Research Article

Web Optimization of Compression Ignition Aviation Engine Crankshaft

Table 2

Design iterations.

IterationThickness [mm]Angle [°]Radius [mm]Δ mass [%]

Reference0
 #0 (Manual)0010-18.8
 #11010-17.9
 #20510-16.4
 #30020-18.0
 #40520-15.6
 #51510-15.2
 #61020-17.2
 #71520-14.1