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Helicopter in-flight rotor tracking system, method, and smart actuator therefor

  • US 6,453,669 B2
  • Filed: 09/19/2001
  • Issued: 09/24/2002
  • Est. Priority Date: 03/03/2000
  • Status: Expired due to Fees
First Claim
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1. A smart-material actuator, comprising:

  • at least one active torsion element formed of a smart material that deforms in response to an applied stimulus so as to cause the torsion element to twist about an axis;

    stimulus means operable to apply a stimulus to the active torsion element;

    a shaft coupled with the torsion element so as to be rotated about a longitudinal axis of the output shaft when the torsion element twists; and

    a locking device operable to engage the shaft and prevent rotation thereof, the locking device being fixed against rotation and encircling the shaft, the locking device being formed of a smart material that deforms in response to an applied stimulus and being fitted about the shaft so as to frictionally grip the shaft to prevent rotation thereof when no stimulus is applied to the locking device, the locking device being operable to release the grip on the shaft and permit rotation thereof when a predetermined stimulus is applied to the locking device.

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