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Title:
AIR CONDITIONING SYSTEM, AIRCRAFT, CONTROL METHOD OF AIR CONDITIONING SYSTEM
Document Type and Number:
Japanese Patent JP2018176846
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To perform air conditioning control before and after take-off or before and after go-around more easily and stably, in an air conditioning system mounted on an aircraft and including an air conditioner for performing air conditioning in the aircraft by engine bleeding.SOLUTION: In the case where take-off start of an aircraft is determined based on a parameter for determining take-off start of the aircraft (Yes in all steps from step S12 to step S14), an air conditioning system automatically stops an air conditioning unit 31 (steps S15, S16). Thereby, a pilot does not need to stop air conditioning by a manual operation during take-off start, so that trouble by a manual operation and failure to stop the air conditioning operation can be avoided.SELECTED DRAWING: Figure 4

Inventors:
梶山 修作
小池 宏樹
Application Number:
JP2017075254A
Publication Date:
November 15, 2018
Filing Date:
April 05, 2017
Export Citation:
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Assignee:
三菱重工業株式会社
International Classes:
B64D13/02; B60H1/00
Attorney, Agent or Firm:
特許業務法人酒井国際特許事務所



 
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