The invention provides a helicopter radar cabin with ventilation and cooling functions, and the helicopter radar cabin comprises a radome which is disposed at the head of a helicopter; wherein the radome and the helicopter head form a radar cabin; the air inlet is formed in the front part of the radar cabin; the air outlet is formed in the rear part of the radar cabin; the fan is arranged at the air outlet; wherein the air with the first temperature flows into the radar cabin from the air inlet, passes through radar equipment in the radar cabin and carries heat generated by the radar equipment to form air with the second temperature, and the air with the second temperature flows out of the machine from the air outlet under the action of the fan; wherein the first temperature is lower than the second temperature; in the use process, the temperature measurement of the radar cabin shows that the temperature in the radar cabin is basically kept consistent with the external environment temperature, and a very good heat dissipation effect is achieved.
本申请提供的一种具有通风降温功能的直升机雷达舱,所述直升机雷达舱包括:雷达罩,设置在直升机机头;其中,所述雷达罩与所述直升机机头形成雷达舱;进风口,设置在所述雷达舱的前部;出风口,设置在所述雷达舱的后部;风机,设置在所述出风口;其中,第一温度的空气从所述进风口流入所述雷达舱,经过所述雷达舱中的雷达设备,并携带所述雷达设备产生的热量,形成第二温度的空气,所述第二温度的空气通过所述风机的作用,从所述出风口流出至机外;其中,所述第一温度小于所述第二温度;本申请使用过程中对其雷达舱测温表明,雷达舱内温度基本保持与外部环境温度一致,达到了非常好的散热效果。
Helicopter radar cabin with ventilation and cooling functions
一种具有通风降温功能的直升机雷达舱
2023-04-04
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |