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ISO 3541-1975 土方机械.燃料加注口尺寸

作者:标准资料网 时间:2024-05-07 09:37:58  浏览:9806   来源:标准资料网
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【英文标准名称】:Earth-movingmachinery;Dimensionsoffuelfilleropening
【原文标准名称】:土方机械.燃料加注口尺寸
【标准号】:ISO3541-1975
【标准状态】:作废
【国别】:
【发布日期】:
【实施或试行日期】:
【发布单位】:国际标准化组织(IX-ISO)
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【标准类型】:()
【标准水平】:()
【中文主题词】:
【英文主题词】:
【摘要】:
【中国标准分类号】:
【国际标准分类号】:
【页数】:
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Product Code:SAE AS5900
Title:Standard Test Method for Aerodynamic Acceptance of SAE AMS 1424 and SAE AMS 1428 Aircraft Deicing/Anti-icing Fluids
Issuing Committee:G-12adf Aircraft Deicing Fluids
Scope: This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements for SAE AMS 1424 Type I and SAE AMS 1428 Type II, III and IV fluids used to deice and/or anti-ice aircraft:a. with takeoff rotation speeds exceeding approximately 100 knots, with time from brake release to rotation speed greater than 20 s, typical for large transport type jet aircraft. This procedure is referred to as the High Speed Ramp Test.and/orb. with takeoff rotation speeds exceeding approximately 60 knots, with time from brake release to rotation speed greater than 15 s typical for commuter type aircraft. This procedure is referred to as the Low Speed Ramp Test.NOTE: When compensating measures, such as increase in rotation speed, are used in the aircraft takeoff procedure, the High Speed Ramp can apply. The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/anti-icing fluids as they flow off aircraft lifting and control surfaces during the takeoff ground acceleration and climb.NOTE: These test methods are based on glycol-based fluids, additional testing may be required for non-glycol-based fluids.
Rationale: This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements for SAE AMS 1424 Type I and SAE AMS 1428 Type II, III and IV fluids used to deice and/or anti-ice aircraft:a. with takeoff rotation speeds exceeding approximately 100 knots, with time from brake release to rotation speed greater than 20 s, typical for large transport type jet aircraft. This procedure is referred to as the High Speed Ramp Test.and/orb. with takeoff rotation speeds exceeding approximately 60 knots, with time from brake release to rotation speed greater than 15 s typical for commuter type aircraft. This procedure is referred to as the Low Speed Ramp Test.NOTE: When compensating measures, such as increase in rotation speed, are used in the aircraft takeoff procedure, the High Speed Ramp can apply. The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/anti-icing fluids as they flow off aircraft lifting and control surfaces during the takeoff ground acceleration and climb.NOTE: These test methods are based on glycol-based fluids, additional testing may be required for non-glycol-based fluids.
基本信息
标准名称:电测量变送器检定规程
英文名称:Verification Regulation of Density Meters of Drilling Fluids
替代情况:JJG(石油)26-92
发布日期:1994-04-06
实施日期:1994-10-01
首发日期:1900-01-01
作废日期:1900-01-01
出版社:人民邮电出版社
出版日期:2006-02-13
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所属分类: 工程建设 电力 核工业工程 发电站工程 能源和热传导工程 电站综合

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