Folded Lightweight Aperture Precision System (FLAPS)

A controllable shape memory alloy (SMA) hinge apparatus comprises multiple SMA elements to effect a first angle of rotation and a second angle of rotation between a first object and a second object. In one example, respective SMA elements are independently activated by Joule heating to rotate the first object and/or the second object. SMA elements undergo a three-dimensional transformation, and a pair of elements may undergo antagonistic transformations so as to provide for a multiple-use bidirectional non-continuous rotary actuator. SMA elements may be trained to achieve different angles of rotations between the objects (e.g., zero degrees and 90 degrees). In some examples, the first object may be a spacecraft (e.g., a satellite) and the second object may be a deployable structure (e.g., a robotic appendage, a deployable solar panel, a deployable aperture, a deployable mirror, a deployable radiator, and at least one actuator to steer an antenna dish).

Researchers

Kerri Cahoy / Christian Haughwout / Derek Barnes / Maxim Khatsenko / James Clark

Departments: Department of Aeronautics and Astronautics
Technology Areas: Communication Systems: Satellites / Energy & Distribution: Electrochemical Devices / Industrial Engineering & Automation: Autonomous Systems

  • shape memory alloy (sma) hinge apparatus, and systems and methods employing same
    United States of America | Granted | 10,899,479
  • folded lightweight aperture precision system (flaps)
    United States of America | Pending

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