Aircraft air-conditioning apparatus with water separators

Details Aircraft air-conditioning apparatus with water separators Aircraft air-conditioning apparatus with water separators

B - Operations, Transporting

64

D

B64D 13/08 (2006.01) B64D 13/06 (2006.01)

Patent

CA 2314998

A system for air-conditioning the cabin of a passenger aircraft using externally provided fresh air as well as bleed air tapped from the engine of the aircraft includes at least one heat exchanger, a blower, a compressor, an expansion turbine, a condenser, a reheater, a first high pressure water separator, and a second low pressure water separator. The several components are connected to each other by air lines such as air ducts, with control valves interposed therein. Two separate air-flow paths representing two different sub-systems are formed. A first air--flow path uses the high pressure water separator while a second air-flow path uses the low pressure water separator. These two air-flow paths or sub-systems can be operated separately and independently of each other by appropriately switching respective shut-off valves. In this manner, the operation of the air--conditioning system can be adaptively switched to achieve an optimal operation under different operating conditions of the aircraft and different air-conditioning requirements.

Affiliated with

Also associated with

Rating

Aircraft air-conditioning apparatus with water separators does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft air-conditioning apparatus with water separators, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft air-conditioning apparatus with water separators will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1804272