Title:
COMBUSTION CHAMBER OF GAS TURBINE ENGINE
Document Type and Number:
Japanese Patent JPS53122004
Kind Code:
A
Abstract:
A gas turbine engine combustion chamber includes an inlet through which primary air can flow and which is capable of receiving a fuel injector. A cylindrical collar extends from this inlet into the interior of the combustion chamber and the collar may be parallel walled or slightly divergent and one or more rows of equi-spaced apertures can be provided in the collar wall. The presence of the collar has the effect of reducing the rate of carbon deposition on the combustion chamber head and of reducing the levels of emitted smoke.
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| JP6535525 | Gas turbine combustor |
Inventors:
JIEFURII DAGURASU UIRISU
NIGERU PATORITSUKU GIBUNII
NIGERU PATORITSUKU GIBUNII
Application Number:
JP1187178A
Publication Date:
October 25, 1978
Filing Date:
February 04, 1978
Export Citation:
Assignee:
ROLLS ROYCE
International Classes:
F23R3/10; F23R3/14; F23R3/16; (IPC1-7): F23R1/08
Domestic Patent References:
| JPS5181802U | 1976-06-30 | |||
| JPS5076423A | 1975-06-23 |
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