TURBOREACTEUR COMPORTANT UN SYSTEME DE PRELEVEMENT DESTINE A PRELEVER DE L'AIR DANS LEDIT TURBOREACTEUR

A turbojet comprising a low-pressure compressor, a high-pressure compressor and a bleeding system configured to bleed air in the turbojet and to deliver the air to an air system. The bleeding system comprises a first air intake configured to bleed air at low pressure, a second air intake configured...

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Bibliographische Detailangaben
Hauptverfasser: PELAGATTI OLIVIER, DEGUIN THOMAS, BODET RONAN
Format: Patent
Sprache:fre
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Beschreibung
Zusammenfassung:A turbojet comprising a low-pressure compressor, a high-pressure compressor and a bleeding system configured to bleed air in the turbojet and to deliver the air to an air system. The bleeding system comprises a first air intake configured to bleed air at low pressure, a second air intake configured to bleed air at high pressure, a first valve and a second valve having inlets connected to the first air intake, a compressor having an inlet connected to an outlet of the second valve, a high-pressure valve connected to the second air intake, a control valve connected to the air system, and a controller to control opening and closing of the valves depending on a pressure at the first air intake.