V40 电气系统与设备 标准查询与下载
共找到 1139 条与 电气系统与设备 相关的标准，共 76 页
The requirements for acquiring the Synchros described hereinshall consist of this specification and the altest issue of SAE AS 20708.
Synchro, Torque Receiver Transmitter, Type 31TRX4A
- ICS
- 49.060
- CCS
- V40
- 发布
- 2011-07-26
- 实施
The requirements for acquiring the Synchros described hereinshall consist of this specification and the altest issue of SAE AS 20708.
Synchro, Torque Receiver Transmitter, Type 31TRX6A
- ICS
- 49.060
- CCS
- V40
- 发布
- 2011-07-25
- 实施
The requirements for acquiring the Synchros described hereinshall consist of this specification and the altest issue of SAE AS 20708.
Synchro, Control Transformer, type 26V-08CT4C
- ICS
- 49.060
- CCS
- V40
- 发布
- 2011-07-25
- 实施
本指导性技术文件对HB 7804-2006条文和附录进行了解释和说明,并给出了实施的要点。本指导性技术文件适用于航空制造业数控加工设备(以下简称“数控设备”)综合应用效率的测评,其他机械加工设备也可参照执行。
Guideline of overall application efficiency and evaluating of NC equipment
- ICS
- CCS
- V40
- 发布
- 2011-07-19
- 实施
- 2011-10-01
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment anticollision light systems. This Aerospace Standard defines minimum light intensity in terms of "effective intensity" as defined in paragraph 3.5 of this standard and specified vertical and horizontal directions about the longitudinal and vertical axis of the airplane. It will also define flash rate and color for the anticollision light system. It is not intended that this standard require the use of any particular light source such as Xenon, LED or any other specific design of lamp.
Minimum Performance Standard for Anticollision Light Systems
- ICS
- 49.045
- CCS
- V40
- 发布
- 2011-06-20
- 实施
Aerospace series - Testing of aircraft wiring.
- ICS
- 49.060
- CCS
- V40
- 发布
- 2011-06-01
- 实施
- 2011-06-04
This document presents minimum criteria for the design and installation of LED assemblies in aircraft. The use of "shall" in this specification expresses provisions that are binding. Non-mandatory provisions use the term "should." The purpose of this SAE Aerospace Recommended Practice (ARP) is to recommend minimum design criteria which will lead to adequate performance standards for LED products in and on aircraft. This document recommends design and performance criteria for developing products subject to CFR Parts 23, 25, 27, and 29 certification that use light emitting diodes (LED) as their primary source of light for luminance and illuminance applications. It is intended as guidance for the certifying authority and lighting design engineers. This document includes but is not limited to commercial aircraft.
LEDs and Aircraft Applications
- ICS
- 49.060
- CCS
- V40
- 发布
- 2011-04-27
- 实施
Aerospace series - Testing of aircraft wiring; German and English version EN 2283:2010
- ICS
- 49.060
- CCS
- V40
- 发布
- 2011-02
- 实施
Aerospace series. Design and installation of aircraft electrical and optical interconnection systems
- ICS
- 49.060;49.090
- CCS
- V40
- 发布
- 2011-01-31
- 实施
- 2011-01-31
Provides guidance on criteria and format for preparing a COTS Assembly Management Plan (CAMP) Need: Requires reaffirmation including incorporation of Lessons Learned since initial release. Emphasis will be given to addressing component selection/qualification concerns and where applicable coordinate with IEC TS-62239.
Standard for Preparing a COTS Assembly Management Plan
- ICS
- 49.060;49.090
- CCS
- V40
- 发布
- 2011
- 实施
Aerospace series. Testing of aircraft wiring
- ICS
- 49.060
- CCS
- V40
- 发布
- 2010-12-31
- 实施
- 2010-12-31
本部分规定了有人驾驶固定翼飞机进行电气系统科研试飞训练的通用要求。 本部分适用于有人驾驶固定翼飞机电气系统科研试飞训练的技术准备、组织实施与评价。特种用途固定翼军用飞机可参照执行。
Training requirements of flight test research for military aircraft.Part 12:Electricity
- ICS
- CCS
- V40
- 发布
- 2010-09-16
- 实施
- 2010-12-01
Aerospace series - Lamps, incandescent - Part 029: Lamp, code 338 - Product standard; German and English version EN 2240-029:2010
- ICS
- 49.060
- CCS
- V40
- 发布
- 2010-09
- 实施
Aerospace series - Bonding straps for aircraft - Part 003: Bonding strap assemblies with flat braided conductor copper, tin plated -65 °C up to 150 °C and copper, nickel plated -65 °C up to 260 °C - Product standard; German and English version EN 4199-003
- ICS
- 49.060
- CCS
- V40
- 发布
- 2010-08
- 实施
Aerospace series - Cable, electrical, for signal transmission - Part 008: Cable, coaxial, 50 ohms, 200 °C, Type WD - Product standard; German and English version EN 4604-008:2009
- ICS
- 49.060
- CCS
- V40
- 发布
- 2010-08
- 实施
This SAE Aerospace Information Report (AIR) is a review of the general characteristics of power sources that may be used to provide secondary, auxiliary, or emergency power for use in aircraft, space vehicles, missiles, remotely piloted vehicles, air cushion vehicles, surface effect ships, or other vehicles in which aerospace technology is used. The information contained herein is intended for use in the selection of the power source most appropriate to the needs of a particular vehicle or system. The information may also be used in the preparation of a power source specification. Considerations for use in making a trade study and an evaluation of the several power sources are included. More detailed information relating to specific power sources is available in other SAE Aerospace Information Reports or in Aerospace Recommended Practices.
Aerospace Auxiliary Power Sources
- ICS
- 49.080
- CCS
- V40
- 发布
- 2010-06-16
- 实施
This standard provides a list of all parts of sleeves in meta-aramid fibres EN 6049 required for the protection of cable and cable bundles for aerospace application.
Aerospace series - Electrical cables, installation - Protection sleeve in meta-aramid fibres - General and list of product standards
- ICS
- 49.060
- CCS
- V40
- 发布
- 2010-05-31
- 实施
- 2010-05-31
The document specifies the required characteristics for lamp, code 83, used on-board aircraft. It shall be used together with EN 2756.
Aerospace series - Lamps, incandescent - Part 009: Lamp, code 83 - Product standard; German and English version EN 2240-009:2009
- ICS
- 49.060
- CCS
- V40
- 发布
- 2010-04
- 实施
The document specifies the required characteristics for lamp, code 47, used on-board aircraft. It shall be used together with EN 2756.
Aerospace series - Lamps, incandescent - Part 004: Lamp, code 47 - Product standard; German and English version EN 2240-004:2010
- ICS
- 49.060
- CCS
- V40
- 发布
- 2010-04
- 实施
The document specifies the required characteristics for lamp, code 44, used on-board aircraft. It shall be used together with ENN 2756.
Aerospace series - Lamps, incandescent - Part 003: Lamp, code 44 - Product standard; German and English version EN 2240-003:2010
- ICS
- 49.060
- CCS
- V40
- 发布
- 2010-04
- 实施
