1615-00-120-1189 BRACKET,ROTOR BRAKE Index 5990-00-120-1192 SYNCHRO,DIFFERENTIAL RECEIVER

National Stock Number:
5990-00-120-1191

Federal Supply Class:
5990

National Item Identification Number:
001201191

Description:
RESOLVER,ELECTRICAL,LINEAR

Detail:
AN ITEM CONSISTING OF A STATOR AND ROTOR INDUCTIVELY COUPLED WHICH PROVIDES ACCURATE LINEAR INDICATION OF SHAFT ROTATION ABOUT A REFERENCE POSITION IN THE FORM OF A POLARIZED VOLTAGE WHOSE MAGNITUDE IS PROPORTIONAL TO ANGULAR DISPLACEMENT AND PHASE RELATIONSHIP INDICATES DIRECTION OF SHAFT ROTATION. ITS WINDINGS AND SLOTS ARE NOT UNIFORMLY DISTRIBUTED, BUT INSTEAD ARE DELIBERATELY MODIFIED TO PRODUCE A LINEAR OUTPUT WHICH IS USUALLY LIMITED TO LESS THAN PLUS OR MINUS 90 DEGREES OF EFFECTIVE ELECTRICAL TRAVEL. NORMALLY IT HAS ONLY ONE ENERGIZATION WINDING AND ONE OUTPUT WINDING. SEE ALSO RESOLVER, ELECTRICAL.


Manufacturer Information:
101P304-D27A06989AMERICAN PRECISION INDUSTRIES, INC
790141593322GE AVIATION SYSTEMS LLC DBA GE AVIATION
8002921W820PATRIOT AMERICAN SOLUTIONS LLC
800292-11W820PATRIOT AMERICAN SOLUTIONS LLC


Techincal Specification:
BODY SIZE10
BODY STYLESTANDARD ROUND A
FLANGE DIAMETER0.9370 INCHES NOMINAL
FLANGE THICKNESS0.0620 INCHES NOMINAL
FRAGILITY FACTORMODERATELY RUGGED
FREQUENCY IN HERTZ400.0 NOMINAL
LINEARITY IN PERCENT1.00
OVERALL LENGTH3.6430 INCHES MAXIMUM
MATERIALSTEEL CORROSION RESISTING BODY
MAXIMUM LINEAR RANGE IN DEG-60.0 TO 60.0
MOUNTING SURFACE TO TERMINAL END DISTANCE2.9040 INCHES MAXIMUM
PILOT DIAMETER0.6875 INCHES MAXIMUM
PILOT LENGTH0.0380 INCHES NOMINAL
PHASE SHIFT ANGLE IN DEG5.000 INPUT TO OUTPUT MINIMUM
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
SCHEMATIC DIAGRAM DESIGNATOR1 ROTOR, 1 STATOR
SHAFT END PLAY0.0020 INCHES MAXIMUM
SHAFT DIAMETER0.1248 INCHES MAXIMUM SINGLE SHAFT
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SHAFT LENGTH0.6810 INCHES NOMINAL SINGLE SHAFT
SHAFT TYPEROUND SINGLE SHAFT
SPECIAL FEATURESMAGNETIC CLUTCH
TERMINAL LOCATIONREAR AND SIDE
TERMINAL TYPE AND QUANTITY6 TURRET
TRANSFORMATION RATIO0.923 STATOR TO ROTOR MINIMUM
UNDERCUT DIAMETER0.8370 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL


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