NSN 5990-00-947-6879
Part Details | ELECTRICAL RESOLVER
5990-00-947-6879 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: 18437951, 1843795-1, 18437951, 1843795-1, 18437951, 1843795-1, AY080KC70A1, 18437951, 1843795-1, 5990-00-947-6879, 00-947-6879, 5990009476879, 009476879
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAR 25, 1966 | 00-947-6879 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-947-6879
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1843795-1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 1843795-1 | 08719 | DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS |
| 1843795-1 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY080KC70A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1843795-1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-947-6879
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 650.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 180.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 350.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 295.00 NOMINAL |
| TRANSFORMATION RATIO | 1.010 ROTOR TO STATOR NOMINAL |
| COMPENSATION METHOD | WINDING COMPENSATED |
| COMPENSATOR DC RESISTANCE IN OHMS | 390.00 NOMINAL |
| COMPENSATOR TRANSFORMATION RATIO IN PERCENT | 1.005 ROTOR TO COMPENSATOR MINIMUM AND 1.020 ROTOR TO COMPENSATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 17.000 INPUT TO OUTPUT NOMINAL |
| INTERAXIS ERROR ANGULAR RANGE IN MINUTES | M5.0/P5.0 |
| OUTPUT VOLTAGE FUNCTIONAL ERROR RANGE IN PERCENT | M0.1/P0.1 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.10 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.7530 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6870 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.3160 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 10 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |
