Turbojet engine for aircraft, propulsion unit comprising...

Power plants – Reaction motor – Including heat exchange means

Reexamination Certificate

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Details

C060S785000, C060S797000

Reexamination Certificate

active

07997061

ABSTRACT:
A propulsion unit comprises a turbojet engine and a thermal exchanger, situated above the turbojet engine. The turbojet engine comprises a regulation device to regulate an air flow-rate in a cooling air lead-in conduit conveying a stream of cooling air into a thermal exchanger, The regulation device regulates the air flow-rate upstream with respect to the cooling air lead-in conduit.

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