V40 电气系统与设备 标准查询与下载

KS W ISO 244:2009 航空器.封装电线

이 표준은 강철 밀봉 철선의 요구사항을 규정한다.

Aircraft-Seal wire

SAE AS5726-2009 迷你军需用品接口,接口标准

This standard only defines interconnect, electrical and logical (functional) requirements for the interface between a Micro Munition and the Host. The physical and mechanical interface between the Micro Munition and Host is undefined. Individual programs will define the relevant requirements for physical and mechanical interfaces in the Interface Control Document (ICD) or system specifications. It is acknowledged that this does not guarantee full interoperability of Interface for Micro Munitions (IMM) interfaces until further standardization is achieved. The purpose of this standard is to minimize proliferation of divergent electrical interfaces between the Host and Micro Munitions to promote interoperability across different programs and services. This standard applies to all Hosts and Micro Munitions that electrically interface with each other. A Micro Munition is a weapon characterized by a mass up to 25 kilograms and a minimum outer diameter of 38 millimeters. Other munitions may use this standard

Interface Standard, Interface for Micro Munitions

BS EN 2240-001:2009 航空航天系列.白炽灯.技术规范

This European Standard specifies the characteristics of incandescent lamps for aerospace applications.

Aerospace series - Lamps, incandescent - Technical specification

SAE AIR5689A-2009 外部航空器照明设备用光传输玻璃罩

This SAE Aerospace Information Report (AIR) provides definitions of an inspection criteria for defects commonly encountered in molded and finished glass covers for exterior aircraft lighting. This document covers, but is not limited to, visual inspection and evaluation recommendations for molded glass covers used in exterior aircraft lighting applications. The included definitions are for those defects most commonly encountered. The goal is to provide specific evaluation criteria in the following areas: a. color; b. internal quality; c. external (surface) quality; d. dimension; and e. coatings. Inspection of glass covers shall be made at a typical reading distance with normal or corrected 20-20 vision under adequate lighting. Covers shall be free from defects which will prevent meeting intensity and beam distribution, strength, thermal shock, and other physical requirements. All covers shall be manufactured and finished using quality workmanship.

Light Transmitting Glass Covers for Exterior Aircraft Lighting

BS EN 61822:2009 机场照明和信标导航用电气装置.恒流调节器

Electrical installations for lighting and beaconing of aerodromes - Constant current regulators

GJB 6769-2009 S频段航天测控网测控信息交换规程

本标准规定了S频段航天测控网各任务控制中心之间、任务控制中心（以下简称中心）与测控站（含测量船，下同）之间以及测控站各设备之间测控信息交换的方式、协议及要求。 本标准适用于S频段航天测控网信息的点到点传输和网络传输，其他频段的测控站和测控设备的信息交换亦可参照使用。

Protocols for exchange of information of the S-band aerospace TT&C network

IEC 61822:2009 机场照明和航路信标的电气装置.恒流调节器

This International Standard specifies the requirements for a Constant Current Regulator (CCR) having a nominal output of 6@6 A for use in an aeronautical ground lighting constant current series circuit. However@ CCRs may be manufactured which have a different power rating (kVA) and current steps than those specified in this standard in order to be used on existing circuits. This standard should be applied where appropriate for these CCRs.

Electrical installations for lighting and beaconing of aerodromes - Constant current regulators

ASTM F2799-09 飞机电线系统维护的标准的方法

This practice is intended to be used as a standard wiring practice for normal and utility category aircraft when not contrary to standards published by the aircraft original equipment manufacturer (OEM) or regulations. This practice is intended to be used for maintenance and preventive maintenance of electrical wiring interconnection systems (EWIS). This practice is not intended to supersede or replace any government specification or specific manufacturer’s instructions regarding EWIS maintenance or repair.1.1 Definition8212;This practice defines acceptable practices and processes for the maintenance, preventative maintenance, and repair of electric systems in general aviation aircraft. This practice does not change or create any additional regulatory requirements nor does it authorize changes in or permit deviations from existing regulatory requirements. 1.2 Applicability8212;The guidance provided in this practice is directed to air carriers, air operators, maintenance providers, repair stations, and anyone performing maintenance or repairs. 1.3 Protections and Warnings8212;This practice provides guidance to minimize contamination and accidental damage to electrical wiring interconnection systems (EWIS) while working on aircraft. 1.4 “Protect and Clean As You Go” Philosophy8212;This philosophy is applied to aircraft wiring through inclusion in operators’ maintenance and training programs. This philosophy stresses the importance of protective measures when working on or around wire bundles and connectors. It stresses how important it is to protect EWIS during structural repairs, (STC) installations, or other alterations by ensuring that metal shavings, debris, and contamination resulting from such work are removed. 1.5 Units8212;The values given in inch-pound units are to be regarded as the standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard. Note 18212;When SI units are required, refer to Annex 5 of ICAO. 1.6 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Maintenance of Airplane Electrical Wiring Systems

SAE ARP4404B-2008 航空器电气装置

It is the purpose of this document to present design recommendations that will provide a basis for satisfactory and safe electrical installations in transport aircraft. This document is not intended to be a complete electrical installation design handbook. However, the requirements for safety extend so thoroughly throughout the electric systems that few areas of the installation are untouched by the document. It is recognized that individual circumstances may alter the details of any design. It is, therefore, important that this document not be considered mandatory but be used as a guide to good electrical application and installation design. Transport aircraft electric systems have rapidly increased in importance over a number of years until they are now used for many functions necessary to the successful operation of the aircraft. An ever increasing number of these functions are critical to the safety of the aircraft and its occupants. The greatly increased power available in electric systems is another factor in aircraft safety. These considerations make it essential that aircraft electrical design practices be carefully considered from the standpoint of safety and reliability. It is believed that this document will be of value in pointing out potential difficulties and in solving many of the problems.

Aircraft Electrical Installations

SAE ARP5602/5-2008 航空航天平台纤维光学培训和航空航天纤维光学安装知识能力的认知教育用指南

This document establishes training guidelines applicable to fiber optic installer technical training for individuals involved in the manufacturing, installation, support, integration and testing of fiber optic systems. Applicable personnel include: Managers; Engineers; Technicians; Trainers/Instructors; Third Party Maintenance Agencies; Quality Assurance; Production

A Guideline for Aerospace Platform Fiber Optic Training and Awareness Education Aerospace Fiber Optics Installer Knowledge Competencies

QJ 3304-2008 弹、箭上电气系统CAN总线应用要求

本标准规定了导弹、运载火箭上电气系统中CAN总线的设计方法、工作方式、应用层协议、网 络拓扑方式和接口、线缆要求、测试要求等。 本标准适用于导弹、运载火箭上电气系统CAN总线的设计、生产、试验和验收。

CAN bus application requirements for bombs and arrows on the electrical system

IEC TS 62239:2008 航空电子设备的工艺管理.电子元件管理计划的制订

This Technical Specification defines the requirements for developing an Electronic Components Management Plan (ECMP) to assure customers and regulatory agencies that all of the electronic components in the equipment of the plan owner are selected and applied in controlled processes compatible with the end application and that the technical requirements detailed in Clause 4 are accomplished. In general, the owners of a complete electronic components management plan are avionics equipment manufacturers.

Process management for avionics - Preparation of an electronic components management plan

KS W ISO 2020-1:2008 航空航天.航空器控制装置的预成形可弯曲钢丝绳.第1部分:尺寸和负载能力

이 표준은 항공기 조종에 사용되는 탄소강 또는 내식 강철 재질로 된, 성형된 유연 강선 로

Aerospace-Preformed flexible steel wire rope for aircraft controls-Part 1:Dimensions and loads

KS W ISO 2020-2:2008 航空航天.航空器控制装置的预成形可弯曲钢丝绳.第2部分:技术规范

이 표준은 항공기 조종에 사용되는 탄소강 또는 내식강 재질로 된 성형된 유연 강선 로프가

Aerospace－Preformed flexible steel wire rope for aircraft controls－Part 2：Technical specification

IEC TS 62500:2008 航空电子过程管理 在航空航天系统中定义和执行高度加速测试 应用指南

This technical specification specifies the targets assigned to highly accelerated tests, their basic principles, their scope of application and their implementation procedures. It is primarily intended for programme managers, designers, test managers, and RAMS experts to facilitate the draft of the specification and execution of highly accelerated tests. This guide is applicable to all programmes and is of primary interest to the industrial firms in charge of designing, developing and producing equipment built for these programmes, and also their customers who, in drafting contractual clauses, may require that their suppliers implement highly accelerated tests. NOTE This technical specification applies to all types of equipment used in systems developed in these programmes, whatever their nature (electronic, electromechanical, mechanical, electro-hydraulic, electro- pneumatic, etc.) and whatever their size, from "low-level" subassemblies (PCBs, mechanical assemblies, connectors, etc.), up to system level groups of equipment.

Process management for avionics - Defining and performing highly accelerated tests in aerospace systems - Application guide

BS EN 4626-002:2008 航空航天系列.2.5mm直径套圈、方框空腔谐振器、机架和面板多触点矩形光学连接器.工作温度为-65℃～125℃(由电缆决定).冲水接触器.性能规范和触点排列

This standard specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test programs and groups for fibre sub-assembly contacts in rack and panel connectors, intended for use in a temperature range from − 65 °C to 125 °C continuous (cable dependent). This standard specifies a pair of adaptors to fit with standard Quadrax cavities and EN 4531-101 optical contact.

Aerospace series - Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule - Operating temperatures -65 °C to 125 °C (cable dependent) - Flush contacts - Specification of performance and contact arrangements

DIN EN 4049-003:2008 航空航天系列.热电偶延伸电缆.工作温度为-65℃～260℃.第003部分:单芯镍铬/镍铝.产品标准

This standard specifies the characteristics of thermocouple cables used for the connection between the ther- mocouple and the equipment. Temperatures between - 65 ~C and 260 ~C (except otherwise specified in the product standard).

Aerospace series - Thermocouple extension cable - Operating temperatures between -65 °C to 260 °C - Part 003: Single core nickel chromium/nickel aluminium - Product standard; German and English version EN 4049-003:2006

DIN EN 4049-001:2008 航空航天系列.热电偶延伸电缆.工作温度为-65℃～260℃.第001部分:产品规范

This standard specifies the required characteristics, test methods, qualification and acceptance conditions of thermocouple used for the connection between the thermocouple and the equipment.

Aerospace series - Thermocouple extension cable - Operating temperatures between -65 °C to 260 °C - Part 001: Technical specification; German and English version EN 4049-001:2006

DIN EN 4049-004:2008 航空航天系列.热电偶延伸电缆.工作温度为-65℃～260℃.第004部分:屏蔽的和置于壳内的双芯镍铬/镍铝电缆.产品标准

This standard specifies the characteristics of thermocouple cables used for the connection between the ther- mocouple and the equipment. Temperatures between - 65 ℃ and 260 ℃ (except otherwise specified in the product standard).

Aerospace series - Thermocouple extension cable - Operating temperatures between -65 °C to 260 °C - Part 004: Two core nickel chromium/nickel aluminium shielded and jacketed - Product standard; German and English version EN 4049-004:2006

GJB 6344-2008 军用直升机供电系统试验要求

本标准规定了军用直升机供电系统地面模型试验、地面功能试验和飞行试验的要求。 本标准适用于各类军用直升机。

Test requirements for electrical power system of military helicopter