Methods and apparatus for cooling gas turbine engines

Details Methods and apparatus for cooling gas turbine engines Methods and apparatus for cooling gas turbine engines

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/12 (2006.01) F02C 7/12 (2006.01)

Patent

CA 2522950

A method for assembling a gas turbine engine assembly (10) that includes mounting a gas turbine engine including an inlet (22) and an exhaust (24) within a module (60) that includes an inlet area (62), an exhaust area (64), and an engine area (66) extending therebetween, such that the gas turbine engine is housed within the module, coupling a first deflector (110) within the module engine area such that when cooling air (160) is channeled past the deflector, the deflector induces a substantially helically-shaped cooling air flowpath (162) around a periphery (164) of the gas turbine engine, and coupling an exhaust duct (82) to an outlet of the module exhaust area.

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