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DIN EN 60730-2-6/A2 Berichtigung 1-2001 DINEN60730-2-6/A2(VDE0631第2-6/A2):1998-11的技术勘误

上一篇: BS EN 60320-1-2001+A1-2007 家用和类似用途设备耦合器.一般要求
下一篇: DIN EN 60730-2-6/A1 Berichtigung 2-2001 DINEN60730-2-6/A1(VDE0631第2-6/A1):1997-10的技术勘误

【英文标准名称】:Communicationnetworksandsystemsforpowerutilityautomation-Part7-420:Basiccommunicationstructure-Distributedenergyresourceslogicalnodes(IEC61850-7-420:2009);EnglishversionEN61850-7-420:2009
【原文标准名称】:公共电力设施自动化通信网络和系统.第7-420部分:基本通信结构,分布式能源逻辑节点(IEC61850-7-420-2009)-英文版本EN61850-7-420-2009
【标准号】:EN61850-7-420-2009
【标准状态】:现行
【国别】:
【发布日期】:2009-10
【实施或试行日期】:2009-10-01
【发布单位】:欧洲标准学会(EN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:建筑设计;自动化;电路网络;指令系统;通信;通信系统;数据元;数据结构;数据传送;定义(术语);分配网;电力系统;电气工程;电气保护设备;电子设备;供能系统(建筑物);英语;支线;馈线;信息交换;信息处理;逻辑层;逻辑终端;铸模;网络控制系统;项目管理;信号传输;规范(验收);站;变电所;系统管理;电讯;电信
【英文主题词】:Architecturaldesign;Automation;Circuitnetworks;Commandsystems;Communication;Communicationsystems;Dataelements;Datastructures;Datatransfer;Definitions;Distributionnetworks;Electricpowersystems;Electricalengineering;Electricalprotectionequipment;Electronicequipment;Energysupplysystems(buildings);Englishlanguage;Feeder;Feederlines;Informationinterchange;Informationprocessing;Logicallayer;Logicalterminals;Modelling;Networkcontrolsystem;Projectmanagement;Signaltransmission;Specification(approval);Stations;Substation;Systemmanagement;Telecommunication;Telecommunications
【摘要】:
【中国标准分类号】:F21
【国际标准分类号】:
【页数】:101P.;A4
【正文语种】:英语


Product Code:SAE AIR5020
Title:Time-Dependent In-Flight Thrust Determination
Issuing Committee:E-33 In Flight Propulsion Measurement Committee
Scope: The purpose and intent of Subcommittee E-33E's effort, the reporting objectives, and the limitations inherent in the reported findings and recommendations are reviewed since these factors are the basis of the information contained in this document. SAE E-33E Subcommittee was formed to assess the level of industry experience that exists in the area of thrust determination during aircraft time-variant operating conditions. A prime objective was to provide a center for gathering expertise and to be a forum for the exchange of ideas and viewpoints. The committee recognized that a practice for the rigorous treatment of time-dependent thrust did not exist and that several critical aspects of its accounting would need to be investigated. The specific objectives of this document are: a. to examine aircraft and engine operating conditions under which the quasi-steady thrust assumption is valid; b. to determine the extent to which time-dependent (nonstationary) force accounting for engine net thrust and propulsion system throttle-dependent terms is required, consistent with existing and developing thrust-minus-drag techniques; c. to report time-dependent thrust methodologies and measurement techniques used for flight and ground testing; d. to present the results of a data review of state-of-the-art methodology appropriate to the determination of aircraft-installed thrust during quasi-steady and dynamic maneuvers; and e. to provide guidelines for validating and improving time-depend thrust and propulsion system throttle-dependent terms is required, consistent with existing and developing thrust-minus-drag techniques; c. to report time-dependent thrust methodologies and measurement techniques used for flight and ground testing; d. to present the results of a data review of state-of-the-art methodology appropriate to the determination of aircraft-installed thrust during quasi-steady and dynamic maneuvers; and e. to provide guidelines for validating and improving time-depend thrust and propulsion system throttle-dependent terms is required, consistent with existing and developing thrust-minus-drag techniques; c. to report time-dependent thrust methodologies and measurement techniques used for flight and ground testing; d. to present the results of a data review of state-of-the-art methodology appropriate to the determination of aircraft-installed thrust during quasi-steady and dynamic maneuvers; and e. to provide guidelines for validating and improving thrust and propulsion system throttle-dependent terms is required, consistent with existing and developing thrust-minus-drag techniques; c. to report time-dependent thrust methodologies and measurement techniques used for flight and ground testing; d. to present the results of a data review of state-of-the-art methodology appropriate to the determination of aircraft-installed thrust during quasi-steady and dynamic maneuvers; and e. to provide guidelines for validating and improving time-dependent thrust determination as appropriate to a specific program.

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