TURBOJET NACELLE EQUIPPED WITH NACELLE COMPONENT COOLING ASSY Russian patent published in 2015 - IPC B64D29/00

Abstract RU 2552574 C2

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering, particularly, to turbojet nacelles. Turbojet nacelle comprises component to be cooled and component cooling assy. Cooling assy comprises at least one composite wall separating cold zone from hot zone. Said composite wall comprises heat emitting component. Cooling assy comprises at least one hole made in composite wall and heat conducting mid element.

EFFECT: decreased weight, higher in-nacelle draft.

8 cl, 6 dwg

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RU 2 552 574 C2

Authors

Mer Pascal

Thouement Jean-Francois

Dates

2015-06-10—Published

2011-02-03—Filed