BS 3283-1-1980 便携式电器用不可逆连接器与电器输入端(250V以下电路用).第1部分:13A连接器与电器输入端规范

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【英文标准名称】:Non-reversibleconnectorsandapplianceinletsforportableelectricalappliances(forcircuitsupto250V)-Specificationfor13Aconnectorandapplianceinlet
【原文标准名称】:便携式电器用不可逆连接器与电器输入端(250V以下电路用).第1部分:13A连接器与电器输入端规范
【标准号】:BS3283-1-1980
【标准状态】:作废
【国别】:英国
【发布日期】:1980-04-30
【实施或试行日期】:1980-04-30
【发布单位】:英国标准学会(BSI)
【起草单位】:BSI
【标准类型】:()
【标准水平】:()
【中文主题词】:插座;弯曲试验;漏电路径;拨拉试验;软导体;热试验;介电强度试验;电触点;试验设备;余隙距离;便携的;电驱动装置;作标记;电插头;电气试验;尺寸;设计;家用电器;机械试验;电连接器;电路;定型试验;腐蚀试验;量规;额定电流
【英文主题词】:
【摘要】:Requirementsandtestsforbothre-wireableandnon-rewireabletypes.Suitableforusewithapplianceswherethetemperatureofthecontactpinsdoesnotexceed120C.
【中国标准分类号】:L23
【国际标准分类号】:29_120_20
【页数】:16P;A4
【正文语种】:英语


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Product Code:SAE AIR1703
Title:In-Flight Thrust Determination
Issuing Committee:E-33 In Flight Propulsion Measurement Committee
Scope: This report reviews the major aspects of processes that may be used for the determination of in-flight thrust. It includes discussions of basic definitions, analytical and ground-test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of the propulsion system during the flight development program of the aircraft. Much of the treatment is necessarily brief due to space limitations. This document and the British Ministry/Industry Drag Analysis Panel (MIDAP) Guide, which SAE Committee E-33 used as a starting point, can be used to understand the processes and limitations involved in the determination of in-flight thrust. (1.1)* Application to a specific in-flight thrust determination program will require the use of many important assumptions not fully developed herein, and these assumptions must be evaluated during the conduct of the program.
Rationale: This report reviews the major aspects of processes that may be used for the determination of in-flight thrust. It includes discussions of basic definitions, analytical and ground-test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of the propulsion system during the flight development program of the aircraft. Much of the treatment is necessarily brief due to space limitations. This document and the British Ministry/Industry Drag Analysis Panel (MIDAP) Guide, which SAE Committee E-33 used as a starting point, can be used to understand the processes and limitations involved in the determination of in-flight thrust. (1.1)* Application to a specific in-flight thrust determination program will require the use of many important assumptions not fully developed herein, and these assumptions must be evaluated during the conduct of the program.【英文标准名称】:Alloy-SteelTurbine-TypeBoltingMaterialSpeciallyHeatTreatedforHigh-TemperatureService
【原文标准名称】:高温用经特殊处理的涡轮型合金钢螺栓材料
【标准号】:ASTMA437/A437M-1994
【标准状态】:作废
【国别】:美国
【发布日期】:1994
【实施或试行日期】:
【发布单位】:美国材料与试验协会(ASTM)
【起草单位】:ASTM
【标准类型】:()
【标准水平】:()
【中文主题词】:温度;钢;螺栓;紧固件;涡轮机;合金钢
【英文主题词】:bolts;fasteners;temperature;steels;turbines;alloysteels
【摘要】:
【中国标准分类号】:J13
【国际标准分类号】:21_060_00;77_080_20
【页数】:
【正文语种】:英语