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COMBUSTION CHAMBER OF GAS TURBINE ENGINE WITH SELF-REGULATING VARIABLE GEOMETRY

机译:燃气轮机燃烧室具有自调节可变几何形状

摘要

The invention relates to a self-adapting gas turbine firebox with variable geometry, comprising at least one system with a variable opening for automatically adjusting a configuration of the combustion inside a combustion chamber (101) according to an air temperature, particularly air from a compressor. The adjustment is performed by a thermosensitive element that controls at least one section towards the combustion chamber, for the air that participates in the combustion of the fuel, or participates in a dilution of the gases effective inside the combustion chamber.
机译:本发明涉及一种自适用的燃气涡轮机Firebox,其具有可变几何形状,包括至少一个具有可变开口的系统,用于根据空气温度,特别是来自压缩机的空气自动调节燃烧室(101)内的燃烧的结构。调节由热敏元件执行,该热敏元件用于控制燃烧室的至少一个部分,用于参与燃料的燃烧的空气,或者参与有效的气体的稀释腔室。

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