V40 电气系统与设备 标准查询与下载

NF L58-100-317*NF EN 2349-317:2007 航空航天系列.继电器和接触器要求和试验程序.第317部分:线圈开关装置使用寿命

Aerospace series - Requirements and test procedures for relays and contactors - Part 317 : service life of coil switching device.

NAVY MIL-PRF-17331 J (1)-2007 一般条件下汽轮机齿轮机润滑油

This specification covers a single classification of steam turbine and gear lubricating oil, moderate service, for use in main and auxiliary turbines and gears, air compressors, and certain hydraulic equipment, as well as for general mechanical lubrication. The lubricating oil will be identified as follows:

LUBRICATING OIL, STEAM TURBINE AND GEAR, MODERATE SERVICE

GJB 1392A-2007 飞机400Hz交流发电系统通用规范

本规范规定了由组合发电装置或交流发电机（以下简称发电机）和发电机控制器等主要部件组成的飞机 400Hz、 115V/200V 三相四线制交流发电系统的通用要求、质量保证规定、交货准备等。 本规范适用于飞机 400Hz 、 115V/200V 三相四线制交流发电系统。

General speciflcation for 400Hz alternating current generator system of aircraft

SAE AS47642A-2007 MIL-STD-1760C航天器配置接口验证方法

This document establishes techniques for validating that an Aircraft Station interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 issued 1995-04 applies. For validation of aircraft designed to MIL-STD-1760B Notice 3 AS47641 Issued 1999-08 applies. The purpose of this document is to provide methods for validating that an aircrafts store electrical interface complies with the aircraft station interface (ASI) requirements of MIL-STD-1760C. This document provides a modular, independent set of methods for each of the requirements in MIL-STD-1760 that applies to aircraft requirements. The methods herein apply to the auxiliary (AUX) interface as well as the primary interface of MIL-STD-1760.

Validation Methods for MIL-STD-1760C Aircraft Station Interfaces

DLA SMD-5962-90954 REV C-2007 硅单块 直流-直流变换器,三倍沟道+5和5瓦特直线式混合电路

This drawing documents five product assurance classes as defined in paragraph 1.2.3 and MIL-PRF-38534. A choice of case outlines and lead finishes which are available and are reflected in the Part or Identifying Number (PIN). When available, a choice of radiation hardness assurance levels are reflected in the PIN.

MICROCIRCUIT, HYBRID, LINEAR, +5 AND ?5 VOLT, TRIPLE CHANNEL, DC/DC CONVERTER

SAE AS5657-2007 军事和宇航飞行器软件应用AS5643 IEEE-1394b接口要求的试验计划/程序

This document establishes test plans/procedures for the AS5643 Standard that by itself defines guidelines for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. This test specification defines procedures and criteria for testing device compliance with the AS5643 Standard.

Test Plan/Procedure for AS5643 IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications

SAE AS5625-2007 静态电力变频器的最低性能标准

This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary alternating current (AC) electrical power sources in aerospace electric power systems. The purpose of this document is to define the guidelines and minimum performance test standards to be met by static electric power frequency converters designed to operate from primary electric power systems. The tests specified herein provide a laboratory means to determine the performance and reliability characteristics of electric power frequency converters under electrical and environmental conditions representative of those encountered in actual aerospace applications.

Minimum Performance Standards for Static Electric Power Frequency Converters

ASTM F2639-07e1 飞机电气布线系统的设计, 改造和认证用标准实施规程

Design8212;The design procedures defined in this practice are intended to provide acceptable guidance in the original design of electrical systems. Alteration8212;The alteration procedures defined in this practice are intended to provide acceptable guidance for modification of general aviation aircraft. Design of any modification shall follow the practices and processes defined in the design sections of this practice. Certification8212;Certification guidance provided in this practice is intended to provide generally accepted procedures and processes for certification of original and modified electrical systems and equipment. Requirements for certification shall be coordinated with the applicable National Aeronautics Association/Civil Aeronautics Administration (NAA/CAA) regulatory agency.1.1 Definition8212;This practice defines acceptable practices and processes for the design, alteration, and certification of electric systems and installations 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, design approval holders, Supplemental Type Certificate (STC) holders, maintenance providers, repair stations, and anyone performing field approval modifications or repairs. 1.3 Protections and Cautions8212;This practice provides guidance for developing actions and cautionary statements to be added to maintenance instructions for the protection of wire and wire configurations. Maintenance personnel will use these enhanced procedures to minimize contamination and accidental damage to electrical wiring interconnection system (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 making sure that metal shavings, debris, and contamination resulting from such work are removed. 1.5 This practice includes the following sections: TitleSection Wire Selection5 General5.1 Aircraft Wire Materials5.2 Table of Acceptable Wires5.3 Severe Wind and Moisture Problems (SWAMP)5.4 Grounding and Bonding5.5 Electrical Wire Chart5.6 Wire and Cable Identification

Standard Practice for Design, Alteration, and Certification of Airplane Electrical Wiring Systems

ASTM F2639-07 飞机电气布线系统的设计、改造和认证用标准实施规程

Design8212;The design procedures defined in this practice are intended to provide acceptable guidance in the original design of electrical systems. Alteration8212;The alteration procedures defined in this practice are intended to provide acceptable guidance for modification of general aviation aircraft. Design of any modification shall follow the practices and processes defined in the design sections of this practice. Certification8212;Certification guidance provided in this practice is intended to provide generally accepted procedures and processes for certification of original and modified electrical systems and equipment. Requirements for certification shall be coordinated with the applicable National Aeronautics Association/Civil Aeronautics Administration (NAA/CAA) regulatory agency.1.1 Definition - This practice defines acceptable practices and processes for the design, alteration, and certification of electric systems and installations 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 Applicability - The guidance provided in this practice is directed to air carriers, air operators, design approval holders, Supplemental Type Certificate (STC) holders, maintenance providers, repair stations, and anyone performing field approval modifications or repairs.1.3 Protections and CautionsThis practice provides guidance for developing actions and cautionary statements to be added to maintenance instructions for the protection of wire and wire configurations. Maintenance personnel will use these enhanced procedures to minimize contamination and accidental damage to electrical wiring interconnection system (EWIS) while working on aircraft.1.4 "Protect and Clean As You Go" Philosophy - 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 making sure that metal shavings, debris, and contamination resulting from such work are removed.1.5 Values - The values given in inch-pound units are to be regarded as the standard. The values in parentheses are for information only. See Appendix X2 for SI-based prefixes and powers of 10.Note 1Where SI units are required, refer to Annex 5 of ICAO.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 Design, Alteration, and Certification of Airplane Electrical Wiring Systems

GJB 572A-2006 飞机外部电源供电特性及一般要求

本标准规定了与GJB 181A-2003要求相适应的飞机外部电源供电特性，以及外部电源与飞机连接、外部电源的安全性等方面的一般要求。 本标准适用于交流额定电压115V/200V额定频率400Hz的三相四线制，直流额定电压为28V和270V的两线制飞机外部电源。其它外部电源也可参照执行。

Electrical power characteristics and general requirements for external electrical power source of aircraft

HB 6637.1-2006 航空电气图编制方法 第1部分:飞机

本部分规定了飞机电气图的编制方法。 本部分适用于飞机电气框图、电路图、接线图、线束图及线束敷设图的编制。

Drawing methods for electrical dragrams of aircraft part 1: Aircraft

GJB 5871-2006 航空电机用耐高温无溶剂绝缘漆规范

本规范规定了航空电机用耐高温无溶剂绝缘漆的要求、质量保证规定、交货准备和说明事项等。 本规范适用于航空电机用耐高温无溶剂绝缘漆（以下简称绝缘漆）。

Specification for high-temperature endurance insulating solventless varnishes used for aviation electrical engines

HB 6637.2-2006 航空电气图编制方法 第2部分:机载设备

本部分规定了机载设备（含系统、分系统和单元（组件））各种电气图的编制方法。 本部分适用于机载设备概略图、电路图、接线图和接线表、印制板图的编制。也适用于航空地面设备上述简图和图样的编制。

Drawing methods for electrical dragrams of aircraft Part 2: Airborne equipment

HB 6636-2006 航空电气系统及设备的参照代号

本标准规定了航空电气系统及设备内项目的参照代号、端子代号等的构成和分类码。 本标准适用于航空产品的电气简图、接线表、元件表、说明书及印制板图等电气技术文件，用以标识航空电气系统及设备内的项目。也可用于将参照代号或其一部分表示在电气设备装置和元器件上方或近旁，以标明其功能、名称、位置等。

Reference designations of electrical system and equipments of aircraft

SAE AIR1351E-2006 航空航天用电气和电子布线设备和附件的制造商鉴定

This SAE Aerospace Information Report (AIR) covers the general requirements for and the listing of manufacturers identification that appear on electrical/electronic wiring devices and accessories as required by individual product specifications. This document provides users of electrical/electronic wiring devices means of identifying the manufacturer by use of distinct marking of the device.

Manufacturers Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories

IEC PAS 62500:2006 航空电子设备的过程管理.航空电子系统高速试验的规定和执行指南

In an increasingly harsh economic context (tighter performance requirements, shorter development cycles, reduced cost of ownership, etc.), it is essential to ensure product maturity rapidly and, in any case, by the time of commissioning. It is with a view to remedying shortcomings in traditional development methods that "highly accelerated" tests have been developed. The main underlying principle behind this new type of test strategy is as follows: rather than reasoning in terms of conformity with a specification and simply performing conventional tests, we on the contrary attempt to push the product to its limits by applying environmental stresses and/or stimuli of levels higher than the specification. The aim is thus to take full advantage of current technologies, by eliminating defects which generate potential failures, as of the first prototypes. A well-conducted accelerated test process should, in a relatively short time, lead to a significant increase in the robustness of a product, as early as the initial prototypes stage at the beginning of the development phase, thus accelerating early maturity of this product. Furthermore, identification of the margins available on a "mature" product helps design and size its future environmental stress screening profile more accurately, by increasing the severity of the loadings applied to just what is needed, leading to a particularly significant boost in the efficiency of this environmental stress screening process.

Process management for avionics - Guide for defining and performing highly accelerated tests in avionic systems

BS ISO 23038:2006 航空航天系统.航空太阳能电池.电子和质子辐射试验方法

ISO 23038:2006 specifies the requirements for electron and proton irradiation test methods of space solar cells. It addresses only test methods for performing electron and proton irradiation of space solar cells and not the method for data analysis.

Space systems - Space solar cells - Electron and proton irradiation test methods

GJB 3225A-2006 飞机电源系统液压恒速传动装置通用规范

本规范规定了飞机电源系统液压恒速传动装置的通用要求和质量保证规定。 本规范适用于飞机发动机驱动的液压恒速传动装置（以下简称恒速）的研制及生产。

General specification for hydraulic constant speed driver of aireraft electric power system

DIN EN 4434:2006 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）

Aerospace series - Copper or copper alloy lightweight conductors for electrical cables - Product standard (Normal and tight tolerances); German and English version EN 4434:2005

SAE ARP5674-2006 安装激光器飞机投影进入航道空间安全性考虑

This document is intended to be used for laser systems mounted on aircraft and intended for use in the navigable airspace. This does not include lasers onboard aircraft where the beam is contained within an enclosure so that the beam cannot enter into airspace, nor does it include lasers from satellites and spacecraft in outer space. It may be used in conjunction with: AS4970, ARP5535, ARP5572, ARP5293, and the ANSI Z136 laser safety standards. The purpose of this document is to provide guidance to regulatory and approving authorities on issues specific to the use of aircraft-mounted laser systems designed for use into navigable airspace.

Safety Considerations for Aircraft-Mounted Lasers Projected Into the Navigable Airspace