Refrigeration – Processes – Reducing pressure on compressed gas
Patent
1992-09-16
1994-05-10
Capossela, Ronald C.
Refrigeration
Processes
Reducing pressure on compressed gas
62172, 62402, F25B 900
Patent
active
053097246
ABSTRACT:
In a normal mode, a primary heat exchanger for heated bleed airflow is situated upstream of an aircraft air conditioner compressor. A secondary heat exchanger is located downstream of the compressor. In response to hot and humid environmental conditions, three-way switching valves reposition the primary heat exchanger downstream of the compressor. The result will be the reduction of heat exchange exit temperature, which translates into lower turbine inlet and outlet temperatures at satisfactory airflow rates.
REFERENCES:
patent: 3878692 (1975-04-01), Steves
patent: 4312191 (1982-01-01), Biagini
patent: 4553407 (1985-11-01), Rannenberg
patent: 5086625 (1992-02-01), Momose et al.
Schreiber Melvin
Yurman Richard
Capossela Ronald C.
Grumman Aerospace Corporation
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