Climatizing of aircraft

• US 4,283,924 A
• Filed: 08/02/1979
• Issued: 08/18/1981
• Est. Priority Date: 08/04/1978
• Status: Expired due to Term

• Current Assignee: Vereinigte Flugtechnische Werke-Fokker GmbH
• Original Assignee: Vereinigte Flugtechnische Werke-Fokker GmbH
• Inventors: Schutze, Horst
• Primary Examiner(s): Capossela, Ronald C.
• Application Number:
  US06/063,075
• Time in Patent Office: 747 Days
• Field of Search: 62/89, 62/172, 62/402, 62/430, 62/201
• US Class Current: 62/402
• CPC Class Codes: B64D 13/06 the air being conditioned pressurising B64D13/02
• CPC Class Codes: B64D 2013/0614 with subsystems for cooling avionics
• CPC Class Codes: F25B 9/004 the refrigerant being air
• CPC Class Codes: F25B 9/06 using expanders F25B9/10 takes precedence
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

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.

Claims

1. 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.

2. In a system as in claim 1, said second turbine also driving said second compressor.

3. The improvement as in claim 1 or 2, wherein the fluid in the first loop is helium.

4. The improvement as in claim 1 or 2, wherein the fluid in the first loop is air.

5. The improvement as in claim 1 or 2, wherein the fluid is a helium air mixture.

6. The improvement as in claim 2, said first turbine and compressor being on a first common shaft, said second turbine and compressor being on a second common shaft, and clutch means for interconnecting the first and second shafts.