F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/14 (2006.01) F01M 5/00 (2006.01) F01P 11/08 (2006.01) F01P 11/10 (2006.01) F02C 7/06 (2006.01)
Patent
CA 2675400
A heat exchanger system for a gas turbine engine includes: (a) a fan (112) having at least two stages of rotating fan blades surrounded by a fan casing, the fan (112) operable to produce a flow of pressurized air at a fan exit; (b) at least one heat exchanger (116) having a first flowpath in fluid communication with the fan (112) at a location upstream of the fan exit; and (c) a fluid system coupled to a second flowpath of the at least one heat exchanger (116). The first and second flowpaths are thermally coupled to each other.
Company General Electric
Craig Wilson And Company
LandOfFree
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