首页> 外国专利> 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

机译:用于衰减液体燃料火箭发动机中燃烧室振动的装置

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.
机译:通过布置在喷射头区域内的减震室,用于衰减在火箭发动机的燃烧室内部在燃烧过程中发生的气体振动的装置,该气体振动与液体推进剂一起作用,该减震室通过这种方式与燃烧室连接通行证。在此,阻尼室设置在注入头的内部,分布在注入头的整个前表面上。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号