KVG 350
- 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
| DIMENSIONS |
5.40"H x 5.50"W x 7.92"D |
|
WEIGHT |
6.8 lbs |
|
TEMPERATURE RANGE |
-55 to 70°C |
|
ALTITUDE |
50 000 feet |
|
POWER REQUIREMENTS |
starting : 88VA, 76.5mA at 115VAC low erection : 30VA, 26mA at 115VAC high erection : 53VA, 46mA at 115VAC |
|
POWER FACTOR |
0.95 (starting), 0.99 (running) |
|
ROTOR SPEED |
22 000 RPM nominal |
|
GIMBAL FREEDOM |
360 deg (roll), more or less 81 deg (pitch) |
|
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 0.050 volt/degree |
|
FLIGHT DIRECTOR OUTPUT |
2-wire transformer type outputs for autopilt roll and pitch attitude; 2 ouputs of 0.20volt/degree |
|
OUTPUT VOLTAGE |
26 more or less 1.5VAC, 310mA max 5 more or less 0.30VAC, 280mA max 26.4 more or less 2.5VDC, 80mA max |
|
ERECTION RATES |
(normal) 2 deg/minute nominal (fast) 11 deg/minute minimum |
|
ERECTION ACCURACY |
more or less 0.25 degrees of vertical within 3 minutes of power application. more or less1 degree of vertical within 1 minute |
|
OUTPUT ACCURACY |
more or less 0.5 degrees |
|
SYNCHRO ACCURACY |
20 minute max angular error |
|
ENVIRONMENTAL |
D2A/MNO/XXXXXXZBABB |
|
TSO |
C4c, C9c, C52a |
| PART NUMBER | DESCRIPTION |
|
060-0026-00 |
actual unit part number on dataplate |
|
060-00026-0000 |
Honeywell Bendix/King catalog part numbe |