Gas turbine engine airfoil integrated heat exchanger

Details Gas turbine engine airfoil integrated heat exchanger Gas turbine engine airfoil integrated heat exchanger

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/14 (2006.01) F01D 9/02 (2006.01) F01D 25/12 (2006.01) F16N 39/02 (2006.01) F28D 1/02 (2006.01)

Patent

CA 2737338

A heat exchanger apparatus includes: (a) an airfoil (42) having opposed pressure and suction sides (54, 52), a root (50), a tip (48), and spaced-apart leading and trailing edges (44, 46); and (b) a plenum (62, 162, 262) integrally formed within the airfoil (42) which is configured to receive a flow of circulating working fluid; and (c) inlet and outlet ports (72, 74) communicating with the plenum (62, 162, 262) and an exterior of the airfoil (42).

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