DIN EN 12067-1/A1-2003 燃气燃烧器和燃气装置用燃气/空气比例控制器.第1部分:气动型.修改件A1

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【英文标准名称】:Gas/airratiocontrolsforgasburnersandgasburningappliances-Part1:Pneumatictypes;AmendmentA1;GermanversionEN12067-1:1998/A1:2003
【原文标准名称】:燃气燃烧器和燃气装置用燃气/空气比例控制器.第1部分:气动型.修改件A1
【标准号】:DINEN12067-1/A1-2003
【标准状态】:作废
【国别】:德国
【发布日期】:2003-08
【实施或试行日期】:2003-08-01
【发布单位】:德国标准化学会(DE-DIN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:产品规范;热环境系统;功能;持久性;燃气技术;燃烧器;煤气;空气;燃气动力装置;气压调速器;结构要求;连接点;压力梯度;特性;技术文献;装配;气动力学;操作规范;控制系统;气压;燃气器具;差压;尺寸;利用;气动的;定义;大气压;机械性能;控制信号;压力调节器;材料;控制器;安全;规范(验收);作标记;耐久性;试验;燃气燃烧器;设计;制造日期;安全工程
【英文主题词】:Air;Atmosphericpressure;Burners;Constructionrequirements;Controlsignals;Controlsystems;Controllers;Dataofthemanufacturer;Definition;Definitions;Design;Differentialpressures;Dimensions;Durability;Functions;Gasappliances;Gasburners;Gaspressure;Gaspressuregovernors;Gastechnology;Gases;Gas-powereddevices;Installation;Junction;Marking;Materials;Mechanicalproperties;Operatingspecification;Permanency;Pneumatic;Pneumatics;Pressuregradients;Pressureregulators;Productspecification;Properties;Safety;Safetyengineering;Specification(approval);Technicaldocuments;Testing;Thermalenvironmentsystems;Utilization
【摘要】:
【中国标准分类号】:Q82
【国际标准分类号】:23_060_40;27_060_20
【页数】:3P.;A4
【正文语种】:德语

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【英文标准名称】:SeeATIST1.114
【原文标准名称】:电信.第7信号系统(SS7).处理能力应用部分(TCAP)
【标准号】:ANSIT1.114-1996
【标准状态】:作废
【国别】:美国
【发布日期】:1996-01-01
【实施或试行日期】:
【发布单位】:美国国家标准学会(ANSI)
【起草单位】:ANSI
【标准类型】:()
【标准水平】:()
【中文主题词】:电信;电信;信号发送系统;面向处理部分;信号传输;应用;综合服务数字网络;处理
【英文主题词】:telecommunications;signallingsystems;transaction-oriented;transactions;signaltransmission;isdn;telecommunication;applications
【摘要】:
【中国标准分类号】:M12
【国际标准分类号】:33_040_30
【页数】:128P;A4
【正文语种】:英语

Product Code:SAE AS94
Title:Snap Ring, Non-Controllable Propeller Hub (NONCURRENT Aug 1973)
Issuing Committee:E-25 General Standards For Aerospace And Propulsion Systems
Scope:The purpose of Section I of this document is to specify the requirements for minimum safe performance of an altimeter system in its normal mode of operation on subsonic aircraft. Compliance with this section is a means of assuring that the altimeter system will satisfactorily perform its intended function when exposed to conditions encountered in routine aeronautical operations (normal operation). The instrument system specified shall accept an input of static pressure and in some equipment other inputs that contribute altitude information to provide a visual indication of pressure altitude. If equipped with an automatic correction mechanism, it shall indicate by a positive means when the automatic correction mechanism is not in use. If the static source pressure error compensating mechanism is operational it shall be functional throughout the required operating envelope of the particular aircraft. Each aircraft type has its own static source error data which shall be obtained from the airframe manufacturer's certified data. When a Central Air Data Computer is used in the altimeter system, the CADC shall be certified to its own governing document and the altimeter system (CADC and display) shall comply with the requirements of this document. NOTE: The instrument system specified herein does not include the aircraft pressure lines and pressure sources