基本信息:
- 专利标题: TWO-PIECE COMBUSTOR
- 申请号:PCT/US2020/034672 申请日:2020-05-27
- 公开(公告)号:WO2021242229A1 公开(公告)日:2021-12-02
- 发明人: KINSMAN, Peter , MORRISON, Jr., Calvin Q. , ROSALES, Luis A.
- 申请人: AEROJET ROCKETDYNE, INC.
- 申请人地址: P.O. Box 13222
- 专利权人: AEROJET ROCKETDYNE, INC.
- 当前专利权人: AEROJET ROCKETDYNE, INC.
- 当前专利权人地址: P.O. Box 13222
- 代理机构: KOZIARZ, Matthew L.
- 主分类号: F23R3/00
- IPC分类号: F23R3/00 ; F23R3/44 ; F23R7/00 ; F23C3/00 ; F42B19/12
摘要:
A combustor includes a pressure-containing housing (22) and a one- piece body (24) disposed along an axis. The one-piece body has an exhaust manifold section (40) and a liner section (42). The exhaust manifold section defines a flow path and the liner section at least partially defines a combustion chamber (26) and extends axially from the exhaust manifold section into the pressure-containing housing. The exhaust manifold section is hermetically sealed to the housing. The liner section loosely abuts the pressure-containing housing at an end opposite the exhaust manifold section. The liner section and pressure-containing housing define an insulation cavity (58).
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F23 | 燃烧设备;燃烧方法 |
----F23R | 高压或高速燃烧生成物的产生,例如燃气轮机的燃烧室 |
------F23R3/00 | 应用液体或气体燃料的连续燃烧室 |