5990-00-115-5850 SYNCHRO,CONTROL TRANSFORMER Index 6680-00-115-5852 COUNTER,ELECTRICAL

National Stock Number:
5990-00-115-5851

Federal Supply Class:
5990

National Item Identification Number:
001155851

Description:
SYNCHRO,CONTROL TRANSFORMER

Detail:
A SYNCHRO CONSISTING OF A STATOR AND ROTOR INDUCTIVELY COUPLED. THE ELECTRICAL OUTPUT OF THE ROTOR IS DEPENDENT UPON BOTH THE POSITION OF THE ROTOR AND THE ELECTRICAL INPUT TO THE STATOR FROM A TRANSMITTER SYNCHRO OR A DIFFERENTIAL SYNCHRO. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, OR VARIABLE TRANSFORMERS.


Manufacturer Information:
10CT-302-E-36/1006989API HAROWE INC DBA API MOTION DIV API MOTION/PMI/API HAROWE
5513999479BOWMAR LLC
7901521-293322GE AVIATION SYSTEMS LLC DBA GE AVIATION
AY100UY-59-A664547HONEYWELL INTERNATIONAL, INC
AY100UY-59-A683298ALLIED SIGNAL INC AEROSPACE EQUIPMENT SYSTEMS EATONTOWN SITE
ETH-10-CKS-004/A00499932MOOG INC.


Techincal Specification:
STATOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
STATOR INPUT CURRENT RATING12.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING80.0 MILLIWATTS NOMINAL
TERMINAL TYPE AND QUANTITY5 SCREW
BODY STYLESTANDARD ROUND C
FREQUENCY IN HERTZ400.0 NOMINAL
BODY SIZE10
ZRO RESISTANCE IN OHMS595.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS2130.00 NOMINAL
ZSO RESISTANCE IN OHMS126.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS427.00 NOMINAL
ZRS RESISTANCE IN OHMS750.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS369.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS410.00 NOMINAL
STATOR DC RESISTANCE IN OHMS126.00 NOMINAL
PHASE SHIFT ANGLE IN DEG11.000 INPUT TO OUTPUT NOMINAL
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-10.0 TO 10.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS20.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS4.0 CENTIMETER-GRAMS NOMINAL
SHOULDER DIAMETER0.8123 INCHES MAXIMUM
PILOT DIAMETER0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6540 INCHES NOMINAL
FLANGE DIAMETER0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.8370 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0630 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES NOMINAL
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT DIAMETER0.0900 INCHES MAXIMUM SINGLE SHAFT
SHAFT LENGTH0.3750 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0250 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0200 INCHES NOMINAL SINGLE SHAFT
TERMINAL LOCATIONREAR
BODY MATERIALSTEEL, CORROSION RESISTING
SHAFT MAXIMUM RADIAL PLAY0.0008 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES NOMINAL
SHAFT RADIAL PLAY DETERMINING WEIGHT1.411 OUNCES
SHAFT END PLAY0.0003 INCHES MINIMUM AND
0.0015 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT3.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR1 Y-ROTOR, 1 STATOR
FRAGILITY FACTORMODERATELY RUGGED


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