Heat transfer system for turbine engine using heat pipes

• US 8,015,788 B2
• Filed: 12/27/2006
• Issued: 09/13/2011
• Est. Priority Date: 12/27/2006
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Stephenson, Justin P., Moniz, Thomas Ory, Venkataramani, Kattalaicheri Srinivasan
• Primary Examiner(s): Look; Edward
• Assistant Examiner(s): Ellis; Ryan H
• Application Number:
  US11/616,555
• Publication Number:
  US 20080159852A1
• Time in Patent Office: 1,721 Days
• Field of Search: 60/390.93, 415/108, 415/114, 415/175, 415/176, 415/177, 415/178
• US Class Current: 60/39.093
• CPC Class Codes: F01D 25/02 De-icing means for engines having icing phenomena
• CPC Class Codes: F01D 25/08 Cooling of machines or engines in general F01P; Heating; Heat-insulation of blade-carrying members, of blades F01D5/00
• CPC Class Codes: F01D 25/10 Heating, e.g. warming-up before starting
• CPC Class Codes: F01D 5/046 Heating, heat insulation or cooling means
• CPC Class Codes: F01D 5/08 Heating, heat-insulating or cooling means specially adapted for radial flow machines or engines F01D5/04
• CPC Class Codes: F02C 7/047 Heating to prevent icing
• CPC Class Codes: F05D 2260/208 using heat pipes
• CPC Class Codes: F28D 15/0275 Arrangements for coupling heat-pipes together or with other structures, e.g. with base blocks; Heat pipe cores
• CPC Class Codes: F28F 2265/30 for preventing vibrations
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A heat transfer system is provided for a turbine engine of the type including an annular inlet cowling. The heat transfer system includes at least one heat pipe disposed in contact with an interior of the casing. The heat pipe is thermally coupled to a heat source, such that heat from the heat source can be transferred through the heat pipe and into the inlet cowling.

Claims

1. A heat transfer system for a turbine engine including an annular cowling structure with a nose portion having an arcuate cross-section, the heat transfer system comprising:

a plurality of heat pipes circumferentially mounted in a spaced-apart relation around an inner surface of the cowling structure, each of the plurality of heat pipes including an aft section, a forward section, and a transition section therebetween, wherein the aft and transition sections are wrapped in thermal insulation and the forward section is uninsulated, wherein forward sections of each of the plurality of heat pipes are arranged within and thermally coupled to the cowling structure in a circumferential array, and wherein the forward section of each heat pipe is mounted to the inner surface of the cowling structure by way of a mounting structure including a damping element;

wherein the plurality of heat pipes are thermally coupled to a heat source, such that heat from the heat source can be transferred through the heat pipes to the cowling structure.

2. The heat transfer system of claim 1 wherein the cowling structure includes:

an annular casing; and

a splitter lip having an arcuate cross-sectional shape disposed at a forward end of the casing so as to define a splitter nose in cooperation with the casing.

3. The heat transfer system of claim 2 wherein the mounting structure includes at least one bracket attached to the casing and securing the heat pipe against an inner surface of the splitter nose, the bracket carrying the damping element in contact with the heat pipe.

4. The heat transfer system of claim 1 further including a thermally conductive paste disposed between the heat pipe and the inner surface of the cowling structure.

5. The heat transfer system of claim 1 wherein the forward and aft sections of each of the plurality of heat pipes are generally circumferentially extending relative to the annular cowling structure, and the transition sections of each of the plurality of heat pipes are generally axially extending relative to the annular cowling structure.

6. The heat transfer system of claim 1 wherein the plurality of heat pipes are disposed in contact with the interior of the cowling, and each of the heat pipes are thermally coupled to the heat source.

7. The heat transfer system of claim 1 wherein each of the plurality of heat pipes includes:

a first end connected to the heat source;

an uninsulated portion disposed at a distal end of the heat pipe; and

an insulated portion disposed between the first end and the uninsulated portion.

8. The heat transfer system of claim 1 wherein each of the plurality of heat pipes includes an elongated outer wall with closed ends cooperatively defining a cavity that contains a working fluid.

9. The heat transfer system of claim 1 wherein the heat transfer system facilitates at least one of preventing ice formation on the cowling and removing ice which has formed on the cowling.

10. The heat transfer system of claim 1 wherein the heat source is engine oil from the turbine engine.

11. The heat transfer system of claim 1 wherein each of the plurality of heat pipes has a non-circular cross-sectional shape.

12. A gas turbine engine including:

an annular cowling structure with a nose portion having an arcuate cross-section;

a plurality of heat pipes circumferentially mounted in a spaced-apart relation around an inner surface of the cowling structure, each of the plurality of heat pipes including an aft section, a forward section, and a transition section therebetween, wherein the aft and transition sections are wrapped in thermal insulation and the forward section is uninsulated, wherein forward sections of each of the plurality of heat pipes are arranged within and thermally coupled to the cowling structure in a circumferential array, and wherein the forward section of each heat pipe is mounted to the inner surface of the cowling structure by way of a mounting structure including a damping element; and

a heat source thermally coupled to the heat pipes such that heat from the heat source can be transferred through the heat pipes to the cowling structure.

13. The heat transfer system of claim 12 wherein the cowling structure includes:

an annular casing; and

a splitter lip having an arcuate cross-sectional shape disposed at a forward end of the casing so as to define a splitter nose in cooperation with the casing.

14. The heat transfer system of claim 13 wherein the mounting structure includes at least one bracket attached to the casing and securing the heat pipe against an inner surface of the splitter nose, the bracket carrying the damping element in contact with the heat pipe.

15. The heat transfer system of claim 12 further including a thermally conductive paste disposed between the heat pipes and the inner surface of the cowling structure.

16. The heat transfer system of claim 12 wherein the forward and aft sections of each of the plurality of heat pipes are generally circumferentially extending relative to the annular cowling structure, and the transition sections of each of the plurality of heat pipes are generally axially extending relative to the annular cowling structure.

17. The heat transfer system of claim 12 wherein each heat pipe includes:

a first end connected to the heat source;

an uninsulated portion disposed at a distal end of the heat pipe; and

an insulated portion disposed between the first end and the uninsulated portion.

18. The gas turbine engine of claim 12 wherein each heat pipe includes an elongated outer wall with closed ends cooperatively defining a cavity that contains a working fluid.

19. The gas turbine engine of claim 12 wherein the heat pipes facilitate at least one of preventing ice formation on the cowling structure and removing ice which has formed on the cowling structure.