Second Generation Smart Actuator
932585
09/01/1993
- Event
- Content
- An actuator has been developed and qualified with all loop-closure and redundancy management functions covered by an electronic package physically located on the actuator manifold assembly. The actuator meets or exceeds all Original Equipment Manufacturer (OEM) requirements of the F/A-18 aileron servocylinder design with the single restriction of 99 °C (210 °F) maximum oil temperature. While the actuator has performed well at temperatures in excess of 135 °C (275 °F), present MIL-SPEC derating for electronics limit the allowable operating range. The basic design offers potential advantages in the areas of weight, maintainability, self-diagnostics, and ease of integration.
- Pages
- 11
- Citation
- Deller, R., "Second Generation Smart Actuator," SAE Technical Paper 932585, 1993, https://doi.org/10.4271/932585.