BS ISO 1540:2006
航空航天.飞机电气系统特性

Aerospace - Characteristics of aircraft electrical systems

BS ISO 1540:2006 发布历史

This International Standard 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 this International Standard because of the penalties associated with multi-application. This document 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.

BS ISO 1540:2006由英国标准学会 GB-BSI 发布于 2006-04-28，并于 2006-04-28 实施。

BS ISO 1540:2006 在中国标准分类中归属于: V40 电气系统与设备，在国际标准分类中归属于: 49.060 航空航天用电气设备和系统。

BS ISO 1540:2006的历代版本如下：

• 2006年 BS ISO 1540:2006 航空航天.飞机电气系统特性

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标准号

BS ISO 1540:2006

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2006年

发布单位

英国标准学会

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BS ISO 1540:2006

 

 

适用范围

This International Standard 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 this International Standard because of the penalties associated with multi-application. This document 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.

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