Gas turbine engine frame flowpath liner support

A gas turbine engine frame liner assembly comprising:

• an annular outer casing,
• an annular wall element mounted to and spaced radially inwardly of said outer casing,
• an annular hanger supporting at least in part said wall element from said outer casing,
• said hanger, casing, and wall element circumscribed about a common centerline,
• a bayonet mount operably associated with said hanger for supporting at least in part said wall element from said outer casing, and
• said hanger having circumferentially spaced apart hanger tabs extending equal axial lengths from the body section.

A gas turbine engine frame assembly comprising:

• a frame having an annular outer casing circumscribed about a centerline,
• an annular inner hub circumscribed about said centerline and spaced radially inwardly from said casing,
• a plurality of circumferentially spaced apart hollow struts extending radially between said outer casing and said hub,
• a circumferentially disposed plurality of annular wall elements mounted to and spaced radially inwardly of said outer casing,
• a circumferentially disposed plurality of annular hangers, each one of said hangers supporting at least in part a corresponding one of said wall elements from said outer casing,
• said hanger and wall elements circumscribed about said centerline,
• bayonet mounts operably associated with said hangers for supporting said wall elements from said outer casing, and
• said hangers having circumferentially spaced apart hanger tabs extending equal axial lengths from the body section.