V40 电气系统与设备 标准查询与下载

SAE AIR6139-2014 飞机电源系统总线能量回复处理滑路

This SAE Aerospace Information Report (AIR) considers the issue of power regeneration into the EPS of an aircraft. A series of options for dealing with this regenerative power are considered and arranged in categories. Advantages and disadvantages of each solution, including the existing solution, are included. Validated simulation results from representative Electrical Power systems are presented in order to demonstrate how some of the solutions may operate in practice and how power quality can be maintained during regeneration. The impact on changes to the electrical generation system are also highlighted in this AIR, as these changes may have an impact o

Ways of Dealing with Power Regeneration onto an Aircraft Electrical Power System Bus

IEC TS 62647-23:2013 航空电子设备工艺管理.包含无铅焊料的航空航天和防御电子系统.第23部分:消除无铅电子设备和混合装配组件可能影响的返修和维修导则

Process management for avionics - Aerospace and defence electronic systems containing lead free solder - Part 23: Rework and repair guidance to address the implications of lead-free electronics and mixed assemblies

SAE AS8700A-2013 飞机电子设备安装和试验的通用规范

This specification covers the general requirements for the installation and test of electronic equipment in piloted aircraft.

Installation and Test of Electronic Equipment in Aircraft, General Specification for

HB/Z 404-2013 民用飞机电气安装设计指南

Civil Aircraft Electrical Installation Design Guidelines

IEC TS 62647-22:2013 航空电子设备工艺管理.包含无铅焊料的航空航天和防御电子系统.第22部分:技术指南

Process management for avionics - Aerospace and defence electronic systems containing lead free solder - Part 22: Technical guidelines

SAE AS81714/67A-2013 系列Ⅱ跟踪反馈型框架装配终端连接系统

Terminal Junction System, Rack Assembly, Track, Feedback Type, Series II

SAE AS35061A-2013 飞机用28伏特直流运行功率矩形外部电力连接器

Connector, Receptacle External Electric Power, Aircraft, 28 Volt DC Operating Power

IEC 60952-2:2013 飞机用蓄电池组.第2部分:设计和制造要求

This part of IEC 60952 series defines the physical design@ construction and material requirements for nickel-cadmium and lead-acid aircraft batteries containing vented or valveregulated cells or monoblocs. The batteries are used for both general purposes and specific aerospace applications. The specific topics addressed in this part serve to establish acceptable quality standards required to qualify a battery as airworthy as defined in Clause 3 of IEC 60952-1:2013. A preferred range of aircraft batteries is specified in Annex A@ but this part of IEC 60952 series may be used for other battery sizes@ arrangements and ratings. For particular applications@ other design requirements may be stipulated. These will be in addition to the requirements of this part and will be covered by specific documents. It is recognised that additional data may be required by other organisations (national standards bodies@ AECMA@ SAE@ etc.). The present standard can be used as a framework to devise tests for generation of the required data

Aircraft batteries - Part 2: Design and construction requirements

IEC 60952-1:2013 飞机用蓄电池组.第1部分:一般试验要求和性能水平

This part of the IEC 60952 series defines test procedures for the evaluation@ comparison and qualification of batteries and states minimum performance and environmental levels for airworthiness. Where specific tests are defined with no pass/fail requirement (to establish performance capability)@ the manufacturer's declared values@ from qualification testing@ will be used to establish minimum requirements for ongoing maintenance of approval for that design of battery. To provide representative examples@ this standard utilises voltage and current values based upon an aircraft electrical system nominally rated at 28 V d.c. Additionally@ the nominal values for cell voltage are assumed to be 1@2 V per cell for nickel-cadmium batteries and 2@0 V per cell for lead-acid batteries. The specific topics addressed in this part of IEC 60952 serve to establish acceptable quality standards required to qualify a battery as airworthy. In cases where the requirements for a specific application exceed those detailed in this standard@ the purchaser will detail said requirements in the product specification and the method of establishing compliance. It is recognised that additional data may be required by other organisations (national standards bodies@ AECMA@ SAE etc.). The present standard can be used as a framework to devise tests for generation of the required data.

Aircraft batteries - Part 1: General test requirements and performance levels

IEC TS 62647-21:2013 IEC/TS 62647-21:航空电子设备工艺管理.含无铅锡焊的航空和防御电子系统.第21部分:项目管理.过渡到无铅电子设备管理的系统工程指南

IEC/TS 62647-21: Process management for avionics - Aerospace and defence electronic systems containing lead free solder - Part 21: Program management - Systems engineering guidelines for managing the transition to lead-free electronics

IEC 60952-3:2013 飞机用蓄电池组.第3部分:产品规格及设计与性能(DDP)的声明

This part of IEC 60952 defines requirements for the product specification as well as procedures for a Declaration of Design and Performance (DDP) for nickel-cadmium and lead-acid aircraft batteries containing vented or valve-regulated cells or monoblocs. The batteries are used for both general purposes and specific aerospace applications. The specific topics addressed in this part serve to establish acceptable quality standards required to qualify a battery as airworthy as defined in Clause 3 of IEC 60952-1:2013. The design construction and test requirements should conform to the requirements specified in IEC 60952-1 and IEC 60952-2. It is recognised that additional data may be required by other organisations (national standards bodies@ AECMA@ SAE etc.). The present standard can be used as a framework to devise tests for generation of the required data.

Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP)

SAE AS26805B-2013 空气/气体压缩机组通用要求

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification has been declared ""NONCURRENT"" as of April 2008. It is recommended, therefore, that this document not be specified for new designs. This specification covers the general requirements for the design and construction of air/gas compressor units (see 6.4.1). The detail requirements for a particular air compressor unit shall be as specified in the individual equipment specification for that particular air

Compressor Units, Air/Gas, General Requirements For

SAE AS55941A-2013 密封电动头拨动开关的通用规格

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers general requirements for direct current electrically held, environmentally sealed toggle switches for use in alternating current (AC) and direct current (DC) applications.

Switches, Toggle, Electrically Head, Sealed, General Specification for

IEC TR 62240-1:2013 航空电子设备的过程管理 运行中电子组件容量 第1部分 温度升级

This Technical Report provides information when using semiconductor devices in wider temperature ranges than those specified by the device manufacturer. The uprating solutions described herein are considered exceptions, when no reasonable alternatives are available;otherwise devices are utilized within the manufacturers'specifications.

Process management for avionics - Electronic components capability in operation - Part 1: Temperature uprating

ISO 13832:2013 航空宇宙.铝合金和包铜铝导线电导线.一般性能要求

Aerospace - Wire, aluminium alloy and copper-clad aluminium conductors - General performance requirements

SAE AS13A-2013 航空器驱动磁电机

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers two types of drive couplings for magnetos as follows: 1. 17-tooth coupling and 2. 33-tooth coupling. This specification also covers three types of magneto shaft ends as follows: 1. tapered shaft end; 2. 6-tooth spline shaft; and 3. 24-tooth spline shaft.

Magnetos, Aircraft, Drives for

BS EN 6049-008:2013 航空航天系列.电缆安装.间位芳纶纤维保护套管.-55℃至200℃灵活布置安装操作的带有镍铜编织带自包裹式(EMI)保护套管.产品标准

Aerospace series. Electrical cables, installation. Protective sleeves in meta-aramid fibres. Self-wrapping shielded (EMI) protective sleeve with nickel copper braid, flexible post installation operating temperature from -55°C to 200°C. Product standard

BS EN 3660-038:2013 航空航天系列.圆形和矩形电连接器和光学连接器用电缆输出配件.EN 3660-033不锈钢防护壳终端带用Z型手动安装工具的电缆输出配件.产品标准

Aerospace series. Cable outlet accessories for circular and rectangular electrical and optical connectors. Manual installation tool, style Z, for installation of stainless steel shield termination band EN 3660-033, to cable outlet accessories. Product sta

SAE AS5553A-2013 欺诈/假冒电子零部件;避免,检测,减轻和处置

This SAE Aerospace Standard standardizes practices to: a. maximize availability of authentic parts, b. procure parts from reliable sources, c. assure authenticity and conformance of procured parts, d, control suspect or confirmed fraudulent/counterfeit EEE parts, e. and report suspect or confirmed fraudulent/counterfeit EEE parts to other potential users and Authority Having Jurisdiction; f. and assess.mitigate, control, and report parts which have been used, refurbished, or reclaimed, but represented as new product.

Fraudulent/Counterfeit Electronic Parts; Avoidance, Detection, Mitigation, and Disposition

SAE AIR5924A-2013 带运输种类(第25部分)和通用航空(第23部分)飞机的发动机电子控制系统指南

This SAE Aerospace Information Report (AIR) provides methodologies and approaches that have been used to install and integrate full-authority-digital-engine-control (FADEC) systems on transport category aircraft. Although most of the information provided is based on turbofan engines installed on large commercial transports, many of the issues raised are equally applicable to corporate, general aviation, regional and commuter aircraft, and to military installations, particularly when commercial aircraft are employed by military users. The word ""engine"" is used to designate the aircraft propulsion system. The engine station designations used in this report.

Guidelines for the Integration of Electronic Engine Control Systems with Transport Category (Part 25) and General Aviation (Part 23) Aircraft