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Fabrication of Two Engine Synchronization for Four Wheeler

An engine synchronization system for a pair of turbo jet engines in a twin jet aircraft includes a subsystem for selecting a power output, a signal generator for producing a first output signal in response to the speed of a first engine and a signal generator for producing a second output signal in response to the speed of a second engine. The system also includes a selector for selecting the fan speed or compressor speed of the engines as a control. The system incorporating an averaging device for calculating the average of the engine speeds and causing the servo driven throttle controller to retard the faster and advance the slower throttles toward the average. The engine synchronization system also includes a split shaft assembly including first and second output shafts which are disposed on a common axis. Each of the output shafts is locked to a servo motor and are free to rotate with respect to one another. The servo driven throttle control also includes a pair of sprag clutches with one of the clutches disposed between each of the shafts and a manual throttle control. The sprag clutch allows the manual throttle control to rotate about the shaft without rotating the shaft and for providing authority to the manual throttle control.