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  • BS ISO 18170:2017

    Current The latest, up-to-date edition.

    Aerospace series. AC induction electric motor driven, variable delivery, hydraulic pumps. General requirements

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  24-05-2017

    Publisher:  British Standards Institution

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

    Foreword
    1 Scope
    2 Normative references
    3 Terms and definitions
    4 General requirements
    5 Functional requirements
    6 Detailed design requirements
    7 Strength requirements
    8 Construction
    9 Installation requirements
    10 Maintenance
    11 Reliability
    12 Quality assurance provisions
    13 Acceptance tests
    14 Qualification tests
    Bibliography

    Abstract - (Show below) - (Hide below)

    Describes the general requirements for electric motor driven, variable delivery, hydraulic pumps suitable for use in aircraft hydraulic systems.

    Scope - (Show below) - (Hide below)

    This document establishes the general requirements for electric motor driven, variable delivery, hydraulic pumps suitable for use in aircraft hydraulic systems.

    This document includes the general requirements for Alternating Current (AC) induction electric motor powered units. The AC power electrical power supply can be either controlled to provide a Constant Frequency (CF) or uncontrolled to provide a Variable Frequency (VF) AC supply to the electric motor.

    This document is intended to be used in conjunction with the detail specification that is particular to each application.

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

    Committee ACE/69
    Development Note Supersedes 16/30282578 DC. (05/2017)
    Document Type Standard
    Publisher British Standards Institution
    Status Current
    Supersedes

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

    ISO 7320:1992 Aerospace Couplings, threaded and sealed, for fluid systems Dimensions
    ISO 8078:1984 Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, undyed coating
    ISO 1540:2006 Aerospace — Characteristics of aircraft electrical systems
    ISO 8625-2:1991 Aerospace Fluid systems Vocabulary Part 2: General terms and definitions relating to flow
    ISO 3323:1987 Aircraft — Hydraulic components — Marking to indicate fluid for which component is approved
    ISO 6771:2007 Aerospace Fluid systems and components Pressure and temperature classifications
    ISO 8625-1:1993 Aerospace Fluid systems Vocabulary Part 1: General terms and definitions related to pressure
    ISO 11218:2017 Aerospace Cleanliness classification for hydraulic fluids
    ISO 8079:1984 Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, dyed coating
    ISO 2093:1986 Electroplated coatings of tin — Specification and test methods
    ISO 7137:1995 Aircraft — Environmental conditions and test procedures for airborne equipment
    ISO 3601-1:2012 Fluid power systems — O-rings — Part 1: Inside diameters, cross-sections, tolerances and designation codes
    ISO 2669:1995 Environmental tests for aircraft equipment — Steady-state acceleration
    ISO 8081:1985 Aerospace process Chemical conversion coating for aluminium alloys General purpose
    ISO 8278:2016 Aerospace series Hydraulic, pressure compensated, variable delivery pumps General requirements
    ISO 2671:1982 Environmental tests for aircraft equipment — Part 3.4 : Acoustic vibration
    ISO 8625-3:1991 Aerospace Fluid systems Vocabulary Part 3: General terms and definitions relating to temperature
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