Heat exchange arrangement

Patent metadata

Field	Value
Publication number	US-9624832-B2
Application number	US-201414229137-A
Country	US
Kind code	B2
Filing date	Mar 28, 2014
Priority date	May 16, 2013
Publication date	Apr 18, 2017
Grant date	Apr 18, 2017

Abstract

A heat exchange arrangement for a gas turbine engine. The arrangement includes a first conduit for an engine component cooling fluid and a second conduit for a second fluid. The arrangement further includes a heat exchange portion in which fluids flowing through the first and second conduits are in a heat exchange relationship. A valve is provided, which is configured to moderate the mass flow rate of one of the fluids through the heat exchange portion. The arrangement includes divert valve in the first conduit which diverts flow to the second conduit as the flow in the second conduit is moderated to reduce thermal shock in the heat exchange portion.

First claim

The invention claimed is:

1. A heat exchange arrangement for a gas turbine engine, the heat exchange arrangement comprising:
a first conduit for an engine component cooling fluid and a second conduit for a second fluid;
a heat exchange portion in which fluids flowing through the first and second conduits are in a heat exchange relationship;
a valve configured to moderate a mass flow rate of the fluid in the second conduit through the heat exchange portion; and
a divertor valve configured to divert fluid from the first conduit into a portion of the second conduit that is upstream of the heat exchange portion.

2. A heat exchange arrangement according to claim 1 , wherein the divertor valve is located downstream of the heat exchange portion.

3. A heat exchange arrangement according to claim 1 , further comprising a controller configured to actuate the valve when a rate of change of temperature with respect to time of the component cooling fluid sensed by a temperature sensor is above a predetermined value.

4. A heat exchange arrangement according to claim 1 , further comprising a controller configured to control the divertor valve in response to a signal to moderate the mass flow rate of the fluid in the second conduit.

5. A heat exchange arrangement according to claim 4 , wherein the divertor valve is a butterfly valve.

6. A heat exchange arrangement according to claim 1 , wherein the second fluid comprises air.

7. A heat exchange arrangement according to claim 6 , wherein the second fluid conduit is located within a bypass duct of the gas turbine engine.

8. A gas turbine engine comprising a heat exchange arrangement according to claim 1 .

9. A method of controlling a heat exchange arrangement according to claim 1 , the method comprising diverting fluid from the first conduit into the second conduit upstream of the heat exchange portion.

10. A method according to claim 9 , wherein fluid is diverted from the first conduit into the second conduit whilst the flow in the second conduit is modulated.

11. A method according to claim 10 , wherein the flow is diverted for a predetermined period to reduce thermal shock in the heat exchange portion.

12. A method according to claim 9 , wherein the fluid is diverted from the first conduit into the second conduit before the flow in the second conduit is modulated.

13. A method according to claim 12 , wherein the flow is diverted for a predetermined period to reduce thermal shock in the heat exchange portion.

Assignees

• Rolls Royce Plc

Inventors

• Fletcher Paul

Classifications

• F02C7/141 Primary

  of working fluid · CPC title

• F05D2260/213

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

• F02K3/115

  by means of indirect heat exchange · CPC title

• Y02T50/676

  Cross-Sectional Technologies · mapped topic

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title