F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
60/183
F02C 7/04 (2006.01) F02C 3/32 (2006.01) F02C 7/042 (2006.01) F02C 7/141 (2006.01) F02K 1/36 (2006.01) F02K 7/12 (2006.01) F04F 5/46 (2006.01)
Patent
CA 1243848
GAS COMPRESSOR FOR JET ENGINE ABSTRACT OF THE DISCLOSURE 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 super- sonic velocity. An injection of coolant is provided into the resulting gas stream to cause a decrease in its stagna- tion 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 up- stream 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.
525099
Fleckenstein (l.w.) Inc.
Macrae & Co.
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