ANSI/EIA 376-1970 直流用有金属及非金属外壳的固定薄膜介质电容器
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【英文标准名称】:FixedFilmDielectricCapacitorsinMetallicandNon-MetallicCasesforDCApplication
【原文标准名称】:直流用有金属及非金属外壳的固定薄膜介质电容器
【标准号】:ANSI/EIA376-1970
【标准状态】:现行
【国别】:美国
【发布日期】:1970
【实施或试行日期】:
【发布单位】:美国国家标准学会(US-ANSI)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:
【英文主题词】:dielectric;electronicequipmentandcomponents;capacitors;electronicengineering
【摘要】:
【中国标准分类号】:L11
【国际标准分类号】:31_060_10
【页数】:
【正文语种】:英语
【原文标准名称】:直流用有金属及非金属外壳的固定薄膜介质电容器
【标准号】:ANSI/EIA376-1970
【标准状态】:现行
【国别】:美国
【发布日期】:1970
【实施或试行日期】:
【发布单位】:美国国家标准学会(US-ANSI)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:
【英文主题词】:dielectric;electronicequipmentandcomponents;capacitors;electronicengineering
【摘要】:
【中国标准分类号】:L11
【国际标准分类号】:31_060_10
【页数】:
【正文语种】:英语
下载地址: 点击此处下载
Product Code:SAE AS8054
Title:Airborne Engine Vibration Monitoring (Evm) System, Guidelines for Performance Standard For
Issuing Committee:E-32 Aerospace Propulsion Systems Health Management
Scope: This SAE Aerospace Standard (AS) provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which is intended for use as a turbojet engine rotor unbalance indicating system, per FAR 25.1305 (D)(3) on transport category airplanes. For the purpose of this document, this means a system which can provide real-time flight deck displays of engine vibration caused by rotor unbalance, throughout the flight envelope, which are suitable for: a. relating to engine vibration limits (where such limits are specified), b. use in ice shedding procedures, and c. helping the flight crew to determine which engine has the higher level of vibration, following an engine damage event. As a minimum, the functional capability for such a system shall include the ability to compute and display vibration levels specifically related to the rotational speed(s) of the engine rotor(s). Systems which can produce only broadband vibration outputs have been used in the past but they are not considered suitable for the above purposes. Some EVM systems may also generate other outputs, suitable for such functions as engine vibration trend monitoring or trim balance calculation, but these are considered to be outside the scope of the requirements for a minimum system. This document also defines some recommended, optional, functions and features which, while they are outside the scope of minimum requirements, are nevertheless considered to be highly desirable for a practical system. It should be noted that systems incorporating capabilities such as described above are also sometimes referred to by the abbreviation AVM. However, there are, or can be, airborne measurements taken of vibrations from sources other than the engines. For the purpose of this document the more descriptive term, engine vibration monitor (EVM), will be used. The purpose of this document is to provide guidance on the requirements for airborne EVM systems for turbojet engines on transport category airplanes.
Rationale: This SAE Aerospace Standard (AS) provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which is intended for use as a turbojet engine rotor unbalance indicating system, per FAR 25.1305 (D)(3) on transport category airplanes. For the purpose of this document, this means a system which can provide real-time flight deck displays of engine vibration caused by rotor unbalance, throughout the flight envelope, which are suitable for: a. relating to engine vibration limits (where such limits are specified), b. use in ice shedding procedures, and c. helping the flight crew to determine which engine has the higher level of vibration, following an engine damage event. As a minimum, the functional capability for such a system shall include the ability to compute and display vibration levels specifically related to the rotational speed(s) of the engine rotor(s). Systems which can produce only broadband vibration outputs have been used in the past but they are not considered suitable for the above purposes. Some EVM systems may also generate other outputs, suitable for such functions as engine vibration trend monitoring or trim balance calculation, but these are considered to be outside the scope of the requirements for a minimum system. This document also defines some recommended, optional, functions and features which, while they are outside the scope of minimum requirements, are nevertheless considered to be highly desirable for a practical system. It should be noted that systems incorporating capabilities such as described above are also sometimes referred to by the abbreviation AVM. However, there are, or can be, airborne measurements taken of vibrations from sources other than the engines. For the purpose of this document the more descriptive term, engine vibration monitor (EVM), will be used. The purpose of this document is to provide guidance on the requirements for airborne EVM systems for turbojet engines on transport category airplanes.【英文标准名称】:SpecificationforHelmetsUsedinShortTrackSpeedIceSkating(NottoIncludeHockey)
【原文标准名称】:短道速滑(不包括冰球)头盔规范
【标准号】:ANSI/ASTMF1849-2007
【标准状态】:现行
【国别】:美国
【发布日期】:2007-05-22
【实施或试行日期】:
【发布单位】:美国国家标准学会(US-ANSI)
【起草单位】:ASTM
【标准类型】:()
【标准水平】:()
【中文主题词】:保健;头盔;冰;体育与娱乐设备;防护服装;头皮防护器;规范(验收)
【英文主题词】:Healthprotection;Helmets;Ice;Leisureequipment;Protectiveclothing;Scalpprotectors;Specification(approval)
【摘要】:Thisspecificationcoversperformancerequirementsforhelmetsusedbyshorttrackspeediceskaters(excludinghockey).Thisspecificationrecognizesthedesirabilityoflightweightconstructionandventilation;however,itisaperformancestandardandisnotintendedtorestrictdesign.AlltestingandrequirementsofthisspecificationshallbeinaccordancewithTestMethodsF1446,exceptwherenotedherein.Partialutilizationofthisspecificationisprohibited.Anystatementofcompliancewiththisspecificationmustbeacertificationthattheheadgearmeetsalloftherequirementsofthespecificationintheirentirety.Aheadgearthatfailstomeetanyoneoftherequirementsofthisspecificationisconsideredtohavefailedthespecification,andshallnotbesoldwithanyindicationthatitmeetspartsofthespecification.1.4ThevaluesstatedinSIunitsaretoberegardedasstandard.Nootherunitsofmeasurementareincludedinthisstandard.Thisstandarddoesnotpurporttoaddressallofthesafetyconcerns,ifany,associatedwithitsuse.Itistheresponsibilityoftheuserofthisstandardtoestablishappropriatesafetyandhealthpracticesanddeterminetheapplicabilityofregulatorylimitationspriortouse.
【中国标准分类号】:Y56
【国际标准分类号】:13_340_20
【页数】:
【正文语种】:英语
Title:Airborne Engine Vibration Monitoring (Evm) System, Guidelines for Performance Standard For
Issuing Committee:E-32 Aerospace Propulsion Systems Health Management
Scope: This SAE Aerospace Standard (AS) provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which is intended for use as a turbojet engine rotor unbalance indicating system, per FAR 25.1305 (D)(3) on transport category airplanes. For the purpose of this document, this means a system which can provide real-time flight deck displays of engine vibration caused by rotor unbalance, throughout the flight envelope, which are suitable for: a. relating to engine vibration limits (where such limits are specified), b. use in ice shedding procedures, and c. helping the flight crew to determine which engine has the higher level of vibration, following an engine damage event. As a minimum, the functional capability for such a system shall include the ability to compute and display vibration levels specifically related to the rotational speed(s) of the engine rotor(s). Systems which can produce only broadband vibration outputs have been used in the past but they are not considered suitable for the above purposes. Some EVM systems may also generate other outputs, suitable for such functions as engine vibration trend monitoring or trim balance calculation, but these are considered to be outside the scope of the requirements for a minimum system. This document also defines some recommended, optional, functions and features which, while they are outside the scope of minimum requirements, are nevertheless considered to be highly desirable for a practical system. It should be noted that systems incorporating capabilities such as described above are also sometimes referred to by the abbreviation AVM. However, there are, or can be, airborne measurements taken of vibrations from sources other than the engines. For the purpose of this document the more descriptive term, engine vibration monitor (EVM), will be used. The purpose of this document is to provide guidance on the requirements for airborne EVM systems for turbojet engines on transport category airplanes.
Rationale: This SAE Aerospace Standard (AS) provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which is intended for use as a turbojet engine rotor unbalance indicating system, per FAR 25.1305 (D)(3) on transport category airplanes. For the purpose of this document, this means a system which can provide real-time flight deck displays of engine vibration caused by rotor unbalance, throughout the flight envelope, which are suitable for: a. relating to engine vibration limits (where such limits are specified), b. use in ice shedding procedures, and c. helping the flight crew to determine which engine has the higher level of vibration, following an engine damage event. As a minimum, the functional capability for such a system shall include the ability to compute and display vibration levels specifically related to the rotational speed(s) of the engine rotor(s). Systems which can produce only broadband vibration outputs have been used in the past but they are not considered suitable for the above purposes. Some EVM systems may also generate other outputs, suitable for such functions as engine vibration trend monitoring or trim balance calculation, but these are considered to be outside the scope of the requirements for a minimum system. This document also defines some recommended, optional, functions and features which, while they are outside the scope of minimum requirements, are nevertheless considered to be highly desirable for a practical system. It should be noted that systems incorporating capabilities such as described above are also sometimes referred to by the abbreviation AVM. However, there are, or can be, airborne measurements taken of vibrations from sources other than the engines. For the purpose of this document the more descriptive term, engine vibration monitor (EVM), will be used. The purpose of this document is to provide guidance on the requirements for airborne EVM systems for turbojet engines on transport category airplanes.【英文标准名称】:SpecificationforHelmetsUsedinShortTrackSpeedIceSkating(NottoIncludeHockey)
【原文标准名称】:短道速滑(不包括冰球)头盔规范
【标准号】:ANSI/ASTMF1849-2007
【标准状态】:现行
【国别】:美国
【发布日期】:2007-05-22
【实施或试行日期】:
【发布单位】:美国国家标准学会(US-ANSI)
【起草单位】:ASTM
【标准类型】:()
【标准水平】:()
【中文主题词】:保健;头盔;冰;体育与娱乐设备;防护服装;头皮防护器;规范(验收)
【英文主题词】:Healthprotection;Helmets;Ice;Leisureequipment;Protectiveclothing;Scalpprotectors;Specification(approval)
【摘要】:Thisspecificationcoversperformancerequirementsforhelmetsusedbyshorttrackspeediceskaters(excludinghockey).Thisspecificationrecognizesthedesirabilityoflightweightconstructionandventilation;however,itisaperformancestandardandisnotintendedtorestrictdesign.AlltestingandrequirementsofthisspecificationshallbeinaccordancewithTestMethodsF1446,exceptwherenotedherein.Partialutilizationofthisspecificationisprohibited.Anystatementofcompliancewiththisspecificationmustbeacertificationthattheheadgearmeetsalloftherequirementsofthespecificationintheirentirety.Aheadgearthatfailstomeetanyoneoftherequirementsofthisspecificationisconsideredtohavefailedthespecification,andshallnotbesoldwithanyindicationthatitmeetspartsofthespecification.1.4ThevaluesstatedinSIunitsaretoberegardedasstandard.Nootherunitsofmeasurementareincludedinthisstandard.Thisstandarddoesnotpurporttoaddressallofthesafetyconcerns,ifany,associatedwithitsuse.Itistheresponsibilityoftheuserofthisstandardtoestablishappropriatesafetyandhealthpracticesanddeterminetheapplicabilityofregulatorylimitationspriortouse.
【中国标准分类号】:Y56
【国际标准分类号】:13_340_20
【页数】:
【正文语种】:英语