V41 导航通讯系统与设备 标准查询与下载

DIN IEC/TS 62668-2:2013 航空电子设备的工艺管理.防伪.第2部分:非经授权来源的管理电子组件(IEC 107/207/CD-2013)

Process management for avionics - Counterfeit prevention - Part 2: Managing electronic components from non-franchised sources (IEC 107/207/CD:2013)

SAE AS8037C-2013 飞机定位航灯用最低性能标准

This Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights. This Aerospace Standard defines minimum light intensity in terms of candelas in vertical and horizontal directions about the longitudinal, vertical, and lateral axes of the aircraft. It also defines color tolerances in terms of limiting chromaticities for the light emitted from the position lights. It is not intended that this standard require the use of any particular light source such as quartz-halogen, incandescent, or any other specific design of lamp.

Minimum Performance Standard for Aircraft Position Lights

IEC 107/207/CD:2013 IEC/TS 62668-2标准:航空电子设备的工艺管理.防伪.第2部分:非经授权来源的管理电子组件

IEC/TS 62668-2: Process management for avionics - Counterfeit prevention - Part 2: Managing electronic components from non-franchised sources

IEC 107/206/DTS:2013 IEC/TS 62647-23: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

IEC/TS 62647-23: 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 AIR5665B-2013 无人驾驶系统用架构框架

This SAE Aerospace Information Report (AIR) describes the Architecture Framework for Unmanned Systems (AFUS). AFUS comprises a Conceptual View, a Capabilities View, and an Interoperability View. The Conceptual View provides definitions and background for key terms and concepts used in the unmanned systems domain. The Capabilities View uses terms and concepts from the Conceptual View to describe capabilities of unmanned systems and of other entities in the unmanned systems domain. The Interoperability View provides guidance on how to put it all together in a way that supports interoperability. The purpose of this Aerospace Information Report is to communicat

Architecture Framework for Unmanned Systems

DIN EN 300676-1:2013 调幅的甚高频 (VHF) 航空流动通信勤务用基于地面的甚高频 (VHF) 手持, 移动和固定无线电发射机, 接收机和收发设备. 第1部分:技术特性和测量方法 (英文版本EN 300 676-1 V1.5.2 (2011-03) 的核准本作为德国标准)

Ground-based VHF hand-held, mobile and fixed radio transmitters, receivers and transceivers for the VHF aeronautical mobile service using amplitude modulation - Part 1: Technical characteristics and methods of measurement (Endorsement of the English versi

SAE ARP5412B-2013 飞行器雷电环境和相关检测波形

The environment and test waveforms defined in this SAE Aerospace Recommended Practice (ARP) account for the best lightning data and analysis currently available. The quantified environment and levels herein represent the minimum currently required by certifying authorities, consistent with the approach applied in related lightning documents. Lightning, like other weather phenomenon, is probabilistic in nature. Levels and waveforms vary considerably from one flash to the next. Within this document, standardized voltage and current waveforms have been derived to represent the lightning environment external to an aircraft. These standardized waveforms are used

Aircraft Lightning Environment and Related Test Waveforms

HB 20112-2012 军用飞机显示字符要求

本标准规定了军用飞机显示器在起飞、导航、地形跟踪/回避、进场着陆状态时使用的基本字符的字体、尺寸、种类、几何形状、显示格式等要求。本标准适用于军用固定翼飞机的平视显示器、下视显示器等机载显示器。

Requirement of military aircraft display symbol

HB 20087-2012 航空电子产品可靠性仿真分析通用要求

本标准规定了航空电子产品可靠性仿真分析的要求。给出了可靠性仿真分析的目标、基本原则、产品对象、实施时机,给出了可靠性仿真分析的一般流程、数据要求、仿真模型要求、环境条件要求与分析软件要求,并规定了可靠性仿真分析各项工作的详细要求。本标准适用于航空电子产品的可靠性仿真分析。

General requirements for reliability simulation analysis of avionics products

HB 20088-2012 航空电子产品可靠性仿真CAD模型建模要求

本标准规定了用于可靠性仿真分析的CAD模型的建模要求,给出了CAD模型建模的目的、建模流程、数据要求、模型完整性要求和输出要求。本标准适用于航空电子产品可靠性仿真CAD模型建模。

CAD modeling requirements for avionics products reliability simulation

ANSI/GEIA STD-0005-3-A-2013 航空航天和包含无铅焊料的高性能电子设备的性能测试

Performance Testing for Aerospace and High Performance Electronic Interconnects Containing Pb-free Solder and Finishes

SAE AS6165-2012 机载光电/红外(EO/IR)系统的维护和试验的接口标准

This standard defines the use of data interfaces between a host platform and an electro-optic/infrared (EO/IR) system for maintenance and test (M&T) purposes. In particular, this standard defines the use of the data interfaces in order to facilitate the: a. confirmation of system performance and function; b. external initiation of built-in-test (BIT) functions; c. performance of other diagnostic tests of system health; d. downloading M&T data; e. uploading software changes. This standard does not cover mechanical or electrical interfaces, nor does it define the basic platform-to-sensor communication protocols and formats. Furthermore, this standard does not

Interface Standard, Airborne EO/IR Systems, Maintenance and Test

SAE AS6129-2012 AS 6129:电气机载光电/红外系统接口标准

This standard defines a generic set of electrical interfaces between a host aircraft ("platform") and an electro-optic/infrared (EO/IR) sensor. This includes connectors, cabling, fiber optics, signals, and power.

AS6129: Interface Standard, Airborne EO/IR Systems, Electrical

SAE AS5716A-2012 机载引信系统的标准电气和逻辑接口

This interface standard applies to fuzes/fuzing systems (referred to as fuzing system hereafter) in airborne weapons that use a MIL-STD-1760 type interface. It defines the powers, the discrete signals and the serial data interface for the communications at the interface between the fuzing system and the remainder of the weapon, including the weapon control unit. The Class 1 interface is an electrical only interface that facilitates use of MIL-STD-1760 type platform store interfaces for the fuze to monitor intentional release and defines the fuze interface bus communications protocol to allow sending and receiving data from fuzing systems. Class 2 interfaces

Standard Electrical and Logical Interface for Airborne Fuzing Systems

DIN EN 303213-1:2012 先进场面活动引导和控制系统(A-SMGCS).第1部分:A-SMGCS等级1包括外部接口用欧洲单一空中互操作性规则EC 552/2004下应用的共同体规范(英文版本EN 303 213-1 V1.3.1 (2012-04)的核准本作为德国标准)

Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 1: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for A-SMGCS Level 1 including external interfaces (Endorsement of the E

SAE AIR6218-2012 集成系统用开发保障计划的构建

This SAE Aerospace Information Report (AIR) supplements ARP4754A by identifying the crucial elements to be considered when constructing the development assurance plans described in Chapter 3 (Development Planning) of ARP4754A for integrated systems. This AIR presents a collection of lessons learned from past certification programs involving integrated systems. This AIR is not guidance for system integration technologies.

Constructing Development Assurance Plan for Integrated Systems

IEC 62396-2:2012 航空电子设备过程管理.环境辐射影响.第2部分:航空电子系统用单粒子事件检测导则

This part of IEC 62396 aims to provide guidance related to the testing of microelectronic devices for purposes of measuring their susceptibility to single event effects (SEE) induced by atmospheric neutrons. Since the testing can be performed in a number of different ways@ using different kinds of radiation sources@ it also shows how the test data can be used to estimate the SEE rate of devices and boards due to atmospheric neutrons at aircraft altitudes. Although developed for the avionics industry@ this process may be applied by other industrial sectors.

Process management for avionics - Atmospheric radiation effects - Part 2: Guidelines for single event effects testing for avionics systems

SAE AIR5532A-2012 通用类航空器储存接口框架(GASIF)

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) defines a Generic Aircraft-Store Interface Framework (GASIF). This is a common framework for modeling and specifiying aircraft-store logical interfaces. GASIF complies with the OSI Basic Reference Model (ITU-T Rec. X.200 / ISO/IEC 7498-1) in that it describes operations and mechanisms which are assignable to layers as specified in the OSI Basic Reference Model. This AIR provides a mapping of the Interface Standard for Aircraft-store Electrical Interconnection System (AEIS), MIL-STD- 1760, in Appendix C. The purpose of GASIF is to foster greater interoperability between aircraft and stores through standards coordination and common approaches to aircraft-store interface and control documents (ICD). The field of application for GASIF is military aircraft/store avionics, where a "store" is a device (such as an air-launched weapon) that when loaded on an aircraft allows it to perform a specific mission.

Generic Aircraft-Store Interface Framework (GASIF)

IEC 62396-1:2012 航空电子设备过程管理.环境辐射影响.第1部分:航空电子设备内部由单粒子效应引起的环境辐射影响的调节

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 radioation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment

NF Z85-842-2:2012 VHF空对地和空对空数字链(VDL)模式4无线电设备. 航空移动(空载)设备的技术特性和测量方法.第2部分:一般描述和数据链路层(V1.3.1)

VHF air-ground and air-air Digital Link (VDL)Mode 4 radio equipment - Technical characteristics and methods of measurement for aeronautical mobile (airborne) equipment - Part 2 : general description and data link layer (V1.3.1).