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Aviation Parts KVG-350 Remote Mounted Vertical Gyro Weight 6.8 lbs

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Aviation Parts KVG-350 Remote Mounted Vertical Gyro Weight 6.8 lbs

Country/Region china
City & Province Shaanxi
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Product Details

                       Aviation Parts KVG-350 Remote Mounted Vertical Gyro Weight 6.8 lbs

 

 

Descriptions of Aviation Parts:

 

The KVG 350 was developed for high performance flight control systems that require precise roll and pitch attitude information. The ARINC 407 data format enables it to be compatible with Primary Instruments, Flight Control, Weather Radar, and Special Mission Equipment that requires highly-accurate roll and pitch information. Roll and pitch is available in 400 HZ Synchro, 200 MV/Degree, or 50MV/Degree.

Easily remote mounted, it works with the following BendixKing Flight Control Systems: KFC 225, KFC 250 (4-inch version), KFC 300, KFC 325 and KFC 400.

The KVG 350 is often used in special-mission Search And Rescue (SAR) radar applications where stabilization is mission critical. The KVG 350 sets the standard in vertical gyro performance.

 

Features of Aviation Parts:

 

 

· Remote mounted vertical gyro

· Designed to be incorporated into KFC-225, KFC-250, KFC-300, KFC-325 and KFC-400 Bendix/King Flight Control Systems

· Supplies an accurate source for roll and pitch attitude reference to flight computer

· 115 VAC, 400 Hz, Single Phase, Sine Wave power requirement

· Optional adapter plates to adapt existing Collins 332D-11 / 332D-11A or Sperry VG-14 / VG-14A to KVG-350

 

 

Specifications of Aviation Parts:

 

WEIGHT:6.8 lbs.DIMENSIONS:5.40"H x 5.50"W x 7.92"D
POWER REQUIREMENTS:(starting) 88VA, 76.5mA at 115VACPOWER REQUIREMENTS:(low erection) 30VA, 26mA at 115VAC
POWER REQUIREMENTS:(high erection) 53VA, 46mA at 115VACPOWER FACTOR:.95 (starting), .99 (running)
GIMBAL FREEDOM:360 deg (roll), +-81 deg (pitch)ROTOR SPEED:22000 RPM nominal
AUTOPILOT OUTPUT:3-wire, 400 Hz synchro outputs in roll and pitch axisRADAR STAB OUTPUT:2-wire transformer type outputs for radar antenna orientation in roll and pitch; 2 outputs of .050 volt/degree
FLIGHT DIRECTOR OUTPUT:2-wire transformer type outputs for autopilt roll and pitch attitude; 2 ouputs of .200 volt/degreeOUTPUT VOLTAGE:26 +- 1.5VAC, 310mA max 5 +- 0.30VAC, 280mA max 26.4 +- 2.5VDC, 80mA max
ERECTION RATES:(normal) 2 deg/minute nominal (fast) 11 deg/minute minimumERECTION ACCURACY:+- .25 degrees of vertical within 3 minutes of power application. +-1 degree of vertical within 1 minute
OUTPUT ACCURACY:+- .5 degreesTEMPERATURE:-67F to 158F
ALTITUDE:50000 feetTSO:C4c, C9c, C52a
ENVIRONMENTAL:D2A/MNO/XXXXXXZBABBSYNCHRO ACCURACY:20 minute max angular error

 

 

 

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