The invention provides an aircraft cooling system (60) and an aircraft (10). An aircraft cooling system (60) is provided with: a rotor (30) capable of generating a thrust force in the vertical direction; a heat generating unit (66) capable of generating a thrust force in the vertical direction; a support unit (cantilever (18)); a structure (second fairing (46)); and a heat exchanger (surface heat exchanger (50)). The heating part (66) is configured below the rotor wing; the supporting part is used for supporting the heating part; the structure protrudes from the supporting part to the rotor wing; the heat exchanger is provided in a structure, the refrigerant heated by the heat-generating unit is introduced into an inlet (fairing inlet (50i)) provided in the heat exchanger, and the refrigerant cooled by the heat exchanger is supplied to the heat-generating unit from an outlet (fairing outlet (50o)) provided in the heat exchanger. Therefore, the heat generating part can be well cooled.
本发明提供一种航空器冷却系统(60)及航空器(10)。航空器冷却系统(60)具有旋翼(30)、发热部(66)、支承部(悬臂(18))、构造物(第2整流罩(46))和换热器(表面换热器(50)),其中,所述旋翼(30)能够产生铅垂方向的推力;所述发热部(66)被配置在旋翼的下方;所述支承部支承发热部;所述构造物从支承部向旋翼突出;所述换热器被设置于构造物,被发热部加热的制冷剂被导入换热器所具备的流入口(整流罩流入口(50i)),被换热器冷却的制冷剂被从换热器所具备的流出口(整流罩流出口(50o))供给到发热部。据此,能良好地冷却发热部。
Aircraft cooling system and aircraft
航空器冷却系统及航空器
2024-09-20
Patent
Electronic Resource
Chinese
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