DIN 5035-7-2004 人工照明.第7部分:带可视工作站的室内照明
时间:2024-05-18 17:09:37 来源: 标准资料网 作者：标准资料网 阅读：9048
【英文标准名称】:ArtificialLighting-Part7:Lightingofinteriorswithvisualdisplaysworkstations
【原文标准名称】:人工照明.第7部分:带可视工作站的室内照明
【标准号】:DIN5035-7-2004
【标准状态】:现行
【国别】:德国
【发布日期】:2004-08
【实施或试行日期】:
【发布单位】:德国标准化学会(DIN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:照明系统;室内照明;室内照明;室内;规范(验收);防护屏蔽;照明工程;信息处理;定义;数据处理;计划;人类工效学;防眩设备;反射;直观显示装置;布置;自然工作条件;荧光屏;工作地点;灯具;显示装置(计算机);反射比因数;人工照
【英文主题词】:
【摘要】:ThisstandardsupplementsthevariouspartsofDIN5035ontheartificiallightingofinteriorsandgivesspecialrequirementsforthelightingofdisplayworkstationsandforworkstationsdisplaysupport.Besidesitgivesrequirementsforthedesignofthoseinteriorsandworkstationswithrespecttolighting.Atthesametimethearrangementoftheseworkplacesandofthedisplaysinregardtotheartificiallightingistakenintoaccount.
【中国标准分类号】:P31
【国际标准分类号】:91_160_10
【页数】:38P;A4
【正文语种】:德语
【英文标准名称】:SealedInsulatedUndergroundConnectorSystemRated600Volts
【原文标准名称】:额定电压为600伏的密封绝缘式地下连接器系统
【标准号】:ANSIC119.1-2002
【标准状态】:作废
【国别】:美国
【发布日期】:2002
【实施或试行日期】:
【发布单位】:美国国家标准学会(US-ANSI)
【起草单位】:ANSI
【标准类型】:()
【标准水平】:()
【中文主题词】:电连接器
【英文主题词】:Electricconnectors
【摘要】:
【中国标准分类号】:K30
【国际标准分类号】:29_120_30
【页数】:
【正文语种】:英语
MIL-HDBK-762, MILITARY HANDBOOK: DESIGN OF AERODYNAMICALLY STABILIZED FREE ROCKETS (17 JUL 1990)., This chapter introduces the handbook. Rocket systems are presented in two broad classes: military rocket systems and research rocket systems. Military rocket systems are discussed in terms of their application in a battle environment. Research rocket systems are discussed in terms of the application to provide the means of placing data gathering equipment into a desired environment. Operational modes for the rocket systems are described. Finally, brief descriptions of the remaining chapters and the appendices are given. Aerodynamically stabilized free rockets offer relatively simple, reliable, small, low-cost means for delivering payloads and, when great accuracy is not required, are often the optimum systems. This handbook provides engineering design information and data for such rockets. Primarily, this handbook is intended to cover the conceptual and preliminary design phases; however, reference is made to the technical approaches and computer programs required for the system development phase. The material includes operational and interface requirements as they influence the design of the total weapon system. The handbook provides 1. The preliminary design engineer with specific design information and data useful in the rapid response situations required of preliminary design activities 2. The specialist in each technical area an introduction to the other disciplines in terms of data requirements and trade-off studies that must be performed. Free flight rockets are those rockets that do not have an in-flight guidance system; they are aimed, guided, or directed by the launching device. These launchers usually have a launching rail or tube to provide initial direction to the rocket. Free flight rockets are of two basic kinds?spin stabilized and aerodynamically stabilized. The spin stabilized rocket, as the name implies, depends upon a high rate of spin and resulting gyroscopic moments to oppose disturbances. The aerodynamically stabilized rocket depends upon aerodynamic forces on the body and fins to oppose disturbing forces. The aerodynamically stabilized rocket generally employs some spin to minimize dispersion caused by nonsymmetrical body characteristics (body asymmetries, fin misalignment, thrust misalignment, etc.). The data and concepts presented in this handbook are limited to aerodynamically stabilized free flight rockets.