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CURRENT MONITORING PULSED DC CONTROLLER, BRINGS TOGETHER POWERFUL LONG-RANGE IONISATION; CLOSED-LOOP FEEDBACK; SELF-MONITORING AND REMOTE REPORTING. A COMPLETE PACKAGE, SELF-MONITORING AND ADJUSTMENT OF PERFORMANCE ALLOWS OPTIMUM CONTROL OF STATIC FOR MUCH LONGER PERIODS THAN PREVIOUSLY POSSIBLE. LOCAL DISPLAY AND OUTPUT SIGNALS ALERT OPERATORS TO THE NEED TO CLEAN THE EQUIPMENT.

A HYDROMECHANICAL UNIT (HMU), A COMPONENT OF AN AIRCRAFT ENGINE SYSTEM. THE HMU RESPONDS TO ELECTRICAL SIGNALS FROM AN EEC TO METER ENGINE FUEL FLOW AND MODULATE MOTIVE FLOW TO SIX EXTERNAL HYDRAULIC SYSTEMS. A COMPONENT IN THE HMU CAUSES SERVO POSITIONING OF THE UNIT MV. THE MV POSITION ESTABLISHES THE PROPER METERED FUEL DELIVERY ORIFICE FOR THE COMMANDED FUEL FLOW. A MECHANICAL OVERSPEED GOVERNOR SWITCH LIMITS ENGINE SPEED TO 106 PERCENT MAXIMUM.

A VEHICLE DYNAMIC CONTROL . IT IS A DRIVER / VEHICLE AID TO CONTROL AND ASSIST THE DRIVER TO SAFELY CONTROL THE VEHICLE IN A STABLE AND OPTIMISED CONDITION. IT MONITORS DRIVER INPUT AND CONDITIONS EFFECTING THE VEHICLE BY MEANS OF ELECTRICAL CIRCUITS AND SENSORS, MAKING ADJUSTMENTS AND APPLYING THE BRAKES DURING MANOEUVRES THAT ENDANGER THE SAFETY OF THE DRIVER AND VEHICLE. IT MANAGES STABILITY BY CONTROLLING BRAKE PRESSURE AND TORQUES FROM ITS POWER SOURCE BY DETECTING YAW RATE ACCELERATION, STEERING ANGLE AND WHEEL SPEED.THE CONTROL UNIT DETERMINES THE VEHICLES CONDITION BY SENSING THE OUTPUT FROM THE SENSOR SIGNAL. AN AMOUNT OF CAREFULLY CALCULATED BRAKE PRESSURE IS AUTOMATICALLY APPLIED TO INDIVIDUAL WHEELS TO CORRECT THE VEHICLES BEHAVOIUR FROM AN OVERSTEER OR UNDERSTEER SITUATION AND ALSO MODERATES THE BRAKE PRESSURE TO PREVENT WHEEL SKIDDING AND THE TORQUE FROM THE POWER SOURCE TO RECOVER THE LOSS OF TRACTION. COMPRISES OF VALVES, CIRCUIT BOARD, AND PART OF THE VEHICLES BRAKE FLUID.IT IS MADE FROM STEELS AND ALUMINIUM AND ELECTRICAL COMPONENTS. IT HAS THREE BASIC FUNCTIONS, ABS PREVENTING THE WHEEL LOCK AND UNCONTROLLED SKIDDING, TCS OPTIMISE GRIP AND STABILITY DURING ACCELERATION, VDC PREVENTING UNSTABLE BEHAVIOUR AND LOSS OF STEERING CONTROL. ADDITIONAL FUNCTIONS, HSA PREVENTING ROLL BACK IN THE CASE OF HILL STARTS., HDC PREVENTING UNSTABLE BEHAVIOUR BY WHEEL LOCK OR INSUFFICIENT ENGINE - DRAG IN CASE OF DOWN HILL.

IGBT GATE DRIVER ASSEMBLY PN 51020195 IS PART OF STARTER GENERATOR CONTROL UNIT THAT CONTROLS THE OPERATION OF THE STARTER GENERATOR SYSTEM. FOR USE IN AIRCRAFT.

A PLASTIC FLOAT SWITCH.FOR SENSING WATER LEVELS. IT IS DESIGNED TO BE MOUNTED THROUGH THE WALL OF A TANK. THE SWITCH CAN BE FITTED TO ACHIEVE EITHER MAKE ON RISE (N/O) OR MAKE ON FALL (N/C) ACTION BY SIMPLY ROTATING THROUGH 180 DEGREES