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Aviation Parts KVG-350 Remote Mounted Vertical Gyro Weight 6.8 lbs
| Model Number | KVG-350 |
|---|---|
| Minimum Order Quantity | 1 pcs |
| Price | Negotiable |
| Packaging Details | boxes |
| Payment Terms | L/C, T/T |
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xProduct Details
| WEIGHT | 6.8 Lbs. | POWER REQUIREMENTS | (high Erection) 53VA, 46mA At 115VAC |
|---|---|---|---|
| DIMENSIONS | (low Erection) 30VA, 26mA At 115VAC | POWER FACTOR | 360 Deg (roll), +-81 Deg (pitch) |
| ROTOR SPEED | 22000 RPM Nominal | AUTOPILOT OUTPUT | 3-wire, 400 Hz Synchro Outputs In Roll And Pitch Axis |
| RADAR STAB OUTPUT | 2-wire Transformer Type Outputs For Radar Antenna Orientation In Roll And Pitch; 2 Outputs Of .050 Volt/degree | OUTPUT ACCURACY | +- .5 Degrees |
| Highlight | Remote Mounted Vertical Gyro |
||
Product Description
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 115VAC | POWER REQUIREMENTS: | (low erection) 30VA, 26mA at 115VAC |
| POWER REQUIREMENTS: | (high erection) 53VA, 46mA at 115VAC | POWER 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 axis | RADAR 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/degree | OUTPUT 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 minimum | ERECTION ACCURACY: | +- .25 degrees of vertical within 3 minutes of power application. +-1 degree of vertical within 1 minute |
| OUTPUT ACCURACY: | +- .5 degrees | TEMPERATURE: | -67F to 158F |
| ALTITUDE: | 50000 feet | TSO: | C4c, C9c, C52a |
| ENVIRONMENTAL: | D2A/MNO/XXXXXXZBABB | SYNCHRO ACCURACY: | 20 minute max angular error |
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