CORRUGATED MID-TURBINE FRAME THERMAL RADIATION SHIELD
    1.
    发明申请
    CORRUGATED MID-TURBINE FRAME THERMAL RADIATION SHIELD 审中-公开
    波纹中涡轮机架热辐射防护罩

    公开(公告)号:WO2014058483A2

    公开(公告)日:2014-04-17

    申请号:PCT/US2013046780

    申请日:2013-06-20

    Abstract: A corrugated shield comprises a mounting base and a corrugated ring section. The mounting base is disposed at an aft end of the ring section for securing the shield ring section within a generally annular cavity. The generally annular cavity is defined at least in part by a hot fluid flow path boundary wall, and a radially adjacent and spaced apart cold fluid flow path boundary wall. The corrugated ring section is configured to substantially block a line of sight between the hot fluid flow path boundary wall and the cold fluid flow path boundary wall.

    Abstract translation: 波纹状防护罩包括安装底座和波纹环部分。 安装基座设置在环形部分的后端,用于将屏蔽环部分固定在大致环形的空腔内。 大致环形腔至少部分地由热流体流动路径边界壁和径向相邻且间隔开的冷流体流动路径边界壁限定。 波纹环部分构造成基本阻挡热流体流动路径边界壁与冷流体流动路径边界壁之间的视线。

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