Invention Grant
- Patent Title: Aircraft air conditioning system and method of operating an aircraft air conditioning system
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Application No.: US16572349Application Date: 2019-09-16
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Publication No.: US10967978B2Publication Date: 2021-04-06
- Inventor: Holger Bammann , Frank Klimpel , Hans Brunswig
- Applicant: Airbus Operations GmbH
- Applicant Address: DE Hamburg
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Greer, Burns & Crain, Ltd.
- Priority: EP14185484 20140919,EP15168140 20150519
- Main IPC: B64D13/06
- IPC: B64D13/06

Abstract:
An aircraft air conditioning system including an ambient air supply line having a first end connected to an ambient air inlet and a second end connected to a mixer of the aircraft air conditioning system so as to supply ambient air to the mixer. A first compressor is arranged in the ambient air supply line and is configured to compress the ambient air flowing through the ambient air supply line. A bleed air supply line allows a flow of bleed air bled off from an engine or an auxiliary power unit therethrough. A bleed air turbine is driven by the bleed air flowing through the bleed air supply line and is coupled to the first compressor so as to drive the first compressor.
Public/Granted literature
- US20200010202A1 AIRCRAFT AIR CONDITIONING SYSTEM AND METHOD OF OPERATING AN AIRCRAFT AIR CONDITIONING SYSTEM Public/Granted day:2020-01-09
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