Gas turbine engine
A heat exchanger arrangement for a gas turbine engine. The arrangement including a flow path within an outer cowl, which flow path locates a heat exchanger part way therealong. A valve is provided at an inlet end of the flow path to selectively receive fluid into the flow path from outside of the cowl and/or from a pressurized fluid flow. An exit from the flow path includes a plenum chamber to receive exhausted coolant flows from the heat exchanger and possibly other exhaust flows. The heat exchanger exhaust flow is then utilized to provide cooling to engine structures.
1. A gas turbine engine comprising a compressor driven by a turbine, with a combustor located between the compressor and the turbine, a main propulsive rotor is provided downstream of the combustor which rotor is driven by a second turbine,
the engine also comprising a heat exchanger arrangement,
the heat exchanger arrangement comprising a flow path within an outer cowl,
a heat exchanger at an intermediate position along the flow path between an inlet and an outlet,
the flow path arranged about a pressurized fluid flow through the engine,
the inlet has a valve selectively movable between a first position to receive into the flow path fluid from outside of the engine, and a second position to receive into the flow path fluid from the pressurized fluid flow, and that the outlet has a plenum chamber associated with the pressurized fluid flow.
2. An engine as claimed in claim 1 wherein the plenum chamber is also associated with an exhaust path from the cowl.
3. An engine as claimed in claim 2 wherein the exhaust path provides a thermal shield between the cowl and the pressurized fluid flow.
4. An engine as claimed in claim 1 wherein the plenum chamber is also associated with an exhaust path to provide cooling to the engine structure.
5. An engine as claimed in claim 1 wherein the heat exchanger is for air cooling of lubricating oil.
6. An engine as claimed in claim 1 wherein the valve is a flap valve.
7. An engine as claimed in claim 1 wherein a controller is provided for moving the valve between the first and second positions.
8. An engine as claimed in claim 7 wherein a sensor to determine external fluid flow past the cowl is provided operatively connected to the controller, and configured such that if external fluid flow above a predetermined value is sensed the valve will be in a first position, but otherwise the valve will be in the second position.
9. An engine as claimed in 7 wherein the valve can be selectively configured to receive into the flow path fluid from both outside of the cowl and from the pressurized fluid flow.
10. An engine as claimed in claim 1 wherein the plenum chamber is associated with the pressurized fluid flow to draw fluid flow along the flow path.
11. An engine as claimed in claim 1 wherein the flow path is provided by distinct ducting.
12. An engine as claimed in claim 11 wherein the ducting is integral with the cowl.
13. An engine as claimed in claim 11 wherein the ducting is provided in cowl doors.
14. An engine as claimed in claim 11 wherein the ducting acts to reinforce the cowl.
15. An engine as claimed in claim 11 wherein the ducting is hinged with the cowl doors.
16. An engine as claimed in claim 1 wherein an exhaust duct from the heat exchanger is arranged to be in contact with an external surface of the cowl to provide cooling in use of the heat exchanger exhaust.
17. An engine as claimed in claim 1 wherein the plenum chamber is arranged to receive other fluid flows through the engine.
18. An engine as claimed in claim 1 wherein an opening is provided in an external surface of the outer cowl, leading to the valve, to receive into the flow path fluid from outside of the engine.
19. An engine as claimed in claim 1 wherein an opening is provided in the air intake of the engine upstream of the compressor, leading to the valve, to receive into the flow path fluid from outside of the engine.