Turbomachinery heat transfer system

Patent metadata

Field	Value
Publication number	US-11603773-B2
Application number	US-202016860431-A
Country	US
Kind code	B2
Filing date	Apr 28, 2020
Priority date	Apr 28, 2020
Publication date	Mar 14, 2023
Grant date	Mar 14, 2023

Abstract

A heat management system for turbomachinery is provided. The heat management system includes a thermal delivery system configured to providing heating, cooling, or a combination thereof, to a turbomachinery. The thermal delivery system includes a first heat transfer conduit and a second heat transfer conduit. The second heat transfer conduit is disposed on the turbomachinery adjacent to the first heat transfer conduit. The heat management system additionally includes a controller operatively coupled to the thermal delivery system and configured to control the heating, the cooling, or the combination thereof, of the turbomachinery via the thermal delivery system.

First claim

The invention claimed is:

1. A heat management system comprising:
a thermal delivery system configured to providing heating, cooling, or a combination thereof, to a turbomachinery, the thermal delivery system comprising:
a first heat transfer conduit; and
a second heat transfer conduit disposed adjacent to the first heat transfer conduit;

a heat sensor disposed adjacent to a section of the first heat transfer conduit; and
a controller operatively coupled to the thermal delivery system and communicatively coupled to the heat sensor, the controller configured to control the heating, the cooling, or the combination thereof, of the turbomachinery via the thermal delivery system based at least on readings from the heat sensor, wherein the section of the first heat transfer conduit comprises an insulating wrap that only encloses the section of the first heat transfer conduit and the heat sensor and that is in direct contact with the heat sensor and the section of the first heat transfer conduit.

2. The system of claim 1 , wherein the second heat transfer conduit is disposed parallel to the first heat transfer conduit.

3. The system of claim 2 , wherein the first heat transfer conduit is offset from the second heat transfer conduit by a distance between 0.25 inches and 5 inches.

4. The system of claim 1 , wherein the first heat transfer conduit comprises a first electrically-powered heating element, and the second heat transfer conduit comprises a second electrically-powered heating element; and wherein the controller is configured to independently control the first electrically-powered heating element and the second electrically-powered heating element.

5. The system of claim 4 , wherein the controller is configured to provide redundant operations by adjusting control of the first electrically-powered heating element when the second electrically-powered heating element is inoperative or by adjusting control of the second electrically-powered heating element when the first electrically-powered heating element is inoperative.

6. The system of claim 1 , wherein the thermal delivery system comprises a radiant barrier layer disposed radially outward of the heat transfer conduit and a casing of the turbomachinery.

7. The system of claim 1 , wherein the turbomachinery comprises a gas turbine engine; and wherein the controller is configured to control a shutdown operation of the gas turbine engine and to control the thermal delivery system during the shutdown operation.

8. A method comprising:
providing heating, cooling, or a combination thereof, to a turbomachinery via a first heat transfer conduit and a second heat transfer conduit included in a thermal delivery system, wherein the second heat transfer conduit is disposed on the turbomachinery adjacent to the first heat transfer conduit, and wherein a section of the first heat transfer conduit comprises an insulating wrap that only encloses the section of the first heat transfer conduit and a heat sensor and that is in direct contact with the heat sensor and the section of the first heat transfer conduit; and
controlling the heating, the cooling, or the combination thereof, of the turbomachinery, via a controller operatively coupled to the thermal delivery system, to minimize or to eliminate positional changes, structural changes, or a combination thereof, in one or more components of the turbomachinery due to thermal energy, wherein the controller uses at least readings from the heat sensor to control the heating, the cooling, or the combination thereof.

9. The method of claim 8 , wherein the second heat transfer conduit is disposed parallel to the first heat transfer conduit, is offset from the first heat transfer conduit, or a combination thereof.

10. The method of claim 8 , wherein the first heat transfer conduit comprises a first electrically-powered heating element, and the second heat transfer conduit comprises a second electrically-powered heating element; and wherein the controller is configured to independently control the first electrically-powered heating element and the second electrically-powered heating element.

11. The method of claim 10 , comprising providing redundant operations, via the controller, by adjusting control of the first electrically-powered heating element when the second electrically-powered heating element is inoperative or by adjusting control of the second electrically-powered heating element when the first electrically-powered heating element is inoperative.

12. The method of claim 8 , wherein at least the first heat transfer conduit provides for a lateral symmetry for heating, for cooling, or a combination thereof, of a casing of the turbomachinery.

13. The method of claim 8 , wherein the section is between 0.5 inches and 10 inches in length.

14. A non-transitory computer readable medium comprising executable instructions which, when executed by a processor, cause the processor to:
provide heating, cooling, or a combination thereof, to a turbomachinery via a first heat transfer conduit and a second heat transfer conduit included in a thermal delivery system, wherein the second heat transfer conduit is disposed on the turbomachinery adjacent to the first heat transfer conduit, and wherein a section of the first heat transfer conduit comprises an insulating wrap that only encloses the section of the first heat transfer conduit and a heat sensor and that is in direct contact with the heat sensor and the section of the first heat transfer conduit; and
control the heating, the cooling, or the combination thereof, of the turbomachinery, via a controller operatively coupled to the thermal delivery system, to minimize or to eliminate positional changes, structural changes, or a combination thereof, in one or more components of the turbomachinery due to thermal energy, wherein the controller uses at least readings from the heat sensor to control the heating, the cooling, or the combination thereof.

15. The computer readable medium of claim 14 , wherein the first heat transfer conduit and the second heat transfer conduit provide for a lateral symmetry for heating, for cooling, or a combination thereof, of a casing of the turbomachinery.

16. The computer readable medium of claim 14 , wherein the controller is configured to control the second heat transfer conduit when the temperature sensor detects that the first heat transfer conduit is inoperative.

17. The computer readable medium of claim 16 , wherein the controller is configured to use zone control to control the second heat transfer conduit when the temperature sensor detects that the first heat transfer conduit is inoperative.

Assignees

• Gen Electric

Inventors

• Black Kenneth D
• Johnson David M
• Klinger Brett Darrick
• Gilchrist George Martin

Classifications

• F01D21/003

  Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title

• F02C7/12 Primary

  Cooling of plants (of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P) · CPC title

• F01D25/14

  Casings modified therefor (double casings F01D25/26) · CPC title

• F05D2260/84

  Redundancy · CPC title

• F01D25/26

  Double casings; Measures against temperature strain in casings · CPC title