Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-072-5450 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: 09CT1247, 13764001, 137640-01, 5990-00-072-5450, 00-072-5450, 5990000725450, 000725450
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-072-5450 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-072-5450
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 09CT1247 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 137640-01 | 35351 | GE AVIATION SYSTEMS LLC |
Technical Data | NSN 5990-00-072-5450
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 40.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 100.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 446.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1887.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 79.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 350.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 548.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 182.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 316.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 67.00 NOMINAL |
| TRANSFORMATION RATIO | 2.159 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 6.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 5.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 20.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 30.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | 2 STANDARD ROUND A |
| SHOULDER DIAMETER | 0.6950 INCHES MINIMUM AND 0.7050 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 3.1830 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.9100 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.7360 INCHES MINIMUM AND 0.7460 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
| PILOT LENGTH | 0.0380 INCHES MINIMUM AND 0.0480 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.0000 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0020 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0020 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |