TURBOJET INCLUDING AN AUTOMATICALLY VARIABLE FLOW RATE BLEED CIRCUIT FOR COOLING AIR

Bleeding cooling air to cool a subassembly, e.g. such as a turbine, with automatic adjustment of the air flow section as a function of the speed of the engine. According to the invention, a shutter element is fastened to co-operate with a bleed hole, with the material that constitutes either the shu...

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Bibliographische Detailangaben
Hauptverfasser: ROUSSELY-ROUSSEAU AMAURY, BURLET GUY, BERCHE EMMANUEL
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:Bleeding cooling air to cool a subassembly, e.g. such as a turbine, with automatic adjustment of the air flow section as a function of the speed of the engine. According to the invention, a shutter element is fastened to co-operate with a bleed hole, with the material that constitutes either the shutter element or the wall in which the hole is formed being of a type in which it is possible to create eddy currents, and a magnet is mounted to move past said arrangement.