Invention Grant
- Patent Title: Cooling system on the basis of suction of a boundary layer
- Patent Title (中): 基于吸附边界层的冷却系统
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Application No.: US12148953Application Date: 2008-04-23
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Publication No.: US08191834B2Publication Date: 2012-06-05
- Inventor: Andreas Westenberger , Martin Arendt , Till Marquardt , Lars Frahm , Geza Schrauf
- Applicant: Andreas Westenberger , Martin Arendt , Till Marquardt , Lars Frahm , Geza Schrauf
- Applicant Address: DE
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE
- Agency: Lerner, David, Littenberg, Krumholz & Mentlik, LLP
- Priority: DE102007019820 20070426
- Main IPC: B64C21/06
- IPC: B64C21/06
Abstract:
A cooling system on board an aircraft includes a device for removing by suction a boundary layer, and a heat exchanger through which flows the boundary layer air that has been removed by suction. Cooling by way of a ram air channel can be reduced or entirely stopped, depending on the flight phase, such that the air drag of the aircraft and thus the fuel consumption can be reduced.
Public/Granted literature
- US20090014593A1 Cooling system on the basis of suction of a boundary layer Public/Granted day:2009-01-15
Information query
