Carbon Nanotube Composite SHM Sensor using Additive Manufacturing
Status: Completed
Start Date: 2017-10-01
End Date: 2018-09-30
Description:
We propose to develop a piezoelectric sensors made of carbon nanotube and lead zirconium titanate (PZT) nanopower dispersed in a polymer matrix. These sensors will be flexible and able to be integrated between composite piles as well as adhered to the structure surfaces.
Benefits:
At the present time strain sensors used on structures require external wires to a computer in order to measure strain. Also these strain sensors are quite brittle. Another type of strain sensor is a fiber optic with Fiber Bragg gratings etched into the material. Again, this limits the sensor to initial proof testing of the structural article.
Lead Organization: Marshall Space Flight Center