The invention discloses an aircraft cabin air conditioning system flow channel, an aircraft cabin air conditioning system and an aircraft, relates to the field of aircrafts, and aims to optimize the structure of the aircraft cabin air conditioning system flow channel. The aircraft cabin air conditioning system flow channel comprises a first flow channel and a second flow channel. The first flow channel comprises a first air inlet and a first air outlet. The flow channels of the second flow channel and the first flow channel are independent of each other, and the second flow channel and the first flow channel are fixed together. The second flow channel comprises a second air inlet and a second air outlet, the first air inlet and the second air inlet are arranged adjacently, and the first air outlet and the second air outlet are arranged adjacently. According to the technical scheme, the two runners are relatively independent, so that the structure of the runner of the aircraft cabin airconditioning system is relatively ingenious, pressure loss caused by mixed airflow is avoided, a fan with high conveying capacity is not needed to compensate the pressure loss, and the fan type selection design is more flexible.
本发明公开了一种飞机机舱空调系统流道、飞机机舱空调系统以及飞机,涉及飞机领域,用以优化飞机机舱空调系统流道的结构。该飞机机舱空调系统流道包括第一流道和第二流道。第一流道包括第一进风口和第一出风口。第二流道与第一流道两者的流道相互独立,且第二流道与第一流道固定在一起。第二流道包括第二进风口和第二出风口,第一进风口和第二进风口邻近设置,第一出风口和第二出风口邻近设置。上述技术方案,两个流道相对独立,使得飞机机舱空调系统流道的结构比较灵巧,不会因为混合气流造成压力损失,不需要采用高输送能力的风机来补偿压力损失,使得风机选型设计更加灵活。
Aircraft cabin air-conditioning system flow channel, aircraft cabin air-conditioning system and aircraft
飞机机舱空调系统流道、飞机机舱空调系统以及飞机
2021-02-05
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |