System and method for assembling a rotational equipment assembly of an aircraft propulsion system

A support assembly for assembling a rotational equipment assembly for an aircraft propulsion system, the support assembly comprising:

• a frame including a side wall portion and an end wall portion, the side wall portion and the end wall portion extending circumferentially about an axis of the support assembly, the side wall portion extending along the axis between and to a first axial side wall end and a second axial side wall end, the end wall portion including an outer ring, an inner ring, and a plurality of arms, the outer ring disposed at the second axial side wall end, the inner ring disposed radially inward of the outer ring, the plurality of arms extending radially between and connecting the outer ring and the inner ring;
• an upper support member including a support ring mounted on the side wall portion at the first axial side wall end, the support ring extending circumferentially about the axis, the support ring forming a first axial assembly end of the support assembly;
• and
• a lower support member extending circumferentially about the axis, the lower support member mounted on the inner ring, the lower support member forming an opening extending through the lower support member along the axis, the lower support member forming a second axial assembly end of the support assembly, the lower support member having a diameter which converges in an axial direction from the inner ring to the second axial assembly end.

A support assembly for assembling a rotational equipment assembly for an aircraft propulsion system, the support assembly comprising:

• a coupling shaft extending on and along an axis of the support assembly between and to a first axial shaft end and a second axial shaft end, the coupling shaft forming a threaded interface at the first axial shaft end;
• an adjustment assembly mounted on the coupling shaft, the adjustment assembly selectively rotatable about the coupling shaft;
• a frame extending circumferentially about the axis, the frame extending along the axis between and to a first axial frame end and a second axial frame end, the frame including a ring at the first axial frame end, the second axial frame end mounted to the adjustment assembly;
• and
• a plurality of arms circumferentially distributed about the axis, each of the plurality of arms extending axially between a first arm end and a second arm end, the second arm end mounted on the ring, each of the plurality of arms forming a slot facing the axis.