particulate sensor is mounted at a corresponding position on the gas turbine engine that is different from the first and second positions, each additional particulate sensor is configured to sense a number of, a size of, and a type of the particulate at its corresponding position and supply additional data representative thereof,
wherein the processor is further coupled to receive the additional data from each of the additional sensor signals, and is further configured, upon receipt of the additional data to:
determine, based at least on the number of, the size of, and the type of the particulate at the corresponding positions, a mass of the particulate accumulated on an additional gas turbine engine component.

11. The system of claim 10 , wherein:
the gas turbine engine component is a first turbine engine component;
the first turbine engine component is a fan; and
the additional turbine engine component includes a first compressor stage and a second compressor stage.

Assignees

• Honeywell Int Inc

Inventors

• Dischinger Dave
• Nolcheff Nick

Classifications

• G01M15/14

  Testing gas-turbine engines or jet-propulsion engines · CPC title

• F05D2260/80

  Diagnostics · CPC title

• F02C7/05

  having provisions for obviating the penetration of damaging objects or particles · CPC title

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title

• F05D2260/607

  Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles · CPC title