• BS G 261-1:1996

    Current The latest, up-to-date edition.

    Specification for aircraft. Electromagnetic relays and contactors General requirements

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  15-07-1996

    Publisher:  British Standards Institution

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

    Committees responsible
    National foreword
    Specification
    1 Scope
    2 Normative references
    3 Definitions
    4 General requirements
    5 Performance detail requirements
    6 Tests
    7 Qualification
    Annexes
    A Example of an individual specification sheet
    B Bibliography
    Tables
    1 Strength of threaded terminals
    2 Contact arrangements, symbols and terminal marking
    3 Auxiliary terminals
    4 Symbols and marking for terminals
    5 Dual coil markings
    6 Dissimilar metals
    7 Contact circuit voltage drop
    8 Minimum values for high voltage tests
    9 Pull force
    10 Categorization of standard vibration test requirements by
        aircraft types and equipment locations
    11 Categorization of severe vibration test requirements for
        fixed-wing turbojet engine aircraft and equipment
        locations
    12 Overload values and durations
    13 Rupture values and durations
    14 Duty cycle
    15 Contact voltage drop
    16 Untitled
    17 Contaminant test temperatures
    18 Untitled
    19 Untitled
    20 Production acceptance tests
    21 Qualification inspection
    Figures
    1 Inspection aid
    2 Contact bounce (typical circuit)
    3 Electromagnetic interference test circuit
    4 Typical transient voltage
    5 Range curve for vibration tests
    6 Standard random vibration test curves for equipment
        installed in fixed-wing aircraft with turbojet engines
    7 Standard sinusoidal vibration test curves for equipment
        installed in fixed-wing aircraft with turbojet engines
    8 Standard sinusoidal vibration test curves for equipment
        installed in fixed-wing aircraft with reciprocating or
        turbopropeller engines
    9 Standard sinusoidal vibration test curves for equipment
        installed in helicopters
    10 Robust random vibration test curves for equipment
        installed in fixed-wing aircraft with turbojet engines
    11 Test circuit, three-phase load transfer
    12 Alternative test circuit, three-phase load transfer

    Abstract - (Show below) - (Hide below)

    States the performance requirements for electromagnetic relays and contactors for use in nominal 28 V d.c. or 115 V/200 V3-phase, 400 Hz a.c. systems with characteristics as in ISO 1540, particularly the performance requirements for relays and contactors with nominal contact ratings of 5 A a.c., 5 A d.c or greater. It applies to single-pole and multi-pole relays and contactors.

    Scope - (Show below) - (Hide below)

    This part of ISO 5867 specifies the performance requirements for electromagnetic relays and contactors for use in nominal 28 V d.c. or 115 V/200 V 3-phase, 400 Hz, a.c. systems having the characteristics specified in ISO 1540.

    This part of ISO 5867 specifies the performance requirements for relays and contactors having nominal contact ratings of 5 A a.c., 5 A d.c. or greater. Auxiliary contacts, where applicable, may be rated at lower currents. Three temperature classes and three classes of sealing are specified.

    This part of ISO 5867 is applicable to single-pole and multi-pole relays and contactors, electromagnetically operated and magnetically held, or electromagnetically operated and mechanically or magnetically latched, controlled by a voltage of 28 V d.c. or 115 V, 400 Hz, a.c.

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

    Committee ACE/6
    Development Note Supersedes 94/706953 DC. Also numbered as ISO 5867-1. (06/2005)
    Document Type Standard
    Publisher British Standards Institution
    Status Current
    Supersedes

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

    ISO 1540:2006 Aerospace — Characteristics of aircraft electrical systems
    IEC 60158-2:1982 Low-voltage controlgear. Part 2: Semiconductor contactors (solid state contactors)
    ISO 2635:2003 Aircraft Conductors for general purpose aircraft electrical cables and aerospace applications Dimensions and characteristics
    ISO/R 224:1961 Standard form of declaration of performance of aircraft electrical equipment
    IEC 60050-446:1983 International Electrotechnical Vocabulary (IEV) - Part 446: Electrical relays
    IEC 60068-2-17:1994 Basic environmental testing procedures - Part 2-17: Tests - Test Q: Sealing
    BS EN 60068-2-17:1995 Environmental testing. Test methods Test Q. Sealing
    BS 4G 229:1996 Schedule for environmental conditions and test procedures for airborne equipment
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