Air conditioning system for aircraft

Details Air conditioning system for aircraft Air conditioning system for aircraft

1975-08-29

1977-03-29

Capossela, Ronald C.

Refrigeration

Processes

Reducing pressure on compressed gas

62 96, 62172, 62402, 62DIG5, 123119CD, 60599, F25B 900

Patent

active

040141799

ABSTRACT:
Inlet air for an internal combustion engine in an airplane is expanded through a turbine to lower its pressure and temperature and is passed through a water chiller wherein heat exchange and evaporative cooling substantially lower the temperature of the water. The air is then fed to a compressor driven by the turbine and its pressure is raised to a level suitable for input to the engine manifold. The chilled water is circulated through a heat exchanger to provide cooling for the cabin of the airplane.

REFERENCES:
patent: 1935186 (1933-11-01), King
patent: 2526103 (1950-10-01), Wood
patent: 2734443 (1956-02-01), Wood
patent: 2767561 (1956-10-01), Seeger
patent: 3208234 (1965-09-01), Messinger

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