Gas turbine drive with devices for branching off compressor...

F - Mech Eng,Light,Heat,Weapons – 02 – C

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F02C 7/12 (2006.01) F02C 7/18 (2006.01)

Patent

CA 1276474

Abstract In a gas-turbine engine with devices to branch-off compressor air to cool hot components of the turbine, the cooling air is passed along a detour path through components having greater thermal capacity and larger surface areas, to the hot components that are to be cooled. By this means, when there is an abrupt change in the temperature of the cooling air as, for instance, during the acceleration phase, the cooling air gives up some of its heat content on the detour path on the components, so that the thermal time behaviour of the cooling air is retarded.

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