Gas turbine combustor employing plural catalytic stages

Details Gas turbine combustor employing plural catalytic stages Gas turbine combustor employing plural catalytic stages

1976-03-03

1978-02-07

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

External-combustion engine type

23288R, 252477R, F02C 722

Patent

active

040720071

ABSTRACT:
A gas turbine combustor of the catalytic reactor type has the catalytic element means formed of a crossflow honeycomb type in which the various series of flow passages extend in oblique relation to each other and to longitudinal axis of the combustor shell so that the combustion gas from different radial locations in a cross section upstream from the catalytic element means is shifted to other radial locations in passing downstream, to promote temperature uniformity of the gas in a radial direction throughout the cross section of the combustor.

REFERENCES:
patent: 2887456 (1959-05-01), Halford et al.
patent: 3088271 (1963-05-01), Smith
patent: 3692497 (1972-09-01), Keith et al.
patent: 3912459 (1975-10-01), Kearsley
patent: 3929419 (1975-12-01), Chapman
patent: 3943705 (1976-03-01), De Corso et al.
patent: 3953176 (1976-04-01), Santala et al.
patent: 3969083 (1976-07-01), Givens et al.

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