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Piezoelectrical Structural Sensor Technology for Extreme Environments (> 1800 F), Phase I

Completed TRL 4 (started at 4, targeting 5)

Description

High temperature piezoelectric crystal (HTP) sensors are desired for future propulsion component structure health monitoring, operating parameters optimization, turbine engine control and health monitoring, as well as improving performance and maintainability of power production facilities and other rotary combustion engines. Recently discovered high temperature piezoelectrics showed stable piezoelectric properties and high resistivity at temperatures close to its melting point (~ 1500 C) , which is very promising for high temperature sensor applications. The preliminary results showed excellent temperature sening performance at temperature up to 1000 C. Piezoelectric structural sensors on the basis of piezoelectric effect (non-resonant) and impedance measurement (resonant) have been widely demonstrated for pressure, stress, strain, temperature, acceleration, etc. measurements because of their high sensitivity, quick response, low profile, high reliability and low cost. The goal of this program is to develop highly sensitive HTPC based piezoelectric structural sensors for temperature, strain and acceleration measurements at temperatures up to 2000 oF.

Benefits

High temperature sensors can be used for turbine engine control and health monitoring, high mach flight tests, as well as improving performance and maintainability of power production facilities and other rotary combustion engines.

Details

Technology areaSensors and Instruments > In Situ Instruments and Sensors > Environment Sensors
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationArmstrong Flight Research Center, Edwards, CA
Start date2009-01-22
End date2009-07-22

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