Gas turbine engines with improved compressor-combustor interface

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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60 3936, 415207, F02C 304

Patent

active

041670973

ABSTRACT:
Gas turbine engines with interfaces between a compressor and a combustor which minimize disturbances in the pattern of air flowing from the compressor to the combustor. Provision is also made for dissipating disturbances which may have been created and for supplying compressor discharge air to the turbine of the engine to cool specified turbine components.

REFERENCES:
patent: 2780060 (1957-02-01), Griffith
patent: 3388888 (1968-06-01), Kercher et al.
patent: 3826084 (1974-07-01), Branstrom et al.
patent: 3904312 (1975-09-01), Exley

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