ISO 1540:2006
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The latest, up-to-date edition.
Aerospace — Characteristics of aircraft electrical systems
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English
02-08-2006
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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