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Device for the damping of combustion chamber vibrations in liquid-fuelled rocket engines
Device for the damping of combustion chamber vibrations in liquid-fuelled rocket engines
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机译:用于衰减液体燃料火箭发动机中燃烧室振动的装置
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摘要
Device for the damping of gas vibrations occurring during the combustion process inside the combustion chamber of rocket engines, which function with liquid propellants, by means of damping chambers arranged in the area of the injection head, which chambers are connected to the combustion chamber by way of through-passages. Here, the damping chambers are provided inside the injection head, distributed over the entire front face of the latter.
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