Gas turbine engine in-board cooled cooling air system
A system for supplying turbine cooling air flow includes a turbofan engine, a heat exchanger, and a door. The turbofan engine includes an engine case that has an inner volume within which at least a gas turbine engine is mounted, and a bypass flow passage that is defined by an outer fan duct and an inner fan duct and that is configured to direct fan air flow therethrough. The heat exchanger is disposed within the turbofan engine, is coupled to receive fluid and cooling air from the bypass flow passage, and is configured to transfer heat between fluid and the cooling air. The door is movably mounted in the turbofan engine and is movable between a closed position, in which the cooling air will not flow through the heat exchanger, and an open position, in which the cooling air may flow through the heat exchanger.
1. A system for supplying turbine cooling air flow, comprising:
a turbofan engine including an engine case and a bypass flow passage, the engine case having an inner volume within which at least a gas turbine engine is mounted, the bypass flow passage defined by an outer fan duct and an inner fan duct and configured to direct fan air flow therethrough;
a plurality of heat exchangers disposed within the turbofan engine, each heat exchanger including a heat exchanger first flow passage and a heat exchanger second flow passage, each heat exchanger first flow passage coupled to receive engine air from within the engine case, each heat exchanger second flow passage coupled to selectively receive fan air from the bypass flow passage, each heat exchanger configured to transfer heat between the engine air and the fan air;
a plurality of doors, each door associated with one of the heat exchangers and movably mounted on the inner fan duct, each door independently movable between a closed position, in which fan air will not flow into its associated heat exchanger second flow passage, and an open position, in which fan air will flow into its associated heat exchanger second flow passage; and
a plurality of door actuators, each door actuator coupled to a different one of the doors and configured to independently move the door to which it is coupled between the closed and open positions.
2. The system of claim 1 , wherein each door actuator comprises a passive actuator.
3. The system of claim 1 , wherein each door actuator is responsive to power from a power source to move between the open and closed positions.
4. The system of claim 1 , wherein:
each heat exchanger is disposed within the inner fan duct and is shaped to conform to at least a portion of the inner fan duct; and
the heat exchangers are coupled together to form an annular ring.