4910-00-124-2554 ANALYZER SET,ENGINE Index 4920-00-124-2560 TEST SET,CONTROL

National Stock Number:
5990-00-124-2556

Federal Supply Class:
5990

National Item Identification Number:
001242556

Description:
RESOLVER,ELECTRICAL

Detail:
An item consisting of a rotor and a stator inductively coupled. It usually has two rotor windings displaced from each other by 90 degrees and two stator windings similarly displaced. The output voltage(s) is a trigonometric function of the input voltage(s) and the angular displacement of the rotor with respect to the stator. See also SYNCHRO (as modified) and GONIOMETER, ELECTRICAL. Excludes TRANSOLVER, ELECTRICAL and potentiometer sine/cosine electrical resolvers.


Manufacturer Information:
080V3408A/L65899932MOOG INC.
5517499479BOWMAR LLC
905050-305257GENERAL DYNAMICS LAND SYSTEMS - CANADA CORPORATION
AY084KJ111A155972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS


Techincal Specification:
OVERALL LENGTH1.4350 INCHES MAXIMUM
FLANGE DIAMETER0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6910 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.0150 INCHES MAXIMUM
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT DIAMETER0.0900 INCHES MAXIMUM SINGLE SHAFT
SHAFT LENGTH0.3530 INCHES MAXIMUM SINGLE SHAFT
SHAFT SLOT DEPTH0.0250 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0250 INCHES NOMINAL SINGLE SHAFT
TERMINAL LOCATIONREAR
BODY MATERIALSTEEL, CORROSION RESISTING
SHAFT MAXIMUM RADIAL PLAY0.0005 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES MAXIMUM
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0003 INCHES MINIMUM AND
0.0008 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT8.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR2 ROTOR, 1 STATOR
TERMINAL DESIGNATOR AND SCHEMATIC POSITIONCONNECTION R1 POSITION A AND
CONNECTION R2 POSITION B AND
CONNECTION S1 POSITION H AND
CONNECTION S2 POSITION F AND
CONNECTION S3 POSITION J AND
CONNECTION S4 POSITION E
FRAGILITY FACTORMODERATELY RUGGED
FREQUENCY IN HERTZ400.0 NOMINAL
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
BODY STYLESTANDARD ROUND A
BODY SIZE8
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING66.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING416.0 MILLIWATTS NOMINAL
ZRO RESISTANCE IN OHMS158.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS490.00 NOMINAL
ZSO RESISTANCE IN OHMS44.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS150.00 NOMINAL
ZRS RESISTANCE IN OHMS263.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS75.50 NOMINAL
ROTOR DC RESISTANCE IN OHMS133.00 NOMINAL
STATOR DC RESISTANCE IN OHMS36.30 NOMINAL
PHASE SHIFT ANGLE IN DEG15.000 INPUT TO OUTPUT 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 CELSIUS16.0 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS4.0 CENTIMETER-GRAMS MAXIMUM
PILOT DIAMETER0.5000 INCHES MAXIMUM


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