DIN EN ISO 13705-2005 石油和天然气工业.一般炼油厂用火焰加热器
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来源:标准资料网
【英文标准名称】:Petroleumandnaturalgasindustries-Firedheatersforgeneralrefineryservice(ISO13705:2001andTechnicalCorrigendum1:2003);GermanandEnglishversionENISO13705:2001+AC:2003
【原文标准名称】:石油和天然气工业.一般炼油厂用火焰加热器
【标准号】:DINENISO13705-2005
【标准状态】:作废
【国别】:德国
【发布日期】:2005-09
【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】:交货条件;燃烧器;空气预热器;石油工业;规范(验收);加热器;技术数据单;熔炼厂;附件;试验;定义;天然气工业;预加热器;多语种的
【英文主题词】:Accessories;Airpreheaters;Burners;Definition;Definitions;Deliveryconditions;Heaters;Multilingual;Naturalgasindustries;Oilindustries;Preheaters;Refineries;Specification(approval);Technicaldatas
【摘要】:
【中国标准分类号】:E97
【国际标准分类号】:75_180_20
【页数】:490P;A4
【正文语种】:德语
【英文标准名称】:Reliabilityofsystems,equipmentandcomponents-Guidetoreliabilitytestconditionsforconsumerequipment-Conditionsprovidingahighdegreeofsimulationforequipmentforstationaryuseinweatherprotectedlocations
【原文标准名称】:系统、设备和部件的可靠性.第13部分:消耗品可靠性试验条件指南.第2节:局部气候保护场所固定工作设备高度仿真条件
【标准号】:BS5760-13.2-1993
【标准状态】:作废
【国别】:英国
【发布日期】:1993-12-15
【实施或试行日期】:1993-12-15
【发布单位】:英国标准学会(GB-BSI)
【起草单位】:BSI
【标准类型】:()
【标准水平】:()
【中文主题词】:试验;电气设备;环境试验;可靠度;消费品;估计可靠性;固定的;静止的;机械试验;试验持续时间;试验条件
【英文主题词】:Electricappliances;Electricalengineering;Electrically-operateddevices;Environmentaltesting;Equipment;Locations;Reliability;Simulation;Stationary;Testing;Testingconditions;Weatherprotectionsystems
【摘要】:ThispartcontainspreferredtestconditionsasreferredtoinSub-clause8.4ofIECPublication605-1.Wheneverpossible,testcyclesshouldbechosenfromamongthosegiveninthisorothersectionsofIECPublication605-3.ForapplicationsnotcoveredbyPart3,appropriatetestcyclesshouldbedesignedusingIECPublication605-2.Thispartisapplicabletoequipmentforstationaryuseinweatherprotectedlocationsandintemperateclimates.Thedegreeofsimulationishigh.Thetestcycleprovidedhereisnotintendedtoreplacetestsforotherpurposes,suchasqualificationtests,functionalperformancetestsandenvironmentaltests.
【中国标准分类号】:J04
【国际标准分类号】:29_020
【页数】:16P;A4
【正文语种】:英语
Product Code:SAE AIR1083
Title:Airborne Hydraulic and Control System Survivability for Military Aircraft
Issuing Committee:A-6a2 Military Aircraft Committee
Scope: This SAE Aerospace Information Report (AIR) provides the hydraulic system designer with the various design options and techniques currently available to enhance the survivability of hydraulic systems. A comprehensive knowledge of the hostile environment to which the air vehicle will be exposed will form form the basis upon which the overall design philosophy is formulated. The designer should strive to achieve at the absolute minimum acceptable flying quality level to complete the operational mission for which the aircraft is designed; i.e., the aircraft can be controlled and the mission terminated safely, including landing. This AIR will attempt to address the following threats: a. typical small arms fire (5,56, 7.62, 12.7 and 14.5 mm AP); b. cannon (20, 30, and 40 mm API/HEI);c. NBC/EMI/EMP/beamed particle; and d. chemical/biological. Protection against missiles is beyond the scope of this AIR. Except for electronic counter-measures or evasive maneuvers, no practice technology exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. Design implementation; c. Subsystem mechanization; and d. Component design. gy exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. Design implementation; c. Subsystem mechanization; and d. Component design.
Rationale: This SAE Aerospace Information Report (AIR) provides the hydraulic system designer with the various design options and techniques currently available to enhance the survivability of hydraulic systems. A comprehensive knowledge of the hostile environment to which the air vehicle will be exposed will form form the basis upon which the overall design philosophy is formulated. The designer should strive to achieve at the absolute minimum acceptable flying quality level to complete the operational mission for which the aircraft is designed; i.e., the aircraft can be controlled and the mission terminated safely, including landing. This AIR will attempt to address the following threats: a. typical small arms fire (5,56, 7.62, 12.7 and 14.5 mm AP); b. cannon (20, 30, and 40 mm API/HEI);c. NBC/EMI/EMP/beamed particle; and d. chemical/biological. Protection against missiles is beyond the scope of this AIR. Except for electronic counter-measures or evasive maneuvers, no practice technology exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. Design implementation; c. Subsystem mechanization; and d. Component design. gy exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. Design implementation; c. Subsystem mechanization; and d. Component design.
