Title:
AIRCRAFT COOLING SYSTEM
Document Type and Number:
Japanese Patent JP2015051747
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide an aircraft cooling system capable of operating depending on a change in power consumption, while suppressing a temperature change of air supplied into an indoor space of an aircraft for which a predetermined ventilation volume is ensured.SOLUTION: This cooling system (aircraft cooling system) 100 includes: vapor cycle devices 2 and 3 for cooling intake air F for ventilation taken in from an outside of an aircraft and circulation air R used by circulating in an indoor space of the aircraft, and supplying the cooled intake air F and circulation air R into the indoor space thereof; and an air conditioning control unit 4 for setting operating conditions for the vapor cycle devices 2 and 3. The air conditioning control unit 4 is configured to control the setting of the operating conditions for the vapor cycle devices 2 and 3 so as to switch over between a normal operation mode for supplying the air into the indoor space at a predetermined temperature and a power consumption suppression mode for changing a humidity of the supplied air while suppressing a change with temperature setting in the normal operation mode, depending on consumable electric energy consumable for cooling the indoor space.
Inventors:
SAITO HIDEFUMI
URYU SHOJI
URYU SHOJI
Application Number:
JP2013186508A
Publication Date:
March 19, 2015
Filing Date:
September 09, 2013
Export Citation:
Assignee:
SHIMADZU CORP
International Classes:
B64D13/08; F25B9/00
Attorney, Agent or Firm:
Hirokazu Miyazono