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Weapons Bay Door Test Rig |
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The customer required a means of measuring the force on an actuator closing a weapons bay door on a fighter aircraft. The installation required an axial force application to the loadcell via a lever system, which required a degree of transverse freedom to function correctly. The loadcell would be able to accommodate a defined internal movement of the input force centre whilst maintaining a solid load path between the actuator and door structure in its axial measurement sense. The design used a standard design pancake loadcell, which incorporated a polarised flexure to allow a ±0.5mm deflection adjacent to the loading axis while still being able to transmit the load to the loadcell. The loadcell itself incorporated a moment insensitive bridge using 16 gauge sites to reduce the effect of the applied moment through the flexure.
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Updated October 2007. |
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