• SAE ARP 6154 : 2017

    Current The latest, up-to-date edition.

    AEROSPACE FLUID POWER ELECTROHYDROSTATIC MODULE, DESIGN, PERFORMANCE AND TEST RECOMMENDATIONS

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  15-03-2017

    Publisher:  SAE International

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

    1. SCOPE
    2. REFERENCES
    3. PROCUREMENT SPECIFICATIONS
    4. ENVIRONMENTAL REQUIREMENTS
    5. TEST REQUIREMENTS
    6. NOTES

    Abstract - (Show below) - (Hide below)

    This Aerospace Recommended Practice provides general requirements for Electrohydrostatic Module (EHM) that is used in Electrohydrostatic Actuator (EHA) for aerospace applications.

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

    Committee A-6B2
    Document Type Standard
    Publisher SAE International
    Status Current

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

    SAE AS 5994A:2000(S2013) PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    SAE AIR 1922 : 2017 AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    ISO 22072:2011 Aerospace — Electrohydrostatic actuator (EHA) — Characteristics to be defined in procurement specifications
    ISO 2678:1985 Environmental tests for aircraft equipment — Insulation resistance and high voltage tests for electrical equipment
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    SAE ARP 4493 : 2013 AEROSPACE - DIRECT DRIVE SERVOVALVES
    MIL-PRF-87257 Revision C:2017 HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE
    SAE AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
    SAE AS 1241 : 2016 FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT
    MIL-PRF-83282 Revision D:1997 HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537
    SAE AS 4059F : 2013 AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS
    SAE ARP 4386 : 2010 TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES
    SAE AS 4941 : 2015 AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS
    SAE AS 595 : 2015 AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP
    SAE ARP 1383 : 2013 AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS
    ISO 2669:1995 Environmental tests for aircraft equipment — Steady-state acceleration
    SAE ARP 490 : 2008 ELECTROHYDRAULIC SERVOVALVES
    SAE ARP 5879 : 2010 AEROSPACE - TEST METHODOLOGY FOR ELECTROHYDROSTATIC ACTUATORS
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