ROTARY ASSEMBLY OF GAS TURBINE FAN, GAS TURBINE ENGINE, FAN WITH SAID ASSEMBLY AND GAS TURBINE ENGINE

FIELD: engines and pumps. ^ SUBSTANCE: proposed fan 12 comprises disc 18 revolving about axis A, multiple vanes 20 with their feet secured thereto and directed radially outward, and multiple sites 30 between said vanes to restrict fluid flow channel section inner profile. Said adjacent vanes 20 have...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: RUSSELEHN STEFAN, BRO MISHEL
Format: Patent
Sprache:eng ; rus
Schlagworte:
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