Part Details | RECEIVER SYNCHRO
5990-01-134-7756 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 17706001, 17706-001, TRH11RCBS2, TRH-11-RCBS-2, TRH11RCBS2, TRH-11-RCBS-2, TRH11RCBS2F219, TRH-11-RCBS-2/F219, 5990-01-134-7756, 01-134-7756, 5990011347756, 011347756
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 09, 1982 | 01-134-7756 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-01-134-7756
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17706-001 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| TRH-11-RCBS-2 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TRH-11-RCBS-2 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TRH-11-RCBS-2/F219 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-01-134-7756
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 90.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 280.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 35.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 288.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 8.10 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 47.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 49.50 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 24.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 18.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.50 NOMINAL |
| TRANSFORMATION RATIO | 0.454 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 3.800 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M30.0/P30.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 7000.0 MILLIMETER-MILLIGRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3500.0 MILLIMETER-MILLIGRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2400.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1770 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6000 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0700 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0020 INCHES MINIMUM AND 0.0050 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
| END ITEM IDENTIFICATION | ID663/ARN |