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