Leidos Innovations NORMARC7033 7033 Dual Frequency Glide Path User Manual General Description 7011

Lockheed Martin Air Traffic Management 7033 Dual Frequency Glide Path General Description 7011

Normarc ILS General Description

©1999 Navia Aviation ASNORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION
©1999 Navia Aviation AS
©1999 Navia Aviation AS Table of contentsGENERAL DESCRIPTIONNORMARC 7033INSTRUMENT LANDING SYSTEMiiiTABLE OF CONTENTSDESCRIPTION OF NORMARC 7033 2-FREQUENCY SYSTEM .....................11 GENERAL DESCRIPTION ..............................................................................11.1 Technical Specifications..................................................................................... 11.1.1 Signal Minimum Performance GP ...............................................................11.1.2 Environmental Characteristics ..................................................................... 21.1.3 EMC Characteristics .................................................................................... 21.1.4 Mechanical Characteristics..........................................................................31.1.5 Power Supply...............................................................................................31.2 General Information............................................................................................ 31.2.1 Introduction.................................................................................................31.2.2 Product Type Numbers................................................................................71.2.3 Abbreviations ............................................................................................... 72 PHYSICAL ORGANIZATION...........................................................................82.1 Module and Assembly Location .........................................................................82.2 Power Supply .....................................................................................................93 SYSTEM DESCRIPTION.................................................................................123.1 Overview ............................................................................................................ 123.2 Physical Description........................................................................................... 123.3 Monitors.............................................................................................................. 133.4 Transmitters / Modulators...................................................................................133.5 TX Control .......................................................................................................... 133.6 Remote Monitoring (RMS) Unit .......................................................................... 143.7 Remote Control Unit........................................................................................... 143.8 Remote Slave Panel........................................................................................... 143.9 Remote Maintenance Monitoring (RMM) ...........................................................143.9.1 RMM Access................................................................................................163.9.2 Local Keyboard/Display Functions ..............................................................163.9.3 Diagnostic functions.....................................................................................174 ELECTRICAL INSTALLATION ........................................................................184.1 Connection Overview .........................................................................................184.2 Power and Battery..............................................................................................184.3 RF Inputs............................................................................................................204.4 RF Outputs......................................................................................................... 204.5 DC Loop ............................................................................................................. 214.6 Remote Control .................................................................................................. 224.7 PC and Modem ..................................................................................................234.8 DME ................................................................................................................... 244.9 Analog Inputs .....................................................................................................254.10 Digital Inputs and Outputs..................................................................................264.11 Battery Warning.................................................................................................. 274.12 Remote control connections...............................................................................284.13 Remote slave connection................................................................................... 304.14 Interlock switch connection ................................................................................31
GENERAL DESCRIPTIONivNORMARC 7033INSTRUMENT LANDING SYSTEMTable of contents ©1999 Navia Aviation AS
©1999 Navia Aviation AS List of FiguresGENERAL DESCRIPTIONNORMARC 7033INSTRUMENT LANDING SYSTEMvLIST OF FIGURESFigure1-1 Typical ILS installation ..........................................................................4Figure1-2 Glidepath block diagram .......................................................................4Figure1-3 Glidepath Antenna ................................................................................5Figure1-4 Glidepath Cabinet Installation ..............................................................6Figure2-1 NM 7033 Module Location - Front view. ...............................................9Figure2-2 NM 7033 Module Location - Rear view of main section. ......................10Figure2-3 NM 7033 Module Location - Front view of wall-mounted section .........11Figure3-1 ILS block diagram. ................................................................................12Figure3-2 The NM 7000 series RMM/RMS systems. ...........................................15Figure3-3 Local Control Panel ..............................................................................17Figure4-1 ILS main cabinet connection overview. ................................................18Figure4-2 Power and backup battery connections. ..............................................19Figure4-3 RF input connections. ...........................................................................20Figure4-4 RF output connections. ........................................................................20Figure4-5 DC loop connections. ...........................................................................21Figure4-6 Remote control connection. ..................................................................22Figure4-7 PC and modem connections. ...............................................................23Figure4-8 DME connections. ................................................................................24Figure4-9 Analog input connections. ....................................................................25Figure4-10 Digital input/output connections. ..........................................................26Figure4-11 Battery warning connections. ...............................................................27Figure4-12 Remote control to ILS connection ........................................................28Figure4-13 Remote control power supply connections ...........................................29Figure4-14 Remote slave connection .....................................................................30Figure4-15 Interlock switch connection ..................................................................31
GENERAL DESCRIPTIONviNORMARC 7033INSTRUMENT LANDING SYSTEMList of Figures ©1999 Navia Aviation AS
©1999 Navia Aviation AS 21446-3.4 List of tablesOPERATING MANUALNORMARC 7033INSTRUMENT LANDING SYSTEMviiLIST OF TABLES
OPERATING MANUALviii21446-3.4NORMARC 7033INSTRUMENT LANDING SYSTEMList of tables ©1999 Navia Aviation AS
GENERAL DESCRIPTIONNORMARC 70331-1©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONDESCRIPTION OF NORMARC 7033 2-FREQUENCY SYSTEM1 General Description1.1 Technical SpecificationsNM 7033 Dual-Frequency Glidepath Cabinet.1.1.1 Signal Minimum Performance GPTransmitterFrequency range 328.6-335.4 MHzFrequency tolerance + 0.002%Output power (CSB + SBO) Course 3-7 W adjustableOutput power (CSB) Clearance 0.3-1 W adjustableHarmonic radiation 2.5 uW maximumRF difference frequency (2-freq. only) 15 kHz + 5 kHzSpurious 25 uW maximumOutput power stability + 0.2 dBCSB/SBO stability + 0.3 dBModulator - Course lineModulation depth 90/150 Hz 40%adjustable range 10-44%SDM stability + 0.8% SDMDDM stability + 0.2% DDMFrequency tolerance + 0.05 HzTotal harmonic dist. (90/150 Hz) 1% maximumPhase locking (90 Hz to 150 Hz) 5° maximum ref 150 HzSBO phaser adjustment range + 30°Modulator - ClearanceModulation depth 80%90 Hz component 20%150 Hz component 60%Adjustable range DDM 20-100% 150 Hz dominanceAdjustable range SDM 20-90%Stability + 0.2 dBFrequency tolerance + 0.05 HzTotal harmonic dist. (90/150 Hz) 1% maximumPhase locking (90 Hz to 150 Hz) 5° maximum ref 150 HzMonitoringAlarm Functions Range (*)RF power reduction 1-5 dBChange of nominal CL + 10-60 uA
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONGENERAL DESCRIPTION ©1999 Navia Aviation AS1-2* asymmetrical limits are possible.1.1.2 Environmental Characteristics1.1.3 EMC CharacteristicsChange of nominal DS from nominal value + 10-60 uAChange of nominal CLR (2-freq only) + 10-60 uAChange of nominal NF + 10-60 uAChange of nominal SDM + 2-8% SDMDifference frequency (2-freq. only) + 2-5 kHzTotal period of radiation out of tolerance 1-6 sec.Additional NF time delay 0-20 sec.Line break, ILS - Remote Control (disa-ble optional)Monitor input levels:Adjustment range, nominal level -5 to –34 dBmAGC range for less than 1% change in SDM 5 dBMonitor stability at nominal levels:RF power values + 0,3 dBDDM values + 1 uASDM values + 1% SDMWarning Functions:RF power reduction 40-75% of Alarm limitChange of nominal CL 40-75% of Alarm limitChange of nominal DS 40-75% of Alarm limitChange of nominal CLR 40-75% of Alarm limitChange of nominal NF 40-75% of Alarm limitChange of SDM 40-75% of Alarm limitDifference frequency 40-75% of Alarm limitMains failureRemote ControlData Transmission Medium 2-wire line, 600 ohmData modulation serial, FSKTransmitter level -10dBm + 2 dBReceiver dynamic range -10dBm to -34dBmOperating temperature -10 to +55 °CStorage temperature -30 to +60 °CEMR: EN 55022 class BSpurious and harmonics: CISPR 22
GENERAL DESCRIPTIONNORMARC 70331-3©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION1.1.4 Mechanical CharacteristicsThe ILS rack is wall mounted. The remote control and slave panels fit a standard 3U (132mm) high 19" subrack.1.1.5 Power Supply1.2 General InformationThis paragraph gives a description of a typical ILS installation and the Normarc Glidepath sys-tem. Conventions and abbreviations used in this manual are also given.1.2.1 IntroductionThis is an overview of Normarc's NM703X ILS glidepath systems.1.2.1.1 ILS OverviewA complete Instrument Landing System comprises:• A LOCALIZER SYSTEM, producing a radio course to furnish lateral guidance to the airport runway.• A GLIDE PATH SYSTEM, producing a radio course to furnish vertical guidance down the correct descent angle to the runway.• MARKER BEACONS, to provide accurate radio fixes along the approach course.Dimensions: (H x W x D)ILS Rack: 1020x600x500 mmRemote control: 129x71x170 mmSlave panels: 129x41x170 mmWeight: 85 kg – 95 kg depending on modelExternal supply:Input voltage: 230V +15%/-20%,45-65 Hz or120V +15%/-20%, 45-65 HzOutput voltage: 27,6VOutput current: 20A maxILS cabinetInput voltage 22-28V DCCurrent consumption: 8A – 14A depending on configurationStand-by Battery 24V DC nominal, 85 Ah-110Ah valve regulated lead-acid battery recommended
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONGENERAL DESCRIPTION ©1999 Navia Aviation AS1-4The layout of a typical ILS airport installation is shown below.Figure1-1 Typical ILS installation1.2.1.2 Glidepath OverviewThe complete ILS Glidepath system comprises:• A GP transmitter/monitor cabinet• An antenna distribution network• A monitor network• A GP antenna array• Near-field monitor antennaA block diagram is shown below: Figure1-2 Glidepath block diagramLocalizer110 MHzGlide Path330 MHzMarker Beacon75MHz3°HBK547-1GP-BLOCK DIAGRAMHBK205-1TRANSMITTER ANDMODULATOR I and IIMONITOR I and IIREMOTECONTROLUNITSLAVEPANELCSB CLSBO CLCSB CLR*CLCLR*DSNFANTENNADISTRIBU-TION NETW.**MONITORNETWORK24VBATTERYSUPPLYPOWERMAINS INPUT220V/110V ACULMILS Localizerand Glide PathGPTRANSMITTER**** CLR signals only used for 2-frequency systems.** Antenna distribution network not used for Null Reference.*** Middle antenna used for M-Array and Modified M-Array.
GENERAL DESCRIPTIONNORMARC 70331-5©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONFigure1-3 Glidepath Antenna
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONGENERAL DESCRIPTION ©1999 Navia Aviation AS1-6Figure1-4 Glidepath Cabinet Installation1.2.1.3 Glidepath DescriptionTo shape the glide path signal, ground plane reflection from an area in front of the antenna array is necessary. The specific requirements to the area are given in the antenna handbook.The glide path site may be located on either side of the runway, but the most reliable operation will be obtained if the site is selected on terrain least obstructed by taxiways, aircraft holding aprons, parking ramps, buildings, power lines etc. The site should offer the widest area of smooth ground with possibilities of levelling without excessive physical or economical effort, if indeed levelling is deemed necessary.The glide path antenna system should be located at a distance of 75-200 m from the runway center line. The distance from the runway threshold is a function of several factors upon which establishment of the optimum operational conditions depend. These factors are:
GENERAL DESCRIPTIONNORMARC 70331-7©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION1. The glide path angle.2 Threshold crossing height requirements.3. Obstruction clearance requirements 4 The slope of the terrain in front of the antenna system.5. The extent of smooth terrain in the site area and beyond the threshold.1.2.2 Product Type NumbersThe Normarc product numbering system is based on the following three levels:•System• Assembly• ModuleSystems have type numbers starting with NM, for example NM 7033. Systems consist of assemblies, modules and parts.Assemblies have type numbers consisting of three letters, a three- or four- digit number and a letter, for example LPA 1230A. LPA is an abbreviation of Localizer Power amplifier Assembly, 1230 is a running number, and the last letter is the variant designator. Assemblies can consist of assemblies, modules and parts.Modules have type numbers consisting of two letters, a three- or four- digit number and a let-ter, for example FD 1235A. FD is an abbreviation of Feedback Detector, 1235 is a running number, and the last letter is the variant designator. Modules consist of parts. Glidepath Cabinet External Label1.2.3 AbbreviationsAC Alternating CurrentADC Analog to Digital ConverterAGC Automatic Gain ControlCL Course LineCLR ClearanceCOU CourseCPU Central Processing UnitCS Course Sector
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONPHYSICAL ORGANIZATION ©1999 Navia Aviation AS2-8DAC Digital to Analog ConverterDC Direct CurrentDDM Difference in Depth of ModulationDF Difference FrequencyDL Dc LoopDS Displacement SensitivityDSP Digital Signal ProcessorEEPROM Electrically Erasable Progammable Read Only MemoryEMC ElectroMagnetic CompatibilityEMI ElectroMagnetic InterferenceEPROM Erasable Programmable Read Only MemoryFFT Fast Fourier TransformFIFO First-In-First-OutFPGA Field Programmable Gate ArrayGPA Glidepath Power amplifier AssemblyI/F InterFaceI²C Inter Integrated CircuitIIC Same as I²CILS Instrument Landing SystemLED Light Emitting DiodeLF Low FrequencyLLZ LocalizerLPA Localizer Power amplifier AssemblyLRU Line Replacable UnitMCU Monitor Combiner UnitNAV NAVigation signalsNF Near FieldPC Personal ComputerRAM Random Access MemoryRF Radio FrequencyRMM Remote Maintenance MonitorRMS Remote Monitoring SystemROM Read Only MemoryRTC Real Time ClockSC Station ControlSDM Sum in Depth of ModulationSPA Same Parameter AlarmSRAM Static Random Access MemorySTB StandbySW SoftWareTRM TeRMinatorTX Transmitter2 Physical Organization2.1 Module and Assembly LocationThe figures on the following pages show the locations of the modules in the main cabinet.Figure 2-1 shows the main section of the GP cabinet from a front view, with indications of the plug-in board locations.
PHYSICAL ORGANIZATIONNORMARC 70332-9©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONFigure 2-2 shows the same section from a rear view, while Figure 2-3 shows the top half of the wall-mounted section.In addition, the Remote Control Assembly RCA1240C/D and Remote Slave SF 1344A are installed in the technical control room and the control tower, respectively.2.2 Power SupplyAn External Power Supply, operating at 230V/120V mains input and providing 27V at 20A, is normally supplied with the equipment. In special cases, a second external power supply is supplied. Figure2-1 NM 7033 Module Location - Front view.11PS 1227ATCA 1218AHBK 536-1MF 1219AOS1221BLF1223ARMA1215AGPA1232AGPA1231ACOA1207CMO1212A
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONPHYSICAL ORGANIZATION ©1999 Navia Aviation AS2-10 Figure2-2 NM 7033 Module Location - Rear view of main section.SBO 1IN IN OUTSBO 2 SBODUMMY OUTSBO CSBDUMMY INCSB SBO 1IN OUTSBO 2 SBODUMMY OUTSBO CSBDUMMYCSBMB 1203COA 1207CTX1CLTX2CLTX1CLRTX2CLRAAVIEW A-AHBK 593-1
PHYSICAL ORGANIZATIONNORMARC 70332-11©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONFigure2-3 NM 7033 Module Location - Front view of wall-mounted sectionCI 1210ATerminal block forpower and battery connectionand decoupling capacitorHBK541-1
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONSYSTEM DESCRIPTION ©1999 Navia Aviation AS3-123 System descriptionThis chapter gives a functional overview of the NM70xx ILS systems.3.1 OverviewThe complete ILS electronic system is housed in a compact, wall mounted cabinet. The cabi-net and the electronics, except for RF units, are common to the LLZ and GP systems.Figure3-1 ILS block diagram.The ILS cabinets can be configured for Cat I, Cat II, or Cat III requirements with no basic changes.Eight models are available:NM 7011 Single frequency LLZ NM 7012 Single frequency LLZ with hot standby monitoring (Cat III)NM 7013 Two frequency LLZNM 7014 Two frequency LLZ with hot standby monitoring (Cat III)NM 7031 Single frequency GPNM 7032 Single frequency GP with hot standby monitoring (Cat III)NM 7033 Two frequency GPNM 7034 Two frequency GP with hot standby monitoring (Cat III)The system is based on modern technology with extensive Remote Monitoring and Mainte-nance capabilities, and very high reliability and integrity. To meet this objective, the monitor comparator and station control are based on digital hardware, while the RMS interface is microprocessor based.3.2 Physical DescriptionThe cabinet contains three sections:• The electronics card cage• The change-over section• The transmitter / PA sectionThe electronics card cage contains the RF oscillators, the LF signal generators, the monitors, MonitorRMSMonitorTX control ChangeoverSectionMonitorinputsignalsMonitorinputsignals TransmitterTransmitterNAVsignalsoutRemoteControlExternalsensorsComm.portsData anddiagnosticsHBK573-1
SYSTEM DESCRIPTIONNORMARC 70333-13©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONthe station control, the RMS processor, and the voltage regulators.The change-over section contains coaxial relays, attenuators and phasers for the RF outputs.The transmitter / PA section contains the PA blocks including couplers etc. for each output.The cabinet is divided in two parts, with the rear part fixed to a wall, and the front part hinged to give access to interior of the cabinet.All external connections are made to the rear part of the cabinet.3.3 MonitorsThe ILS has duplicated monitors with inputs for Course Line (CL), Displacement Sensitivity (DS), Near Field (NF), and Clearance (CLR) (Dual Freq. only). The signals are detected by the input stage, and then digitized. In the next block they are filtered by a Fast Fourier Trans-form performed by a signal processor. The results for each parameter is then compared with stored limits in a digital hardware comparator.Each of the two monitors consists of two modules. For Cat III use, Hot Standby monitoring can be added by using one additional monitor and associated RF couplers and combiners.The design of the monitors ensures a very high integrity due to the use of digital hardware for the alarm comparators and a very simple Fast Fourier filtering with a signal processor. In addi-tion, the monitor is checked by automatic self-tests.The alarm limits are stored locally in EEPROM, and can be updated from the RMS processor, with a separate hardware write protection to ensure that the integrity is not affected by the RMS system.3.4 Transmitters / ModulatorsThe transmitters are duplicated, either single frequency or dual frequency. Each transmitter consists of a RF oscillator, a LF generator, and one or two PA blocks (single or dual fre-quency).The RF oscillator uses a synthesizer for easy frequency changes and simple logistics. The oscillator has two outputs for use in dual frequency systems.The LF generator contains the generators for 90Hz, 150Hz and 1020Hz signals, the ident keyer / sequencer and interface for DME master or slave keying. All signals are generated by division from a common clock oscillator, ensuring very stable phase relations between the modulation signals.The modulation balance, modulation sum, RF level and Ident morse code are set in this mod-ule by means of multiplying digital to analog converters. The values are stored locally in EPROM and can be updated from the RMS processor with hardware write protection.The same LF generator is used for single and dual frequency systems.3.5 TX ControlThe TX control unit controls the system dependent on alarms from the monitors and inputs
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONSYSTEM DESCRIPTION ©1999 Navia Aviation AS3-14from the local control, the remote control and, optionally, the RMS system. It also generate status information to the same units. The local control and status indicators are a part of the TX Control unit.All functions in the TX Control are based on digital hardware to ensure the highest integrity.3.6 Remote Monitoring (RMS) UnitThe RMS unit contains the system microprocessor. It handles storage and read-out of monitor parameters, measurements for maintenance and fault finding, and performs fault analysis to isolate faults to line replaceable modules. It is also used to set monitor limits and transmitter adjustments.The RMM handles communication to local and remote RMS computers, and in addition it han-dles a small display and keyboard for parameter setting and readout.3.7 Remote Control UnitThe remote control unit is used in the tower or in the technical control room. It has indicators for operating status as well as detailed warnings and an aural alarm device with reset. It can control equipment on/off and change-over, and has an Access Grant-switch to allow remote control from the RMS system.The Remote Control Unit is connected to the ILS by one telephone pair cable.3.8 Remote Slave PanelThe slave panel is connected to the remote control by a multipair wire. It is intended for use in the control tower. It has indicators for normal / warning / alarm and has an aural alarm device. in addition it can turn the equipment on and off, and has an aural alarm reset.Optionally a slave panel with remote control functionality can be delivered.3.9 Remote Maintenance Monitoring (RMM)The NM7000 series has a built-in Remote Maintenance Monitoring system. This system con-sists of the RMS system, remote PC terminals with the RMM program installed, and the local keyboard/display. Figure 3-2 illustrates the RMM/RMS systems
SYSTEM DESCRIPTIONNORMARC 70333-15©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION.Figure3-2 The NM 7000 series RMM/RMS systems.The centre of the RMS system is a CPU with the RMS core program. The RMS collects mea-surements and diagnostic data, and makes them available to the user. The collected informa-tion allows easy and cost effective maintenance, fault finding and routine reporting. In addition, system settings are distributed and parameter readings are collected via the RMS/CPU.External personal computers are used for a user-friendly interface to the RMM system. The equipment has three serial output ports, typically used to connect a local PC, a PC in the air-port technical equipment room, and a modem for connection to a central maintenance facility.RMShardwareRMScoreprogramLocalmeasuringpointsMaintenancedata busRMS data busLocalparameterstoragesLocalKeyboard/DisplayModemNM70xxRMS systemRMM systemLocal Remote 1 Remote 2RMM program RMM program RMMprogramModem ModemModemHBK 598-1
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONSYSTEM DESCRIPTION ©1999 Navia Aviation AS3-16The local keyboard/display allow readings and control through an LCD display and a seven-button keypad. This gives access to the RMM functionality without the need for a PC.3.9.1 RMM AccessAccess to the RMM system is controlled by multiple hardware and software access controls. One password is required for each access level, i.e. one password for level 1, two for level 2 and three for level 3. Optional hardware controls may inhibit writing in the upper access levels.Access level 1• Readout of all the monitor values, warning and alarm limits.• Readout of all the maintenance values and warning limits.• Readout of all the delays.• Readout of all the monitor DDM offsets.Access level 2• TX1 and TX2: 90/150 Hz on/off.• TX1 and TX2: morse normal, continuous, TST or off.• TX1 and TX2: test-signal 90 Hz or 150 Hz dominance on/off.• Diagnostics.Access level 3• Settings of all the monitor warning and alarm limits.• Settings of all the maintenance warning limits.• Settings of all the delays.• Settings of all the monitor DDM offsets.3.9.2 Local Keyboard/Display FunctionsThrough a menu-based interface all main commands, adjustments and monitor limits are accessible from the front panel keypad and LCD display. In addition a quick-read function gives read-out of all main monitor parameters in a glance.
SYSTEM DESCRIPTIONNORMARC 70333-17©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONFigure3-3 Local Control Panel3.9.3 Diagnostic functionsThe system contains internal measuring points and diagnostic functions to isolate faults to failed modules. The values measured are referred to as maintenance parameters. Please refer to the NM70xx Operating Manual.
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONELECTRICAL INSTALLATION ©1999 Navia Aviation AS4-184 Electrical InstallationThis paragraph describes the external electrical connections of the NM 7033 main cabinet.4.1 Connection OverviewThe ILS main cabinet consists of three connector sites, illustrated in Figure 4-1• The ILS RF signals to and from the antenna system are connected at the top of the main cabinet. These connectors may be moved to the bottom, see Mechanical Installation.• The power supply (supplies) and the backup battery are connected to the power connector rail inside the cabinet back section.• All other external connections are sited on the Connection Interface board CI1210A inside the cabinet back section. Figure4-1 ILS main cabinet connection overview.4.2 Power and BatteryThe power supply and the backup battery are connected to the power connector rail inside the cabinet back section as shown in Figure 4-2. If two power supplies are used, these are parallel RF CONNECTIONSCABLE FEEDTHROUGHCOU/SBOCLR/SBOCLR/CSBOUTCOU/CSBCLRDSNFIN CL1 AC LEVEL MEASUREMENTCI 1210A CONNECTIONS8 DIGITAL INPUT/OUTPUT3 DIFFERENTIAL ANALOG2 TEMP SENSORS1 DME1 REMOTE CONTROL3 RS 2324 DC LOOPSBATTERY +27V0VPOWER RAIL CONNECTIONSSUPPLYPOWER +27V0VHBK574-2
ELECTRICAL INSTALLATIONNORMARC 70334-19©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONcoupled outside the cabinet. The cables used should have 4mm2 intersection.Figure4-2 Power and backup battery connections.A DC powered modem or other external equipment designed for 22V - 27V DC can be con-nected to the fused terminal block marked Modem. Maximum current consumption should be 1 A.Battery0V +27VPower Supply0V +27VHBK576-3Fuse 27AT+27VModem
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONELECTRICAL INSTALLATION ©1999 Navia Aviation AS4-204.3 RF InputsThe RF inputs are:• Course Line - CL.• Near Field Antenna - NF.• Displacement Sensitivity - DS.• Clearance - CLR (two frequency applications only).These are connected as shown in Figure 4-3 (front view). Figure4-3 RF input connections.4.4 RF OutputsThe RF outputs are sited at the cabinet top as illustrated in Figure 4-4. The connections are:All applications:• COU SBO - COUrse Tx SideBand Only.• COU CSB - COUrse Tx Carrier and SideBand.Two frequency applications:• CLR SBO - CLeaRance Tx SideBand Only.• CLR CSB - CLeaRance Tx Carrier and SideBand Figure4-4 RF output connections.NF CL CLR DSHBK577-2CSBSBOCLRCSBCLRSBOHBK578-3
ELECTRICAL INSTALLATIONNORMARC 70334-21©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION4.5 DC Loop The DC loops are connected to the Connection Interface board CI1210A in the cabinet back section. Location and pin out are illustrated in Figure 4-5•DL_REF* are the reference voltages from the main cabinet.•DL_DETECT* are the return voltages from the antennas.•GND is main cabinet ground.Suitable female connectors are Weidemüller BLZ-5.08/6 or equivalent.Figure4-5 DC loop connections. TEMPINDOOR TEMPOUTDOOR ACLEVEL ANALOGCH.1 ANALOGCH.2 ANALOGCH.3 DIGITALPORT A DIGITALPORT B DIGITALPORT C DIGITALPORT DTO MB1203RS232 RS232 RS232 REMOTECONTROLDC-LOOP DC-LOOP DMELOCAL REMOTE 2 REMOTE 1 CH.1&2 CH.3&416DC-LOOPCH.1&2DC-LOOPCH.3&41 - Ch 1 In2 - Ch 1 Out3 - GND4 - Ch 2 In5 - Ch 2 Out6 - GNDCI 1210A1 - Ch 3 In2 - Ch 3 Out3 - GND4 - Ch 4 In5 - Ch 4 Out6 - GND16BATTERYWARNINGHBK579-2RADIO LINK
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONELECTRICAL INSTALLATION ©1999 Navia Aviation AS4-224.6 Remote ControlThe remote control is connected to the Connection Interface board CI1210A as illustrated in Figure 4-6. The connection of the remote control, remote slave panel and interlock switch is done at the remote control site and covered in chapter 4.12 - 4.14•FSK_[P,N] is the modem line pair.•GND is main cabinet ground.For normal FSK modem operation the straps S9-11 on CI1210A should be mounted.A suitable female connector is Weidemüller BLZ-5.08/4 or equivalent.Figure4-6 Remote control connection.TEMPINDOOR TEMPOUTDOOR ACLEVEL ANALOGCH.1 ANALOGCH.2 ANALOGCH.3 DIGITALPORT A DIGITALPORT B DIGITALPORT C DIGITALPORT DTO MB1203RS232 RS232 RS232 REMOTECONTROLDC-LOOP DC-LOOP DMELOCAL REMOTE 2 REMOTE 1 CH.1&2 CH.3&4REMOTECONTROL1 - GND2 - FSK_P3 - FSK_N4 - GNDCI1210A14S9-14BATTERYWARNINGHBK580-1RADIO LINK
ELECTRICAL INSTALLATIONNORMARC 70334-23©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION4.7 PC and ModemPC terminals and modems are connected to the standard pin out RS232, 9 pins DSUB con-nectors on the Connection Interface board CI1210A as illustrated in Figure 4-7Recommended connections are:• LOCAL - the PC located at the ILS main cabinet site.• REMOTE 1 - the PC located at the airport technical maintenance site.• REMOTE 2 - distant PC terminals connected through a modem.Figure4-7 PC and modem connections.TEMPINDOOR TEMPOUTDOOR ACLEVEL ANALOGCH.1 ANALOGCH.2 ANALOGCH.3 DIGITALPORT A DIGITALPORT B DIGITALPORT C DIGITALPORT DTO MB1203RS232 RS232 RS232 REMOTECONTROLDC-LOOP DC-LOOP DMELOCAL REMOTE 2 REMOTE 1 CH.1&2 CH.3&4CI1210A15691 - CD (REMOTE 2 only)2 - RXD3 - TXD4 - DTR (REMOTE 2 only)5 - GND6 - DSR (REMOTE 2 only)7 - RTS8 - CTS9 - Not connectedBATTERYWARNINGHBK581-1RADIO LINK
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONELECTRICAL INSTALLATION ©1999 Navia Aviation AS4-244.8 DME Distance Measurement Equipment DME is connected to the Connection Interface board CI1210A as illustrated in Figure 4-8•ACT_DME[P,N] is the positive and negative terminal of the DME active signal from the DME, respectively.•IN_DME[P,N] is the positive and negative terminal of the morse code envelope signal from the DME, respectively.•OUT_DME[P,N] is the positive and negative terminal of the morse code envelope signal to the DME, respectively.A suitable female connector is Weidemüller BLZ-5.08/6 or equivalent.Figure4-8 DME connections.TEMPINDOORTEMPOUTDOORACLEVELANALOGCH.1ANALOGCH.2ANALOGCH.3DIGITALPORT ADIGITALPORT BDIGITALPORT CDIGITALPORT DTO MB1203RS232 RS232 RS232 REMOTECONTROLDC-LOOP DC-LOOP DMELOCAL REMOTE 2 REMOTE 1 CH.1&2 CH.3&41 - ACT_DMEP2 - ACT_DMEN3 - IN_DMEP4 - IN_DMENCI1210A16S1-8DME5 - OUT_DMEP6 - OUT_DMENBATTERYWARNINGHBK582-1RADIO LINK
ELECTRICAL INSTALLATIONNORMARC 70334-25©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION4.9 Analog InputsThe analog inputs are connected to the Connection Interface board CI1210A as illustrated in Figure 4-9 The inputs are:• ANALOG CH.1-3 - three differential DC analog inputs, P is the positive and N is the nega-tive terminal.Maximum voltage: ±15VInput impedance: 10kohms.• TINDOOR, TOUTDOOR - temperature measurement inputs with interface to an LM35 tem-perature sensor.Maximum voltage: ±15V.Input impedance: 10kohms.• AC LEVEL - AC level measurement input. Intended for use with a battery eliminator (i.e. 220/9VAC) to monitor the mains voltage.Maximum voltage: 24Vpp.Input impedance: 10kohms.Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent.Figure4-9 Analog input connections.TEMPINDOOR TEMPOUTDOOR ACLEVEL ANALOGCH.1 ANALOGCH.2 ANALOGCH.3 DIGITALPORT A DIGITALPORT B DIGITALPORT C DIGITALPORT DTO MB1203RS232 RS232 RS232 REMOTECONTROLDC-LOOP DC-LOOP DMELOCAL REMOTE 2 REMOTE 1 CH.1&2 CH.3&4TEMP*1 - VDD2 - T*DOOR3 - GND4 - Not connectedCI1210A14LM35Bottomview1 - VACP2 - GND3 - VACN4 - Not connectedACLEVEL1 - ANLG*P2 - GND3 - ANLG*N4 - Not connectedANALOGCH.*1414141414V+VtempGNDBATTERYWARNINGHBK583-1RADIO LINK
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONELECTRICAL INSTALLATION ©1999 Navia Aviation AS4-264.10 Digital Inputs and OutputsEight bidirectional digital channels (numbered 0-7) are located on the Connection Interface board CI1210A as illustrated in Figure 4-10Logic levels: TTL.Input impedance: 560ohms.Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent.Figure4-10 Digital input/output connections.TEMPINDOOR TEMPOUTDOOR ACLEVEL ANALOGCH.1 ANALOGCH.2 ANALOGCH.3 DIGITALPORT A DIGITALPORT B DIGITALPORT C DIGITALPORT DTO MB1203RS232 RS232 RS232 REMOTECONTROLDC-LOOP DC-LOOP DMELOCAL REMOTE 2 REMOTE 1 CH.1&2 CH.3&4CI1210A1 - USER_DIG52 - GND3 - USER_DIG44 - GND14141414DIGITALPORT C1 - USER_DIG32 - GND3 - USER_DIG24 - GNDDIGITALPORT B1 - USER_DIG12 - GND3 - USER_DIG04 - GNDDIGITALPORT A1 - USER_DIG72 - GND3 - USER_DIG64 - GNDDIGITALPORT DBATTERYWARNINGHBK575-1RADIO LINK
ELECTRICAL INSTALLATIONNORMARC 70334-27©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION4.11 Battery WarningTwo inputs for main power supply failure (backup battery active) are sited on the CI1210A connection interface board as illustrated in Figure 4-11Logic levels: Normally high 5V or 0V =battery warning.Input impedance: 10kohms.Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent.Figure4-11 Battery warning connections.TEMPINDOOR TEMPOUTDOOR ACLEVEL ANALOGCH.1 ANALOGCH.2 ANALOGCH.3 DIGITALPORT A DIGITALPORT B DIGITALPORT C DIGITALPORT DTO MB1203RS232 RS232 RS232 REMOTECONTROLDC-LOOP DC-LOOP DMELOCAL REMOTE 2 REMOTE 1 CH.1&2 CH.3&4BATTERYWARNING1 - BATT.WARN. CHARGER 12 - GND3 - BATT.WARN. CHARGER 24 - GNDCI 1210A14BATTERYWARNINGHBK602-2RADIO LINK
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONELECTRICAL INSTALLATION ©1999 Navia Aviation AS4-284.12 Remote control connectionsThe remote control is connected to the corresponding ILS by connecting the REMOTE CON-TROL connector on Connection Interface CI1210 to P9 on Motherboard MB1346, as shown in Figure 4-12.Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent. 600 ohms cable should be used.Figure4-12 Remote control to ILS connectionThe power supply to the remote control is connected according to Figure 4-13. The battery charger is connected to P2 on the MB1347 - power supply motherboard. Output connector P3 on MB1347 is connected to input connector P4 on MB1346 - remote control motherboard. Several MB1346's are serial linked by connecting P5 on one board to P4 on the next.Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent.REMOTECONTROL1 - GND2 - FSK_P3 - FSK_N4 - GNDJ2 P3P6P7P4P5P9P10P8NORMARCOPTO OUT2-ALARM (E)1-ALARM (C)4-NORM (E)5-WARN (C)6-WARN (E)7-STBAL (C)8-STBAL (E)3-NORM (C)GND5V24VV_DIMGND5V24VV_DIMPOWER OUT POWER INAUX IN/OUTSLAVEDIRECTINTERLOCKTXOFFALARMLINE ALINE BRX ARX BTX ATX BSLAVE RS485J1ABC153020251510ALT.LINKMB1346P91 - TXOFF2 - ALARM3 - LINE_A4 - LINE_BCI1210 on corresponding ILSorCI 1376oncorrespondingMarker BeaconHBK772-2
ELECTRICAL INSTALLATIONNORMARC 70334-29©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONFigure4-13 Remote control power supply connectionsJ2 P3P6P7P4P5P9P10P8NORMARCOPTO OUT2-ALARM (E)1-ALARM (C)4-NORM (E)5-WARN (C)6-WARN (E)7-STBAL (C)8-STBAL (E)3-NORM (C)GND5V24VV_DIMGND5V24VV_DIMPOWER OUT POWER INAUX IN/OUTSLAVEDIRECTINTERLOCKTXOFFALARMLINE ALINE BRX ARX BTX ATX BSLAVE RS485J1ABC153020251510ALT.LINKMB1346P2P3S1GND24VPOWER INGND5V24VV_DIMPOWER OUTV_DIM=24VMB1347NORMARC302520151051ABJ1J2 P3P6P7P4P5P9P10P8NORMARCOPTO OUT2-ALARM (E)1-ALARM (C)4-NORM (E)5-WARN (C)6-WARN (E)7-STBAL (C)8-STBAL (E)3-NORM (C)GND5V24VV_DIMGND5V24VV_DIMPOWER OUT POWER INAUX IN/OUTSLAVEDIRECTINTERLOCKTXOFFALARMLINE ALINE BRX ARX BTX ATX BSLAVE RS485J1ABC153020251510ALT.LINKMB1346From 24VDCpowersupplyHBK773-1
NORMARC 7033INSTRUMENT LANDING SYSTEMGENERAL DESCRIPTIONELECTRICAL INSTALLATION ©1999 Navia Aviation AS4-304.13 Remote slave connectionThe remote slave panel SF1344 is connected to the corresponding remote control's mother-board by connecting P3 on MB1346 to P1 on SF1344. P10 on MB1346 is not used. See Fig-ure 4-14.Suitable connectors are standard 25 pins female DSUB (Harting 0967 025 0442 and 0967 225 4704 or equivalent), connected by a 10 wire 1:1 cable.Figure4-14 Remote slave connectionJ2 P3P6P7P4P5P9P10P8NORMARCOPTO OUT2-ALARM (E)1-ALARM (C)4-NORM (E)5-WARN (C)6-WARN (E)7-STBAL (C)8-STBAL (E)3-NORM (C)GND5V24VV_DIMGND5V24VV_DIMPOWER OUT POWER INAUX IN/OUTSLAVEDIRECTINTERLOCKTXOFFALARMLINE ALINE BRX ARX BTX ATX BSLAVE RS485J1ABC153020251510ALT.LINKMB1346To P1 onSF134411314251 - GND2 - ALARM3 - WARNING4 - NORMAL7 - GND15 - V24P19 - ON_OFF21 - SILENCE23 - INTERLOCK (if used)25 - BUZZER1:1HBK 774-1
ELECTRICAL INSTALLATIONNORMARC 70334-31©1999 Navia Aviation ASINSTRUMENT LANDING SYSTEMGENERAL DESCRIPTION4.14 Interlock switch connectionThe interlock switch is either connected to P8 on MB1346 (remote control motherboard) or to P2 on SF1344 (remote slave panel), see Figure 4-15.Figure4-15 Interlock switch connectionNote:When MB1346A is used with Remote Control Assembly RCA1240C or D and Interlock func-tion is not used (connected), a jumper plug must be installed in P8 (or P2).21MB1346 / P8ORSF1344 / P2INTERLOCK SWITCHRWYA RWYB211212INTERLOCKGND1254 21LLZ runway AGP runway ALLZ runway BGP runway BHBK775-2

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