Azimut Doppler Radio Beacon DVOR 2000 | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Azimut Doppler Radio Beacon DVOR 2000PDF, 304.3 KB
FunctionThe Radio Beacon is designed to generate and send out radio signals which provide measuring of the azimuthal angle of an aircraft equipped with VOR avionics. The Radio Beacon is used in airports and on flight lanes of civil aircrafts. Principle of Operation and Signal FormatThe DVOR 2000 Radio Beacon has the signal format of VOR avionics and conforms to the requirements applied to this equipment as set forth in «Appendix 10 to Convention on International Civil Aviation (ICAO)». The Radio Beacon can be used in package with distance measuring DME/N Radio Beacon as well as independently. Radio Beacon Structure
The Radio Beacon consists of the hardware system (a rack containing the apparatus), the aerial assembly, two control aerials and the RCE 2000 remote control device. The signal generating, operating and control equipment of the Radio Beacon is contained in a rack equipped with a heat controlling system. The aerial assembly consists of one central and 48 radial radiating elements arranged along a circumference with a diameter of 13.5 meters. The radiating elements of the aerial assembly are situated on a reflective unit with a diameter of 30 meters. OperationThe Beacon can be operated using a local control panel or the RCE 2000 remote control device which can be located up to 10 km away. Changes in the state of the hardware and in the Radio Beacon functionality are followed by light indication and audio alarm. The RCE 2000 equipment provides access to the information regarding the state of the Radio Beacon functionality when necessary through the local Ethernet network using the TCP/IP protocol or through the ATN network in accordance with the CCITT X.25 protocol. ControlThe
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| Coverage: | |
| in the horizontal plane | 360° |
| in the vertical plane | 40° |
| in the range (in conditions of direct visibility), at least | 340 km (at the flight altitude of 12 000 m) 240 km (at the flight altitude of 6000 m) |
| Inaccuracy in data regarding azimuth | ±1° |
| Frequency range | 108.000 MHz to 117.950 MHz |
| Signal parameters (reference phase, alternating phase, detection, radiotelephone communication) | As required by ICAO |
| Control Over Output Parameters | |
|---|---|
| Control over the main parameters (azimuth and signal strength) | As required by ICAO |
| Azimuth measurement range | 0° to 360° |
| Azimuth measurements inaccuracy | ±0.2° |
| Dimensions | |
| Hardware (width × length × height) | 2.5 × 4.5 × 2.7 m |
| Aerial assembly (diameter) | 13.5 m |
| Aerial assembly reflective unit (diameter) | 30 m |
| Power Supply | |
| Main and reserve network | 3 ~ 380/220 (+10 %; -15 %) V, 50 Hz |
| Power consumption, at most | |
| of the main equipment | 2 kVA |
| when the thermoregulation system is on | 8 kVA |
| Operational time from UPS (storage battery), at least | 30 minutes |
| Operating Conditions | |
| Equipment outside of the container: | |
| environment temperature | −50°Ñ to +50°Ñ |
| precipitation effect (rain intensity), at most | 3 mm/min |
| wind force effect (wind speed), at most | 50 m/s |
| Equipment inside of the container | −40°C to +50°Ñ |
Reliability | |
| MTBF, at least | 30 000 hours |
| Life cycle | 15 years |