GAS TURBINE ROTOR COOLING DEVICE

FIELD: machine building. ^ SUBSTANCE: gas turbine rotor cooling device includes pneumatic drives, cooler, cooled rotating blades with independent cooling systems of entry edge and feather of blade, which are connected to channels in the shank, annular swirling pneumatic device, labyrinth seals and a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ROGALEV NIKOLAJ DMITRIEVICH, ZARJANKIN ARKADIJ EFIMOVICH, BELJAEV VJACHESLAV EVGEN'EVICH, KOSOJ ALEKSANDR SEMENOVICH
Format: Patent
Sprache:eng ; rus
Schlagworte:
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