V40 电气系统与设备 标准查询与下载

GB/T 13536-1992 飞机地面供电连接器

本标准规定了飞机地面供电连接器的产品分类、技术要求、试验方法、检验规则、标志、包装、运输、贮存及质量保证期。 本标准适用于地面交流（400Hz）及直流电源向飞机供电的连接器。

Connectors for ground electeical supplies

HB 8666-2022 民用飞机照明设备安装通用要求

General installation requirements of civil aircraft lighting equipments

HB 8653-2022 民用飞机400Hz交流主发电系统通用要求

General requirements for 400Hz alternation current main generation system of civil aircraft

HB 8656-2022 民用飞机冲压空气涡轮驱动的应急交流发电系统通用要求

General requirements for emergency AC power system based on RAT ofthe civil aircraft

HB 8657-2022 民用飞机电源频率变换器通用规范

General specification for electric power frequency converters of civil aircraft

HB 8654-2022 民用飞机变频交流发电系统通用要求

General requirements for variable-frequency alternation current generation system of civil aircraft

HB 8568-2020 民用飞机电气系统模型试验通用要求

General requirements for civil aircraft electric system mockup tests

ASTM F3239-19 飞机电力推进系统标准规范

1.1 This specification addresses airworthiness requirements for the design and installation of electric propulsion systems for aeroplanes. Hybrid-electric propulsion systems are addressed implicitly unless explicitly stated otherwise. This specification was written with the focus on electric propulsion systems with conventional system layout, propulsion characteristics, and operation. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance. 1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this standard (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to the ASTM Committee F44 web page (www.astm.org/COMMITTEE/F44.htm). 1.3 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. 1.4 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 Specification for Aircraft Electric Propulsion Systems

ASTM F3231/F3231M-19 内燃机发电飞机用电气系统的标准规范

1.1 This specification covers electrical systems, electrical equipment, and electrical power distribution aspects of airworthiness and design for aeroplanes with combustion engine generation of electrical power. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Normal Category Aeroplanes. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance. 1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this specification (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to ASTM Committee F44 web page (www.astm.org/COMMITTEE/F44.htm). 1.3 Units—This standard may present information in either SI units, English Engineering units, or both; the values stated in each system are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined. 1.4 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. 1.5 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 Specification for Electrical Systems for Aircraft with Combustion Engine Electrical Power Generation

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 3375-001:2018 航空航天系列. 数字数据传送用电缆. 技术规范

Aerospace series. Cable, electrical, for digital data transmission. Technical specification

BS ISO 23038:2018 航空航天系统.航空太阳能电池.电子和质子辐射试验方法

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

DIN EN 4674-001:2017 航空航天系列.电缆安装.自卷式屏蔽(EMI)保护套管.第001部分:技术规格;德文和英文版本EN 4674-001-2017

Aerospace series - Electrical cables, installation - Self-wrapping shielding (EMI) protective sleeve - Part 001: Technical specification; German and English version EN 4674-001:2017

ISO 2635:2003/Amd 1:2017 航空器.一般用途的飞机电缆和航空航天应用的导线.尺寸和特性.修改件1:修正表1

Aircraft - Conductors for general purpose aircraft electrical cables and aerospace applications - Dimensions and characteristics - Amendment 1: Correction of table 1

BS EN 6138:2017 航空航天系列.接头端用非金属保护帽<= 3 000 PSI液压系统

Aerospace series. Cap, protective, non-metallic for fitting ends 3 000 PSI hydraulic systems

BS EN 6059-302:2017 航空航天系列. 电缆安装. 保护套管. 试验方法. 高温暴露

Aerospace series. Electrical cables, installation. Protection sleeves. Test methods. High temperature exposure

BS EN 6059-301:2017 航空航天系列. 电缆安装. 保护套管. 试验方法. 日照

Aerospace series. Electrical cables, installation. Protection sleeves. Test methods. Sun light exposure

BS EN 6059-304:2017 航空航天系列. 电缆安装. 保护套管. 试验方法. 易燃性

Aerospace series. Electrical cables, installation. Protection sleeves. Test methods. Flammability

IEC TS 62239-2:2017 航空电子设备过程管理. 管理计划. 第2部分: 电子COTS集成管理计划的准备和维护

This part of IEC 62239, which is a technical specification, applies to the development of COTS assembly management plans (CAMPs) for the integration and management of electronic COTS assemblies (see 3.3 and 3.0) in electronic systems used in the ADHP markets where reliability is generally critical. NOTE 1 Best practices for managing the electronic components within the electronic assemblies are described in IEC TS 62239-1 and SAE EIA-STD-4899 which describe the electronic component management program (ECMP). In cases where the electronic components can be identified and managed at the component level, ECMP can be considered as an option to manage the components. NOTE 2 The distinction between an electronic component and an electronic assembly is provided by the definitions in Clause 3. This distinction between an electronic component and an electronic assembly is not always recognized by industry: for example, filters, contactors, power supply modules, relays, magnetic assemblies, etc., can be considered as either components or assemblies. In each application it is considered a best practice for the user of this document to clarify this distinction. Depending on program or product line requirements and/or the technical characteristics of the electronic COTS assemblies and in agreement with the customer, the electronic COTS assembly management plans (CAMPs) could consider tailoring the requirements of this document. See Annex A. Although developed for the avionics industry, this document can be applied by other high performance and high reliability industries at their discretion.

Process management for avionics - Management plan - Part 2: Preparation and maintenance of an electronic COTS assembly management plan

MH/T 9009-2017 便携式电子设备的机载供电系统

本标准规定了便携式电子设备的机载供电系统的术语和定义、技术要求、试验方法、装机测试方法、检验规则、标识、随附文件、包装、运输和贮存。 本标准适用于便携式电子设备的机载供电系统，该系统输入电源为115 V/200 V或230 V /400 V，恒频(400 Hz)/窄变频(360 Hz~650 Hz)/宽变频(360 Hz~800 Hz)的机载三相交流电，输出为110 V/60 Hz或220 V/50 Hz交流电源和5 V直流电源。

Airborne power supply system for portable electronic device