System and method for controlling engine speed with bowed rotor mitigation

Patent metadata

Field	Value
Publication number	US-11359546-B2
Application number	US-202016852856-A
Country	US
Kind code	B2
Filing date	Apr 20, 2020
Priority date	Apr 20, 2020
Publication date	Jun 14, 2022
Grant date	Jun 14, 2022

Abstract

Systems and methods to operate an engine in a bowed rotor mitigation mode. An engine starting system includes a starter coupled to the engine and with a compressor. A conduit system communicates a portion of the compressed air from the compressor to the starter. A load control valve controls compressed air from the compressor to the starter and to other loads. A starter air valve controls compressed air through the conduit system to the starter. At least one controller: receives a start signal from the engine; determines whether to initiate a bowed rotor mitigation of the engine; operates either the load control valve or the starter air valve to move to a predetermined static position; and operates the other of the load control valve or the starter air valve to achieve a target speed of the engine.

First claim

What is claimed is:

1. An engine starting system, comprising:
an engine system including an engine;
a starter coupled to the engine and configured to rotate the engine;
an air source including a compressor configured to deliver compressed air;
a conduit system coupled between the compressor and the starter, wherein the conduit system is configured to communicate compressed air from the compressor to the starter and to other compressed air loads;
a load control valve disposed in the conduit system between the compressor and the starter, and configured to control communication of compressed air from the compressor to the starter and to the other compressed air loads;
a starter air valve disposed in the conduit system between the load control valve and the starter, and configured to control communication of compressed air to the starter; and
at least one controller coupled with the engine and with the air source, the at least one controller configured to:
when a start signal is received from the engine system, determine whether to initiate a bowed rotor mitigation start mode of the engine;
if the bowed rotor mitigation start mode is initiated, operate one of the load control valve and the starter air valve to move to a predetermined static position that was previously stored for access by the at least one controller for bowed rotor mitigation, and operate, by modulating via an actuator during the bowed rotor mitigation, the other of the load control valve or the starter air valve to achieve a target speed of the engine,
wherein, the predetermined static position of the starter air valve for the bowed rotor mitigation corresponds to a start engine open position that is also used during normal start of the engine without bowed rotor mitigation, and the predetermined static position of the load control valve is a bowed rotor mitigation open position that differs from a normal start open position used during normal start of the engine without bowed rotor mitigation and a full open position used to supply compressed air to the compressed air loads.

2. The system of claim 1 , wherein the load control valve is disposed in a section of the conduit system extending between the air source and the other compressed air loads, and comprising a surge control valve disposed in the conduit system and configured to divert compressed air out of the conduit system, bypassing a part of the air source, and effecting a flow reduction through the section, wherein the at least one controller is configured to set the surge control valve to be initially closed during the bowed rotor mitigation start mode to avoid the flow reduction.

3. The system of claim 2 , wherein the conduit system includes a first branch extending between the section and the starter air valve, wherein the starter air valve is disposed in the first branch, and comprising an engine bleed valve disposed in a second branch of the conduit system, the second branch extending between the section and the engine, the engine bleed valve controlling communication through the second branch between the section and at least a portion of the engine other than the starter, wherein the at least one controller is configured to set the engine bleed valve to be closed during the bowed rotor mitigation start mode.

4. The system of claim 1 , wherein the at least one controller is configured to operate the load control valve to the predetermined static position of the load control valve during the bowed rotor mitigation start mode and to modulate the starter air valve to achieve the target speed of the engine, wherein the predetermined static position of the load control valve is selected to produce a torque in the starter to produce a bowed rotor mitigation speed in the engine.

5. The system of claim 1 , wherein the at least one controller is configured to operate the starter air valve to the predetermined static position during the bowed rotor mitigation start mode and to operate the load control valve to achieve a target speed of the engine.

6. The system of claim 1 , comprising an engine bleed valve configured to control communication between the conduit system and at least a portion of the engine; and
a surge control valve configured to divert compressed air passing from the air source to the load control valve,
wherein, upon initiation of the bowed rotor mitigation start mode, the controller is configured to set the load control valve to the predetermined static position of the load control valve, set the surge control valve to a second static position, set the engine bleed valve to a third static position, and modulate the starter air valve,
wherein the controller is configured to maintain the load control valve, the engine bleed valve and the surge control valve in their respective static positions for the duration of the bowed rotor mitigation start mode.

7. The system of claim 1 , comprising a surge control valve disposed in the conduit system and configured to divert compressed air out of the conduit system, bypassing a part of the air source, wherein the at least one controller is configured to:
operate the load control valve to the predetermined static position of the load control valve during the bowed rotor mitigation start mode;
operate the surge control valve to avoid surge conditions in the air source; and
modulate the starter air valve to achieve the target speed of the engine.

8. The system of claim 1 , comprising:
a surge control valve disposed in the conduit system and configured to divert compressed air from reaching the load control valve and the starter, compressed air downstream of the surge control valve passing out of the conduit system; and
an engine bleed valve disposed in the conduit system to control communication between the conduit system and at least a portion of the engine,
wherein the at least one controller is configured to:
set the surge control valve to closed during the bowed rotor mitigation start mode;
set the engine bleed valve to closed during the bowed rotor mitigation start mode;
set the load control valve to the predetermined static position of the load control valve during the bowed rotor mitigation start mode; and
modulate the starter air valve during the bowed rotor start mitigation mode to achieve the target speed of the engine.

9. The system of claim 8 , wherein the predetermined static position of the load control valve is configured to effect a rotation of the engine at a speed that is less than a normal start speed of the engine.

10. The system of claim 1 , comprising a sensor set configured to determine parameters relevant to the bowed rotor mitigation of the engine, wherein the at least one controller is configured to initiate the bowed rotor mitigation start mode when the parameters are within a predetermined range and to initiate the normal start of the engine when the parameters are outside the predetermined range, wherein the parameters are indicative of bowed rotor conditions and comprise time form engine shutdown, ambient temperature and internal engine temperature.

11. The system of claim 1 , wherein the air source comprises an auxiliary power unit of an aircraft and the system further comprises:
a compressor in the engine;
a section of the conduit system that extends from the auxiliary power unit to the other compressed air loads;
a first branch of the conduit system that extends from the section to the starter and includes the starter air valve; and
a second branch of the conduit system that extends from the section to the compressor of the engine and includes an engine bleed valve,
wherein the starter air valve is configured to control flow through the first branch and wherein the en

Assignees

• Honeywell Int Inc

Inventors

• Lam Cecilia

Classifications

• F01D25/34

  Turning or inching gear · CPC title

• F02C7/277 Primary

  the starter being a {separate} turbine · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F05D2260/85

  Starting · CPC title

• F05D2220/50

  for auxiliary power units (APU's) · CPC title