NSN 5990-00-644-0076
Part Details | ELECTRICAL RESOLVER
5990-00-644-0076 An item consisting of a rotor and a stator inductively coupled. It usually has two rotor windings displaced from each other by 90 degrees and two stator windings similarly displaced. The output voltage(s) is a trigonometric function of the input voltage(s) and the angular displacement of the rotor with respect to the stator. See also SYNCHRO (as modified) and GONIOMETER, ELECTRICAL. Excludes TRANSOLVER, ELECTRICAL and potentiometer sine/cosine electrical resolvers.
Alternate Parts: 0D10101, VRA234110A, VRA23-41-10A, 12Z1301060, 12Z13010-60, 13320, 13-320, 113D8H, 5990-00-644-0076, 00-644-0076, 5990006440076, 006440076
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-644-0076 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-644-0076
Part Number | Cage Code | Manufacturer |
---|---|---|
0D10101 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
VRA23-41-10A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
12Z13010-60 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
13-320 | 97497 | UNITED AIRCRAFT CORPNORDEN DIVISION KETAY DEPT |
113D8H | 97497 | UNITED AIRCRAFT CORPNORDEN DIVISION KETAY DEPT |
Technical Data | NSN 5990-00-644-0076
Characteristic | Specifications |
---|---|
BODY SIZE | 23 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 30.0 MAXIMUM |
FREQUENCY IN HERTZ | 1000.0 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 1.80 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 2.60 NOMINAL |
TRANSFORMATION RATIO | 0.090 ROTOR TO STATOR NOMINAL |
COMPENSATION METHOD | WINDING COMPENSATED |
COMPENSATOR DC RESISTANCE IN OHMS | 5.80 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 1.900 INPUT TO OUTPUT NOMINAL |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 20.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
BODY STYLE | STANDARD ROUND D |
SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
PILOT DIAMETER | 0.5990 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM |
SECOND SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
SECOND SHOULDER LENGTH | 0.1700 INCHES MAXIMUM |
OVERALL LENGTH | 4.7360 INCHES MINIMUM AND 4.7870 INCHES MAXIMUM |
FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
FLANGE THICKNESS | 0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM |
BODY DIAMETER | 0.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
PILOT LENGTH | 0.0460 INCHES NOMINAL |
SHOULDER LENGTH | 0.2420 INCHES MINIMUM AND 0.2520 INCHES MAXIMUM |
AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.9230 INCHES MINIMUM AND 3.9380 INCHES MAXIMUM |
TERMINAL TYPE AND QUANTITY | 8 SCREW |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |