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.
Turbojet comprising a bleeding system for bleeding air in said turbojet
2018-07-03
Patent
Electronic Resource
English
Turbojet comprising a bleeding system for bleeding air in said turbojet
European Patent Office | 2018
|Online Contents | 1996
SLUB | 1958
|Engineering Index Backfile | 1956
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