• BS 3G 100-3:1979

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    Specification for general requirements for equipment for use in aircraft Characteristics of aircraft electrical power supplies

    Available format(s):  Hardcopy, PDF

    Withdrawn date:  02-08-2013

    Language(s):  English

    Published date:  28-02-1979

    Publisher:  British Standards Institution

    Add To Cart

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

    Foreword
    Specification
    1 Scope
    2 Definitions
    3 General requirements
    4 Constant-frequency a.c. power system characteristics
    5 Variable-frequency a.c. power system characteristics
        (including rotorcraft applications)
    6 D.C. power system characteristics
    7 Utilization equipment
    8 Explanatory details
    Appendix
    A Transient voltage check tests
    Tables
    1 Steady-state a.c. voltage limits
    2 Steady-state d.c. voltage limits
    Figures
    1 Diagram of phase sequence and line designations
    2 R.M.S. voltage of components of voltage modulation
        envelope
    3 Characteristics of a.c. frequency modulation
    4 Envelopes for step-functions for a.c. surges
        (constant-frequency systems)
    5 Envelopes of frequency transients on a.c. supplies
    6 Envelopes for step-functions for a.c. surges
        (variable-frequency systems)
    7 Frequency characteristics of ripple in d.c. systems
    8 Envelopes for step-functions for d.c. surges where
        the d.c. power source is a d.c. generator or a TRU
        supplied from a variable-frequency a.c. system
    9 Envelopes for step-functions for d.c. surges where
        the d.c. power source is a TRU fed from a constant-
        frequency a.c. supply
    10 Power factor limits for a.c. equipment
    11 Conversion of a transient voltage surge to its
        equivalent step functions
    12 Typical voltage spike test arrangement
    13 Voltage spike waveform

    Abstract - (Show below) - (Hide below)

    Gives characteristics of electrical power supplied to the terminals of airborne equipment and provides limits for those aspects of utilization equipment that may adversely affect the characteristics of electrical power supplied to other equipment. Aims to achieve compatibility between airborne utilization equipment and aircraft electrical power supplies. Includes transient voltage check tests.

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

    Committee ACE/6
    Development Note Partially supersedes BS 2G100-2(1962) Supersedes 76/75818 DC and BS 3G100-3(1972) (07/2005) Inactive for the new design. (11/2009)
    Document Type Standard
    Publisher British Standards Institution
    Status Withdrawn

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

    BS 2G 219:1983 Specification for general requirements for ground support electrical supplies for aircraft
    ISO 7137:1995 Aircraft — Environmental conditions and test procedures for airborne equipment
    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective