HAS TURBINE ENGINE COOLING DEVICE Russian patent published in 2012 - IPC F02C7/18 

Abstract RU 2460893 C1

FIELD: machine building.

SUBSTANCE: proposed device comprises noise-and-heat protection casing to make together with engine housing an annular chamber, set of fans communicated with annular manifold with orifices directed toward gas turbine unit engine cooled surface. Annular manifold orifices are directed so that their axes extend parallel with engine lengthwise axis. Annular waste (hot) air receiver is arranged behind engine cooled surface to communicate with ambient air.

EFFECT: higher efficiency of cooling and engine reliability.

3 dwg

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RU 2 460 893 C1

Authors

Kustov Jurij Ivanovich

Makarevich Jurij Leonidovich

Zaritskij Vladimir Ignat'Evich

Dates

2012-09-10Published

2010-12-20Filed