Gas turbine engine frame having struts connected to rings with morse pins

A gas turbine engine frame comprising:

• concentric radially spaced apart inner and outer rings,
• axially spaced apart inner ring flanges extending radially outwardly from the inner ring,
• axially spaced apart outer ring flanges extending radially inwardly from the outer ring,
• a plurality of strut segments extending between and connected to the inner and outer rings,
• each of the strut segments having a strut extending radially between co-annular radially inner and outer platforms,
• axially spaced apart inner platform flanges extending radially inwardly from the inner platform and interdigitated with the inner ring flanges,
• axially spaced apart outer platform flanges extending radially outwardly from the outer platform and interdigitated with the outer ring flanges, and
• at least one inner set of coaxial tapered inner holes extending axially through the inner platform and ring flanges,
• at least one outer set of coaxial tapered outer holes extending axially through the outer platform and ring flanges,
• the inner set of coaxial inner holes define an inner conical surface,
• the outer set of coaxial outer holes define an outer conical surface, and
• inner and outer pins having tapered conical inner and outer shanks disposed though the inner and outer sets of coaxial inner and outer holes respectively.