Fuel-air premixing device for a gas turbine

Power plants – Combustion products used as motive fluid – Combustion products generator

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60746, 60 3923, F02C 314

Patent

active

050164430

ABSTRACT:
A fuel-air premixing device of a gas turbine has a double-cylinder structure composed of an inner cylinder and an outer cylinder defining therebetween flow passages such that a fuel is supplied into air flowing through the passages so that a pre-mixture of the fuel and air is formed and discharged. The premixing device further has a plurality of radially spaced fuel nozzles capable of supplying the fuel into the passages, and fuel supply rate regulator valves for independently controlling the rates of supply of the fuel from the radially spaced nozzles.

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patent: 4263780 (1981-04-01), Stettler
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