Compound clearance control engine

Details Compound clearance control engine Compound clearance control engine

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/14 (2006.01) F01D 11/24 (2006.01)

Patent

CA 2609279

A gas turbine engine (10) includes a compressor (18), combustor (20), and turbine (22) having a row of blades (40) mounted inside a surrounding turbine shroud (44). A heat exchanger (56) is used for cooling pressurized air bled from the compressor (18). A distribution network (60-66) joins the heat exchanger (56) to the turbine (22) for selectively channeling air from the heat exchanger (56) below the blades (40) and above the shroud (44) for controlling blade tip clearance.

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