ANNULUS FILLER FOR A GAS TURBINE ENGINE
    1.
    发明公开

    公开(公告)号:US20240360770A1

    公开(公告)日:2024-10-31

    申请号:US18636837

    申请日:2024-04-16

    CPC classification number: F01D11/008 F01D5/14 F01D5/30 F05D2220/36

    Abstract: An annulus filler for mounting to a rotor disc of a gas turbine engine includes a coupling portion and an outer lid coupled to the coupling portion. The outer lid includes a leading edge, a trailing edge, and a main portion including an outer radial surface. The outer lid further includes a protruding portion connected to the main portion and extending radially outwardly from the main portion. The protruding portion is axially disposed between and spaced apart from the leading edge and the trailing edge. The protruding portion includes a protruding surface contiguous with and extending radially outwardly from the outer radial surface, such that the protruding surface is configured to redirect air drawn through the gas turbine engine.

Patent Agency Ranking