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Title:
HIGHLY UNIFORM INJECTION SYSTEM
Document Type and Number:
Japanese Patent JP3954165
Kind Code:
B2
Abstract:

PROBLEM TO BE SOLVED: To provide a highly uniform air and fuel injection system particularly in a combustion chamber of a turbine engine.
SOLUTION: A fuel injector 2 around an axis A injects a fuel into a premixing chamber 3 defined by a convergent/divergent internal configuration 5 of a housing 6 disposed upstream a bowl 8. There are provided three swirlers: a first radial swirler 10 disposed upstream the housing from the upstream side to the downstream side, a second radial swirler 14a, 14b disposed in an upstream side part 12 of the housing 6, and a third axial swirler 18a, 18b disposed on the downstream side of the housing 6 around the same. Air is supplied to the third swirler from a passage 16a, 16b alternately arranged with the second radial siwirler passage 14a, 14b.


Inventors:
Douni Rozier Henri Ansar
Jill Therael Claude Repletor
Douni Jiyan Morris Sandoori
Application Number:
JP24130697A
Publication Date:
August 08, 2007
Filing Date:
September 05, 1997
Export Citation:
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Assignee:
SNECMA
International Classes:
F02C7/232; F23R3/14; F23R3/12; F23R3/28; F23R3/30; (IPC1-7): F23R3/12; F02C7/232; F23R3/28; F23R3/30
Domestic Patent References:
JP4227413A
Attorney, Agent or Firm:
Yoshio Kawaguchi
Makoto Ono
Akio Ichiiri
Katsuma Osaki