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ISO 10294-3-1999 耐火试验用于空气调节系统的防火阀第3部分:试验方法指南

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【英文标准名称】:Fireresistancetests-Firedampersforairdistributionsystems-Part3:Guidanceonthetestmethod
【原文标准名称】:耐火试验用于空气调节系统的防火阀第3部分:试验方法指南
【标准号】:ISO10294-3-1999
【标准状态】:现行
【国别】:国际
【发布日期】:1999-04
【实施或试行日期】:
【发布单位】:国际标准化组织(ISO)
【起草单位】:ISO/TC92
【标准类型】:()
【标准水平】:()
【中文主题词】:火焰表面传播;试验结果;防火;空调系统;火炉调节闸;说明书;试验;说明;使用;通风道工程;燃烧试验;建筑物
【英文主题词】:Air-conditioningsystems;Applications;Buildings;Explanation;Firedampers;Fireprotection;Firetests;Instructions;Surfacespreadofflame;Testresults;Testing;Ventilationductwork
【摘要】:ThispartofISO10294givesguidanceontheapplicationofthetestmethodspecifiedinISO10294-1:1996.Thistestmethodisconcernedwiththeassessmentofafiredampertopreventthespreadoffireandhotgasesfromonecompartmenttoanother.Itisnotintendedfordampersusedonlyinsmokecontrolsystems.Itisapplicabletofiredampersincludedinanairdistributionsystem.Thetestisnotdesignedtotestfireprotectiondeviceswhichonlydealwithairtransferapplications,orwhenadamperisusedinsuspendedceilingsastheinstallationofthedamperandductmayhaveanadverseeffectontheperformanceofthesuspendedceilingandothermethodsofevaluationmayberequired.NOTE"Airtransfer"isalow-pressureapplicationthroughafireseparationdoor(orwall,floor)withoutanyconnectiontoanairduct.
【中国标准分类号】:P16
【国际标准分类号】:13_220_40;91_140_30
【页数】:12P;A4
【正文语种】:英语


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【英文标准名称】:Aluminiumladderandstepladder
【原文标准名称】:铅合金活动梯及梯子
【标准号】:JISS1121-1992
【标准状态】:作废
【国别】:日本
【发布日期】:1992-05-01
【实施或试行日期】:
【发布单位】:日本工业标准调查会(JISC)
【起草单位】:ConsumerLife
【标准类型】:()
【标准水平】:()
【中文主题词】:梯子;踏步(楼梯);铝合金;家用的;家用设备
【英文主题词】:steps(stairs);ladders;domestic;aluminiumalloys;householdequipment
【摘要】:
【中国标准分类号】:P32
【国际标准分类号】:97_145
【页数】:20P;A4
【正文语种】:日语


Product Code:SAE AIR34
Title:Penalties in Performance of Three-Phase, Four-Wire, 400-Cycle Motors Causes By the Opening of One Phase
Issuing Committee:Ae-7a Generators And Controls Motors And Magnetic Devices
Scope:The scope of this SAE Aerospace Information Report (AIR) is to present a guide for the determination of probable power output and the effect on the aircraft system that will be experienced when operating three-phase motors with one phase open. Unfortunately, the above subject cannot be resolved by specific rules. Modern aircraft or missile electrical systems are composed of a wide variety of electrical and electronic components. These components react differently under identical impetus due to the latitude of their design. This latidue of design must be allowed wherever possible to the accessory designer due to the various specification requirements. Therefore, it cannot be over-emphasized that the effect on the airplane or missile system, as well as motor operation, of three-phase motors on two-phase power must be thoroughly investigated.