NSN 5990-01-087-6466
Part Details | ELECTRICAL RESOLVER
5990-01-087-6466 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: 16333901, 163339-01, 5990-01-087-6466, 01-087-6466, 5990010876466, 010876466
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | DEC 21, 1979 | 01-087-6466 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
2 ROTOR, 1 STATOR
Cross Reference | NSN 5990-01-087-6466
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 163339-01 | 35351 | GE AVIATION SYSTEMS LLC |
Technical Data | NSN 5990-01-087-6466
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 0.5 MINIMUM AND 57.5 MAXIMUM |
| ROTOR INPUT CURRENT RATING | 33.8 MILLIAMPERES MAXIMUM |
| FREQUENCY IN HERTZ | 1600.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 405.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1852.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 112.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 460.00 NOMINAL |
| ZSS RESISTANCE IN OHMS | 30.50 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 4.50 NOMINAL |
| TRANSFORMATION RATIO | 0.488 ROTOR TO STATOR NOMINAL |
| TRANSFORMATION RATIO EQUALITY IN PERCENT | 0.5 NOMINAL |
| MAXIMUM TEMP RISE | 125.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 80.00 INPUT |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9800 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.0550 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0610 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0450 INCHES MINIMUM |
| PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6000 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 8 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.120 INCHES NOMINAL |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SCHEMATIC DIAGRAM DESIGNATOR | 2 2 ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
