5960-00-504-8790 SHIELD,ELECTRON TUBE Index 5990-00-504-8797 RESOLVER,ELECTRICAL

National Stock Number:
5990-00-504-8795

Federal Supply Class:
5990

National Item Identification Number:
005048795

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:
791436-1555972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
791436-1596774HONEYWELL INTERNATIONAL INC.
AY221S5B55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
AY221S5B96774HONEYWELL INTERNATIONAL INC.
AYS221S5B55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS


Techincal Specification:
FREQUENCY IN HERTZ30.0 NOMINAL
TERMINAL TYPE AND QUANTITY7 WIRE LEAD
BODY STYLESTANDARD ROUND B
BODY SIZE15
ROTOR INPUT VOLTAGE RATING IN VOLTS1.0 NOMINAL
ROTOR INPUT CURRENT RATING2.5 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING2.2 MILLIWATTS NOMINAL
ZRO RESISTANCE IN OHMS396.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS146.00 NOMINAL
ZSO RESISTANCE IN OHMS174.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS84.30 NOMINAL
ZRS RESISTANCE IN OHMS435.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS125.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS400.00 NOMINAL
STATOR DC RESISTANCE IN OHMS175.00 NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT5.00 INPUT
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-20.0 TO 20.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS15.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS5.0 CENTIMETER-GRAMS NOMINAL
SHOULDER DIAMETER1.3115 INCHES MINIMUM AND
1.3120 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND
0.5000 INCHES MAXIMUM
OVERALL LENGTH2.1310 INCHES NOMINAL
FLANGE DIAMETER1.4360 INCHES MINIMUM AND
1.4370 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT WIDTH0.0680 INCHES MINIMUM AND
0.0880 INCHES MAXIMUM
PILOT LENGTH0.0400 INCHES NOMINAL
SHOULDER LENGTH0.1320 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.4590 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT DIAMETER0.1195 INCHES MINIMUM AND
0.1200 INCHES MAXIMUM SINGLE SHAFT
SHAFT LENGTH0.5000 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0210 INCHES MINIMUM AND
0.0310 INCHES MAXIMUM SINGLE SHAFT
SHAFT SLOT WIDTH0.0210 INCHES MINIMUM AND
0.0310 INCHES MAXIMUM SINGLE SHAFT
TERMINAL LOCATIONREAR
BODY MATERIALALUMINUM
SHAFT MAXIMUM RADIAL PLAY0.0010 INCHES
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0003 INCHES MINIMUM AND
0.0015 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR1 T-ROTOR, 2 STATOR
FRAGILITY FACTORMODERATELY RUGGED
THE MANUFACTURERS DATA
MANUFACTURERS CODE96774
DESIGN CONTROL REFERENCEAY221S5B


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