NSN 5990-00-140-4559
Part Details | TRANSMITTER SYNCHRO
5990-00-140-4559 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 7202122, 5990-00-140-4559, 00-140-4559, 5990001404559, 001404559
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | SEP 10, 1971 | 00-140-4559 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-140-4559
Part Number | Cage Code | Manufacturer |
---|---|---|
7202122 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
Technical Data | NSN 5990-00-140-4559
Characteristic | Specifications |
---|---|
BODY SIZE | 10 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 130.0 MILLIAMPERES MAXIMUM |
ROTOR INPUT ELECTRICAL POWER RATING | 340.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO IMPEDANCE MAGNITUDE IN OHMS | 200.00 MINIMUM AND 300.00 MAXIMUM |
ZRO IMPEDANCE ANGLE IN DEG | 80.50 MINIMUM AND 84.00 MAXIMUM |
ZSS IMPEDANCE MAGNITUDE IN OHMS | 6.00 MINIMUM AND 12.00 MAXIMUM |
ZSS IMPEDANCE ANGLE IN DEG | 18.00 MINIMUM AND 30.00 MAXIMUM |
TRANSFORMATION RATIO | 0.445 ROTOR TO STATOR MINIMUM AND 0.463 ROTOR TO STATOR MAXIMUM |
PHASE SHIFT ANGLE IN DEG | 2.500 INPUT TO OUTPUT MINIMUM AND 5.500 INPUT TO OUTPUT MAXIMUM |
MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 12.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 19.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M3.0/P3.0 |
BODY STYLE | STANDARD ROUND B |
SHOULDER DIAMETER | 0.9950 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
OVERALL LENGTH | 2.3580 INCHES NOMINAL |
FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0620 INCHES NOMINAL |
SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7320 INCHES NOMINAL |
ALIGNMENT HOLE QUANTITY | 4 |
TERMINAL TYPE AND QUANTITY | 5 SCREW |
TERMINAL LOCATION | REAR |
BODY MATERIAL | ANY ACCEPTABLE |