Patent ID: 11958618
Assignee: LIEBHERR-AEROSPACE TOULOUSE SAS
Field: Transport (Mechanical engineering)
Classification: CPC B  F  Y | IPC B

Claim 9:
10. An air conditioning system for a cabin of an aircraft, comprising:
an air bleed device;
an air cycle turbine engine comprising at least one compressor and a turbine mechanically coupled to one another, said compressor comprising an air inlet connected to said air bleed device, and an air outlet, and said turbine comprising an air inlet and an air outlet that is connected to said cabin in order to be able to supply said cabin with air at a controlled pressure and temperature;
at least one heat exchanger, comprising a main cooling exchanger, which is arranged in a channel for the circulation of rain air drawn from outside the aircraft, between said air outlet of said compressor and said air inlet of said turbine, said main exchanger comprising a primary circuit supplied with a flow of hot air from said compressor, and a secondary circuit supplied with said rain air, which forms a flow of cold air for cooling said flow of hot air;
a water extraction loop that is arranged between said main heat exchanger and said turbine and is designed to extract water from the flow of hot air cooled by said main exchanger which supplies said turbine; and
a pipe for distributing water extracted by said extraction loop, which pipe extends between said water extraction loop and said rain-air channel, upstream of said main exchanger, in order to be able to spray the water extracted by said water extraction loop into the rain-air flow of said rain-air channel, wherein said main cooling exchanger is an exchanger for cooling hot primary air by means of cold secondary air, comprising:
a plurality of channels, referred to as secondary channels, placed one on top of the other and intended for the circulation of said secondary air, each extending in the same direction, comprising a secondary direction, between an air inlet, comprising a secondary air inlet, and an air outlet, comprising secondary air outlet; and
a plurality of channels, comprising primary channels, for the circulation of said primary air, each interposed between two secondary channels and extending in the same direction, comprising a primary direction, which is different from said secondary direction, between an air inlet, referred to as the primary air inlet, and an air outlet, comprising primary air outlet so as to allow heat exchanges between the primary air of said primary channels and the secondary air of said secondary channels;
wherein said exchanger further comprises:
water circulation channels, each extending adjacently to a secondary channel in said secondary direction in the vicinity of the primary air outlets, between a water inlet and a water outlet, so as to allow this water to be heated by heat exchanges with said flow of primary air of said primary channels; and
water-spray micro-perforated hollow bars, each extending adjacently to a primary channel in said primary direction, between a water inlet, which is fluidically connected to at least one water outlet of said water circulation channels, and water-spray micro-perforations leading toward the secondary air inlets, so as to allow evaporation of the heated water sprayed at the inlet of said secondary channels, which thus helps to cool the flow of secondary air at the inlet of the exchanger,

wherein said water distribution pipe leads into said water circulation channels of said exchanger, said primary channels forming said primary circuit of said main exchanger, which circuit is supplied with a flow of hot air from said compressor, and said secondary channels forming said secondary circuit supplied with said rain air.