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ROTATING DETONATION COMBUSTOR WITH DISCRETE DETONATION ANNULI

机译:离散爆震环形旋转爆轰燃烧器

摘要

The present disclosure is directed to a rotating detonation combustor that includes a forward wall, a radially inner wall, and a radially outer wall. The forward wall is disposed at an inlet end of the rotating detonation combustor. The radially inner wall surrounds a longitudinal axis and extends downstream from the forward wall to an outlet end of the rotating detonation combustor. The radially outer wall extends downstream from the forward wall to the outlet end and surrounds the radially inner wall to define at least one annular plenum between the radially inner wall and the radially outer wall. At least one partition is proximate to the inlet end and defines at least two mixing zones. A plurality of oxidizer inlets and a plurality of fuel inlets are disposed at the inlet end in fluid communication with the at least two mixing zones.
机译:本公开针对一种旋转爆震燃烧器,其包括前壁,径向内壁和径向外壁。前壁布置在旋转爆震燃烧器的入口端。径向内壁围绕纵轴并且从前壁向下游延伸至旋转爆震燃烧器的出口端。径向外壁从前壁向下游延伸至出口端,并且围绕径向内壁,以在径向内壁和径向外壁之间限定至少一个环形气室。至少一个隔板靠近入口端并限定至少两个混合区域。多个氧化剂入口和多个燃料入口设置在入口端,与至少两个混合区域流体连通。

著录项

  • 公开/公告号US2020248905A1

    专利类型

  • 公开/公告日2020-08-06

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号US201916267473

  • 发明设计人 KAPIL KUMAR SINGH;NARENDRA DIGAMBER JOSHI;

    申请日2019-02-05

  • 分类号F23R3/56;F23R3/28;

  • 国家 US

  • 入库时间 2022-08-21 11:20:32

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