High-temperature gas exhausted to outside of an aircraft including exhaust air from an air conditioner is prevented from thermally influencing an airframe. An aircraft includes, in an airframe, an exhaust port configured to exhaust, to outside of the aircraft, high-temperature gas that flows through an exhaust duct provided in an air conditioner and has temperature higher than allowable temperature of GFRP used as a material of a fairing, and a partition as a turning reduction portion configured to reduce a turning component contained in flow of the high-temperature gas before the high-temperature gas is exhausted to the outside of the aircraft.
AIRCRAFT, AND AIRCRAFT MAINTENANCE METHOD
02.01.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Engineering Index Backfile | 1942
|SLUB | 1950
|Engineering Index Backfile | 1940
Engineering Index Backfile | 1950
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