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ISO 1540:2006

Current

Current

The latest, up-to-date edition.

Aerospace — Characteristics of aircraft electrical systems

Available format(s)

Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English

Published date

02-08-2006

US$225.00
Excluding Tax where applicable

ISO 1540:2006 specifies the characteristics of electrical power supplied to the terminals of electrical utilization equipment installed in an aircraft. It is intended to support the interface definition for user equipment designed to accept electrical power on a variety of new civil aircraft applications, such as those certified via the Technical Standard Order (TSO) certification process. It might not be desirable for equipment targeted to a single application or specific military application to follow ISO 1540:2006 because of the penalties associated with multi-application.

ISO 1540:2006 also attempts to provide background to the development of these requirements that may be useful to those designing and/or integrating modern aircraft electrical systems. The delivered quality of this electrical power is a result of the combined characteristics of the electrical power source, distribution and user equipment. While only user equipment restrictions are specifically defined, background to key source and distribution equipment interfaces are identified in order to support development of the overall system.

A wide variety of electrical supply types and distribution parameters have been considered, as may be found on both small and large transport aircraft. Sources considered include physically rotating and static types, provided either on-aircraft, or as part of the ground support equipment. Distribution voltages addressed are

  • nominal 14 V, 28 V and 42 V d.c.;
  • nominal 26 V a.c., 400 Hz, one-phase;
  • nominal 115/200 V rms and 230/400 V rms a.c., both one-phase and three-phase, at either a nominal 400 Hz constant frequency (CF), or over a variable frequency (VF) range which includes 400 Hz.

Committee
ISO/TC 20/SC 1
DevelopmentNote
Supersedes ISO 222 (04/2001) Supersedes ISO/DIS 1540 (02/2006)
DocumentType
Standard
Pages
56
PublisherName
International Organization for Standardization
Status
Current
Supersedes

Standards Relationship
BS ISO 1540:2006 Identical

13/30265035 DC : 0 BS ISO 27027 - AEROSPACE - SOLID-STATE REMOTE POWER CONTROLLERS - GENERAL PERFORMANCE REQUIREMENTS
DEFSTAN 00-76(PT1)/1(2005) : INTERIM ASAAC STANDARDS - PART 1: PROPOSED STANDARDS FOR COMMON FUNCTIONAL MODULES
18/30334464 DC : 0 BS ISO 20949 - AIRCRAFT - SMART CONTACTOR - GENERAL REQUIREMENTS
PREN 4660-002 : 200P1 AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 002: FINAL DRAFT OF PROPOSED STANDARDS FOR COMMON FUNCTIONAL MODULES
ISO 12384:2010 Aerospace — Requirements for digital equipment for measurements of aircraft electrical power characteristics
NF EN 4660-002 : 2011 AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 002: COMMON FUNCTIONAL MODULES
ISO 27027:2014 Aerospace Solid-state remote power controllers General performance requirements
BS 2G 219:1983 Specification for general requirements for ground support electrical supplies for aircraft
STANAG 3456 : 0 AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS
SAE ARP 5584 : 2011 DOCUMENT FOR ELECTRIC POWER MANAGEMENT
I.S. EN 4660-002:2011 AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 002: COMMON FUNCTIONAL MODULES
ISO 2277:1973 Static invertors for aircraft
DIN EN 2282:1992-05 AEROSPACE SERIES; CHARACTERISTICS OF AIRCRAFT ELECTRICAL SUPPLIES
BS ISO 18170:2017 Aerospace series. AC induction electric motor driven, variable delivery, hydraulic pumps. General requirements
15/30290190 DC : 0 BS ISO 6858 - AIRCRAFT - GROUND SUPPORT ELECTRICAL SUPPLIES - GENERAL REQUIREMENTS
PREN 2282 : 200P1 AEROSPACE SERIES - CHARACTERISTICS OF AIRCRAFT ELECTRICAL SUPPLIES
ISO 18170:2017 Aerospace series — AC induction electric motor driven, variable delivery, hydraulic pumps — General requirements
SAE ARP 5015 : 2011 GROUND EQUIPMENT - 400 HERTZ GROUND POWER PERFORMANCE REQUIREMENTS
EN 2282:1992 Aerospace series - Characteristics of aircraft electrical supplies
STANAG 4626 : 2013 MODULAR AND OPEN AVIONICS ARCHITECTURE
10/30197456 DC : 0 BS ISO 12384 - AEROSPACE - REQUIREMENTS FOR DIGITAL EQUIPMENT FOR MEASUREMENTS OF AIRCRAFT ELECTRICAL POWER CHARACTERISTICS
BS G 261-1:1996 Specification for aircraft. Electromagnetic relays and contactors General requirements
BS ISO 27027:2014 Aerospace. Solid-state remote power controllers. General performance requirements
EN 4660-002:2011 Aerospace series - Modular and Open Avionics Architectures - Part 002: Common Functional Modules
BS ISO 12384:2010 Aerospace. Requirements for digital equipment for measurements of aircraft electrical power characteristics
BS EN 4660-002:2011 Aerospace series. Modular and open avionics architectures Common functional modules
16/30282578 DC : 0 BS ISO 18170 - AEROSPACE - AC INDUCTION ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, HYDRAULIC PUMPS - GENERAL REQUIREMENTS
ISO 6858:2017 Aircraft — Ground support electrical supplies — General requirements

ISO 6858:1982 Aircraft Ground support electrical supplies General requirements
ISO 7137:1995 Aircraft — Environmental conditions and test procedures for airborne equipment

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