Disclosed is an air-conditioning system for a helicopter. According to one aspect of the present invention, the air-conditioning system for a coaxial reversal type helicopter having first and second rotor blades includes: a pair of outer units arranged on the left and the right of an outer side of a side surface of a fuselage; an inner unit arranged in the fuselage adjacent to the outer units; and an air blowing unit supplying air cooled through the inner unit into a cabin, wherein the outer units include a condenser and are formed to exchange heat between a refrigerant and a downward wind generated from the first and second rotor blades and the inner unit includes an evaporator and is formed to cool the in-flight air through the refrigerator supplied from the condenser.
헬리콥터 에어컨디셔닝 시스템이 개시된다. 본 발명의 일 측면에 따르면, 제1, 2로터블레이드를 가지는 동축 반전식 헬리콥터의 에어컨디셔닝 시스템에 관한 것으로, 기체의 측면 외측에 좌우 한 쌍이 배치되는 외부유닛; 외부유닛과 인접한 기체 내부에 배치되는 내부유닛; 및 내부유닛을 통해 냉각된 공기를 기내로 공급하는 송풍부;를 포함하고, 외부유닛은, 응축기를 포함하고, 제1, 2로터블레이드로부터 생성된 하강풍을 냉매와 열 교환시키도록 형성되며, 내부유닛은, 증발기를 포함하고, 응축기로부터 제공되는 냉매를 통해 기내 공기를 냉각시키도록 형성되는, 헬리콥터 에어컨디셔닝 시스템이 제공된다.
HELICOPTER AIR CONDITIONING SYSTEM
헬리콥터 에어컨디셔닝 시스템
2020-11-04
Patent
Electronic Resource
Korean
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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