F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
60/185
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.
507081
Grigo Dietrich
Hennecke Dietmar
Pfaff Klaus
Grigo Dietrich
Hennecke Dietmar
Marks & Clerk
Mtu Motoren Und Turbinen-Union Munchen Gmbh
Pfaff Klaus
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