High speed propulsion system with inlet cooling

Patent metadata

Field	Value
Publication number	US-10590849-B2
Application number	US-201514663871-A
Country	US
Kind code	B2
Filing date	Mar 20, 2015
Priority date	Mar 27, 2014
Publication date	Mar 17, 2020
Grant date	Mar 17, 2020

Abstract

A cooling system for a turbine engine including a heat exchanger in fluid communication with a first fluid inlet stream and disposed upstream and in fluid communication with a core engine. The heat exchanger operative to cool the first fluid inlet stream. The heat exchanger including a heat exchanger inlet for input of a heat exchanging medium for exchange of heat from the first fluid inlet stream to the heat exchanging medium. The heat exchanger further including a heat exchanger outlet for discharge of a heated output stream into one of a turbine of a downstream engine, an augmentor or a combustor of the core engine. The heated output stream provides an additional flow to the downstream engine. A turbine engine including the cooling system is disclosed.

First claim

The invention claimed is:

1. A turbine engine including a cooling system, the turbine engine comprising:
a core engine comprising an intake side and an exhaust side, the core engine configured to receive a first fluid stream and discharge a primary exhaust flow stream, the core engine comprising a compressor, a combustor, and a turbine;
a bypass flow turbomachine comprising a plurality of rotor blades, an inboard portion of the plurality of rotor blades defining a bypass flow turbomachine compressor disposed to receive a second fluid stream and an outboard portion of the plurality of rotor blades defining a plurality of turbine stages disposed to receive the primary exhaust flow stream from the core engine and discharge a secondary exhaust flow stream, the bypass flow turbomachine including an augmentor; and
an inlet heat exchanger in fluid communication with the first fluid stream and disposed upstream and in fluid communication with the core engine, the inlet heat exchanger operative to cool the first fluid stream, the inlet heat exchanger comprising:
a heat exchanger inlet for input of a heat exchanging medium for exchange of heat from the first fluid stream to the heat exchanging medium; and
a heat exchanger outlet for discharge of a heated output stream, wherein the heated output stream comprises steam, and wherein the steam bypasses the compressor, the combustor, and the turbine of the core engine and provides an additional flow into the bypass flow turbomachine.

2. The turbine engine of claim 1 , wherein the heat exchanging medium is comprised of at least one of water or of water and fuel.

3. The turbine engine of claim 2 , wherein the fuel is at least one of a liquid natural gas and a thermally stabilized liquid fuel.

4. The turbine engine of claim 2 , wherein at least a portion of the heated output stream is output to at least one of the plurality of turbine stages of the bypass flow turbomachine, an injector of the augmentor and the combustor of the core engine.

5. The turbine engine of claim 1 , wherein the steam from the heat exchanger outlet of the inlet heat exchanger merges with the primary exhaust flow stream from the core engine at a location downstream of the turbine of the core engine.

6. A cooling system for a turbine engine, the turbine engine comprising a core engine and a bypass flow turbomachine, the core engine having a compressor, a combustor, and a turbine and the bypass flow turbomachine having a plurality of rotor blades, the plurality of rotor blades having an inboard portion defining a bypass flow turbomachine compressor and an outboard portion defining a bypass flow turbomachine turbine, the cooling system comprising:
a heat exchanger in fluid communication with a first fluid inlet stream and disposed upstream and in fluid communication with the core engine, the heat exchanger operative to cool the first fluid inlet stream, the heat exchanger comprising:
a heat exchanger inlet for input of a heat exchanging medium for exchange of heat from the first fluid inlet stream to the heat exchanging medium; and
a heat exchanger outlet for discharge of a heated output stream onto an the outboard portion of the plurality of rotor blades of the bypass flow turbomachine, wherein the heated output stream comprises steam, the plurality of rotor blades defining a plurality of turbine stages of the bypass flow turbomachine turbine, whereby the steam bypasses the compressor, the combustor, and the turbine of the core engine and provides an additional flow to the bypass flow turbomachine.

7. The cooling system of claim 6 , wherein the heat exchanging medium is comprised of at least one of water or of water and fuel.

8. A turbine engine including a cooling system, the turbine engine comprising:
a core engine comprising an intake side and an exhaust side, the core engine configured to receive a first fluid stream and discharge a primary exhaust flow stream, the core engine comprising a compressor, a combustor, and a turbine;
a bypass flow turbomachine comprising a plurality of rotor blades, an inboard portion of the plurality of rotor blades defining a bypass flow turbomachine compressor disposed to receive a second fluid stream and an outboard portion of the plurality of rotor blades defining a plurality of turbine stages disposed to receive the primary exhaust flow stream from the core engine and discharge a secondary exhaust flow stream, the bypass flow turbomachine including an augmentor; and
an inlet heat exchanger in fluid communication with the first fluid stream and disposed upstream and in fluid communication with the core engine, the inlet heat exchanger operative to cool the first fluid stream, the inlet heat exchanger comprising:
a heat exchanger inlet for input of a heat exchanging medium for exchange of heat from the first fluid stream to the heat exchanging medium; and
a heat exchanger outlet for discharge of a heated output stream, wherein at least a portion of the heated output stream bypasses the compressor, the combustor, and the turbine of the core engine and is output to at least one of the plurality of turbine stages of the bypass flow turbomachine or an injector of the augmentor.

9. The turbine engine of claim 8 , wherein the heat exchanging medium is at least one of water or water and fuel, wherein the heated output stream comprises steam.

10. The turbine engine of claim 8 , wherein the portion of the heated output stream from the heat exchanger outlet of the inlet heat exchanger merges with the primary exhaust flow stream from the core engine at a location downstream of the turbine of the core engine.

Assignees

• Gen Electric

Inventors

• Kenyon Ross Hartley
• Joshi Narendra Digamber

Classifications

• F02C7/14 Primary

  of fluids in the plant {, e.g. lubricant or fuel (F02C7/185 takes precedence)} · CPC title

• F02C9/18

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title

• F05D2260/213

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

• F05D2220/323

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

• F01D13/003

  with at least two independent shafts, i.e. cross-compound · CPC title