ILS520 Instrument Landing System(ILS)
Product Overview
1、The instrument landing system (ILS) provides guidance information for the airport approach and landing aircraft to align with the runway center line and a 3 ° glide angle。
2、The equipment consists of LLZ521 Localizer, GP522 Glide-Path and remote controller。
3、Provide the most advanced technology and the most reasonable system architecture for the performance selection of ClassⅠ、Ⅱand Ⅲ equipment, and provide users with friendly Windows based The graphical software interface integrates, the latest technical features to reduce the number of system boards。
4、35U standard cabinet design reduces the installation, maintenance and logistics costs of ILS equipment. Software design and certification meet the strict RTCA DO-178 B/278 standard。
Product Appearance
1、Local or remote computer to access the RMM software operating system of the ILS equipment.
2、Remote control (navigation duty room) and repeat display (tower).
3、Localizer LLZ521 main cabinet.
4、Glide-Path GP522 main cabinet.
LLZ521 course beacon
ELECTRICAL
1、Frequency Range:108 — 111.975 MHz.
2、Modulation Tones:90Hz and 150Hz(Single tone Modulation Depth 20%),1020Hz(Modulation Depth 10%).
3、CSB Power Output:5 — 30W(adjustable).
4、SBO Power Output:0.1 — 1W(adjustable).
5、Frequency Stability:±0.0001%.
6、Frequency Control:Synthesizer.
7、Coverage: Per ICAO Annex 10.
8、Monitors:Dual Parallel And/Or configuration,and built-in-test generator.
9、RMM Software:Local or remote operation equipment software.
10、Primary Power:110V — 220V AC±10%,47 — 63 Hz,single phase.
11、Standby Power:24V DC backup battery, working for at least 4 hours.
MECHANICAL
Weight:220kg.
Size:170cm(H)X 60cm(W)X 60cm(D),Standard 35U cabinet.
ENVIRONMENTAL
Temperature:Indoor -10°C —+50°C,Outdoor - 40°C — +70°C.
Relative Humidity:Indoor and outdoor equipment 0 — 95%.
Altitude:0 — 4500m MSL.
Duty Cycle:Continuous, unattended.
Wind:Up to 161km/hr , with 1.5cm ice.
LLZ521 localizer (main cabinet)
Other performance
1、Single and dual transmitter configurations (optional).
2、Single and dual frequency transmitter configurations (optional).
3、Localizer 12, 14, 16 and 20 unit LPDA antenna array (optional).
4、IP port of PC accesses RMM software of equipment.
5、Dual monitor configuration, cold or hot backup system configuration mode.
6、Automatic diagnosis of equipment failure, one click upload and download of equipment parameters.
7、One click printing of monitoring parameter report.
8、The IP port of the remote controller is connected to the ILS cabinet to monitor the working status of the equipment in real time.
9、The system can be upgraded from class I to class II and class III equipment performance at any time.
10、Meet the requirements of ICAO, annex 10,aviation telecommunications, volume 1,radio navigation equipment。
11、Comply with CAAC, aeronautical radio navigation aids Part 1:Technical requirements for Instrument landing system (ILS), MH/T- 4006.1-1998.
12 unit LPDA antenna system of localizer
Equipment Configuration List
P522 Glipe-Slope
ELECTRICAL
1、Frequency Range:328.6 — 335.4 MHz.
2、Modulation Tones:90Hz and 150Hz(Single tone Modulation Depth 40%).
3、COU CSB Power Output:2 — 10W(adjustable).
4、COU SBO Power Output:0.1 — 1W(adjustable).
5、CLR CSB Power Output:0.2 — 1W(adjustable).
6、Frequency Stability:±0.0001%.
7、Frequency Control:Synthesizer.
8、Coverage:Per ICAO Annex 10.
9、Monitors:Dual Parallel And/Or configuration, and built-in-test generator。10、RMM software:Local or remote operation equipment software.
11、Primary Power:110V — 220V AC±10%,47 — 63 Hz,single phase.
12、Standby Power:24V DC backup battery, working for at least 4 hours.
MECHANICAL
Weight:200kg.
Size:170cm(H)X60cm(W)X60cm(D),Standard 35U cabinet.
ENVIRONMENTAL
Temperature:Indoor -10°C —+50°C,Outdoor - 40°C — +70°C.
Relative Humidity:Indoor and outdoor equipment 0 — 95%.
Altitude:0 — 4500m MSL.
Duty Cycle:Continuous, unattended.
Wind:Up to 161km/hr , with 1.5cm ice.
GP522 Glipe-Slope (main cabinet)
Other performance
1、Single and dual transmitter configurations (optional)。
2、Single and dual frequency transmitter configurations (optional)。
3、M-type capture effect LPDA antenna array。
4、IP port of PC accesses RMM software of equipment。
5、Dual monitor configuration, cold or hot backup system configuration mode.
6、Automatic diagnosis of equipment failure, one click upload and download of equipment parameters。
7、One click printing of monitoring parameter report。
8、The IP port of the remote controller is connected to the ILS cabinet to monitor the working status of the equipment in real time。
9、The system can be upgraded from classⅠto classⅡand class Ⅲ equipment performance at any time。
10、Meet the requirements of ICAO, annex 10,aviation telecommunications, volume 1,radio navigation equipment。
11、Comply with CAAC, aeronautical radio navigation aids Part 1:Technical requirements for Instrument landing System (ILS), MH/T- 4006.1-1998.
GP M-type Antenna System
Equipment Configuration List
Remote Control and Repeat Display
ELECTRICAL
The remote controller communicates with the ILS equipment through the Ethernet IP interface.
The remote controller communicates with the repeating display through RS-485 protocol.
Primary Power:110V — 220V AC±10%,47 — 63 Hz,single phase.
Standby Power:24V DC backup battery, working for at least 4 hours.
MECHANICAL
Weight:4kg.
Dimensions:13.4cm(H)X60cm(W)X20cm(D),Standard 3U cabinet.
ENVIRONMENTAL
Temperature:Indoor -10°C 至+ 50°C.
Relative Humidity:0 — 95%.
Altitude:0 — 4500m MSL.
Equipment Configuration List
1、Remote Control ,RCU4101CA,1 set(One 3U chassis).
2、Repeat Display,RMU4102CA,1 set(One 3U chassis).
3、Transmission Equipment,1 set.
Product Appearance
RMM Software
The RMM software interface provides Chinese and English operating languages to facilitate user operation and maintenance of equipment, as shown in the figure below。
Localizer "monitoring unit" interface (Chinese)
Localizer "monitoring unit" interface (English)
Certificate
Type approval certificate of radio transmission equipment issued by the Ministry of Industry and Information Technology.
EMC Environment Test Report
LS520 ILS equipment CNAS certification, electrostatic discharge immunity test, electrical fast transient burst immunity test, surge (impact) immunity test, voltage sag, short interruption and voltage change immunity test, electromagnetic compatibility environment test report。
Environmental Test Report
ILS520 ILS equipment CNAS certification , damp heat test, low temperature test, high temperature test, low pressure test, salt spray test, vibration test, impact test, environmental test report。
Reliability Test Report
ILS520 ILS equipment CNAS certification , 5000 hour reliability test report。
Reference Standards
CAAC, Aeronautical radio navigation aids Part 1:Technical requirements for Instrument landing system (ILS), MH/T-4006.1-1998.
CAAC, Electromagnetic environment requirements for aeronautical radio navigation stations, GB 6364-2013.
CAAC, Specification for aeronautical communication navigation and surveillance station siting criteria - Part 1: Navigation, MH/T 4003.1—2021.
CAAC, China civil aviation instrument landing system classⅡoperation regulations, CAAC order No. 57.
Convention on international civil aviation, annex 10, aviation telecommunications, radio navigation equipment (Volume I), 6th edition, July 2006.
ICAO, Document 8071, test Manual for radio navigation equipment (Volume 3, 1972).
Standard Comparison
Some technical indicators of ILS520 type ILS equipment are compared with ICAO Annex 10 and CAAC ILS equipment technical requirements, as follows.