HEAT TRANSFER SYSTEM Russian patent published in 2012 - IPC F02C7/47 

Abstract RU 2447300 C2

FIELD: engines and pumps.

SUBSTANCE: heat transfer system for gas turbine engine comprising annulus casing to accommodate several post elements extending, in fact, radially, includes, at least, one arc-shaped heat tube. Heat tube stay in contact with housing outer surface and communicates with heat source to allow heat to be transferred via heat tube and housing to post elements.

EFFECT: simplified system ruling out fire inside engine.

10 cl, 4 dwg

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RU 2 447 300 C2

Authors

Venkataramani Kattalajkheri Srinivasan

Moniz Tomas Ori

Stefenson Dzhastin P.

Dates

2012-04-10Published

2007-07-27Filed