Turbine support case with axial spokes and brackets

An aircraft engine, comprising:

• a turbine including a turbine rotor rotatable about a central axis;
• a scroll case having an inlet fluidly connected to a source of combustion gases and an outlet fluidly connected to the turbine, and a conduit extending around the central axis from the inlet to the outlet;
• a bearing housing extending around the central axis, the bearing housing including a support flange;
• a turbine support case secured to the bearing housing, the scroll case disposed axially between the turbine support case and the bearing housing, the turbine support case having spokes distributed around the central axis and extending along a direction having an axial component relative to the central axis, the spokes extending through the scroll case and radially supported by the bearing housing, a spoke of the spokes having a distal end secured to the support flange via:
• one or more fasteners, and
• a bracket secured to the support flange, the bracket engaged in a slot defined proximate the distal end of the spoke, the slot having an axially facing surface trapped between the bracket and the support flange of the bearing housing.