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HomeNSNInstruments and Laboratory EquipmentAutomatic Pilot Mechanisms and Airborne Gyro Components871137-1 NSN 6615-01-354-9253 - 607be89a

871137-1 NSN 6615-01-354-9253 - 607be89a

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NSN 6615-01-354-9253 - (6615013549253) Technical Details :

MRCNameDetails
ACDCCURRENT TYPEAC/DC
AGBCSHOCK MOUNTNOT PROVIDED
APGFDESIGN TYPENONCAGEABLE
APQBIII UNIT TYPEDIRECTIONAL
APQBUNIT TYPEDIRECTIONAL
BBWDWHEEL POWER METHODELECTRIC
BBWFFREEDOM AXIS QUANTITY2
BBWGGIMBAL QUANTITY2
BBWHAXIS DISPLACEMENT LIMITATION IN DEGNON-G-SENSITIVE DRIFT NOT TO EXCEED 25 DEG/R AND G-SENSITIVE DRIFT SHALL BE 10 DEG/HR/G MAXIMUM ABOUT THE INPUT AXIS WITHIN THE PLANE
BBWJGIMBAL TORQUE APPLICATION METHODAC TORQUE MOTOR
BBWKTORQUED GIMBAL QUANTITY2
BBWLSENSING OUTPUT/SIGNAL LEVEL METHODSINGLE X AND Y PICKOFF FROM A POSITIVE AND A NEGATIVE COMPARATOR AND PICKOFF EXCITATION THRU A TRANSFORMER
BBWMTEMP CONTROL METHODEXTERNALLY APPLIED
BBWNINSTRUMENT TYPEUNFLOATED
FAAZPHASETWO
FEATSPECIAL FEATURES"GGYRO IS A 2 DEG OF FREEDOM,DRY FLEXURE SUSPENDED TUNED ROTOR GYRO,HERMETICALLY SEALED,WITH SPECIAL ROTATING FLEXURE SUSPENSION MOUNTED TO ONE END OF ROTATING SHAFT. THE FLEXURE SUPPORTS AND PIVOTS THE INERTIAL FLYWHEEL,A COMPENSATOR IS TUNED TO ELIMINATE PIVOT RESTRAINTS,THE OTHER SHAFT END IS DRIVEN BY A SYNCHRONOUS MOTOR. THE VARIABLE INDUCTANCE PICKOFF PROVIDES ELECTRICAL SIGNALS IN PROPORTION TO CASE DISPLACEMENT ANGLES ABOUT ITS 2 ORTHOGONAL AXES"
FREQFREQUENCY IN HERTZ400.0

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