H. Fessler et Cj. Moore, STRESSES IN A SPLINELESS DRIVE FOR AERO-ENGINES, Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 210(G2), 1996, pp. 189-202
This paper describes an alternative to splines for connecting turbine
discs to shafts. The trilobe shape consists of six smoothly blending 6
0 degrees circular arcs of two alternating radii; it is between a circ
le (both radii equal) and a triangle (smaller radius zero, larger radi
us infinite). Frozen-stress, photoelastic models of a realistic disc a
nd a tubular shaft have been designed, made and loaded centrifugally,
under static torsion and under combined torsion and rotation. The resu
lts show that the greatest centrifugal stresses in the disc occur in t
he bore at the tips of the trilobe and the greatest contact stresses o
ccur near the transition from the larger to the smaller radius. The ce
ntrifugal stress concentrations due to the trilobe were small. Bore de
formation and backlash due to differential centrifugal expansion were
measured and found to be acceptable for a similar ceramic or nickel al
loy disc.