NASA Logo, National Aeronautics and Space Administration
NESB Nondestructive Evaluation Sciences Branch

NESB Nondestructive Evaluaton Sciences Branch

NESB Nondestructive Evalutation Sciences Branch

Shape Sensing Sensor using Optical Fibers

The shape sensing sensor technology co-locates Fiber Bragg Grating (FBG) sensors in the 3-core optical fiber. The sensing fibers are bonded or embedded in the airframe. Each of the 3 cores in the fiber is strained differently according to the bend radius and the FBG sensor gives 3 different strain measurements.

The shape algorithms calculates the strain at every discrete element along the fiber length and recontructs the fiber in 3D space curves.

  • Surface shape mesurements can provide feedback in morphing wing systems.
  • Multi-core fiber is highly flexible, conforms to shapes, and can be secured to an airframe using ordinary methods.
  • Airframe or wing deflections induce bending along the multi-core fiber. Even during multi-axis bending, the fiber conforms to the surface.
  • Fiber bending is measured and converted to 3D space curves using shape algorithms.
  • Deviations from baseline shapes can indicate airframe fatigue

RELEVANT LINKS

Research and Technology Directorate

RELATED SITES

American Society For Nondestructive Testing
American Society for Testing and Materials
British Institute for Non-Destructive Testing
Center for NDE at Iowa State
The e-Journal of Nondestructive Testing & Ultrasonics
Southwest Research Institute
[an error occurred while processing this directive]
NASA Logo - nasa.gov