V40 电气系统与设备 标准查询与下载

ARMY MIL-STD-1275 D-2006 在军用车辆上的28伏直流电.电气系统规格参数表

This standard covers the limits of steady state and transient voltage characteristics 28 VDC electrical power systems for military ground vehicles.

CHARACTERISTICS OF 28 VOLT DC ELECTRICAL SYSTEMS IN MILITARY VEHICLES

SAE ARP378C-2006 乘客阅读灯

The purpose of this SAE Aerospace Recommended Practice (ARP) is to recommend minimum design criteria which will lead to adequate performance standards for passenger reading lights in aircraft. This document presents criteria for design and location of passenger reading lights in commercial aircraft.

Passenger Reading Lights

BS DD IEC/TS 62396-1:2006 航空电子设备过程管理.大气辐射效应.调节航空电子设备内经单粒子效应的大气辐射作用

This Technical Specification is intended to provide guidance on Atmospheric Radiation effects on Avionics electronics used in aircraft operating at altitudes up to 60 000 feet (18,3 km). It defines the radiation environment, the effects of that environment on electronics and provides design considerations for the accommodation of those effects within avionics systems. This Technical Specification is intended to help aerospace equipment manufacturers and designers to standardise their approach to Single Event Effects in Avionics by providing guidance, leading to a standard methodology. Details of the radiation environment are provided together with identification of potential problems caused as a result of the atmospheric radiation received. Appropriate methods are given for quantifying Single Event Effect (SEE) rates in electronic components. The overall system safety methodology should be expanded to accommodate the Single Event Effects rates and to demonstrate the suitability of the electronics for the application at the component and system level.

Process management for avionics - Atmospheric radiation effects - Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment

AECMA PREN 2854-003-2006 航天系列电缆,电气,通用截面等于和大于9平方mm操作温度之间-55摄氏度和260摄氏度的一部分003:一般

This "Aerospace series" Standard has been drawn up under the responsibilit of AECMA.

Aerospace series Cables, electrical for general purpose Cross sections equal to and greater than 9 mm2 Operating temperatures between - 55 癈 and 260 癈 Part 003: Product standard Edition P 2

AECMA PREN 2854-002-2006 航天系列电缆,电气,通用截面等于和大于9平方mm操作温度之间-55摄氏度和260摄氏度的一部分002:一般

This draft is now available for public comment and your views and technical comments on it would be appreciated. If you have no specific comments to make but find it generally acceptable it would be helpful if you would notify us accordingly. Suggestions entailing revision of the text should indicate the preferred wording.

Aerospace series Cables, electrical for general purpose Cross sections equal to and greater than 9 mm2 Operating temperatures between - 55 癈 and 260 癈 Part 002: General Edition P 2

NF L53-201-008:2006 航空航天系列.连接部件中用电连接器.第008部分: S级、A型、压紧、电连接器插头.产品标准

Aerospace series - Electrical contacts used in elements of connection - Part 088 : contacts, electrical, male, type A, crimp, class S - Product standard.

NF L53-201-018:2006 航空航天系列.连接部件中用电连接器.第018部分: S级、压紧、A型电连接器插头.产品标准

Aerospace series - Electrical contacts used in elements of connection - Part 018 : Contacts, electrical, male, type A, crimp, class S - Product standard.

NAVY QPL-7032-36-2006 飞机逆变器一般规定

This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense. All products listed herein have been qualified under the requirements for the product as specified in the latest effective issue of the applicable specification. This list is subject to change without notice; revision or amendment of this list will be issued as necessary. The listing of a product does not release or otherwise affect the obligation of the manufacturer to comply with the specification requirements.

INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR

GJB 5665-2006 机载通信对抗测向设备试验场试验方法

本标准规定了机载通信对抗测向设备在试验场进行试验的基本要求、试验项目和试验方法。 本标准适用于机载通信对抗测向设备（不包含短波测向设备，以下简称被试设备）的鉴定、定型及验收试验，科研性试验可参照使用。

Test method of airborne communication EW direction-finding equipment on test site

GJB 860A-2006 飞机电气负载和电源容量分析

本标准规定了飞机交、直流电气负载（以下简称“负载”）和电源容量分析的方法和要求。 本标准适用于飞机研制、改装、改型时对负载和电源系统容量所进行的系统分析。

Analysis for electric load and power source capacity of aircraft

GJB 5686-2006 军用直升机作战模拟系统通用要求

本标准规定了军用直升机作战模拟系统的通用要求。 本标准适用于军用直升机作战模拟系统（以下简称系统）的开发、使用和维护。

General requirements for operational simulation system of military helicopter

GJB 5552-2006 飞机直流无刷发电机和起动发电机通用规范

本规范规定了飞机直流无刷发电机和直流无刷起动发电机的通用要求和质量保证规定。 本规范适用于飞机28V供电体制和270V供电体制电源系统的直流无刷发电机和直流无刷起动发电机（以下统称电机，其中28V供电体制电源系统的电机简称为28V体制电机；270V供电体制电源系统的电机简称为270V体制电机。电机一般由电机本体、控制器、交换器和滤波器组成。）的设计、制造、试验、验收和质量保证规定等。

Electric brushless direct current generator

GJB 5558-2006 飞机供电特性测试要求

本标准规定了对飞机供电特性测试与所用测试设备的要求。 本标准适用于飞机电源系统、配电系统以及用电设备电源输入端供电特性的测试。

Requirements for test characteristic in aircraft electric power system

GJB 5588-2006 线性机电驱动器通用规范

本规范规定了线性机电驱动器（以下简称驱动器）的要求。 本规范适用于机载悬挂发射装置和机载武器系统的驱动器。

Actuator,linear,electromechanical

GJB 5559-2006 飞机变压整流器通用规范

本规范规定了将额定电压为115V/200V，额定频率为400Hz或稳态频率范围为320Hz～640Hz的Y形连接中线接地的三相四线制飞机交流电变换成额定电压为28V直流电的飞机变压整流器（以下简称变压整流器）的通用要求。 本规范适用于变压整流器的设计、生产和检验。

General specification for transformer-rectifier units of aircraft

BS ISO 1540:2006 航空航天.飞机电气系统特性

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.

Aerospace - Characteristics of aircraft electrical systems

BS EN 4434:2005 航空航天系列.电缆的铜和铜合金轻型导体.产品质量（正常和紧公差）

This standard specifies the dimensions, linear resistance, mechanical characteristics, construction and mass of lightweight conductors, normal and tight tolerances, in copper or copper alloy for electrical cables for aerospace applications. It applies to stranded conductors, with a nominal cross-sectional area of 0,15 mm2 to 14 mm2 inclusive. The conductors for thermocouple extension and fire-resistant cables are not covered by this standard.

Copper or copper alloy lightweight conductors for electrical cables — Product standard (Normal and tight tolerances)

ISO 1540:2006 航空航天.飞行器电气系统的特性

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.

Aerospace - Characteristics of aircraft electrical systems

DIN EN 3841-407:2006 航空航天系列.断路器.试验方法.第407部分:温度变化

Aerospace series - Circuit breakers - Test methods - Part 407: Temperature variation; German and English version EN 3841-407:2004

AECMA PREN 4604-004-2006 航天系列电缆,电气,信号传输部分,004 :电缆,内有双线,高免疫力,50欧姆,200摄氏度,类型是产品标准 版本P3

This industrial standard for the aerospace sector has been drawn up under the responsibility of AECMA (Associa tion Européenne des Constructeurs de Matériel Aérospatial). it is published on yellow paper in three equivalent versions (English, French, German). it will be submitted to GEN (European Committee for Standardization) as a draft European Standard.

Aerospace series Cable, electrical, for signal transmission Part 004: Cable, microcoaxial, high immunity, 50 Ohms, 200 Degrees C, type WS Product standard Edition P 3