초록 ▼

An aircraft cabin is climatized by tapping air from the engine compressors and feeding it into the cabin through a loop which includes a compressor, a cooling turbine driving the compressor, and several cooling stages. A second loop, using preferably helium, includes a second compressor and a second

An aircraft cabin is climatized by tapping air from the engine compressors and feeding it into the cabin through a loop which includes a compressor, a cooling turbine driving the compressor, and several cooling stages. A second loop, using preferably helium, includes a second compressor and a second turbine, the second compressor being driven by both turbines, and the cooled helium is in heat exchange with another cooling loop which runs through instrument compartments. Discharged cabin air is used to precool the compressed helium.

대표청구항 ▼

In a system for climatizing and air conditioning interior compartments of an aircraft, including the passenger cabin, under utilization of air tapped from a compressor of an engine of the aircraft, the system including a cooling turbine for driving a compressor for the tapped air, the turbine coolin

In a system for climatizing and air conditioning interior compartments of an aircraft, including the passenger cabin, under utilization of air tapped from a compressor of an engine of the aircraft, the system including a cooling turbine for driving a compressor for the tapped air, the turbine cooling this tapped air as compressed by the compressor prior to discharge into the passenger cabin, the improvement comprising: a second compressor connected to be driven by said first turbine and having an input and discharge output; a closed cooling loop which includes (i) said second compressor, (ii) a second turbine for cooling and compressing fluid in the closed loop, (iii) a first heat exchanger connected between the discharge output of the second compressor for compressed fluid and an input for the second turbine for passing thereto fluid cooled by the first heat exchanger, and (iv) a second heat exchanger connected between a discharge output of the second turbine after expanding work and said input of the second compressor; means for feeding air discharged from the cabin to the first heat exchanger, for precooling the fluid as it flows from the second compressor to the second turbine; and a second loop for cooling other compartments and being connected for being cooled by the second heat exchanger and by the fluid as it flows through the second heat exchanger from the second turbine to the second compressor.