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NF S56-102-1998 休闲膳宿车.旅居车.第2部分:使用者的有效负载

作者:标准资料网 时间:2024-05-04 01:47:22  浏览:9574   来源:标准资料网
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【英文标准名称】:Leisureaccommodationvehicles.Caravans.Part2:userpayloads.
【原文标准名称】:休闲膳宿车.旅居车.第2部分:使用者的有效负载
【标准号】:NFS56-102-1998
【标准状态】:作废
【国别】:法国
【发布日期】:1998-11-01
【实施或试行日期】:1998-11-05
【发布单位】:法国标准化协会(AFNOR)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:设备;最小值;;规范(验收);质量(物质);负荷;定义;定义;有效荷载;载荷分布;设计;居住挂车;旅游居住车
【英文主题词】:Caravanettes;Caravans;Definition;Definitions;Design;Equipment;Leisurevehicles;Load;Loaddistributions;Mass;Minimalvalues;Specification(approval);Usefulload
【摘要】:
【中国标准分类号】:T75
【国际标准分类号】:43_100
【页数】:8P.;A4
【正文语种】:其他


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基本信息
标准名称:客车 门窗用橡胶密封条
英文名称:Buses--Rubber sealing strips of doors and windows
中标分类: 车辆 >> 汽车底盘与车身 >> 车身(驾驶室)及附件
替代情况:调整为QC/T 639-2000
发布日期:1900-01-01
实施日期:1991-05-01
首发日期:1900-01-01
作废日期:1900-01-01
出版日期:1900-01-01
页数:3页
适用范围

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前言

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引用标准

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所属分类: 车辆 汽车底盘与车身 车身(驾驶室)及附件
Product Code:SAE ARP5413
Title:Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning
Issuing Committee:Ae-2 Lightning Committee
Scope:This SAE Aerospace Recommended Practice (ARP) provides guidance for a means of showing compliance with the regulations for hazards caused by the lightning environment to electrical/electronic systems installed either on or within aircraft. Equipment hazards addressed include those due to indirect effects on equipment and its associated wiring that is mounted on the aircraft exterior as well as indirect effects on equipment and its associated wiring located within the aircraft interior. This document applies to new aircraft and equipment designs, modifications of existing aircraft or equipment, and applications of existing (off the shelf) equipment on new aircraft.NOTE: This ARP does not address direct effects such as burning, eroding, blasting, of aircraft structure nor does it address fuel ignition hazards (see related reading material in 2.3 of this document). This ARP does not address lightning zoning methods or lightning test requirements, methods, and techniques. Coverings (fairing, skin, cowl, etc.) should normally prevent direct attachment of the lightning channel to underlying system components. However, if a direct lightning strike attachment to a system component can occur, a complete evaluation of both direct and indirect effects will be necessary.It should be noted that electrical/electronic systems or components are sometimes exposed to lightning currents directly conducted from the aircraft exterior, as may happen when an antenna is struck and a portion of lightning current flows in its cable. Care should be taken to identify any such possibilities and either eliminate these situations by design modifications, or address them in the certification plan. No further discussion of these situations is included in this ARP.

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