Title:
航空機のための空調方法およびシステム
Document Type and Number:
Japanese Patent JP6412010
Kind Code:
B2
Abstract:
Air conditioning system for the pressurized cabin of an aircraft, said system (1) being characterized in that it comprises an air withdrawal module (3) configured for withdrawing ambient air from outside the aircraft, an air compression module (5) configured for compressing the withdrawn air flow (F1) and an air cooling module (10) comprising means (15) for storing at least one coolant configured for cooling the compressed air flow (F2, F3).
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Inventors:
L'Orain, Usaille
Application Number:
JP2015542329A
Publication Date:
October 24, 2018
Filing Date:
November 07, 2013
Export Citation:
Assignee:
Saffron Helicopter Engines
International Classes:
B64D13/08; F24F5/00; F25B9/02
Domestic Patent References:
JP10089823A | ||||
JP2003279215A | ||||
JP2003148845A | ||||
JP2010065993A | ||||
JP2010528829A |
Foreign References:
US20080032616 | ||||
US20120240599 | ||||
US20100064701 | ||||
US5730216 |
Attorney, Agent or Firm:
Kawaguchi International Patent Office
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