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
71569041NZ85EMCORE SPACE & NAVIGATION CORPORATION
5990PL01923329009HINSPEKTORAT WSPARCIA SIL ZBROJNYCH
507278-196214RAYTHEON COMPANY
68C4000997151AIR FORCE LIFECYCLE MANAGEMENT CENTER ELECTRONIC COMPONENTS (AFLCMC/EZSS)
CL4090200209301KEARFOTT CORP SOMA FORWARDING DIV
7156904-11NZ85EMCORE SPACE & NAVIGATION CORPORATION
CL4090200288818KEARFOTT CORPORATION


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


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