NSN 5990-01-184-6830

Part Details | LINEAR ELECTRICAL RESOLVER

5990-01-184-6830 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.

Alternate Parts: 75A7711759AAC, 75A771175-9AAC, 5M1899002, 5M1899-002, LTH10RQS6F340, LTH-10-RQS-6/F340, 5990-01-184-6830, 01-184-6830, 5990011846830, 011846830

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUL 21, 198401-184-683031780 ( RESOLVER, ELECTRICAL, LINEAR )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND D

Cross Reference | NSN 5990-01-184-6830
Part Number Cage Code Manufacturer
75A771175-9AAC76301BOEING COMPANY, THEDBA BOEING
5M1899-00276301BOEING COMPANY, THEDBA BOEING
LTH-10-RQS-6/F34099932MOOG INC.DBA MOOG COMPONENTS GROUP
Technical Data | NSN 5990-01-184-6830
Characteristic Specifications
BODY SIZE10
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING40.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING1090.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS680.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS280.00 NOMINAL
ZSO RESISTANCE IN OHMS24.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS28.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS520.00 NOMINAL
STATOR DC RESISTANCE IN OHMS20.00 NOMINAL
PHASE SHIFT ANGLE IN DEG11.000 INPUT TO OUTPUT NOMINAL
MAXIMUM LINEAR RANGE IN DEGM33.0/P33.0
LINEARITY IN PERCENT0.50
OUTPUT VOLTAGE CHANGE PER DEG IN VOLTS0.4
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS16.0 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS4.0 CENTIMETER-GRAMS MAXIMUM
BODY STYLE STANDARD ROUND D
SHOULDER DIAMETER0.8116 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
SECOND SHOULDER DIAMETER0.8350 INCHES MINIMUM AND 0.8450 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.0630 INCHES MINIMUM AND 0.0700 INCHES MAXIMUM
OVERALL LENGTH1.7490 INCHES MAXIMUM
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM
BODY DIAMETER0.9290 INCHES MINIMUM AND 0.9390 INCHES MAXIMUM
PILOT LENGTH0.0330 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM
SHOULDER LENGTH0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM
AFT OF FIRST FLANGE DIAMETER0.9320 INCHES MINIMUM AND 0.9420 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY4 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
SHAFT MAXIMUM RADIAL PLAY0.0005 INCHES
SHAFT END PLAY0.0003 INCHES MINIMUM AND 0.0008 INCHES MAXIMUM
SHAFT MAXIMUM RUNOUT0.0010 INCHES