Fuel nozzle guide and seal for a gas turbine engine

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

Patent

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Details

60740, 60756, F23R 310, F02C 718

Patent

active

043654703

ABSTRACT:
This invention relates to the construction of the fuel nozzle guide of a turbine power plant and provides sealing while allowing relative movement between the fuel nozzle and combustion liner, and includes the judicious location of cooling passages that permit constant cooling and purging for preventing local hot spots resulting from unwanted flame holding.

REFERENCES:
patent: 3032990 (1962-05-01), Rogers
patent: 3721089 (1973-03-01), Morrison et al.
patent: 3724207 (1973-04-01), Johnson
patent: 3853273 (1974-12-01), Bahr et al.

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