4820-00-033-5153 VALVE,SAFETY RELIEF Index 5990-00-033-5156 SYNCHRO,DIFFERENTIAL RECEIVER

National Stock Number:
5990-00-033-5155

Federal Supply Class:
5990

National Item Identification Number:
000335155

Description:
SYNCHRO,DIFFERENTIAL TRANSMITTER

Detail:
A SYNCHRO, THE ROTOR OF WHICH IS MECHANICALLY POSITIONED FOR MODIFYING ELECTRICAL ANGULAR INFORMATION, RECEIVED FROM A TRANSMITTER SYNCHRO AND TRANSMITTING TO RECEIVER SYNCHRO OR CONTROL TRANSFORMER SYNCHRO ELECTRICAL INFORMATION CORRESPONDING TO THE SUM OR DIFFERENCE OF THE ELECTRICAL INPUT ANGLE AND ITS ROTOR POSITION ANGLE. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, VARIABLE TRANSFORMERS, OR ITEMS WITH DIALS.


Manufacturer Information:
15-4039-0399932MOOG INC.
1JD2136-1165054WESTINGHOUSE ELECTRIC CORP POWER GENERATION-GENERATOR DIV
1JD2136-1179500WESTINGHOUSE ELECTRIC CORP
1JD2136P1179500WESTINGHOUSE ELECTRIC CORP
1JD2136PT1179500WESTINGHOUSE ELECTRIC CORP
AY2315319315HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX NAVIGATION AND CONTROL SYSTEMS
AY231S2519315HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX NAVIGATION AND CONTROL SYSTEMS
AY231S2596774HONEYWELL INTERNATIONAL INC.
AY231S319315HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX NAVIGATION AND CONTROL SYSTEMS
CP35-9-9-1L25500LOCKHEED MARTIN CORPORATION
M01026E80249BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.


Techincal Specification:
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-12.0 TO 12.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS15.00 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS7.00 CENTIMETER-GRAMS NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8750 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
BODY MATERIALALUMINUM
BODY SIZE15
BODY STYLESTANDARD ROUND B
FLANGE DIAMETER1.4370 INCHES NOMINAL
FLANGE THICKNESS0.0930 INCHES NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
OVERALL LENGTH2.1310 INCHES NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT15.00
MOUNTING SURFACE TO TERMINAL END DISTANCE1.4590 INCHES NOMINAL
PILOT DIAMETER0.5000 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
PHASE SHIFT ANGLE IN DEG35.500 INPUT TO OUTPUT NOMINAL
PLUS J ZRO REACTANCE IN OHMS200.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS14.00 NOMINAL
SHAFT DIAMETER0.1200 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0310 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0310 INCHES NOMINAL SINGLE SHAFT
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT LENGTH0.5400 INCHES NOMINAL SINGLE SHAFT
SHOULDER DIAMETER1.3120 INCHES NOMINAL
SHOULDER LENGTH0.1320 INCHES NOMINAL
STATOR DC RESISTANCE IN OHMS10.80 NOMINAL
STATOR INPUT CURRENT RATING120.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING1.3 WATTS NOMINAL
STATOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ZRO RESISTANCE IN OHMS90.00 NOMINAL
TERMINAL LOCATIONREAR
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
TRANSFORMATION RATIO0.450 ROTOR TO STATOR NOMINAL
UNDERCUT WIDTH0.0780 INCHES NOMINAL


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