Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-162-6080 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 8CD300B1, 8CD-300-B-1, CM01044707, CM01044707, CM0-1044-707, CDH8A2, CDH-8-A-2, CDH8A2, CDH-8-A-2, 2076431, 207643-1, 5990-00-162-6080, 00-162-6080, 5990001626080, 001626080
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | AUG 21, 1972 | 00-162-6080 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
1 Y-ROTOR, 1 Y-STATOR
Cross Reference | NSN 5990-00-162-6080
Part Number | Cage Code | Manufacturer |
---|---|---|
8CD-300-B-1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
CM01044707 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
CM0-1044-707 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
CDH-8-A-2 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
CDH-8-A-2 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
207643-1 | 1W820 | PATRIOT AMERICAN SOLUTIONS LLC |
Technical Data | NSN 5990-00-162-6080
Characteristic | Specifications |
---|---|
BODY SIZE | 8 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
STATOR INPUT CURRENT RATING | 33.0 MILLIAMPERES NOMINAL |
STATOR INPUT ELECTRICAL POWER RATING | 73.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 109.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 362.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 81.00 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 330.00 NOMINAL |
ZRS RESISTANCE IN OHMS | 120.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 35.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 98.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 64.00 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
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 | 6.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
BODY STYLE | STANDARD ROUND A |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.6010 INCHES MINIMUM AND 1.6310 INCHES MAXIMUM |
FLANGE DIAMETER | 0.7600 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0370 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, STAINLESS |
SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
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 |
SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 Y-STATOR |
FRAGILITY FACTOR | MODERATELY RUGGED |