5990-00-539-7080, SYNCHRO,RECEIVER

National Stock Number:
5990-00-539-7080

Federal Supply Class:
5990

National Item Identification Number:
005397080

Description:
SYNCHRO,RECEIVER

Detail:
A SYNCHRO CONSISTING OF A STATOR AND ROTOR INDUCTIVELY COUPLED. THE ROTOR IS FREE TO TURN IN ACCORDANCE WITH THE ELECTRICAL INPUT FROM A TRANSMITTER SYNCHRO OR A DIFFERENTIAL SYNCHRO. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, VARIABLE TRANSFORMERS, OR ITEMS WITH DIALS.

Manufacturer Information:

790552-4	55972	HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
790552-4	96774	HONEYWELL INTERNATIONAL INC.
AY200-2B	96774	HONEYWELL INTERNATIONAL INC.
AY200S-2-B	55972	HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
AY200S-2-B	96774	HONEYWELL INTERNATIONAL INC.
E39423-1PC103	27847	UNICONTROL INC HAYS CLEVELAND DIV
E39424-1PC103	27847	UNICONTROL INC HAYS CLEVELAND DIV

Techincal Specification:

ROTOR INPUT VOLTAGE RATING IN VOLTS	26.0 NOMINAL
ROTOR INPUT CURRENT RATING	100.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING	450.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ	400.0 NOMINAL
TERMINAL TYPE AND QUANTITY	5 WIRE LEAD
BODY SIZE	15
BODY MATERIAL	ALUMINUM
ZRO RESISTANCE IN OHMS	45.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS	255.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS	16.00 NOMINAL
STATOR DC RESISTANCE IN OHMS	6.70 NOMINAL
TRANSFORMATION RATIO	1.000 ROTOR TO STATOR MINIMUM AND
	2.200 ROTOR TO STATOR MAXIMUM
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES	-40.0 TO 40.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS	4.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS	2.0 CENTIMETER-GRAMS NOMINAL
TORQUE GRADIENT PER ANGULAR DEG	2250.0 MILLIMETER-MILLIGRAMS NOMINAL
BODY STYLE	STANDARD ROUND C
SHOULDER DIAMETER	1.3115 INCHES MINIMUM AND
	1.3120 INCHES MAXIMUM
PILOT DIAMETER	0.4995 INCHES MINIMUM AND
	0.5000 INCHES MAXIMUM
OVERALL LENGTH	1.8810 INCHES NOMINAL
FLANGE DIAMETER	1.4360 INCHES MINIMUM AND
	1.4370 INCHES MAXIMUM
FLANGE THICKNESS	0.0930 INCHES NOMINAL
UNDERCUT DIAMETER	1.3120 INCHES NOMINAL
UNDERCUT WIDTH	0.0780 INCHES NOMINAL
PILOT LENGTH	0.0400 INCHES NOMINAL
SHOULDER LENGTH	0.1320 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE	1.5910 INCHES NOMINAL
ALIGNMENT HOLE DEPTH	0.1250 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER	0.5000 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY	4
SHAFT TYPE	ROUND, SLOTTED SINGLE SHAFT
SHAFT DIAMETER	0.1195 INCHES MINIMUM AND
	0.1200 INCHES MAXIMUM SINGLE SHAFT
SHAFT LENGTH	0.2900 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH	0.0210 INCHES MINIMUM AND
	0.0310 INCHES MAXIMUM SINGLE SHAFT
SHAFT SLOT WIDTH	0.0210 INCHES MINIMUM AND
	0.0310 INCHES MAXIMUM SINGLE SHAFT
TERMINAL LOCATION	REAR
FRAGILITY FACTOR	MODERATELY RUGGED

Click here to Register for Free 30-day Trial