V40 电气系统与设备 标准查询与下载

GJB 6359-2008 武装直升机夜瞄系统通用规范

本规范规定了武装直升机夜瞄系统的通用要求。 本规范适用于武装直升机夜瞄系统。其它直升机昼/夜观瞄系统亦可参照使用。

General specification for night sight system of arming helicopter

GJB 3367A-2008 飞机变速恒频发电系统通用规范

本规范规定了由交流发电机（以下简称发电机）、功率交换器和发电机控制器等主要通道部件组成的飞机变速恒频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115V/200V、4010Hz三相四线制变速恒频交流发电系统。

General specification for electric power generating system of variable speed and constant frequency of aircraft

GJB 6186-2008 宇航用行程开关总规范

本规范规定了宇航用行程开关（以下简称开关）的技术要求、质量保证规定和交货准备。 本规范适用于机械式宇航用行程开关的设计、生产、试验和验收。

General specification for limit switches for aerospace

SAE AIR4365A-2008 400HZ飞行器电气线路维修程序

This SAE Aerospace Information Report (AIR) describes field-level procedures to determine if 400 Hz electrical connections for external power may have been subjected to excessive wear, which may result in inadequate disengagement forces.

400 Hz Connection Aircraft Electrical Maintenance Procedures

DIN EN 4533-001:2008 航空航天系列.纤维光学系统.手册.第001部分:终端法和工具

This Part of EN 4533 examines the termination aspects of fibre optic design for avionic installations. By termination is meant the mechanism used to interface from one component (usually a fibre) to another. This is normally performed by a connector, which aligns the fibre with another component (usually another connector) to a sufficient accuracy to allow continued transmission of an optical signal throughout the operational envelope. This Part will explain the need for high integrity terminations, provide an insight into component selection issues and suggests best practice when terminating fibres into connectors for high integrity applications. A detailed review of the termination process can be found in Clause 4 of this part and is organised broadly in line with the sequence of a typical termination procedure. The vast number of cable constructions and connectors available make defining a single termination instruction that is applicable to all combinations almost impossible. Because of the problems of defining a generic termination instruction, this handbook has concentrated on defining best practice for current to near future applications of fibre optics on aircraft. This has limited the studies within this part to currently available 'avionic' silica fibre cables and adhesive filled butt-coupled type connectors. Many of the principles described however would still be applicable for other termination techniques. Other types of termination are considered further in the repair part of this handbook. 1.2 Need for high integrity terminations In order to implement a fibre optic based system on an aircraft it is vital to ensure that the constituent elements of the system will continue to operate, to specification, over the life of the system. An important aspect of this requirement is the need for reliable interconnection components. This is often expressed as the need for reliable connectors, but in reality it is the need for a reliable cable to connector termination process. The essence of this requirement is the need to assure reliable light transmission through each optical connector throughout the operational envelope. This needs to be achieved through a robust process that enables a high level of optical performance over the lifetime of the terminations. Many factors can contribute to an optical connector's in-service performance, such as basic connector design, choice of optical fibre, cable, operating and maintenance environment etc. However, one of the main factors governing in-service connector performance is the quality of the cable to connector termination.

Aerospace series - Fibre optic systems - Handbook - Part 001: Termination methods and tools; German and English version EN 4533-001:2006

DIN EN 4533-003:2008 航空航天系列.纤维光学系统.手册.第003部分:航行灯及设备的使用

Looming and installation practices are a critical aspect of any aircraft electrical/avionics installation. In order to provide a reliable and efficient system it is important that the harness installation is designed for reliability and maintainability. This concept holds true for both copper based and fibre optic harnesses. The objective of this part of EN 4533 is to provide technical advice and assistance to designers and engineers on the incorporation of fibre optic harnesses into an airframe, while maintaining maximum compliance with current aircraft electrical harness procedures. This part considers the looming and installation aspects during initial design, throughout the manufacture and installation of the fibre optic harness and how the practices chosen affect through life support of the harness.

Aerospace series - Fibre optic systems - Handbook - Part 003: Looming and installation practices; German and English version EN 4533-003:2006

DIN EN 4533-004:2008 航空航天系列.纤维光学系统.手册.第004部分:修理、维护和检测

The original task headings in the Fibre Optic Harness Study were 'Inspection and Fault Analysis' and 'Repair and Maintenance'. However, to create a more coherent and readable handbook these have been re-arranged in this part of EN 4533 to make two new topic headings - 'Fault analysis and repair' and 'Scheduled maintenance and inspection'. The first deals with what to do when something goes wrong - how to go from a fault notification to locating the fault, and finally, repairing it. The second covers the recommended procedures for upkeep and maintaining harness health over the lifetime of its installation. It is beneficial to read both sections together as many of the practices and techniques are applicable to both situations. Two supplemental sections consider designing a harness with repair and maintenance in mind and good practices when maintaining or repairing a harness. To keep the handbook to a reasonable size, other Hamess Study reports are called up where more detail is required. This handbook does not contain sufficient information, for example, to be the sole reference for harness fault finding but it should provide adequate background for somebody working in that field.

Aerospace series - Fibre optic systems - Handbook - Part 004: Repair, maintenance and inspection; German and English version EN 4533-004:2006

DIN EN 3708-002:2007 航空航天系列.模块化互连系统.终端连接系统.第002部分:性能规范

Aerospace series - Modular interconnection systems - Terminal junction systems - Part 002: Performance specification; German and English version EN 3708-002:2006

DIN EN 3708-001:2007 航空航天系列.模块化互连系统.终端连接系统.第001部分:技术规范

Aerospace series - Modular interconnection systems - Terminal junction systems - Part 001: Technical specification; German and English version EN 3708-001:2006

DIN EN 3708-004:2007 航空航天系列.模块化互连系统.终端连接系统.第004部分:非密封移动式反馈模块版本.产品标准

Aerospace series - Modular interconnection systems - Terminal junction systems - Part 004: Removable feedback modules version, unsealed - Product standard; German and English version EN 3708-004:2006

DIN EN 3708-003:2007 航空航天系列.模块化互连系统.终端连接系统.第003部分:密封移动式反馈模块版本.产品标准

Aerospace series - Modular interconnection systems - Terminal junction systems - Part 003: Removable feedback modules version, sealed - Product standard; German and English version EN 3708-003:2006

DIN EN 3708-005:2007 航空航天系列.模块化互连系统.终端连接系统.第005部分:密封和非密封反馈模块版本用带附件的框架.产品标准

Aerospace series - Modular interconnection systems - Terminal junction systems - Part 005: Frames with accessories for feedback modules version, sealed and unsealed - Product standard; German and English version EN 3708-005:2006

KS W ISO 224:2007 飞行器.设计的说明和飞行器设备的性能.标准型式

이 규격은 항공기 장비에 대한 설계와 성능 내용의 고지에 대한 표준양식을 규정한다. 설계와

Aircraft-Declaration of design and performance for aircraft equipment-Standard form

GJB 5994-2007 舰船电机绝缘用聚酰亚胺薄膜聚芳酰胺纤维纸柔软复合材料制品规范

本规范规定了舰船电机绝缘用聚酰亚胺薄膜聚芳酰胺纤维纸柔软复合材料制品（以下简称复合材料）的技术要求、质量保证规定和交货准备等。 本规范适用于复合材料制品的制造、检验和验收。

Specifications for combined flexibIe materials consist of calendered aramid paper laminated on both side poyimide film used for electrical insulating on naval ship

DIN EN 2714-008:2007 航空航天系列.一般用途用单芯和多芯电缆.工作温度为-55℃～260℃.第008部分:可UV激光打印屏蔽的(编织的)和置于壳内的电缆.产品标准

This standard specifies the characteristics of UV laser printable, single and multicore screened (braided) and jacketed electrical cables for use in the on-board electrical systems of aircraft, at operating temperatures between - 55 ℃ and 260 ℃. It shall also be possible to mark these cables by hot stamp printing or ink jet printing. These markings shall be in accordance with EN 3838. This standard is not valid for new study.

Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between -55 °C and 260 °C - Part 008: Screened (braided) and jacketed, UV laser printable - Product standard; German and English version EN 2714-008:2

DIN EN 2714-006:2007 航空航天系列.一般用途用单芯和多芯电缆.工作温度为-55℃～260℃.第006部分:可CO₂激光打印屏蔽的(编织的)和置于壳内的电缆.产品标准

This standard specifies the characteristics of CO2 laser printable single and multicore screened (braided) and jacketed electrical cables for use in the on-board electrical systems of aircraft, at operating temperatures between - 55 ℃ and 260 ℃. It shall also be possible to mark these cables by hot stamp printing or ink jet printing. These markings shall be in accordance with EN 3838. This standard is not valid for new study.

Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between -55 °C and 260 °C - Part 006: Screened (braided) and jacketed, CO₂ laser printable - Product standard; German and English version EN

DIN EN 2995-004:2007 航空航天系列.额定电流1A～25A温度补偿的单极断路器.第004部分:带单独触点的断路器.产品标准

This standard specifies the characteristics of single-pole circuit breakers, temperature compensated with a rated currentand at from 1A to 25A, used in aircraft on-board circuits at a temperature between -55 ℃ and 125 ℃ and at an altitude of 22 000 m max. These circuit breakers are operated by a push-pull type single push button (actuator), with delayed action "trip-tree" tripping with a signal contact which is open when main contacts are closed, and inversely They will continue to function up to the short-circuit current.

Aerospace series - Circuit breakers, single-pole, temperature compensated, rated current 1 A to 25 A - Part 004: With signal contact - Product standard; German and English version EN 2995-004:2006

DIN EN 2995-001:2007 航空航天系列.额定电流为1A～25A温度补偿的单极断路器.第001部分:技术规范

This standard specifies the single-pole temperature compensated circuit breakers with signal contacts, polarized or not, rated from 1 A to 25 A and used in aircraft on-board circuits. It describes specific environmental, electrical and mechanical characteristics and the stringency of tests to be applied according to test methods of EN 3841-100. These circuit breakers are intended for use in aircraft with electrical supplies in accordance with EN 2282 (all categories).

Aerospace series - Circuit breakers, single-pole, temperature compensated, rated current 1 A to 25 A - Part 001: Technical specification; German and English version EN 2995-001:2006

DIN EN 2995-005:2007 航空航天系列.额定电流为1A～25A温度补偿的单极断路器.第005部分:带偏振信号触点的断路器.产品标准

This standard specifies the characteristics of single-pole circuit breakers, temperature compensated with a rated current from I A to 25 A, used in aircraft on-board circuits at a temperature between -55 ℃ and 125 ℃ and at a maximum altitude of Z = 22 000 m. These circuits breakers are operated by a push-pull type single push button (actuator), with delayed action "trip-free" tripping with a polarized signal contact which is open when main contacts are closed, and inversely. They will continue to function up to the short-circuit current.

Aerospace series - Circuit breakers, single-pole, temperature compensated, rated current 1 A to 25 A - Part 005: With polarized signal contact - Product standard; German and English version EN 2995-005-2006

DIN EN 2713-011:2007 航空航天系列.一般用途用单芯和多芯电缆.工作温度为-55℃～200℃.第011部分:可UV激光打印屏蔽的(螺旋式的)和置于壳内的镀银铜电缆.产品标准

This standard specifies the characteristics of UV laser printable, single and multicore silver plated copper screened (spiral) and jacketed electrical cables for use in the on-board electrical systems of aircraft, at operating temperatures between - 55 ℃ and 200 ℃. It shall also be possible to mark these cables by hot stamp printing or ink jet printing. These markings shall be in accordance with EN 3838.

Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between -55 °C and 200 °C - Part 011: Silver plated copper, screened (spiral) and jacketed, UV laser printable - Product standard; German and English