Gas turbine engine heat exchanger system

Patent metadata

Field	Value
Publication number	US-9915202-B2
Application number	US-201314104299-A
Country	US
Kind code	B2
Filing date	Dec 12, 2013
Priority date	Mar 5, 2013
Publication date	Mar 13, 2018
Grant date	Mar 13, 2018

Abstract

An apparatus includes a gas turbine engine and a heat transfer system. The gas turbine engine includes an inlet particle separator that separates inlet air into scavenge air and clean air. A scavenge air path conveys the scavenge air from the inlet particle separator to the heat transfer system. A heat exchange fluid path conveys a heat exchange fluid to the heat transfer system and a cooled heat exchange fluid away from the heat transfer system. The heat transfer system is configured to transfer heat from the heat exchange fluid path to the scavenge air path to cool the heat exchange fluid.

First claim

What is claimed is:

1. An apparatus comprising:
a gas turbine engine including an inlet particle separator that separates inlet air into scavenge air and clean air, the clean air passing into the gas turbine engine;
a heat transfer system;
a scavenge air path that conveys all the scavenge air from the inlet particle separator to the heat transfer system;
a heat exchange fluid path that conveys a heat exchange fluid to the heat transfer system and away from the heat transfer system, wherein the heat transfer system transfers heat from the heat exchange fluid path to the scavenge air path to cool the heat exchange fluid;
a flow control mechanism positioned between the heat transfer system and the inlet particle separator such that all of the scavenge air passes through the flow control mechanism; and
a blower positioned downstream from the heat transfer system such that the scavenge air that passes through the heat transfer system also passes through the blower;
wherein the flow control mechanism controls a flow of the scavenge air to modulate a temperature of the heat exchange fluid; and
wherein the flow control mechanism is a pump.

2. The apparatus of claim 1 , further comprising a source component from which the heat exchange fluid path conveys the heat exchange fluid to the heat transfer system, in which the source component comprises a turbomachinery component of the gas turbine engine.

3. The apparatus of claim 1 , further comprising a component to be cooled to which the heat exchange fluid path conveys the cooled heat exchange fluid from the heat transfer system.

4. The apparatus of claim 3 , in which the component to be cooled further comprises a turbomachinery component of the gas turbine engine.

5. The apparatus of claim 1 , wherein the blower draws the scavenge air through the flow control mechanism to the heat transfer system.

6. The apparatus of claim 1 , wherein the blower draws the scavenge air at a rate that is dependent on operating conditions of the gas turbine engine.

7. An apparatus comprising:
a gas turbine engine having a compressor and a turbine, the gas turbine engine including an engine inlet particle separator that separates inlet air into debris air and clean air, the clean air passing through the gas turbine engine;
a debris air path that conveys the debris air;
a cooling air path that conveys a cooling air;
a thermal transfer system that transfers heat from the cooling air path to the debris air path to cool the cooling air, wherein the cooling air path passes from the compressor to the thermal transfer system and then to the turbine;
a flow control mechanism passing all of the debris air therethrough to the thermal transfer system; and
a blower positioned downstream from the thermal transfer system such that all the debris air that passes through the thermal transfer system also passes through the blower;
wherein the flow control mechanism controls an amount of flow of scavenge air to modulate a temperature of the cooling air; and
wherein the flow control mechanism is a pump.

8. The apparatus of claim 7 , in which the debris air path extends from the thermal transfer system to the blower.

9. The apparatus of claim 7 , in which the cooling air path is configured to convey the cooling air from a first component of the gas turbine engine to the thermal transfer system and from the thermal transfer system to a second component of the gas turbine engine to cool the second component.

10. The apparatus of claim 9 , in which the first component is the compressor and the second component is the turbine.

11. The apparatus of claim 7 , in which the blower is a pump that draws the debris air through the debris air path and to the thermal transfer system.

12. The apparatus as claimed in claim 7 , in which the blower is a fan for drawing the debris air from the inlet particle separator to the thermal transfer system.

13. The apparatus of claim 7 , wherein the blower draws the debris air at a rate that is dependent on operating conditions of the gas turbine engine.

14. A method of operating a gas turbine engine comprising:
using an inlet particle separator of the gas turbine engine to separate inlet air into scavenge air and clean air;
conveying all the scavenge air through a scavenge air channel from the inlet particle separator to a heat transfer system;
conveying a cooling air through a cooling air channel that passes from the gas turbine engine to the heat transfer system;
transferring heat, in the heat transfer system, from the cooling air channel to the scavenge air channel to cool the cooling air and then conveying the cooling air away from the heat transfer system to the gas turbine engine;
drawing all the scavenge air that passes through the heat transfer system using a blower that is positioned downstream of the heat transfer system;
modulating a temperature of the cooling air by controlling a rate of flow of the scavenge air with a flow control mechanism; and
drawing the scavenge air, using the blower, at a rate that is dependent on operating conditions of the gas turbine engine.

15. The method of claim 14 , in which the flow control mechanism is a pump.

16. The method of claim 14 , in which the flow control mechanism is a valve.

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Donovan Eric S
• Vonderwell Daniel J
• Heathco Craig

Classifications

• F05D2260/205

  Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes · CPC title

• F02C7/052 Primary

  with dust-separation devices · CPC title

• F02C7/12

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

• F05D2260/213

  by the provision of a heat exchanger within the cooling circuit · CPC title

• F02C7/05 Primary

  having provisions for obviating the penetration of damaging objects or particles · CPC title