IP Library Granted Patent US 11,555,455
Granted Patent B2
US 11,555,455 · App. 16/783,512 · Granted Jan 17, 2023

Adaptive model predictive control for hybrid electric propulsion

Inventors: Timothy J. Crowley (Tolland, CT); Sorin Bengea (Glastonbury, CT); Manuj Dhingra (Glastonbury, CT); David Gelwan (West Hartford, CT); Kevin Hendricks (Vernon, CT); Joshua Adams (New Hartford, CT); Martin Richard Amari (Glastonbury, CT); Richard P. Meisner (Glastonbury, CT); David Lei Ma (Avon, CT)
Assignee: RAYTHEON TECHNOLOGIES CORPORATION
F02C9/00B64D27/02B64D2027/026F05D2220/323F05D2220/76F05D2240/60F05D2260/80F05D2270/09F05D2270/20F05D2270/44F05D2270/80
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Quick Facts
Patent No.
US 11,555,455
App. No.
16/783,512
Granted
Jan 17, 2023
Kind
B2
Abstract

A hybrid electric propulsion system includes a gas turbine engine having at least one compressor section and at least one turbine section operably coupled to a shaft. The hybrid electric propulsion system includes an electric motor configured to augment rotational power of the shaft of the gas turbine engine. A controller is operable to determine an estimate of hybrid electric propulsion system parameters based on a composite system model and sensor data, determine a model predictive control state and a prediction based on the hybrid electric propulsion system parameters and the composite system model, determine a model predictive control optimization for a plurality of hybrid electric system control effectors based on the model predictive control state and the prediction using a plurality of reduced-order partitions of the composite system model, and actuate the hybrid electric system control effectors based on the model predictive control optimization.

Claims (41)

1. A hybrid electric propulsion system comprising:

a gas turbine engine comprising at least one compressor section and at least one turbine section operably coupled to a shaft;

an electric motor configured to augment rotational power of the shaft of the gas turbine engine; and

a controller operable to:

determine an estimate of a plurality of hybrid electric propulsion system parameters based on a composite system model and a plurality of sensor data;

determine a model predictive control state and a prediction based on the hybrid electric propulsion system parameters and the composite system model;

determine a model predictive control optimization for a plurality of hybrid electric system control effectors based on the model predictive control state and the prediction using a plurality of reduced-order partitions of the composite system model; and

actuate the hybrid electric system control effectors based on the model predictive control optimization.

2. The hybrid electric propulsion system of claim 1 , wherein the controller is further configured to update a plurality of composite system model states of the composite system model based on detection of one or more faults.

3. The hybrid electric propulsion system of claim 2 , wherein the controller is further configured to update one or more reduced-order values based on the reduced-order partitions of the composite system model states of the composite system model.

4. The hybrid electric propulsion system of claim 3 , wherein the one or more reduced-order values are reduced-order Jacobian values based on a plurality of Jacobian equations associated with the composite system model.

5. The hybrid electric propulsion system of claim 4 , wherein the reduced-order partitions comprise partitions of a propulsion system model comprising a gas turbine engine model, a mechanical power transmission model, and an electrical power system model that preserve a plurality of dominant states for each partition.

6. The hybrid electric propulsion system of claim 5 , wherein the composite system model comprises the propulsion system model, an optimization objective function, and a plurality of constraints.

7. The hybrid electric propulsion system of claim 6 , wherein the Jacobian equations associated with the composite system model comprise a plurality of model sensitivity matrices that are updated based on the detection of one or more faults.

8. The hybrid electric propulsion system of claim 7 , wherein the model predictive control optimization uses the model sensitivity matrices to determine a set of changes to the hybrid electric system control effectors that optimizes the optimization objective function over a finite time horizon while maintaining the constraints.

9. The hybrid electric propulsion system of claim 1 , further comprising an electric generator configured to extract power from the shaft, wherein the composite system model comprises a plurality of electrical and mechanical physics-based models of at least the gas turbine engine, the electric motor, the electric generator, and one or more mechanical power transmissions.

10. A hybrid electric propulsion system comprising:

a gas turbine engine;

an electrical power system;

a mechanical power transmission operably coupled between the gas turbine engine and the electrical power system;

a plurality of hybrid electric system control effectors operable to control a plurality of states of one or more the gas turbine engine and the electrical power system; and

a controller for controlling the hybrid electric system control effectors based on a model predictive control that is dynamically updated during operation of the hybrid electric propulsion system, the controller operable to:

determine an estimate of a plurality of hybrid electric propulsion system parameters based on a composite system model and a plurality of sensor data;

determine a model predictive control state and a prediction based on the hybrid electric propulsion system parameters and the composite system model;

determine a model predictive control optimization for the hybrid electric system control effectors based on the model predictive control state and the prediction using a plurality of reduced-order partitions of the composite system model; and

actuate the hybrid electric system control effectors based on the model predictive control optimization.

11. The hybrid electric propulsion system of claim 10 , wherein the controller is further configured to update a plurality of composite system model states of the composite system model based on detection of one or more faults and update one or more reduced-order values based on the reduced-order partitions of the composite system model states of the composite system model.

12. The hybrid electric propulsion system of claim 11 , wherein the one or more reduced-order values are reduced-order Jacobian values based on a plurality of Jacobian equations associated with the composite system model, and the reduced-order partitions comprise partitions of a propulsion system model comprising a gas turbine engine model, a mechanical power transmission model, and an electrical power system model that preserve a plurality of dominant states for each partition.

13. The hybrid electric propulsion system of claim 12 , wherein the composite system model comprises the propulsion system model, an optimization objective function, and a plurality of constraints, and the Jacobian equations associated with the composite system model comprise a plurality of model sensitivity matrices that are updated based on the detection of one or more faults.

14. The hybrid electric propulsion system of claim 13 , wherein the model predictive control optimization uses the model sensitivity matrices to determine a set of changes to the hybrid electric system control effectors that optimizes the optimization objective function over a finite time horizon while maintaining the constraints.

15. The hybrid electric propulsion system of claim 10 , wherein the electrical system comprises at least two electric motors, at least two electric generators, and an energy storage system.

16. A method for controlling a hybrid electric propulsion system, the method comprising:

determining, by a controller, an estimate of a plurality of hybrid electric propulsion system parameters based on a composite system model and a plurality of sensor data;

determining, by the controller, a model predictive control state and a prediction based on the hybrid electric propulsion system parameters and the composite system model;

determining, by the controller, a model predictive control optimization for a plurality of hybrid electric system control effectors based on the model predictive control state and the prediction using a plurality of reduced-order partitions of the composite system model; and

actuating, by the controller, the hybrid electric system control effectors based on the model predictive control optimization.

17. The method of claim 16 , further comprising:

updating a plurality of composite system model states of the composite system model based on detection of one or more faults; and

updating one or more reduced-order values based on the reduced-order partitions of the composite system model states of the composite system model.

18. The method of claim 17 , wherein the one or more reduced-order values are reduced-order Jacobian values based on a plurality of Jacobian equations associated with the composite system model, and the reduced-order partitions comprise partitions of a propulsion system model comprising a gas turbine engine model, a mechanical power transmission model, and an electrical power system model that preserve a plurality of dominant states for each partition.

19. The method of claim 18 , wherein the composite system model comprises the propulsion system model, an optimization objective function, and a plurality of constraints, and the Jacobian equations associated with the composite system model comprise a plurality of model sensitivity matrices that are updated based on the detection of one or more faults, wherein the model predictive control optimization uses the model sensitivity matrices to determine a set of changes to the hybrid electric system control effectors that optimizes the optimization objective function over a finite time horizon while maintaining the constraints.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE SPELLING ON THE ADDRESS 10 FARM SPRINGD ROAD FARMINGTONCONNECTICUT 06032 PREVIOUSLY RECORDED ON REEL 057190 FRAME 0719. ASSIGNOR(S) HEREBY CONFIRMS THE CORRECT SPELLING OF THE ADDRESS 10 FARM SPRINGS ROAD FARMINGTON CONNECTICUT 06032. Recorded Aug 19, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 057226/0390 →
CHANGE OF NAME Recorded Aug 16, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 057190/0719 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 6, 2020
From: CROWLEY, TIMOTHY J.; BENGEA, SORIN; DHINGRA, MANUJ; GELWAN, DAVID; HENDRICKS, KEVIN; ADAMS, JOSHUA; AMARI, MARTIN RICHARD; MEISNER, RICHARD P.; MA, DAVID LEI
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 051740/0433 →