Invention Grant
- Patent Title: Turbojet comprising a bleeding system for bleeding air in said turbojet
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Application No.: US14623037Application Date: 2015-02-16
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Publication No.: US09885284B2Publication Date: 2018-02-06
- Inventor: Olivier Pelagatti , Thomas Deguin , Ronan Bodet
- Applicant: Airbus Operations (SAS)
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations (SAS)
- Current Assignee: Airbus Operations (SAS)
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1451235 20140217
- Main IPC: F02C6/08
- IPC: F02C6/08 ; F02C3/10 ; F02C6/06 ; B64D13/04 ; F02C6/04 ; B64D13/02 ; B64D13/06 ; F02C9/18

Abstract:
A turbojet comprising a high-pressure compressor with several compression stages in which the pressure rises in a direction of air flow, from a low pressure to a high pressure, passing through intermediate pressures, and a system to bleed air in the turbojet and deliver the air to an air system. The bleeding system comprises a first air intake to bleed air at low pressure, a second air intake to bleed air at an intermediate pressure, a first valve and a second valve having inlets connected to the first air intake, a compressor having an inlet connected to the second valve outlet, a high-pressure valve connected to the second air intake, and a control valve connected to the air system, and a controller to control the opening and closing of the valves depending on the pressures at the first and second air intakes.
Public/Granted literature
- US20150233291A1 TURBOJET COMPRISING A BLEEDING SYSTEM FOR BLEEDING AIR IN SAID TURBOJET Public/Granted day:2015-08-20
Information query
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