A New Mathematical Modeling Method for Four-Stage Helicopter Main Gearbox and Dynamic Response Optimization

Figure 2

Dynamic response regarding tooth deflection in each gear pair.

(a) Meshing pair A

(b) Meshing pair B

(c) Meshing pair C

(d) Meshing pair D

(e) Meshing pair E

(f) Meshing pair F

(g) Meshing pair G