NSN 5990-01-093-8328
Part Details | TRANSMITTER SYNCHRO
5990-01-093-8328 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 31CX4A, CX314N1, CX31-4N1, 5990-01-093-8328, 01-093-8328, 5990010938328, 010938328
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | APR 25, 1980 | 01-093-8328 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-01-093-8328
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 31CX4A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| CX31-4N1 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
Technical Data | NSN 5990-01-093-8328
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 31 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 950.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 8.3 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 121.00 MINIMUM AND 166.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 82.00 MINIMUM AND 87.00 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 3.40 MINIMUM AND 5.90 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 51.00 MINIMUM AND 72.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 1.500 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 35.00 INPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 100.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M8.0/P8.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.50 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 2.7000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5950 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 2.7500 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.3750 INCHES NOMINAL |
| OVERALL LENGTH | 5.1150 INCHES MAXIMUM |
| FLANGE DIAMETER | 3.1000 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 2.7000 INCHES MAXIMUM |
| PILOT LENGTH | 0.0300 INCHES NOMINAL |
| SHOULDER LENGTH | 0.3750 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 2.7500 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.3800 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 16.0 OUNCES |
| SHAFT END PLAY | 0.0030 INCHES NOMINAL |
| SHAFT END PLAY DETERMINING WEIGHT | 16.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0008 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
