Leidos NORMARC7013 Users Manual

NORMARC 7013
INSTRUMENT LANDING SYSTEM
GENERAL DESCRIPTION
©1999 Navia Aviation AS
©1999 Navia Aviation AS
GENERAL DESCRIPTIONNORMARC 7013
INSTRUMENT LANDING SYSTEM
DESCRIPTION OF NORMARC 7013 2-FREQUENCY LOCALIZER SYSTEM.1
1 GENERAL DESCRIPTION..............................................................................1
1.1 Technical Specifications.....................................................................................1
1.1.1 Signal Minimum Performance LLZ ..............................................................1
1.1.2 Environmental Characteristics.....................................................................2
1.1.3 EMC Characteristics.................................................................................... 2
1.1.4 Mechanical Characteristics..........................................................................2
1.1.5 Power Supply............................................................ .. .. ......................... .. ....3
1.2 General Informati on................... .........................................................................3
1.2.1 Introduction.................................................................................................3
1.2.2 Product Type Numbers........................................... ................................. ....6
1.2.3 Abbreviations...............................................................................................6
2 PHYSICAL ORGANIZATION...........................................................................8
2.1 Module and Assembly Location.........................................................................8
2.2 Power Supply...................... .. ........................ .. ........................ ....................... ....8
3 SYSTEM DESCRIPTION.................................................................................12
3.1 Overview ............................................................................................................ 12
3.2 Physical Description...........................................................................................12
3.3 Monitors..............................................................................................................13
3.4 Transmitters / Modulators.................................. .................... .............................13
3.5 TX Control ...... .. ............................. ............... ............................. ............... ..........13
3.6 Remote Monit o ri n g (R MS) Unit......... .. .. ................ ............... ................ .............. 14
3.7 Remote Control Unit...........................................................................................14
3.8 Remote Slave Panel...........................................................................................14
3.9 Remote Maintenance Monitoring (RMM) ..................................................... ......14
3.9.1 RMM Access................................................................................................16
3.9.2 Local Keyboard/Display Functions ..............................................................16
3.9.3 Diagnostic functions...................................................... .. .................... .........17
4 ELECTRICAL INSTALLATION........................................................................18
4.1 Connection Overview.........................................................................................18
4.2 Power and Battery................... .................... .................... .. .................... .............18
4.3 RF Inputs............................................................................................................20
4.4 RF Outputs....... .. .. ................ ............................ ................ ............... ................ ...20
4.5 DC Loop........................ ................ ............... ............... ................ .......................21
4.6 Remote Control..................................................................................................22
4.7 PC and Modem..................................................................................................23
4.8 DME ...................................................................................................................24
4.9 Analog Inputs.....................................................................................................25
4.10 Digital Inputs and Outputs..................................................................................26
4.11 Batte ry Wa rn i n g ............... ................ .. ............... ................ ............... ................ ...27
4.12 Remote control connections...............................................................................28
4.13 Remote slave connection.................................................................. .................30
4.14 Interlock switch connection............................. .................. .................. ...............31
©1999 Navia Aviation AS Table of contents
iii
GENERAL DESCRIPTION
NORMARC 7013
INSTRUMENT LANDING SYSTEM
Table of contents ©1999 Navia Aviation AS iv
GENERAL DESCRIPTIONNORMARC 7013
INSTRUMENT LANDING SYSTEM
LIST OF FIGURES
Figure1-1 Typical ILS installation ..........................................................................3
Figure1-2 Localizer block d i ag ra m ... .. ............... ................ ............................. .......4
Figure1-3 Localizer Antenna .................................................................................5
Figure1-4 Localizer Cabin e t In s ta llation ...................................... ............... ..........5
Figure2-1 NM 7013 Module Location - Front view. ...............................................9
Figure2-2 NM 7013 Module Location - Rear view of main section. ......................10
Figure2-3 NM 7013 Module Location - Front view of wall-mounted section .........11
Figure3-1 ILS block diagram. ................................................................................12
Figure3-2 The NM 7000 series RMM/RMS systems. ...........................................15
Figure3-3 Local Control Panel ..............................................................................17
Figure4-1 ILS main cabinet connection overview. ................................................18
Figure4-2 Power and backup battery connections. ..............................................19
Figure4-3 RF input connections. ...........................................................................20
Figure4-4 RF output connections. ........................................................................20
Figure4-5 DC loop connections. ...........................................................................21
Figure4-6 Remote control connection. .................... ..............................................22
Figure4-7 PC and modem connections. ...............................................................23
Figure4-8 DME connections. ................................................................................24
Figure4-9 Analog input connections. ................................. .. .................................25
Figure4-10 Digital input/output connections. ..........................................................26
Figure4-11 Battery warning connections. ...............................................................27
Figure4-12 Remote control to ILS connection ........................................................28
Figure4-13 Remote control power supply connections ................. .. .................... ....29
Figure4-14 Remote slave connection ........................... ...................... ....................30
Figure4-15 Interlock switch connection .......................... .................. ......................31
©1999 Navia Aviation AS List of Figures
v
GENERAL DESCRIPTION
NORMARC 7013
INSTRUMENT LANDING SYSTEM
List of Figures ©1999 Navia Aviation AS vi
INSTRUMENT LANDING SYSTEM
OPERATING MANUALNORMARC 7013
LIST OF TABLES
©1999 Navia Aviation AS 21446-3.4 List of tables
vii
OPERATING MANUAL
NORMARC 7013
INSTRUMENT LANDING SYSTEM
List of tables ©1999 Navia Aviation AS viii
21446-3.4
NORMARC 7013
INSTRUMENT LANDING SYSTEM
GENERAL DESCRIPTION
DESCRIPTION OF NORMARC 7013 2-FREQUENCY LOCALIZER SYS-
TEM

1 General Description

1.1 Technical Specifications

NM 7013 Dual-Frequency Localizer Cabinet.

1.1.1 Signal Minimum Performance LLZ

Transmitter
Frequency range 108-112 MHz Frequency tolerance + Output power (CSB) 5-15 W adjustable Harmonic radiation 2.5 uW maximum RF difference frequency (2-freq. only) 10 kHz + Spurious 25 uW maximum Output power stability + CSB/SBO stability +
Modulator
Modulation depth 90/150 Hz 20%
adjustable range 10-25% SDM stability +
DDM stability + Frequency tolerance + Total harmonic dist. (90/150 Hz) 1% maximum Phase locking (90 Hz to 150 Hz) 5° maximum ref 150 Hz SBO phaser adjustment range +
0.002%
2 kHz
0.2 dB
0.3 dB / +-5°
0.3% SDM
0.1% DDM
0.05 Hz
10°
Identity Keyer
Modulation frequency 1020 Hz + Modulation depth 5-15% adjustable Distortion 6% Maximum Speed of identification 7 Words/Min. approx.
Monitoring
Alarm Functions Range (*) RF power reduction 1-5 dB Change of nominal CL + Change of nominal DS from nominal
value Change of nominal CLR (2-freq only) + Change of nominal NF + Change of nominal SDM + Difference frequency (2-f req. only) + Total period of radiation out of tolerance 1-10 sec.
©1999 Navia Aviation AS
4-25 uA
+
10-50 uA
10-60 uA 4-25 uA 2-6% SDM 2-5 kHz
10 Hz
GENERAL DE SCRIPTION
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GENERAL DESCRIPTION
Additional NF time delay 0-20 sec. Line break, ILS - Remote Control (disa-
ble optional) Identification lost or continuous
(optional) Monitor input levels:
Adjustment range, nominal level -5 to –34 dBm
AGC range for less than 1%
change in SDM Monitor stability at nominal levels:
RF power values +
DDM values +
SDM values + Warning Functio ns:
RF power reduction 40-75% of Alarm limit
Change of nominal CL 40-75% of Alarm limit
Change of nominal DS 40-75% of Alarm limit
Change of nominal CLR 40-75% of Alarm limit
Change of nominal NF 40-75% of Alarm limit
Change of SDM 40-75% of Alarm limit
Difference frequency 40-75% of Alarm limit
Mains failure Remote Control
Data Transmission Medium 2-wire line, 600 ohm
Data modulation serial, FSK
Transmitter level -10dBm +
Receiver dynamic range -10dBm to -34dBm
NORMARC 7013
INSTRUMENT LANDING SYSTEM
5 dB
0,2 dB 1 uA 0,5% SDM
2 dB
* asymmetrical limits are possibl e.

1.1.2 Environmental Characteristics

Operating temperature -10 to +55 °C Storage temperature -30 to +60 °C

1.1.3 EMC Characteristics

EMR: EN 55022 class B Spurious and harmonics: CISPR 22

1.1.4 Mechanical Characteristics

Dimensions: (H x W x D)
ILS Rack: 1020x600x500 mm Remote control: 129x71x170 mm Slave panels: 129x41x170 mm
Weight: 85 kg – 95 kg depending on model
GENERAL DESCRIPTION ©1999 Navia Aviation AS
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NORMARC 7013
INSTRUMENT LANDING SYSTEM
GENERAL DESCRIPTION
The ILS rack is wall mounted. The remote control an d slave panel s fit a st andard 3U (132mm) high 19" subrack.

1.1.5 Power Supply

External supply:
Input voltage: 230V +15%/-20%,45-65 Hz or120V +15%/-20%,
45-65 Hz Output voltage: 27,6V Output current: 20A max
ILS cabinet
Input voltage 22-28V DC Current consumption: 8A – 14A depending on configuration Stand-by Battery 24V DC nominal, 85 Ah-110Ah valve regulated
lead-acid battery recommended

1.2 General Information

This paragraph gives a description of a typical ILS installation and the Normarc Localizer sys­tem. Conventions and abbreviations used in this manual are also given.

1.2.1 Introduction

This is an overview of Normarc's NM701X ILS localizer systems

1.2.1.1 ILS Overview

A complete Instrument Landing System comprises:
A LOCALIZER SYSTEM, producing a radio course to furn ish lateral guidance to th e 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.
The layout of a typical ILS airport installation is shown below.
Glide Path 330 MHz
Localizer 110 MHz
Marker Beacon
©1999 Navia Aviation AS
75MHz
HBK547-1
Figure1-1 Typical ILS installation
GENERAL DE SCRIPTION
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GENERAL DESCRIPTION

1.2.1.2 Localizer Overview

The complete ILS Localizer system comprises:
A LLZ transmitter/monitor cabinet
An antenna distribution network
A monitor network
A LLZ antenna array
Near-field monitor antenna
A block diagram is shown below:
ILS LOCALIZER
TRANSMITTER
NORMARC 7013
INSTRUMENT LANDING SYSTEM
LOCALIZER ANTENNA
ARRAY
ILS Localizer
REMOTE
CONTROL
UNIT
SLAVE PANEL
RMM SYSTEM
TRANSMITTER
AND
MODULATOR
I and II
MONITOR I and II
CSB CL SBO CL CSB CLR* SBO CLR*
CL CLR* DS
NF
ANTENNA DISTRIBU­TION NETW.
MONITOR
NETWORK
24V
BATTERY
POWER
SUPPLY
MAINS INPUT
220V/110V AC
* CLR SIGNALS N/A on single-frequency equipment
Figure1-2 Localizer block diagram
RUNWAY CL.
MONITOR OUTPUT PROBE
HBK204-1
GENERAL DESCRIPTION ©1999 Navia Aviation AS
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