发明申请
US20120198852A1 MULTIPOINT INJECTOR FOR A TURBINE ENGINE COMBUSTION CHAMBER 有权
涡轮发动机燃烧室多点喷油器

MULTIPOINT INJECTOR FOR A TURBINE ENGINE COMBUSTION CHAMBER
摘要:
A fuel injector device for an annular combustion chamber including a pilot circuit feeding an injector and a multipoint circuit feeding injection orifices formed in a front face of an annular chamber, an annular ring being mounted in the annular chamber to define therein a fuel feed circuit for the injection orifices and a cooling circuit operating by passing the fuel feeding the injector and extending over the front face of the chamber in immediate vicinity of the injection orifices.
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