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Shake test using applied force vs moment

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vorwald

Aerospace
Joined
May 25, 2001
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94
Location
US
Has anyone ever used applied moment in a shake test? A friend asked me to comment on the pro/cons of force/moment on a heliocopter shake test.
 
Yes, we use a torsional shaker for driveline development. They are available commercially.

To be honest the advantages are not enormous since we don't have torsional accelerometers to go with them.
Cheers

Greg Locock
 
Yes, in looking at optical point-track system stability in an aircraft external pod rocking-mode situation. It was easier to design a fixture with a pivot at one end and a pivot over the shaker head. Then translational shaker motion creates uniaxial rotary random motion, which input into the optical system stresses the stability control algorithms/hardware. To prevent simultaneous correlated translation (if desired) you have to mount the payload at the stationary hinge. Note all this was done in the preliminary design phases on paper/computer sim. What was ACTUALLY done and the experience was the province of the engineers who stayed with the program.
 
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