Gas turbine combustion system utilizing renewable and non-critic

Details Gas turbine combustion system utilizing renewable and non-critic Gas turbine combustion system utilizing renewable and non-critic

1984-08-17

1985-11-05

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

60 39464, 110264, 110347, F02C 326

Patent

active

045505632

ABSTRACT:
Pressurized comminuted solid fuel particles are mechanically reground in a fuel injector prior to being radially injected in a swirling motion into a combustor where the fuel is mixed with oxidizing fluid in a swirling motion that is opposite to the swirling motion imparted to the solid fuel particles and burned to form both solid and gaseous products of combustion. The products of combustion are passed through an inertia separator where the solid products of combustion are removed by inertia. Means are also provided for injecting liquid or gaseous fuels into the combustor to assist in the combustion process and in meeting varying load demands on the engine.

REFERENCES:
patent: 1591679 (1926-07-01), Hawley
patent: 1618808 (1927-02-01), Burg
patent: 1910735 (1933-05-01), Zikesch
patent: 2699039 (1955-01-01), Yellott
patent: 2888804 (1959-06-01), Yellott et al.
patent: 2900930 (1959-08-01), Cermak
patent: 4338782 (1982-07-01), Marchand
patent: 4457695 (1984-07-01), Kummel

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