Two-pass orbital rotary flanging is performed and the value of critical contact area ratio
Xc during orbital rotary flanging is experimentally determined. In the two-pass orbital rotary flanging, 1050 aluminum and 5052 aluminum alloy tube-ends are conical flared using a tool in the first pass and then subjected to orbital rotary flanging in the second pass. The experimental results indicate that the values of the tilt angle of the tool ω
2 and the non-dimensional tool feed
F significantly affect the prevention of curling and that the initial contact area ratio
X0 is the principle factor in the prevention of curling; the curling is prevented by setting
X0 below
Xc. In addition, it is also experimentally found that
Xc increases with increasing
F for
F<0.1; however, the rate of increase gradually decreases and
Xc becomes constant (0.05) for
F≥0.1.
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