5930-00-073-1759 SWITCH,ELECTRONIC Index 5935-00-073-1763 CONNECTOR,RECEPTACLE,ELECTRICAL

National Stock Number:
5990-00-073-1760

Federal Supply Class:
5990

National Item Identification Number:
000731760

Description:
TRANSOLVER,ELECTRICAL

Detail:
AN ITEM CONSISTING OF A ROTOR AND A STATOR INDUCTIVELY COUPLED. IT HAS WYE CONNECTED AND QUADRATURE WINDINGS, EITHER OF WHICH CAN BE STATOR OR THE ROTOR AND SERVE AS THE PRIMARY FOR INPUT VOLTAGES. THE OUTPUT VOLTAGES ARE TRIGONOMETRIC FUNCTIONS OF THE INPUT VOLTAGES AND THE ANGULAR DISPLACEMENT OF THE ROTOR WITH RESPECT TO THE STATOR. SEE ALSO SYNCHRO (AS MODIFIED). EXCLUDES RESOLVER, ELECTRICAL AND POTENTIOMETER SINE/COSINE ELECTRICAL RESOLVERS.


Manufacturer Information:
10CRD100B106989API HAROWE INC DBA API MOTION DIV API MOTION/PMI/API HAROWE
137702-0135351GE AVIATION SYSTEMS LLC
507278-196214RAYTHEON COMPANY
5990PL01923329009HINSPEKTORAT WSPARCIA SIL ZBROJNYCH
68C4000997151AIR FORCE LIFECYCLE MANAGEMENT CENTER ELECTRONIC COMPONENTS (AFLCMC/EZSS)
71569041NZ85EMCORE SPACE & NAVIGATION CORPORATION
7156904-11NZ85EMCORE SPACE & NAVIGATION CORPORATION
CL4090200209301KEARFOTT CORP SOMA FORWARDING DIV
CL4090200288818KEARFOTT CORPORATION


Techincal Specification:
BODY SIZE10
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING42.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING103.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS85.40 NOMINAL
PLUS J ZRO REACTANCE IN OHMS281.00 NOMINAL
ZSO RESISTANCE IN OHMS77.60 NOMINAL
PLUS J ZSO REACTANCE IN OHMS363.00 NOMINAL
ZRS RESISTANCE IN OHMS84.30 NOMINAL
PLUS J ZRS REACTANCE IN OHMS31.10 NOMINAL
ROTOR DC RESISTANCE IN OHMS75.50 NOMINAL
STATOR DC RESISTANCE IN OHMS41.00 NOMINAL
TRANSFORMATION RATIO1.041 STATOR TO ROTOR NOMINAL
PHASE SHIFT ANGLE IN DEG10.800 OUTPUT TO INPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-7.0 TO 7.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS6.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS NOMINAL
BODY STYLESTANDARD ROUND C
SHOULDER DIAMETER1.0000 INCHES NOMINAL
PILOT DIAMETER0.5000 INCHES NOMINAL
OVERALL LENGTH1.6280 INCHES MAXIMUM
FLANGE DIAMETER0.9370 INCHES NOMINAL
FLANGE THICKNESS0.1250 INCHES NOMINAL
UNDERCUT DIAMETER0.8123 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.1000 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6780 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY3
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT DIAMETER0.0900 INCHES NOMINAL SINGLE SHAFT
SHAFT LENGTH0.4130 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0300 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0200 INCHES NOMINAL SINGLE SHAFT
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATIONREAR
BODY MATERIALSTEEL, CORROSION RESISTING
SPECIAL FEATURESRESOLVER IS CRITICAL FOR FIT FORM AND FUNCTION TOLERANCE AND APPLICATION FOR THE AMPLIFIER POWER SUPPLY FOR THE E-3 AIRCRAFT
CRITICALITY CODE JUSTIFICATIONFEAT
FRAGILITY FACTORMODERATELY RUGGED


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