Reversible system for dissipating thermal power generated in a gas-turbine engine

Patent metadata

Field	Value
Publication number	US-10794231-B2
Application number	US-201716302184-A
Country	US
Kind code	B2
Filing date	May 19, 2017
Priority date	May 20, 2016
Publication date	Oct 6, 2020
Grant date	Oct 6, 2020

Abstract

A reversible system for dissipating heat power generated in a gas turbine engine, the system including a condenser-forming first heat exchanger, an evaporator-forming second heat exchanger, a scroll compressor suitable for operating as a compressor when the temperature of the cold source is higher than a predefined threshold temperature and as a turbine when the temperature of the cold source is lower than the threshold temperature, an expander and a pump arranged in parallel, and a control valve arranged upstream from the expander and the pump and suitable for directing the refrigerant fluid to the expander when the temperature of the cold source is higher than the threshold temperature and to the pump when the temperature of the cold source is lower than the threshold temperature.

First claim

The invention claimed is:

1. A reversible system for dissipating heat power generated in a gas turbine engine, the system comprising:
a condenser-forming first heat exchanger for exchanging heat between a refrigerant fluid and a cold source;
an evaporator-forming second heat exchanger for exchanging heat between the refrigerant fluid and a hot source generating heat power;
a scroll compressor arranged upstream from the first heat exchanger and downstream from the second heat exchanger; the scroll compressor for operating as a compressor when a temperature of the cold source is higher than a predefined threshold temperature and as a turbine when the temperature of the cold source is lower than the predefined threshold temperature;
an expander and a pump arranged in parallel downstream from the first heat exchanger and upstream from the second heat exchanger; and
a control valve arranged upstream from the expander and the pump for directing the refrigerant fluid to the expander when the temperature of the cold source is higher than the threshold temperature and to the pump when the temperature of the cold source is lower than the threshold temperature.

2. The system according to claim 1 , wherein the hot source generating heat power is an oil of an oil circuit of the gas turbine engine and the cold source is air coming from a flow passage for a secondary stream through the gas turbine engine.

3. The system according to claim 2 , wherein the first heat exchanger is for positioning in the flow passage for the secondary stream through the gas turbine engine.

4. The system according to claim 2 , wherein the second heat exchanger, the scroll compressor, the expander, and the pump are positioned in a nacelle gas turbine of the engine.

5. A gas turbine engine including an oil circuit and a reversible system, the reversible system comprising:
a condenser-forming first heat exchanger for exchanging heat between a refrigerant fluid and a cold source;
an evaporator-forming second heat exchanger for exchanging heat between the refrigerant fluid and a hot source generating heat power;
a scroll compressor arranged upstream from the first heat exchanger and downstream from the second heat exchanger; the scroll compressor for operating as a compressor when a temperature of the cold source is higher than a predefined threshold temperature and as a turbine when the temperature of the cold source is lower than the predefined threshold temperature;
an expander and a pump arranged in parallel downstream from the first heat exchanger and upstream from the second heat exchanger; and
a control valve arranged upstream from the expander and the pump for directing the refrigerant fluid to the expander when the temperature of the cold source is higher than the threshold temperature and to the pump when the temperature of the cold source is lower than the threshold temperature, and
wherein the reversible system dissipates heat power generated by an oil of the oil circuit.

6. A method of operating a reversible system according to claim 1 , wherein:
the control valve is activated to direct all of the refrigerant fluid that has passed through the first heat exchanger to the expander when the temperature of the cold source is higher than the predefined threshold temperature, the scroll compressor then acting as a compressor; and
the control valve is activated to direct all of the refrigerant fluid that has passed through the first heat exchanger to the pump when the temperature of the cold source is lower than the predefined threshold temperature, the scroll compressor then operating as a turbine.

Assignees

• Safran

Inventors

• Maalouf Samer

Classifications

• F02C1/10

  Closed cycles · CPC title

• F02C7/16

  characterised by cooling medium · CPC title

• F01K25/02 Primary

  the fluid remaining in the liquid phase · CPC title

• F02C7/18

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• F02C7/14 Primary

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