49.060 航空航天用电气设备和系统 标准查询与下载

BS EN 4839-001:2018 航空航天系列 电弧故障断路器 三极 温度补偿 额定电流 3 A 至 25 A 115 V 交流 400 Hz 恒定频率 技术规格

What is this standard about? This European Standard specifies the three-poles temperature compensated arc fault circuit breakers without signal contacts, rated from 3 A to 25 A and used in aircraft on-board circuits. In any operating state a "trip-free" tripping is ensured. These Items are designed to protect aircraft wiring system from circuit overload and arc faults. It describes specific environmental, electrical and mechanical characteristics and the stringency of tests to be applied according to test methods of EN 3841-100. If the design of the arc fault circuit breakers contains software or complex hardware, as a minimum, the software and hardware shall be developed in accordance with RTCA DO-178B or C, DAL C and RTCA DO-254, DAL C, respectively. These circuit breakers are intended for use in aircraft with electrical supplies in accordance with EN 2282.

Aerospace series. Arc fault circuit breakers, three-poles, temperature compensated, rated current 3 A to 25 A - 115 V a.c. 400 Hz constant frequency - Technical specification

BS EN 4611-006:2018 航空航天系列 通用电气电缆 单芯和多芯组件 XLETFE 系列 镀银铜 工作温度在 65 °C 至 150 °C 之间 双挤压壁适合开放式应用 可紫外激光打印 ...

What is BS EN 4611-006  - Silver-plated electrical cables about ?    BS EN 4611‑006 specifies the characteristics of UV laser printable, silver-plated copper conductor electrical cables Crosslinked Ethylene Tetra Fluoro Ethylene copolymer (XLETFE) family for use in the onboard electrical systems of aircraft operating at temperatures between – 65 °C and 150 °C. The voltage rating is 600 V rms at sea level. This insulation system has been used in aerospace applications using 115 V ac (phase-to-neutral) 400 Hz and 28 V dc.     Who is BS EN 4611-006 - Silver-plated electrical cables for ?   BS EN 4611‑006 on silver-plated conductor electrical cables (Dual extruded wall for open applications) for aerospace applications is applicable to:  

Aerospace series. Cables, electrical, for general purpose, single and multicore assembly. XLETFE Family - Silver plated copper Operating temperatures, between - 65 °C and 150 °C. Dual extruded wall for open applications. UV laser printable.…

BS EN 4839-003:2018 航空航天系列 电弧故障断路器 三极 温度补偿 额定电流 3 A 至 25 A 115/200 V 交流 400 Hz 恒定频率 不带辅助触点 产品标准

This European Standard specifies the required characteristics for three-pole, arc fault circuit breakers, rated currents from 3 A to 25 A, switching capacity 65 In, for use in aircraft electrical systems. Their operating temperatures are between − 40 °C to 85 °C at a maximum altitude of Z = 15 000 m. The thermal protection is temperature compensated and operates between − 55 °C and 125 °C. These arc fault circuit breakers are operated by a push-pull type single pushbutton (actuator), with delayed action "trip-free" tripping. They will continue to function up to the short-circuit current.

Aerospace series. Arc Fault Circuit breakers, three-pole, temperature compensated, rated currents 3 A to 25 A, 115/200 V a.c. 400 Hz constant frequency - Without auxiliary contacts. Product standard

BS EN 4611-007:2018 航空航天系列 通用电气电缆 单芯和多芯组件 XLETFE 系列 镀镍铜 工作温度为 65 °C 至 150 °C 双挤压壁适合开放式应用 可紫外激光打印 ...

What is BS EN 4611-007  - Nickel-plated cables about ?    BS EN 4611 ‑ 007 specifies the characteristics of UV laser printable, nickel-plated copper conductor electrical cables Crosslinked Ethylene Tetra Fluoro Ethylene copolymer (XLETFE) family for use in the onboard electrical systems of aircraft operating at temperatures between – 65 °C and 150 °C. The voltage rating is 600 V rms at sea level. This insulation system has been used in aerospace applications using 115 V ac (phase-to-neutral) 400 Hz and 28 V dc.   These cables are suitable for air flame use.   Who is BS EN 4611-007  - Nickel-plated cables for ?   BS EN 4611 ‑ 007 on nickel-plated ...

Aerospace series. Cables, electrical, for general purpose, single and multicore assembly. XLETFE Family - Nickel plated copper. Operating temperatures, between - 65 °C and 150 °C. Dual extruded wall for open applications. UV laser printable.…

BS EN 4708-106:2018 航空航天系列 热收缩套管 用于捆绑、绝缘和识别 火灾危险有限的套管 工作温度 30°C 至 105°C 产品标准

What is BS EN 4708-106 - Fire hazard sleeving about ?     BS EN 4708-106 is a European Standard that specifies the required characteristics for four types of heat-shrinkable limited fire hazard sleeving for use in aircraft electrical systems at operating temperatures between – 30 °C and 105 °C.   This sleeving is flexible, flame retarded and emits minimum smoke, gases and corrosive by-products when exposed to fire. It is available with various wall thicknesses and, also in a higher shrink ratio according to the application and degree of mechanical protection required. It is suitable for use (e.g., as cable protection) in areas where smoke, gases or corrosive by-products would constitute a particular hazard.   Type A: Thick wall shrink ratio 2:1 and is normally supplied with internal diameters up to 102,0 mm  

Aerospace series. Sleeving, heat-shrinkable, for binding, insulation and identification - Limited fire hazard sleeving. Operating temperatures. 30 °C to 105 °C. Product standard

BS EN 4708-102:2018 航空航天系列 热收缩套管 用于粘合、绝缘和识别 非常柔韧的聚合物 工作温度 75°C 至 150°C 产品标准

What is BS EN 4708-102 - Flexible polymer about ?    BS EN 4708-102 is a European Standard specifies the required characteristics for a heat-shrinkable, very flexible polymer sleeving for use in aircraft electrical systems at operating temperatures between ‒ 75 °C to 150 °C. This sleeving has very good flexibility, is flame retarded, and has a thick wall for mechanical protection. It is suitable for use as cable protection in areas where wiring is subject to contamination by aircraft fuels and hydraulic fluids.   These sleevings are normally supplied with internal diameters up to 102 mm for shrink ratios of 2:1. They are available in black only.   Sizes other than those specifically listed in BS EN 4708-102 may be available. These items shall be considered to comply with BS EN 4708-102 if...

Aerospace series. Sleeving, heat-shrinkable, for binding, insulation and identification - Very flexible polymer. Operating temperature. 75 °C to 150 °C. Product standard

BS EN 4611-005:2018 航空航天系列 通用电气电缆 单芯和多芯组件 XLETFE 系列 镀银铜 工作温度在 65 °C 和 150 °C 之间 适用于封闭应用的单挤压壁 紫外激光…

What is BS EN 4611-005  - Silver-plated cables about ?    BS EN 4611-005 specifies the characteristics of UV laser printable, silver-plated copper conductor electrical cables Crosslinked Ethylene Tetra Fluoro Ethylene copolymer (XLETFE) family for use in the onboard electrical systems of aircraft operating at temperatures between – 65 °C and 150 °C. The voltage rating is 600 V rms at sea level. This insulation system has been used in aerospace applications using 115 V ac (phase-to-neutral) 400 Hz and 28 V dc.    These cables are only suitable for air flame use with additional protection against mechanical abuse. BS EN 4611-005 outlines the terms, definitions, symbols and abbreviations, materials and construction, required characteristics, quality assurance, designation, identification and marking, packaging, labelling and delivery lengths, and technical specifications.   Who is BS EN 4611-005  - Silver-plated cables

Aerospace series. Cables, electrical, for general purpose, single and multicore assembly. XLETFE Family - Silver plated copper. Operating temperatures between - 65 °C and 150 °C. Single extruded wall for enclosed applications. UV laser…

BS EN 3745-202:2018 航空航天系列. 飞行器用光纤和光缆. 试验方法. 纤维尺寸

Aerospace series. Fibres and cables, optical, aircraft use. Test methods. Fibre dimensions

ASTM F2639-18 飞机电气接线系统的设计 改造和认证标准实践

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 Cautions—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” 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 This practice includes the following sections: Title Section Wire Selection 5 General 5.1 Aircraft Wire Materials 5.2 Table of Acceptable Wires 5.3 Severe Wind and Moisture Problems (SWAMP) 5.4 Grounding and Bonding 5.5 Electrical Wire Chart 5.6 Wire and Cable Identification 6 General 6.1 Wire and Cable Identification 6.2 Types of Markings 6.3 Sleeve and Cable Marker Selection 6.4 Placement of Identification Markings 6.5 Wiring Installation 7 General 7.1 Wire Harness Installation 7.2 Power Feeders 7.3 Service Loops 7.4 Drip Loops 7.5 Soldering 7.6 Strain Relief 7.7 Grounding and Bonding 7.8 Splicing 7.9 Fuel Tank Wiring 7.10 Corrosion Preventative Compounds (CPC) (MIL-C-81309) 7.11 Electrical Load Considerations 8 General 8.1 Methods for Determining the Current-Carrying Capacity of Wires 8.2 Acceptable Means of Monitoring and Controlling the Electrical Load 8.3 Electrical System Components 9 General 9.1 Alternators 9.2 Generators 9.3 Ground Power Units 9.4 Auxiliary Power Units 9.5 Batteries 9.6 Circuit Protection Devices 9.7 Conduit 9.8 Connectors 9.9 Inverters and Power Converters 9.10 Junctions 9.11 Junction Boxes 9.12 Electronic Assemblies 9.13 Relays 9.14 Studs 9.15 Switches 9.16 Terminals and Terminal Blocks 9.17 Waveguides 9.18 Electrical System Component Installation 10 General 10.1 Alternators 10.2 Generators 10.3 Auxiliary Power Units (APUs) 10.4 Batteries 10.5 Circuit Protection Devices 10.6 Conduit 10.7 Connectors 10.8 Inverters and Power Converters 10.9 1 This practice is under the jurisdiction of ASTM Committee F39 on Aircraft Systems and is the direct responsibility of Subcommittee F39.01 on Design, Alteration, and Certification of Electrical Systems. Current edition approved Oct. 1, 2018. Published November 2018. Originally approved in 2007. Last previous edition approved in 2015 as F2639 – 15. DOI: 10.1520/F2639-18. Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee. 1 Junctions 10.10 Junction Boxes, Panels, Shields, and Microswitch Housings 10.11 PC Board Assemblies 10.12 Relays 10.13 Studs 10.14 Switches 10.15 Terminals and Terminal Blocks 10.16 Waveguides 10.17 EMI/RFI 11 General 11.1 Grounding and Bonding 11.2 HIRF 11.3 Lightning 11.4 Alterations 12 General 12.1 Wire Substitutions 12.2 Commercial Off-the-Shelf (COTS) Components 12.3 Electrical Load Considerations 12.4 Batteries 12.5 Circuit Breakers 12.6 Junction Boxes 12.7 Relays 12.8 Switches 12.9 Wire Marking 12.10 Wire Bundle Routing 12.11 Wire Bundle Combing 12.12 Interference Tests 12.13 System Safety Assessments 12.14 Certification Processes 13 General 13.1 Certification 13.2 Alterations and Maintenance 13.3 1.6 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 1—Where SI units are required, refer to Annex 5 of ICAO. 1.7 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.8 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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

DIN EN 4604-010:2018 航空航天系列 信号传输用电气电缆 第010部分：轻型同轴电缆，50 欧姆，200°C，KX 型（轻型 WD） 产品标准

This European Standard specifies the required characteristics of a light weight coaxial cable, 50 Ω, type KX for use in aircraft electrical systems at operating temperature between -55 °C and 200 °C and specially for high frequency up to 6 GHz. Nevertheless, if needed, -65 °C is also acceptable as shown by rapid change of temperature test.

Aerospace series - Cable, electrical, for signal transmission - Part 010: Cable, coaxial, light weight, 50 Ohms, 200 °C, type KX (light WD) - Product standard; German and English version EN 4604-010:2018

DIN EN 4840-101:2018 航空航天系列 热收缩成型件 第101部分：聚烯烃，半刚性，有限火灾危险 温度范围 30°C 至 105°C 产品标准

This European Standard specifies the required characteristics for heat-shrinkable polyolefin semi-rigid, limited fire hazard heat-shrinkable boots for use in aircraft electrical systems at operating temperatures between -30 °C and 105 °C. The moulded shapes may be supplied with a pre-coated adhesive. Refer to the manufacturers/suppliers for options. A guide to adhesive compatibility is given in Annex A. These moulded shapes are normally supplied in the styles and dimensions given in EN 4840-002 Tables 1 to 22. The colour is normally black. Styles and dimensions other than those specifically listed in EN 4840-002 Tables 1 to 22 may be available as custom items. These items shall be considered to comply with this standard if they comply with the property requirements listed in Table 1 with the exception of dimensions.

Aerospace series - Heat shrinkable moulded shapes - Part 101: Polyolefin, semi-rigid, limited fire hazard - Temperature range - 30 °C to 105 °C - Product standard; German and English version EN 4840-101:2018

BS ISO 20894:2018 飞机 基于 LED 的滑行灯系统 一般要求

1   Scope This document specifies characteristics and interface requirements for the LED taxiing light system .

Aircraft. LED based taxiing lightsystem. General requirements

IEC 62239-1:2018 航空电子学程序管理 - 管理计划 - 第1部分:电子元件管理计划的准备和维护

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

BS EN 6049-003:2018 航空航天系列 电缆、安装 间位芳纶纤维保护套 编织、管状、可扩展 产品标准

Aerospace series. Electrical cables, installation. Protection sleeve in meta-aramid fibres. Braided, tubular, expandable. Product standard

BS EN 6049-001:2018 航空航天系列 电缆安装 间位芳香族聚酰胺纤维保护套管 技术规格

Aerospace series. Electrical cables, installation. Protection sleeve in meta-aramid fibres. Technical specification

DIN EN 4641-001:2018 航空航天系列.外经为125µm的包层光缆.第001部分:技术规范; 德文和英文版本EN 4641-001-2018

This European Standard specifies the general characteristics, conditions for qualification, acceptance and quality assurance, as well as the test methods and groups for fibre optic cables with a cladding of 125 µm outside diameter.

Aerospace series - Cables, optical, 125 µm diameter cladding - Part 001: Technical specification; German and English version EN 4641-001:2018

ISO 20894:2018 飞机.基于LED的滑行灯系统.一般要求

This document specifies characteristics and interface requirements for the LED taxiing light system.

Aircraft - LED based taxiing lightsystem - General requirements

BS EN 2084:2018 航空航天系列 通用电气电缆 带铜或铜合金导体 技术规格

Aerospace series. Cables, electrical, general purpose, with conductors in copper or copper alloy. Technical specification

BS EN 4611-002:2018 航空航天系列 单芯和多芯组件的一般用途的电缆 XLETFE族 总则

Aerospace series. Cables, electrical, for general purpose, single and multicore assembly. XLETFE Family. General

BS EN 3646-006:2018 航空航天系列 连接器 电气 圆形 卡口耦合 工作温度 175 $0DC 或 200 $0DC 连续 插座 密封 锁紧螺母安装 产品标准

Aerospace series. Connectors, electrical, circular, bayonet coupling, operating temperature 175 $0DC or 200 $0DC continuous. Receptacle, hermetic, jam-nut mounting. Product standard