Multi-engine performance margin synchronization adaptive control system and method

Patent metadata

Field	Value
Publication number	US-9458771-B2
Application number	US-201313870302-A
Country	US
Kind code	B2
Filing date	Apr 25, 2013
Priority date	Mar 25, 2013
Publication date	Oct 4, 2016
Grant date	Oct 4, 2016

Abstract

A system and method of adaptively synchronizing the performance margin of a multi-engine system includes continuously, and in real-time, determining the performance margin of a first engine and the performance margin of the second engine. A difference between the performance margins of the first and second engines is calculated, and the first and second engines are controlled to attain a predetermined difference between the performance margins of the first and second engines.

First claim

What is claimed is:

1. A method of adaptively synchronizing performance margins of a multi-engine system, the method comprising the steps of:
continuously, and in real-time, determining a performance margin of a first engine and a performance margin of a second engine;
calculating a difference between the performance margins of the first and second engines;
creating a load imbalance between the first and second engines whenever the calculated difference between the performance margins of the first and second engines is non-zero; and
controlling the first and second engines to attain a predetermined difference between the performance margins of the first and second engines.

2. The method of claim 1 , further comprising:
continuously determining a control parameter of the first engine and a control parameter of the second engine; and
calculating a difference between the control parameters of the first and second engines to thereby determine a control parameter difference.

3. The method of claim 2 , wherein the first and second engines are controlled based in part on the control parameter difference.

4. The method of claim 2 , further comprising:
generating a bias signal from the calculated difference between the performance margins.

5. The method of claim 4 , further comprising:
limiting the bias signal to a maximum allowable split between the first and second engines.

6. The method of claim 5 , wherein the first and second engines are controlled based on the control parameter difference and the bias signal.

7. The method of claim 1 , wherein one or more of turbine inlet temperature at a first predefined power condition or turbine speed at a second predefined power condition is used in the determining of the performance margins of the first and second engines.

8. The method of claim 2 , wherein the control parameter of the first engine and the control parameter of the second engine are each one or more of torque, turbine inlet temperature, and turbine speed.

9. A system for adaptively synchronizing performance margins of a multi-engine system, comprising:
a first engine configured to generate a first torque and having a determinable first engine performance margin;
a second engine configured to generate a second torque and having a determinable second engine performance margin;
a first engine controller coupled to, and associated with, the first engine, the first engine controller configured to continuously, and in real-time, determinable the first engine performance margin; and
a second engine controller coupled to, and associated with, the second engine, the second engine controller configured to continuously, and in real-time, determine the determinable second engine performance margin,
wherein the first and second engine controllers are in operable communication with each other, and each of the first and second engine controllers is further configured to:
calculate a difference between the determinable first engine performance margin and the determinable second engine performance margin;
create a load imbalance between the first and second engines whenever the calculated difference between the determinable first performance margin of the first engine and the determinable second performance margin of the second engine is non-zero; and
control the first and second engines, respectively, to attain a predetermined difference between the determinable first performance margin of the first engine and the determinable second performance margin of the second engine.

10. The system of claim 9 , wherein the first and second engine controllers are each:
coupled to receive a first signal representative of a control parameter of the first engine and a second signal representative of a control parameter of the second engine; and
further configured to calculate a difference between the control parameters of the first and second engines to thereby generate a control parameter difference.

11. The system of claim 10 , wherein the first and second engine controllers are each configured to control the first and second engines, respectively, based in part on a calculated torque difference.

12. The system of claim 10 , wherein the first and second engine controllers are each further configured to generate a bias signal from the calculated difference between the determinable first engine performance margin and the second determinable engine performance margin.

13. The system of claim 12 , wherein the first and second engine controllers are each further configured to limit the bias signal to a maximum allowable split between the first and second engines.

14. The system of claim 12 , wherein the first and second engine controllers are each further configured to control the first and second engines, respectively, based on the calculated control parameter difference and the bias signal.

15. The system of claim 9 , wherein one or more of turbine inlet temperature at a first predefined power condition or turbine speed at a second predefined power condition is used in the determining of the determinable first performance margin of the first engine and the determinable second performance margin of the second engine.

16. The system of claim 9 , wherein the control parameter of the first engine and the control parameter of the second engine are each one or more of torque, turbine inlet temperature, and turbine speed.

Assignees

• Honeywell Int Inc

Inventors

• Ling Richard
• Gordon Grant
• Moeckly Kevin

Classifications

• F05D2270/02

  to control rotational speed (n) · CPC title

• F05D2270/303

  Temperature · CPC title

• F05D2270/052

  Torque · CPC title

• F02C9/42 Primary

  specially adapted for the control of two or more plants simultaneously · CPC title

• F05D2270/44

  active, predictive, or anticipative · CPC title