AIRCRAFT AND FUSELAGE COOLING STRUCTURE

摘要

Under constraints on the space and the weight of an aircraft, the present invention aims to protect structural members from a heat generation part. An aircraft includes: a fuselage; an air conditioning pack installed on the outside of a lower part of the fuselage; a fairing covering the air conditioning pack; an outer heat insulation material disposed in a region of the fuselage, which corresponds to the air conditioning pack, from the outside of the fuselage; and an inner heat insulation material disposed around the region on the inside of the fuselage.

主权项

1. An aircraft comprising:
a fuselage; a heat generation part installed on the outside of the fuselage; a fairing covering the heat generation part; an outer heat insulation material disposed in a corresponding region of the fuselage, which corresponds to the heat generation part, from the outside of the fuselage; and an inner heat insulation material disposed around the corresponding region on the inside of the fuselage.