Simplified support device for nozzles of a gas turbine stage

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

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F02C 7/00 (2006.01) F01D 11/00 (2006.01) F16J 15/44 (2006.01)

Patent

CA 2430444

A simplified support device (110) for nozzles (112) of a gas turbine stage, of the type in which the support device (110) is interposed in a rotor of the gas turbine, between an upstream blading disc (122) and a downstream blading disc (124) of the nozzles (112), and is provided with honeycomb-type alveolar seals (120); the nozzles (112) of the gas turbine stage comprise an annular body which is divided into nozzle segments (112) and the honeycomb-type alveolar seals (120) are anchored directly to these nozzle segments (112).

Support simplifié (110) de distributeurs (112) d'étage de turbine à gaz, ledit support (110) étant interposé dans un rotor de la turbine de gaz, entre un disque d'aube amont (122) et un disque d'aube aval (124) des distributeurs (112), et doté de joints d'étanchéité de type alvéolaire (120); les distributeurs (112) d'étage de la turbineà gaz comportent un corps annulaire qui est divisé en segments (112), et les joints d'étanchéité de type alvéolaire (120) sont fixés directement à ces segments (112).

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