Cooling arrangement for radial flow gas turbines having coaxial combustors
United States Patent 2631429

Inventors:
Jacklin Jr., Harold M.
Publication Date:
03/17/1953
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Assignee:
Jacklin Jr., Harold M.
Primary Class:
Other Classes:
415/177, 60/726, 60/39.080, 60/39.511
International Classes:
F01D3/02; F02C3/05; F02C3/14; F02C3/16; F23R3/54; F01D3/00; F02C3/00; F23R3/00
US Patent References:
2392622Gas turbine plant
2471892Reactive propulsion power plant having radial flow compressor and turbine means
Foreign References:
FR383966A