NSN 5990-00-295-8235
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-295-8235 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: 7856712, 785671-2, 785671REVADPT2, 785671REVADPT2, 7856712, 785671-2, 5990-00-295-8235, 00-295-8235, 5990002958235, 002958235
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-295-8235 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-295-8235
Part Number | Cage Code | Manufacturer |
---|---|---|
785671-2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
785671REVADPT2 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
785671REVADPT2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
785671-2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-295-8235
Characteristic | Specifications |
---|---|
BODY SIZE | 15 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
STATOR INPUT CURRENT RATING | 650.0 MILLIAMPERES NOMINAL |
STATOR INPUT ELECTRICAL POWER RATING | 330.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZSO RESISTANCE IN OHMS | 18.30 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 85.00 NOMINAL |
TRANSFORMATION RATIO | 1.600 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 7.000 INPUT TO OUTPUT NOMINAL |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
BODY STYLE | STANDARD ROUND B |
SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 2.4310 INCHES NOMINAL |
FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
PILOT LENGTH | 0.0400 INCHES NOMINAL |
SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5910 INCHES NOMINAL |
ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
ALIGNMENT HOLE QUANTITY | 4 |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, STAINLESS |
FRAGILITY FACTOR | MODERATELY RUGGED |