Integrated control and health monitoring capacitive displacement sensor development task. Orbit transfer rocket engine technology program
The development of a miniature multifunction turbomachinery shaft displacement sensor using state-of-the-art non-contract capacitive sensing technology is described. Axial displacement, radial displacement, and speed are sensed using a single probe within the envelope normally required for a single function. A survey of displacement sensing technology is summarized including inductive, capacitive, optical and ultrasonic techniques. The design and operation of an experimental triple function sensor is described. Test results are included showing calibration tests and simultaneous dynamic testing of multiple functions. Recommendations for design changes are made to improve low temperature performance, reliability, and for design of a flight type signal conditioning unit.
Final Report Aerojet TechSystems Co
- Pub Date:
- July 1989
- Orbit Transfer Vehicles;
- Performance Tests;
- Instrumentation and Photography