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    • 8. 发明公开
    • ELECTRICAL SYSTEM COOLING IN A MULTI-AXIS PASSENGER-CARRYING AIRCRAFT
    • 电动系统在多轴客运飞机上的冷却
    • EP3184430A1
    • 2017-06-28
    • EP16159553.3
    • 2016-03-10
    • Guanghou Ehang Intelligent Technology Co., Ltd.
    • Du, HaoLin, Zuming
    • B64D13/06B64D13/08B64D27/24F25B21/02H01L35/28H05K7/00
    • B64D13/08B64D13/06B64D27/24B64D33/08B64D2013/0614B64D2013/0674F25B21/02F25B21/04F25B2321/0252H05K7/00H05K7/005Y02T50/62
    • A multi-axis passenger-carrying aircraft is provided, comprising: an electrical system; a heat exchange system; a cabin; and an accommodating compartment arranged inside the cabin; wherein the electrical system is arranged inside the accommodating compartment, and wherein the heat exchange system comprises at least an air inlet communicated with the exterior of the cabin, an air outlet communicated with the accommodating compartment, and a cooler with an air inlet end communicated with the air inlet and an air outlet end communicated with the air outlet. In operation, air outside the aircraft may enter the heat exchange system via the air inlet and the cooler via the air inlet end to be cooled by the cooler. The cooled air may be discharged via the air outlet end and then enter the accommodating compartment via the air outlet, providing cool air to the accommodating compartment and dissipating heat from the electrical system. In this way, it allows more stable operation of the electrical system and higher safety factor of the aircraft to ensure its safety.
    • 提供了一种多轴载客飞机,包括:电气系统; 一个热交换系统; 一间小屋 以及布置在驾驶室内的容纳室; 其中所述电气系统布置在所述容纳室内部,并且其中所述热交换系统包括与所述机舱的外部连通的至少一个进气口,与所述容纳室连通的出气口以及具有与所述进气口连通的冷却器 进风口和出风口与出风口连通。 在运行中,飞机外部的空气可以通过空气入口和冷却器经由空气入口端进入热交换系统以被冷却器冷却。 被冷却的空气可以通过空气出口端排出,然后通过空气出口进入容纳室,为容纳室提供冷空气并从电气系统散发热量。 这样可以使电气系统运行更稳定,飞机安全系数更高,确保了飞机的安全。