This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Solid State Proximity Switches/Logic for Aircraft Electrical System Applications
Annotation ability available
Sector:
Language:
English
Abstract
The development of solid state proximity switches, sensors, logic and self-test circuits for aircraft electrical applications has led to switching systems for actuators, thrust reversers, and integrated sensor/switch units with improved reliability, maintainability, and simplicity of application. The advantages of proximity switches over medhanical switches, design objectives, operational details, and features of the system are discussed.
Recommended Content
Technical Paper | Evolution of an Optical Control System for Aircraft Hydraulics |
Progress In Technology | The Electrification of Civil Aircraft and the Evolution of Energy Storage |
Technical Paper | Throttle Position Sensor Termination and Connector Reliability |
Authors
Citation
Gidlund, T., "Solid State Proximity Switches/Logic for Aircraft Electrical System Applications," SAE Technical Paper 700305, 1970, https://doi.org/10.4271/700305.Also In
References
- “ATA Workshop Landing Gear System,” American Airlines, Inc. May 27 1968 Sept. 13 1968
- “World's Largest Aircraft Poises for Maiden Flight,” Product Engineering Special Report June 17 1968