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

1979-11-23

1982-07-13

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Using special fuel or oxidizer

60 3946P, 60744, F02C 326

Patent

active

043387829

ABSTRACT:
Pressurized communited 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 imported to the solid fuel particles and burned to form both solid and gaseous products of combustion. The products of combustion are passed through separator where the solid products of combustor are removed by inertia. Means are also provided for injecting liquid or gaseous fuels into the combustor to assist in the combustion process and meeting varying load demands on the engine.

REFERENCES:
patent: 1618808 (1927-02-01), Burg
patent: 2625791 (1953-01-01), Yellott
patent: 2651176 (1953-09-01), Yellott
patent: 2699039 (1955-01-01), Yellott
patent: 2888804 (1959-06-01), Yellott
patent: 2911065 (1959-11-01), Yellott
patent: 4089631 (1978-05-01), Giles

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