Dual entry radial turbine gas generator

Details Dual entry radial turbine gas generator Dual entry radial turbine gas generator

F - Mech Eng,Light,Heat,Weapons

02

C

60/153

F02C 3/04 (2006.01) F02C 3/10 (2006.01)

Patent

CA 1262638

ABSTRACT OF THE DISCLOSURE A compact, highly efficient single spool gas turbine gas generator uses a double-entry centrifugal first stage compressor, a single-entry centrifugal second stage compressor, and a radial inflow turbine to achieve an overall pressure ratio of greater than 15:1. The first stage pressure ratio is more than twice the second stage pressure ratio, and the first stage entrance Mach numbers are greater than about 1.4. The specific speed of each the compressors ranges from 0,65 to 0.85, and of the turbine from 0.50 to 0.75.

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