NSN 5990-00-007-7833
Part Details | ELECTRICAL RESOLVER
5990-00-007-7833 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.
Alternate Parts: AY523G47A2, 5990-00-007-7833, 00-007-7833, 5990000077833, 000077833
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 12, 1972 | 00-007-7833 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
2 ROTOR, 2 STATOR
Cross Reference | NSN 5990-00-007-7833
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY523G47A2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-007-7833
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 5.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 2.8 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 3.6 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSO RESISTANCE IN OHMS | 457.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 1727.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 364.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 304.00 NOMINAL |
| TRANSFORMATION RATIO | 0.767 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 10.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 40.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M30.0/P30.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 30.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 10.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6540 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0625 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0625 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0625 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0781 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6750 INCHES MINIMUM AND 0.6810 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 7 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 1.4 OUNCES |
| SHAFT END PLAY | 0.0001 INCHES MINIMUM AND 0.0005 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 3.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 3 2 ROTOR, 2 STATOR |
| TERMINAL DESIGNATOR AND SCHEMATIC POSITION | CONNECTION R1 POSITION A AND CONNECTION R2 POSITION B AND CONNECTION R3 POSITION C AND CONNECTION S1 POSITION H AND CONNECTION S2 POSITION E AND CONNECTION S3 POSITION J AND CONNECTION S4 POSITION F |
| FRAGILITY FACTOR | MODERATELY RUGGED |