NSN 5990-01-107-8682
Part Details | ELECTRICAL TRANSOLVER
5990-01-107-8682 An item consisting of a rotor and a stator inductively coupled. It has wye connected and quadrature windings, either of which can be stator or the rotor and serve as the Primary for input voltages. The output voltages are trigonometric functions of the input voltages and the angular displacement of the rotor with respect to the stator. See also SYNCHRO (as modified). Excludes RESOLVER, ELECTRICAL and potentiometer sine/cosine electrical resolvers.
Alternate Parts: 145730, CM41005009, 5990-01-107-8682, 01-107-8682, 5990011078682, 011078682
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | FEB 14, 1981 | 01-107-8682 | 33272 ( TRANSOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-01-107-8682
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 145730 | 35351 | GE AVIATION SYSTEMS LLC |
| CM41005009 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
Technical Data | NSN 5990-01-107-8682
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| ROTOR INPUT CURRENT RATING | 43.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 120.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 800.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 72.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 270.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 82.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 342.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 81.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 27.00 NOMINAL |
| ZSS RESISTANCE IN OHMS | 101.00 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 37.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 61.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 49.50 NOMINAL |
| TRANSFORMATION RATIO | 1.022 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 10.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 5.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 9.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.7460 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 7 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.250 INCHES MAXIMUM |
| 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 |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |
