• SAE AS 6858 : 2017

    Current The latest, up-to-date edition.

    INSTALLATION OF FUEL CELL SYSTEMS IN LARGE CIVIL AIRCRAFT

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  02-03-2017

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. REFERENCES
    3. GENERAL
    4. FCS INTEGRATION WITH THE AIRCRAFT
    5. SAFETY
    6. PROOF AND BURST
    7. MATERIAL COMPATIBILITY
    8. AFFECTED CERTIFICATION REQUIREMENTS
    9. ENVIRONMENTAL
    10. GASEOUS H2 STORAGE AND DISTRIBUTION
    11. OXIDANT SUPPLY AND DISTRIBUTION
    12. FUEL CELL MODULE CONSIDERATIONS
    13. BALANCE OF PLANT CONSIDERATIONS
    14. THERMAL MANAGEMENT CONSIDERATIONS
    15. CONTROLLER / SYSTEM INTERFACE CONSIDERATIONS
    16. SENSORS
    17. ELECTRICAL POWER CONDITIONING
    18. POWER STORAGE
    19. ELECTRICAL POWER INTERFACE
    20. MAINTENANCE
    21. NOTES

    Abstract - (Show below) - (Hide below)

    Describes the technical requirements for the safe integration of gaseous hydrogen fueled Proton Exchange Membrane (PEM) Fuel Cell Systems (FCS) within the aircraft.

    General Product Information - (Show below) - (Hide below)

    Document Type Standard
    Publisher SAE International
    Status Current

    Standards Referencing This Book - (Show below) - (Hide below)

    EN 2282 : 1992 AEROSPACE SERIES - CHARACTERISTICS OF AIRCRAFT ELECTRICAL SUPPLIES
    SAE AIR 6464 : 2013 EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES
    RTCA DO 347 : 2013 CERTIFICATION TEST GUIDANCE FOR SMALL AND MEDIUM SIZED RECHARGEABLE LITHIUM BATTERIES AND BATTERY SYSTEMS
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    ISO 11119-2:2012 Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 2: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450 l with load-sharing metal liners
    MIL STD 704 : F AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    SAE AIR 825/13 : 2003 GUIDE FOR EVALUATING COMBUSTION HAZARDS IN AIRCRAFT OXYGEN SYSTEMS
    SAE AIR 1957 : 2015 HEAT SINKS FOR AIRBORNE VEHICLES
    SAE ARP 4418 : 2008 PROCEDURE FOR SAMPLING AND MEASUREMENT OF ENGINE AND APU GENERATED CONTAMINANTS IN BLEED AIR SUPPLIES FROM AIRCRAFT ENGINES
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    SAE AS 8010 : 2012 AVIATOR'S BREATHING OXYGEN PURITY STANDARD
    MIL DTL 7891 : G FILLER VALVE, AIRCRAFT OXYGEN
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    RTCA DO 227 : A2017 MINIMUM OPERATIONAL PERFORMANCE STANDARDS (MOPS) FOR NON-RECHARGEABLE LITHIUM BATTERIES
    IEC 60952-3:2013 Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP)
    SAE J 2601 : 2016 FUELING PROTOCOLS FOR LIGHT DUTY GASEOUS HYDROGEN SURFACE VEHICLES
    IEC 60952-2:2013 Aircraft batteries - Part 2: Design and construction requirements
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    SAE ARP 5021 : 2016 OXYGEN CYLINDER INSTALLATION GUIDE
    RTCA DO 293 : A2009 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR NICKEL-CADMIUM, NICKEL METAL-HYDRIDE, AND LEAD ACID BATTERIES
    SAE ARP1870A:1987(S2012) Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)
    SAE AS 861 : 2016 MINIMUM GENERAL STANDARDS FOR OXYGEN SYSTEMS
    SAE AIR 1277 : 2005 COOLING OF MILITARY AVIONIC EQUIPMENT
    SAE ARP 1532 : 2015 AIRCRAFT OXYGEN SYSTEM LINES, FABRICATION, TEST AND INSTALLATION
    SAE AIR 1059 : 2014 OXYGEN CYLINDER QUALITY, SERVICEABILITY, MAINTENANCE TRANSFILLING AND MARKING
    EN 2570 : 1996 AEROSPACE SERIES - NICKEL-CADMIUM BATTERIES - TECHNICAL SPECIFICATION
    FAA AC 20-184 : 2015 GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT
    SAE J 2579 : 2013 STANDARD FOR FUEL SYSTEMS IN FUEL CELL AND OTHER HYDROGEN VEHICLES
    SAE AIR 1168/8 : 2011 AIRCRAFT FUEL WEIGHT PENALTY DUE TO AIR CONDITIONING
    ISO 11119-1:2012 Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 1: Hoop wrapped fibre reinforced composite gas cylinders and tubes up to 450 l
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    SAE AIR 64 : 1992 ELECTRICAL AND ELECTRONIC EQUIPMENT COOLING IN COMMERCIAL TRANSPORTS
    UL 1642 : 5 LITHIUM BATTERIES
    IEC 60952-1:2013 Aircraft batteries - Part 1: General test requirements and performance levels
    AIAA G 095 : 2004 GUIDE TO SAFETY OF HYDROGEN AND HYDROGEN SYSTEMS
    ISO 11119-3:2013 Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 3: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450L with non-load-sharing metallic or non-metallic liners
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