SAE AS15005 Fitting, Lubrication, Hydraulic, Throat Or Surface Check, 1/8 Pipe Threads, Nickel-Copper Alloy, Type V
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来源:标准资料网
Product Code:SAE AS15005
Title:Fitting, Lubrication, Hydraulic, Throat Or Surface Check, 1/8 Pipe Threads, Nickel-Copper Alloy, Type V
Issuing Committee:G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Scope:No scope available.
上一篇:
SAE AS15006 Fitting, Lubrication, Hydraulic, Leakproof, 1/8 Pipe Threads, Steel, Type Vi下一篇:
SAE AS15004 Fitting, Lubrication, Hydraulic, Surface Check, .250-28 Taper Threads, Nickel-Copper Alloy, Type Iv
基本信息
| 标准名称： | 碳石墨材料 抗冲击强度试验方法 |
| 中标分类： |
电工 >>
电工材料和通用零件 >>
电碳制品 |
| 替代情况： | 被JB/T 7609-2006代替 |
| 发布日期： | 1995-06-01 |
| 实施日期： | 1994-12-09 |
| 首发日期： | 1900-01-01 |
| 作废日期： | 2007-07-01 |
| 出版社： | 机械工业出版社 |
| 出版日期： | 1994-12-09 |
| 页数： | 2 页 |
适用范围
没有内容
前言
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目录
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引用标准
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所属分类： 电工 电工材料和通用零件 电碳制品
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.
