GB 1406.4-2003 灯头的型式和尺寸 第4部分: 圆筒式和凹式灯头
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基本信息
| 标准名称： | 灯头的型式和尺寸 第4部分: 圆筒式和凹式灯头 |
| 英文名称： | Types and dimensions of cylindrical and recessed caps |
| 中标分类： | 电工 >> 电气照明 >> 灯具附件 |
| ICS分类： | 电气工程 >> 电灯及有关装置 >> 灯头和灯座 |
| 替代情况： | 替代GB/T 2798-1981;被GB/T 1406.4-2008代替 |
| 发布部门： | 中国轻工业联合会 |
| 发布日期： | 2003-08-06 |
| 实施日期： | 2004-02-01 |
| 首发日期： | 1981-11-04 |
| 作废日期： | 2008-12-01 |
| 主管部门： | 中国轻工业联合会 |
| 提出单位： | 中国轻工业联合会 |
| 归口单位： | 全国照明电器标准化技术委员会 |
| 起草单位： | 北京电光源研究所 |
| 起草人： | 全红、杨小平、屈素辉、赵秀荣、朱志英 |
| 出版社： | 中国标准出版社 |
| 出版日期： | 2004-02-01 |
| 页数： | 18页 |
| 书号： | 155066.1-20079 |
适用范围
本部分规定了圆筒式和凹式灯头的型式和尺寸。
本部分适用于那些使用本部分中规定型号的灯头作为灯用附件的电光源产品的设计和生产，也适用于其他电光源产品的设计
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 电气照明 灯具附件 电气工程 电灯及有关装置 灯头和灯座
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【英文标准名称】:Industrialautomationsystemsandintegration-Productdatarepresentationandexchange-Part1645:Applicationmodule:Assemblymodulewithpackagedconnectorcomponent
【原文标准名称】:工业自动化系统和集成.产品数据表示和交换.第1645部分:应用模块:带组件连接件的集合模块
【标准号】:ISO/TS10303-1645-2006
【标准状态】:作废
【国别】:国际
【发布日期】:2006-12
【实施或试行日期】:
【发布单位】:国际标准化组织(IX-ISO)
【起草单位】:ISO/TC184
【标准类型】:()
【标准水平】:()
【中文主题词】:使用;组装件;自动化;自动化系统;连接器;数据交换;数据表示;工业产品;信息交换;信息技术;模数;过程自动化;产品数据;表示法
【英文主题词】:Applications;Assemblies;Automation;Automationsystems;Connectors;Dataexchange;Datarepresentation;Industrialproducts;Informationinterchange;Informationtechnology;Modules;Processautomation;Productdata;Representations
【摘要】:ISO/TS10303-1645:2006specifiestheapplicationmoduleforAssemblymodulewithpackagedconnectorcomponent.ThefollowingarewithinthescopeofISO/TS10303-1645:2006:assemblyphysicaldesign;detailedspecificationofjoinedfeaturesofcomponentsinthedesign;detailedtraceabilityofdesignrequirements;asdesignedimplementationofconnectionrequirement;shapeofassemblydesign;configurationmanagementofassemblydesign;in-processchangemanagementofassemblydesign;connectorsusedascomponentsintheassembly;itemswithinthescopeofapplicationmoduleAssemblymoduledesign,ISO/TS10303-1636;itemswithinthescopeofapplicationmoduleInterfacecomponent,ISO/TS10303-1691.
【中国标准分类号】:N18
【国际标准分类号】:35_240_50
【页数】:40P.;A4
【正文语种】:英语
Product Code:SAE MA4872
Title:Paint Stripping of Commercial Aircraft - Evaluation of Materials and Process
Issuing Committee:Ams J Aircraft Maintenance Chemicals And Materials Committee
Scope: This document details the technical requirements to be used in the evaluation of materials and processes developed for use in stripping organic finishes from fixed wing commercial aircraft.The requirements herein are intended to ensure that the materials and processes used are not detrimental to the commercial aircraft when used as specified. These requirements are not intended to judge performance of the stripping method.These requirements are intended to cover the use of both single and duplex processes involving mechanical, chemical, or thermal means, which include the following: 1) high pressure water blasting (with/without use of chemical paint softeners); 2) dry media blasting (e.g., wheat starch, plastic media blast (PMB), etc.); 3) wet media blasting (e.g., sodium bicarbonate); 4) ice-pellet blasting (e.g., CO2 or water, with/without use of chemical paint softeners); 5) chemical paint stripping (e.g., with/without a dedicated or strippable layer in the paint system); 6) thermal paint stripping (e.g., with/without the use of ice pellet stripping); and 7) other processes, may require different or additional requirements as determined necessary by the user and OEM.The requirements are based on the materials and finishes present on the aircraft at the time of delivery. If the materials, finishes or the processing are changed subsequent to delivery, the individual user may require that additional or different tests be included in any evaluation.The means of compliance with the requirements of this document will have to be negotiated between the user and the relevant regulatory authorities.The test methods defined in this document constitute a recommended means of compliance.The final responsibility for safety, health, environmental consequences, the selection of a process for stripping and the number of stripping cycles rests with the user.It is the responsibility of the user to verify that all testing has been accomplished to the requirements of this specification. This includes verification of laboratory capabilities.A formal instruction and training program for material and equipment operators, to include operator certification, shall be established and maintained by the user.These requirements are not intended to cover repair materials. The individual user shall incorporate process control procedures and inspection to ensure damage to repair materials has not occurred. Repair material guidelines are located in Annex K.Evaluation of strip processes may be performed on metallic and/or composite substrates for use on representative structure as defined by the user. Process limitations shall be well documented by the end user.
Rationale: This document details the technical requirements to be used in the evaluation of materials and processes developed for use in stripping organic finishes from fixed wing commercial aircraft.The requirements herein are intended to ensure that the materials and processes used are not detrimental to the commercial aircraft when used as specified. These requirements are not intended to judge performance of the stripping method.These requirements are intended to cover the use of both single and duplex processes involving mechanical, chemical, or thermal means, which include the following: 1) high pressure water blasting (with/without use of chemical paint softeners); 2) dry media blasting (e.g., wheat starch, plastic media blast (PMB), etc.); 3) wet media blasting (e.g., sodium bicarbonate); 4) ice-pellet blasting (e.g., CO2 or water, with/without use of chemical paint softeners); 5) chemical paint stripping (e.g., with/without a dedicated or strippable layer in the paint system); 6) thermal paint stripping (e.g., with/without the use of ice pellet stripping); and 7) other processes, may require different or additional requirements as determined necessary by the user and OEM.The requirements are based on the materials and finishes present on the aircraft at the time of delivery. If the materials, finishes or the processing are changed subsequent to delivery, the individual user may require that additional or different tests be included in any evaluation.The means of compliance with the requirements of this document will have to be negotiated between the user and the relevant regulatory authorities.The test methods defined in this document constitute a recommended means of compliance.The final responsibility for safety, health, environmental consequences, the selection of a process for stripping and the number of stripping cycles rests with the user.It is the responsibility of the user to verify that all testing has been accomplished to the requirements of this specification. This includes verification of laboratory capabilities.A formal instruction and training program for material and equipment operators, to include operator certification, shall be established and maintained by the user.These requirements are not intended to cover repair materials. The individual user shall incorporate process control procedures and inspection to ensure damage to repair materials has not occurred. Repair material guidelines are located in Annex K.Evaluation of strip processes may be performed on metallic and/or composite substrates for use on representative structure as defined by the user. Process limitations shall be well documented by the end user.
【原文标准名称】:工业自动化系统和集成.产品数据表示和交换.第1645部分:应用模块:带组件连接件的集合模块
【标准号】:ISO/TS10303-1645-2006
【标准状态】:作废
【国别】:国际
【发布日期】:2006-12
【实施或试行日期】:
【发布单位】:国际标准化组织(IX-ISO)
【起草单位】:ISO/TC184
【标准类型】:()
【标准水平】:()
【中文主题词】:使用;组装件;自动化;自动化系统;连接器;数据交换;数据表示;工业产品;信息交换;信息技术;模数;过程自动化;产品数据;表示法
【英文主题词】:Applications;Assemblies;Automation;Automationsystems;Connectors;Dataexchange;Datarepresentation;Industrialproducts;Informationinterchange;Informationtechnology;Modules;Processautomation;Productdata;Representations
【摘要】:ISO/TS10303-1645:2006specifiestheapplicationmoduleforAssemblymodulewithpackagedconnectorcomponent.ThefollowingarewithinthescopeofISO/TS10303-1645:2006:assemblyphysicaldesign;detailedspecificationofjoinedfeaturesofcomponentsinthedesign;detailedtraceabilityofdesignrequirements;asdesignedimplementationofconnectionrequirement;shapeofassemblydesign;configurationmanagementofassemblydesign;in-processchangemanagementofassemblydesign;connectorsusedascomponentsintheassembly;itemswithinthescopeofapplicationmoduleAssemblymoduledesign,ISO/TS10303-1636;itemswithinthescopeofapplicationmoduleInterfacecomponent,ISO/TS10303-1691.
【中国标准分类号】:N18
【国际标准分类号】:35_240_50
【页数】:40P.;A4
【正文语种】:英语
Product Code:SAE MA4872
Title:Paint Stripping of Commercial Aircraft - Evaluation of Materials and Process
Issuing Committee:Ams J Aircraft Maintenance Chemicals And Materials Committee
Scope: This document details the technical requirements to be used in the evaluation of materials and processes developed for use in stripping organic finishes from fixed wing commercial aircraft.The requirements herein are intended to ensure that the materials and processes used are not detrimental to the commercial aircraft when used as specified. These requirements are not intended to judge performance of the stripping method.These requirements are intended to cover the use of both single and duplex processes involving mechanical, chemical, or thermal means, which include the following: 1) high pressure water blasting (with/without use of chemical paint softeners); 2) dry media blasting (e.g., wheat starch, plastic media blast (PMB), etc.); 3) wet media blasting (e.g., sodium bicarbonate); 4) ice-pellet blasting (e.g., CO2 or water, with/without use of chemical paint softeners); 5) chemical paint stripping (e.g., with/without a dedicated or strippable layer in the paint system); 6) thermal paint stripping (e.g., with/without the use of ice pellet stripping); and 7) other processes, may require different or additional requirements as determined necessary by the user and OEM.The requirements are based on the materials and finishes present on the aircraft at the time of delivery. If the materials, finishes or the processing are changed subsequent to delivery, the individual user may require that additional or different tests be included in any evaluation.The means of compliance with the requirements of this document will have to be negotiated between the user and the relevant regulatory authorities.The test methods defined in this document constitute a recommended means of compliance.The final responsibility for safety, health, environmental consequences, the selection of a process for stripping and the number of stripping cycles rests with the user.It is the responsibility of the user to verify that all testing has been accomplished to the requirements of this specification. This includes verification of laboratory capabilities.A formal instruction and training program for material and equipment operators, to include operator certification, shall be established and maintained by the user.These requirements are not intended to cover repair materials. The individual user shall incorporate process control procedures and inspection to ensure damage to repair materials has not occurred. Repair material guidelines are located in Annex K.Evaluation of strip processes may be performed on metallic and/or composite substrates for use on representative structure as defined by the user. Process limitations shall be well documented by the end user.
Rationale: This document details the technical requirements to be used in the evaluation of materials and processes developed for use in stripping organic finishes from fixed wing commercial aircraft.The requirements herein are intended to ensure that the materials and processes used are not detrimental to the commercial aircraft when used as specified. These requirements are not intended to judge performance of the stripping method.These requirements are intended to cover the use of both single and duplex processes involving mechanical, chemical, or thermal means, which include the following: 1) high pressure water blasting (with/without use of chemical paint softeners); 2) dry media blasting (e.g., wheat starch, plastic media blast (PMB), etc.); 3) wet media blasting (e.g., sodium bicarbonate); 4) ice-pellet blasting (e.g., CO2 or water, with/without use of chemical paint softeners); 5) chemical paint stripping (e.g., with/without a dedicated or strippable layer in the paint system); 6) thermal paint stripping (e.g., with/without the use of ice pellet stripping); and 7) other processes, may require different or additional requirements as determined necessary by the user and OEM.The requirements are based on the materials and finishes present on the aircraft at the time of delivery. If the materials, finishes or the processing are changed subsequent to delivery, the individual user may require that additional or different tests be included in any evaluation.The means of compliance with the requirements of this document will have to be negotiated between the user and the relevant regulatory authorities.The test methods defined in this document constitute a recommended means of compliance.The final responsibility for safety, health, environmental consequences, the selection of a process for stripping and the number of stripping cycles rests with the user.It is the responsibility of the user to verify that all testing has been accomplished to the requirements of this specification. This includes verification of laboratory capabilities.A formal instruction and training program for material and equipment operators, to include operator certification, shall be established and maintained by the user.These requirements are not intended to cover repair materials. The individual user shall incorporate process control procedures and inspection to ensure damage to repair materials has not occurred. Repair material guidelines are located in Annex K.Evaluation of strip processes may be performed on metallic and/or composite substrates for use on representative structure as defined by the user. Process limitations shall be well documented by the end user.
