V40 电气系统与设备 标准查询与下载

HB 20107-2012 MK7系列耐环境屏蔽组合式矩形电连接器规范

本规范规定了MK7系列耐环境屏蔽组合式矩形电连接器的技术要求、质量保证规定和交货准备。本规范适用于MK7系列耐环境屏蔽组合式矩形电连接器(以下简称电连接器)的设计、制造和检验。

Specification for MK7 series environment resistant shield multiple insert type rectangular electrical connectors

SAE ARP4102/14C-2012 全格式打印机

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 document recommends criteria for the installation and operation of a printer intended for use by flight crew members on the flight deck. The printer is used to supply the flight crew with hard copies of information that originates from data sources such as FMS, ELS/EDMS, ACMS, CMS, and data link. These criteria are in addition to the specifications of the referenced ARINC Characteristic 744A.

Full-Format Printer (Stabilized Type)

IEC TS 62239-1:2012 航空电子设备的过程管理.管理计划.第1部分:电子元件管理计划的编制和维护

Process management for avionics - Management plan - Part 1: Preparation and maintenance of an electronic components management plan

DIN IEC/TS 62564-1:2012 航空电子学的过程管理. 航天合格电子元件 (AQEC). 第1部分:集成电路和分立半导体 (IEC/TS 62564-1-2011)

Process management for avionics - Aerospace qualified electronic component (AQEC) - Part 1: Integrated circuits and discrete semiconductors (IEC/TS 62564-1:2011)

SAE AIR1245B-2012 射流控制用电源

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 SAE Aerospace Information Report (AIR) presents a review of the types and general characteristics of power sources that may be used to provide the power for gaseous or liquid fluidic control systems. Fluidic definitions, terminology, units and symbols are defined in Reference 2.1.1. The power systems described and the data contained herein apply to all types of aerospace vehicles including: aircraft, helicopters, missiles, space vehicles, remotely piloted vehicles, or in any other vehicles or applications to which aerospace technology applies.

Power Sources for Fluidic Controls

SAE AS1613B-2012 射线照相术图像质显示器

This document has been declared "Stabilized" and will no longer b subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability of technical requirements. Newer technology may exist. This Aerospace Standard establishes an identification system and provides design and tolerance information in describing two series of image quality indicators currently used in radiography of aerospace components, especially in electronic component evaluation and radiographic film and paper classification.

Image Quality Indicator, Radiographic

SAE AS4710A-2012 Pi-总线

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 standard defines a bus and module interface to the Pi-Bus. This standard specifies the requirements/functions for the Pi-Bus side of a bus interface unit (BIU) needed to facilitate the interoperability of modules on a Pi-Bus for avionics systems. The corresponding software/device side interface requirements are not specified in this standard.

Pi-Bus

SAE AIR4289A-2012 SAE AS4075 高速环形总线标准手册

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 Handbook has been prepared by the Ring Implementation Task Group of the SAE AS-2 Committee, and is intended to support AS4075 by providing explanation of the standard itself and guidance on its use. The principal objective in the preparation of a standard is to provide a statement of operational and performance requirements, and an unambiguous definition of the functions to be realized in any implementation, primarily from the view point of interoperability. While efforts have been made within the AS4075 standard to provide a readable general description of the HSRB, detailed explanations, rationale and guidance to the use are incompatible with the purpose and, indeed, the format of a standard. Accordingly, this Handbook contains a paragraph-by-paragraph explanation of the main sections of the standard, and a discussion of application and implementation issues.

Handbook for the SAE AS4075 High Speed Ring Bus Standard

SAE AIR4288A-2012 线性令牌传送多路传输总线用户手册

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 document is intended to explain, in detail, the rationale behind the features and functions of the AS4074, Linear, Token-passing, Bus (LTPB). The discussions also address the considerations which a system designer should take into account when designing a system using this bus. Other information can be found in these related documents: AIR 4271 - Handbook of System Data Communication and AS 4290 - Validation Test Plant for AS 4074.

Linear Token Passing Multiplex Data Bus Users Handbook

SAE ARP4255A-2012 用于宇航和其他方面的电气驱动系统

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 Aerospace Recommended Practice (ARP) is intended as a guide in the preparation of Procurement Specifications for electrical actuator systems to be used in aerospace and other applications. Detail requirements, as necessary to completely define a specific actuator, are the responsibility of the procuring agency.

Electrical Actuation Systems for Aerospace and Other Applications

SAE AIR512E-2012 机舱照明

This document covers the general recommendations for cabin lighting in order to provide satisfactory illumination for, but not limites to:provides the aircraft designer, architect, industrial designer and electrical engineer with design criteria to properly illuminate aircraft cabin interiors: boarding and deplaning; movement about the cabin; reading; use of lavatories; use of work areas; exiting under emergency conditions; using stowage compartments, coat rooms and closets; and using interior stairways and elevators (lifts).

Aircraft Cabin Illumination

SAE ARP693D-2012 着陆与滑行照明灯具的安装设计准则

This document includes requirements of installations of adequate landing and taxiing lighting systems in aircraft of the following categories: a) single engine personal and/or liaison type; b) light twin engine; c) large multiengine propeller; d) large multiengine turbojet; e) military high performance fighter and attack; and f) helicopter. The purpose of this document is to provide certain basic considerations and design criteria for installation of landing and taxiing light systems for night operation.

Landing and Taxiing Lights - Design Criteria for Installation

ANSI/GEIA STD-0005-1-A-2012 无铅焊料和抛光剂在航空,防御中的使用管理和高性能电子设备的标准

This Standard communicates technical and administrative processes and procedures needed to mitigate the risks associated with the use of Pb-free solder and finishes in Aerospace High Performance Electronic Systems

Standard for Managing the Use of Pb-Free Solder and Finishes in Aerospace, Defense and High Performance Electronic Systems

SAE AIR4276A-2011 设计中可靠性,可维护性和可支持性(RM&S)的电脑化

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 Aerospace Information Report (AIR) is the primary vehicle for providing the survey results to industry and government. The Institute of Defense Analysis (IDA), has performed a study which concludes that computerized techniques must be developed to integrate RM&S into product design in order to permit design influence from inception throughout the product life cycle. This AIR addresses the DoD initiative for developing Computer Aided Acquisition and Logistic Support (CALS) and industry's role in its evolution. AIR 4276 provides the detailed results of an industry/government survey inquiring into the extent of computerization of RM&S into the design process. Background information describes the evolution of the survey and why it was developed. The results provide demographic information about the respondents, the existence and extent of their CALS policy and plans, the priority placed on each RM&S task, and the extent to which these tasks have been computerized into the design process. Recommendations based on the survey results are included

Computerization of Reliability, Maintainability and Supportability (RM&S) in Design

SAE ARP5475A-2011 可配置座位视频系统的滥用负载试验

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 SAE Aerospace Recommended Practice (ARP) provides guidelines for abuse load testing of a deployable Individual Video System (IVS). The abuse load testing defined in this ARP is intended to only address the evaluation of the deployable IVS regarding stowage of the system and injurious projections/protrusions as a result of passenger interaction with the video system. Other aspects of the video system design or qualification may require additional testing or analysis and are outside the scope of this ARP. This ARP is not intended to address customer satisfaction or reliability aspects of individual designs. The deployable IVS includes, for the purpose of this ARP, all video system components from the monitor to the interface at the primary seat structure. It should be shown that the system meets the performance criteria of Section 4 after being subjected to the forces defined in 3.2. This can be demonstrated by the test procedure described in this ARP or by similarity analysis to a system previously shown to comply with this ARP.

Abuse Load Testing for In-Seat Deployable Video Systems

SAE ARP711B-2011 照明标志

This Aerospace Recommended Practice (ARP) covers the general design and performance characteristics of illuminated information signs for service in the passenger compartment of passenger transport aircraft. "Illuminated information sights" are lighted signs used to inform occupants of the passenger compartment. Signs may use symbols or letters to convey messages. This ARP does not apply to "EXIT" signs which are the subject of SAE ARP 503.

Illuminated Signs

SAE AIR860B-2011 航空器电加热系统

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. It is intended that the scope of this information report be limited to electrical heating of passenger, crew, and cargo compartments only. No attempt has been made to develop the complete electrical circuitry associated with the electrical heating components; however, the electrical circuitry required for heating component operation, safety, and monitoring will be included as available. Specific design information is given for various modern aircraft utilizing electrical heating. Each aircraft discussed will be identified by alphabetical letter designation and included in the appropriate appendix.

Aircraft Electrical Heating Systems

SAE AIR6052-2011 可配平的水平稳定装置致动器说明

The purpose of this AIR is to provide a comprehensive description document that displays various examples of transport and business aircraft systems driving Trimmable Horizontal Stabilizers. The main focus is on mechanical systems which may be actuated hydraulically or electrically. The document is intended as an overview for those specifying or designing Horizontal Stabilizer Trim Actuators in order to compare existing solutions as reference for implementation in new aircraft programs.

Trimmable Horizontal Stabilizer Actuator Descriptions

IEC 61821:2011 机场照明和航路信标电气设备.航空用地面照明恒流串联电路的维修

This International Standard applies to the maintenance of AGL constant current series circuits. This International Standard ? covers constant current series circuits for AGL installed at aerodromes and heliports; ? concentrates on providing the safety requirements for the maintenance of an AGL constant current series circuit. It is recognised that AGL constant current series circuits of different design characteristics and parameters are in existence; ? is mainly concerned with safety to persons by specifying the rules and fundamental principles for the maintenance of AGL constant current series circuits; ? is not intended to apply to AGL primary series circuits supplied directly from a mains constant voltage source; ? is not intended to be used for public street lighting@ roadway lighting or any other installation requiring the use of constant current series circuits.

Electrical installations for lighting and beaconing of aerodromes - Maintenance of aeronautical ground lighting constant current series circuits

DIN EN 4660-003:2011 航空航天系列.模块化和开放的航空电子设备架构.第003部分:通信/网络.德文和英文版本EN 4660-003-2011

This standard details the functionality and principle interfaces for the ASAAC (Allied Standard Avionics Architecture Council) Network to ensure the interoperability of Common Functional Modules and design guidelines to assist in implementation of such a network. It is one of a set of standards that define an ASAAC Integrated Modular Avionics (IMA) System.

Aerospace series - Modular and Open Avionics Architectures - Part 003: Communications/Network; German and English version EN 4660-003:2011