Temperature stratified turbine compressors

Details Temperature stratified turbine compressors Temperature stratified turbine compressors

1977-03-07

1979-01-09

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 3952, F02C 700, F02C 708

Patent

active

041331710

ABSTRACT:
A method and apparatus for improving the efficiency of a compressor of a gas turbine engine is disclosed. The inlet gas entering the compressor is stratified into two portions of different temperatures. The higher temperature gas is introduced adjacent the outer tips of the compressor blades to reduce the relative Mach number of the flow at that area.

REFERENCES:
patent: 3194015 (1965-07-01), Pacault
patent: 3703807 (1972-11-01), Rice
patent: 3844113 (1974-10-01), Lockwood

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