Panel burn through tolerant shell design

    公开(公告)号:US11098899B2

    公开(公告)日:2021-08-24

    申请号:US15903592

    申请日:2018-02-23

    Abstract: A dual wall liner for a gas turbine engine may comprise a shell having a first side and a second side, a panel contacting the shell, the panel at least partially defining a hot gas path through which a hot gas flows, wherein the first side of the shell faces the panel, wherein the shell includes a thermal barrier coating (TBC) disposed on the first side of the shell. The TBC may thermally protect the shell from heat from a hot gas path.

    PANEL BURN THROUGH TOLERANT SHELL DESIGN
    7.
    发明申请

    公开(公告)号:US20190219265A1

    公开(公告)日:2019-07-18

    申请号:US15903592

    申请日:2018-02-23

    CPC classification number: F23R3/002 F23R2900/00018 F23R2900/03043

    Abstract: A dual wall liner for a gas turbine engine may comprise a shell having a first side and a second side, a panel contacting the shell, the panel at least partially defining a hot gas path through which a hot gas flows, wherein the first side of the shell faces the panel, wherein the shell includes a thermal barrier coating (TBC) disposed on the first side of the shell. The TBC may thermally protect the shell from heat from a hot gas path.

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