Hole (notch) flexure hinge
Normal and rotational stiffness, and maximum rotation angle, of a circular-hole (notch) flexure hinge in a flat plate.
Plane-strain modulus, E'78.02 10⁹ Pa
Normal stiffness, c_xx118.42 10⁶ N/m
Shear/normal stiffness ratio0.1 -
Torsional (bending) stiffness, k = dψ/dT23.06 Nm/rad
Maximum rotation angle, ψ_max19.2 10⁻³ rad
Maximum rotation angle, α_max1.101 deg
Maximum torsion moment, T = kψ0.443 Nm
Method & references
- Design chart for hole (notch) flexure hinges (Fig. 14.6).
The computation is a literal port of the original client-side JavaScript from /calculators/c14_2.htm. Results are verified equal to the original by an automated golden-master test. No formula has been re-derived or “improved”.