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Multi-point fuel injector for turbine engine combustion chamber

机译:用于涡轮发动机燃烧室的多点燃油喷射器

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.
机译:一种用于环形燃烧室的燃料喷射器装置,其包括给喷射器供油的先导回路和给形成在环形室的前表面中的喷射孔供料的多点回路,一环形环安装在环形室中以在其中限定用于燃料的供油回路。喷射孔和冷却回路通过使供入喷射器的燃料通过并在紧邻喷射孔的腔室的正面上方延伸而工作。

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