Lifing and performance optimization limit management for turbine engine

Patent metadata

Field	Value
Publication number	US-10965231-B2
Application number	US-201916361691-A
Country	US
Kind code	B2
Filing date	Mar 22, 2019
Priority date	Mar 15, 2013
Publication date	Mar 30, 2021
Grant date	Mar 30, 2021

Abstract

A control for a multi-shaft turbine engine system using electrical machines seeks optimal system performance while accommodating hard and soft component limits. To accommodate the component limits, the control may generate a number of possible operating point options reflecting potential trade-offs in performance, lifing, efficiency, or other objectives.

First claim

The invention claimed is:

1. A system for control of a turbine engine, the system comprising:
a low pressure turbine, coupled to the turbine engine via a low pressure shaft;
a high pressure turbine, coupled to the turbine engine via a high pressure shaft;
one or more electrical machines coupled to each of the low pressure shaft and the high pressure shaft, the electrical machines configured to extract rotational power from the low pressure shaft and the high pressure shaft and output electrical power;
one or more generator control units coupled to each of the electrical machines to control the amount of rotational power extracted by the electrical machines; and
a hardware controller configured to (i) determine a first operating point for the system associated with a first vehicle operating mode based on a first optimization objective, wherein the first operating point is indicative of a first available power value for thrust, and (ii) determine a second operating point for the system associated with a second vehicle operating mode based on a second optimization objective having a higher priority than the first optimization objective, wherein the second operating point is indicative of load shedding to increase available power for thrust by reducing electrical power supplied by the one or more electrical machines to an electrical component;
wherein each of the first operating point and the second operating point represents an objective trade-off involving a modification of the corresponding optimization objective to maintain component limits or a modification of one or more of the component limits, wherein each component limit comprises a bound on an operating condition of a component of the turbine engine system.

2. The system of claim 1 , wherein:
the first optimization objective comprises at least one of efficiency, lifing, reliability, or stability; and
the second optimization objective comprises available power.

3. The system of claim 1 , wherein the second operating point is indicative of a second available power value for thrust, wherein the second available power value is greater than the first available power value, and wherein the second operating point reduces electrical power supplied by the one or more electrical machines to the electrical component.

4. The system of claim 1 , wherein:
the first operating point indicates that the electrical component is supplied power by the one or more electrical machines; and
the second operating point indicates that the electrical component is not supplied power by the one or more electrical machines.

5. The system of claim 4 , wherein the electrical component comprises a vehicle accessory component.

6. The system of claim 1 , wherein the hardware controller is further to select the electrical component based on a predetermined priority level associated with the electrical component.

7. The system of claim 1 , wherein the hardware controller is further to:
communicate a first power extraction control signal to the one or more generator control units in response to a determination of the first operating point; and
communicate a second power extraction control signal to the one or more generator control units in response to a determination of the second operating point.

8. The system of claim 7 , wherein:
the one or more generator control units achieve the first operating point in response to communication of the first power extraction control signal; and
the one or more generator control units achieve the second operating point in response to communication of the second power extraction control signal.

9. The system of claim 1 , wherein the hardware controller is further configured to (i) determine the first optimization objective, wherein the first optimization objective is associated with the first vehicle operating mode, and (ii) determine the second optimization objective, wherein the second optimization objective is associated with the second vehicle operating mode, and wherein the second optimization objective comprises available power;
wherein to determine the first operating point comprises to determine the first operating point based on the first optimization objective; and
wherein to determine the second operating point comprises to determine the second operating point based on the second optimization objective.

Assignees

• Rolls Royce Corp

Inventors

• Armstrong Michael
• French Mat

Classifications

• F02C7/32 Primary

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• F05D2270/101

  Compressor surge or stall · CPC title

• H02P2101/30

  for aircraft · CPC title

• F01D21/12

  responsive to temperature · CPC title

• H02P9/04 Primary

  Control effected upon non-electric prime mover and dependent upon electric output value of the generator · CPC title