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Title:
ARRANGEMENT STRUCTURE FOR AIR CONDITIONER IN AIRPLANE
Document Type and Number:
Japanese Patent JP2003205899
Kind Code:
A
Abstract:

To avoid reduction of effective cabin volume and shorten air conditioning piping by rationally arranging an air conditioner of an airplane.

A carry-through 12 integrally connecting spars 11 of left and right main wings WL and WR of the airplane is arranged below a fuselage F, and fairing 14 covering the carry-through 12 is protruded from a lower face of the fuselage F. The air conditioner C producing air for air-conditioning a cabin 13 by exchanging heat of high temperature bleed air extracted from an engine E provided on the main wings WL and WR with the low temperature atmosphere is arranged in a space 15 partitioned between the lower face of the fuselage F and the fairing 14. By this, large effective cabin volume can be secured and the piping of the air conditioner C can be shortened.


Inventors:
GOTO KENICHI
FUJII TOSHIAKI
Application Number:
JP2002007280A
Publication Date:
July 22, 2003
Filing Date:
January 16, 2002
Export Citation:
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Assignee:
HONDA MOTOR CO LTD
International Classes:
B64D13/06; (IPC1-7): B64D13/06
Attorney, Agent or Firm:
Ken Ochiai (1 person outside)



 
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