Power plants – Reaction motor – Including mechanical air compressor or air flow inducing means
Patent
1985-12-30
1987-02-24
Casaregola, Louis J.
Power plants
Reaction motor
Including mechanical air compressor or air flow inducing means
60728, 417 73, 417151, 417173, F02C 712
Patent
active
046447466
ABSTRACT:
A gas compressor is provided having a source of supersonic velocity gases acting to accelerate inlet gases through a mixing region and diffuser. The inlet gas is introduced into the mixing chamber through a converging-diverging nozzle, causing said gas to accelerate to supersonic velocity. An injection of coolant is provided into the resulting gas stream to cause a decrease in its stagnation temperature and an increase in its stagnation pressure. Also provided is a means for modifying the nuclear spin orientations of the gases involved in the mixing region upstream of the combustion chamber to increase the stagnation pressure and decrease the stagnation temperature of the gas flowing into the combustion chamber. The gas compressor can be utilized in a jet engine for producing a flow of pressurized gases which may be expanded through a thrust producing nozzle.
REFERENCES:
patent: 1375601 (1921-04-01), Morize
patent: 2631774 (1953-03-01), Plummer
patent: 2920448 (1960-01-01), Coanda
patent: 3323304 (1967-06-01), Llobet et al.
patent: 3382679 (1968-05-01), Spoerlein
patent: 3442086 (1969-05-01), Nieman
patent: 3750400 (1973-08-01), Sharpe
Casaregola Louis J.
L. W. Fleckenstein, Inc.
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