Rotational inertia frequency domain detection method based on floating torsion pendulum table
A technology of moment of inertia and detection method, which is applied in the detection of moment of inertia and the field of frequency domain detection of moment of inertia, and can solve problems such as affecting the measurement accuracy of moment of inertia and the instability of torsional motion cycle
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specific Embodiment approach 1
[0046] Specific Embodiment 1: A frequency-domain detection method based on the moment of inertia of an air-bearing torsion table described in this embodiment is characterized in that the method includes the following steps:
[0047] Step 1. According to Hooke's law, the restoring moment M generated by the torsion bar is twisted n It is proportional to the angle θ turned, that is
[0048] m n =-Kθ (1)
[0049] In the formula, K is the stiffness coefficient of the torsion bar. When the air resistance and the damping torque generated by the mechanical friction of the bearing are considered, the resultant moment of the air-floating torsion table is expressed as the sum of the restoring moment of the torsion bar and the damping moment, that is,
[0050] M=M n +M z (2)
[0051] In the formula, M n is the restoring moment under the action of the torsion bar, M z is the damping torque generated by the damping effect. Under the condition of the linear model of damping, t...
specific Embodiment approach 2
[0061] Specific embodiment two: the difference between this embodiment and specific embodiment one is: the damping coefficient c described in step one uses damping ratio ζ, undamped natural frequency ω n and moment of inertia I three parameters to represent, namely c=2ζω n I, ω is the instantaneous angular velocity of the swing. Other steps are the same as in the first embodiment.
specific Embodiment approach 3
[0062] Specific implementation mode three: the difference between this implementation mode and specific implementation mode one or two is: the calculation process of the torsional motion differential equation described in step two is as follows: according to the law of rotation,
[0063] β = M I - - - ( 6 )
[0064] β is the angular acceleration, and I is the moment of inertia of the measured product revolving around the uranium, so that Then there is the differential equation of motion:
[0065] I d 2 θ dt 2 + c dθ dt + kθ = 0 - - - ( 7 ...
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