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About Barco About BarcoView Avionics Defense Air Traffic Control Vetronics C4I Avionics Vetronics Medical Imaging Medical I maging ATC BarcoView Geographical Locations Manufacturing, sales, support and marketing in four locations


  1. About Barco About BarcoView Avionics Defense Air Traffic Control Vetronics C4I Avionics Vetronics Medical Imaging Medical I maging ATC

  2. BarcoView Geographical Locations • Manufacturing, sales, support and marketing in four locations Duluth, Kortrijk, Georgia, USA Belgium Beaverton, Toulouse, France Oregon, USA

  3. Avionics

  4. BarcoView Avionics Mission Statement “Become a leader in Visualization and Associated Man-Machine Interfacing Subsystems for the cockpit environment”

  5. Market Approach • Avionics Display System Integrator • Active Matrix Liquid Crystal Display Technology • Modular Open System Architecture (MOSA) • Barco’s strength is in the integration of traditionally separate functions into the display – Symbol Generator – Avionics I nterfaces – Mission Processor – FMS • Intended for both New A/ C and Retrofit Market • Civil and Military versions are available (Dual use) • Suitable for Military Transport, Commercial Airliners, Commuter A/ C, BA A/ C, Fighter A/ C, Helicopters

  6. Airborne Platform Experience C-130 Hercules Super Puma RC-135 Rivet Joint T-33 Be-200 Tu-214 C-5 Galaxy V-22 Osprey C-27 Spartan Eurocopter Tiger

  7. Standard Avionics Display Product Groups COCKPIT MULTIFUNCTION DISPLAYS - Primary Flight Displays - Navigation Displays - Engine Instrument Displays - TAWS, Weather Radar Information VIDEO DISPLAY UNITS - Head Down Displays - Sensor Video - Digital Map CONTROL DISPLAY and MANAGEMENT SYSTEM - Control Display Units - Color Multifunction Displays - Integrated FMS Platform

  8. MFD-6.8 Multifunction Display Features 6x8 inch AMLCD 640x480 Resolution 0-200 fL NVG Compatibility Automatic Light Control PowerPC ARINC 429 Mil-Std-1553B Discrete I/ O ARINC 708-453 Weather Radar Synchro/ Analog 28VDC @ 70W MIL-STD-810E DO160D DO178B, Level B Cockpit Configuration Pilatus PC-21

  9. MFD-6.8 Split-Box Multifunction Display Optimized form factor for space-constrained applications. T-33 Il-114 Il-96 RC-135 SARAS C-130 Tu-324

  10. MFD-5.4 Multifunction Display Features 5x4 inch AMLCD 640x480 Resolution 0-200 fL NVG Compatibility Automatic Light Control PowerPC ARINC 429 Mil-Std-1553B Discrete I/ O ARINC 708-453 Eurocopter Super Puma Weather Radar Synchro/ Analog Video Input Options 28VDC @ 60W MIL-STD-810E DO160D DO178B, Level B

  11. CHDD-5.4 Video Display Unit Features 5x4 inch AMLCD 640x480 Resolution 0-200 fL NVG Compatibility Multiple Video Options: RS170 PAL/ NTSC Stanag 3350B/ C Mi-24 Hind VGA Smart Motion Deinterlacing Programmable Cropping RS-422 Display Control 28VDC @ 70W MIL-STD-810E BO-105 Cessna Encore 560

  12. CHDD-5.4 Split-Box Video Display Unit Optimized form factor for space-constrained applications.

  13. CHDD-6.8 Digital Video Display Unit Features 6x8 inch AMLCD 640x480 Resolution 0-200 fL NVG Compatibility LVDS Digital Video Interface RS-422 Keyboard Control Ambient Luminance Control 28VDC @ 60W MIL-STD-810E DO-160D Mako Demonstrator C-130

  14. Control Display and Management System Features 3x4 inch AMLCD 320x234 Resolution NVG Compatibility ARINC429 C-130J MIL-STD-1553 68360 or PowerPC 16+ Discrete I/ O Ada Programmable PCMCIA Data Loader Suitable for FMS Platform C-27J Eurocopter Tiger Be-200

  15. Rugged Optical Stack Unique bonding technique to protect the LCD against extreme environmental conditions and to significantly improve the optical performance AR Coating Protective Glass EMI Shield LCD Heater NVIS Filter Collimater Diffuser Backlight System

  16. Optical Performance • Less than 0.0008% defective sub-pixels • Greater than 2000: 1 dimming range for Non NVIS Stack • Greater than 8000: 1 dimming range for NVIS Stack • 200 fL maximum white luminance • 0.03 fL minimum white luminance with no flicker or uniformity degradation for NVIS B Stack • Less than 20% non-uniformity • Diffuse reflection less than 0.2% • Specular reflection less than 1.5% • Greater than 3: 1 contrast ratio when subjected to MIL-L- 85762A lighting conditions • Greater than 100: 1 peak contrast ratio under low ambient conditions • 64 Gray scale/ color performance providing 262,144 color/ gray scale combinations • NVIS Option compliance to Mil-L-85762A / Mil-Std-3009 • DUAL BACKLIGHT principle

  17. Barco Avionics Family Concept • Open Systems Architecture (OSA) – C-PCI – PowerPC – Ada – Arinc-249 – Mil-STD-1553 • Modularity – Processor board – Power Module – Interface Cards – Hardware options – Optical Stacks • Flexibility • Commonality – Reduced ILS cost – Identical SRUs for CDMS and MFD

  18. Qualification • CIVIL – RTCA - DO - 160D : Environmental Conditions – RTCA - DO - 178B : Software level B or C Level A for Single Pilot I FR • BARCO – TSO certification : Barco has TSO certification for the C130J CDU (CAA/ FAA) – ANSI 610A - III : Avionics Workmanship – FAR 21 : Certified as component Developer and Manufacturer for Civil Aviation according to the Belgian Ministerial decree n° 16471 – JAR 145 : Applied for – I SO 9001

  19. Qualification • Military – Mil - Std - 810 E : Environmental Specs – Mil - Std - 461/ 462 : EMI/ EMC measurement – Mil - Std - 704A : Electrical Power Requirements – Mil - Std - 498, 2167A: Software Certification • BARCO – AQAP 110 : R&D and Manufacturing – AQAP 150 : Pending – ANSI 610A - III : Avionics Workmanship – ISO 9001

  20. Environmental Qualification Test RTCA/DO-160D Mil-Std-810 General Limits High Temperature Sect. 4, B1 501.3, Proc II +55°C Oper (70 hrs.), +85°C Stor. Low Temperature Sect. 4, B1 502.3, Proc II -40°C Oper (20hrs.), -45°C Stor. Altitude Sect. 4, B1 500.3, Proc III 50,000 ft. Temperature Altitude Sect. 4, B1 504.1, Cat 5 -2K to 70K FT, -57°C to 71°C Humidity Sect. 6, B 507.3, Proc I 240Hrs @+25-60°C, 95% RH Shock Sect. 7, B 516.4, Proc I 15 g Oper Crash Safety Sect. 7 513.4 Acceleration 513.2, Proc I/II +16 g Vibration Sect. 8, T or T2 5.14.2, Cat B1, Pr I Three axis Rain (Drip-proof) Sect. 10, W 506.3, Proc II 280 l/m²/hr Fluid Susceptibility Sect. 11 Sand/Dust Sect. 12, D 510.3, Proc I&II Blowing sand & dust Fungus Sect. 13, F Analysis Explosive Atmosphere 511.3, Proc I 71°C, 50K FT Salt Fog Sect. 14, S 509.3, Proc I 48 Hr's Magnetic effect Sect. 15, Z 0.3m Bench Handling 516.4, Proc VI Solar Radiation 505.3, Proc I&II RE = (1120 ± 112) W/m2

  21. EMI/ EMC Qualification Test Mil-Std-461C RTCA/DO-160D Class Chapter, Category Conducted Emission, DC/AC Power Leads CE03, A1b 21.3a, Z Conducted Emission, power Leads, Spikes CE07, A1b none Conducted Susceptibility CS01, A1b 18, A Conducted Susceptibility DC/AC Power Leads CS02, A1b none 50kHz-400MHz Conducted Susceptibility, Power Leads, Spikes CS06, A1b none Conducted Susceptibility, Damped Sinusoidal CS11, A1b none Transients, Cables Radiated Emission, Electric Field RE02, A1b 21.4, Z Radiated Susceptibility, Magnetic Induction RS02, A1b none Radiated Susceptibility, Electric Field RS03, A1b 20.5, W Chattering Relay RS06,A1b 16.3.4, Z Induced Signal Susceptibility none 19.3.1 / 19.3.2 / 19.3.3 , Z Radio Frequency Conducted Susceptibility none 20.4, W Conducted Emission, Interconnect Cables none 21.3b, Z Lightning Induced Transient Susceptibility none 22, XXC2

  22. Future Growth possibilities/ options • GPS/GLONASS • High Performance Graphics • Additional Memory • Worldwide Data Base (Jeppesen) • Additional Interfacing capabilities • PCMCIA Data Loader Interface • Adaptability to different form factors • Fiber Optic • Customer selected processors • Customer selected Operating System • Voice Entry • Synthetic Voice • FANS • .......

  23. Display Symbology Autopilot Engage Indication Lateral Armed Mode Indication Comparator Warning Lateral Capture Mode Indication AHRS Source Vertical Capture Mode Indication Air Data Source SG Source Marker g Indicator Vertical Armed Mode Attitude Director Indicator Indication Airspeed Indicator Target Altitude Flight Director Indicator Glide Slope / Vertical Aircraft Symbol Navigation Indicator Expanded Localizer Indicator Altitude Indicator Decision Height Rising Runway Comparator Warning Mach Indicator DME and Hold Indicator Barometric Setting Comparator Warning Angle Of Attack Indicator Radio Altitude Rate Of Turn Indicator Bearing Pointer 1 Indicator FMS/LRN Message Desired Track Pointer Heading Bug position Bearing Pointer Source Vertical Speed Indicator Indicator Heading Compass Card Selected Course Indicator Ground Speed Indicator Comparator Warning Bearing Pointer 2 Indicator Navigation Source Indicator Wind Display Indicator

  24. Alternative Display Symbology

  25. Alternative Display Symbology

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