NSN 5990-00-106-6608

Part Details | ELECTRICAL RESOLVER


5990-00-106-6608 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: 6807630111, 68076-301-11, 4660072001, 466-0072-001, 4660072001, 466-0072-001, 38PX1, 5990-00-106-6608, 00-106-6608, 5990001066608, 001066608

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUL 17, 196800-106-660822966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A


Cross Reference | NSN 5990-00-106-6608
Part Number Cage Code Manufacturer
68076-301-1194756BOEING COMPANY, THEDBA BOEING
466-0072-00194756BOEING COMPANY, THEDBA BOEING
466-0072-00108719DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS
38PX108719DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS

Technical Data | NSN 5990-00-106-6608
Characteristic Specifications
STATOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
BODY STYLE3 STANDARD ROUND A
TERMINAL LOCATION REAR
BODY MATERIAL ANY ACCEPTABLE
SUPPLEMENTARY FEATURESTWO-TANDEM MOUNTED PANCAKE-TYPE RESOLVER
FRAGILITY FACTOR MODERATELY RUGGED
FUNCTIONAL DESCRIPTIONUSED TO TRANSMIT ANGLE BTWN STABLE PLATFORM AND AIRCRAFT REFERENCE LINE; FORMS PART OF STRUCTURE FOR PLATFORMGIMBAL ASSY
END ITEM IDENTIFICATION6605010453894BJ INERTIAL REFERENCE UNIT
FSC APPLICATION DATA5990-00-138-6775,SYNCHRO ASSY,P/N 4660072-001