SJ/T 9527-1993 微型数字电子计算机质量分等标准
作者:标准资料网 时间:2024-05-15 18:14:16 浏览:9169
来源:标准资料网
基本信息
| 标准名称： | 微型数字电子计算机质量分等标准 |
| 英文名称： | Digital micro-computer-Quality grading standard |
| 中标分类： |
矿业 >>
矿业综合 >>
技术管理 |
| 发布部门： | 中华人民共和国电子工业部 |
| 发布日期： | 1993-07-13 |
| 实施日期： | 1993-11-01 |
| 首发日期： | 1900-01-01 |
| 作废日期： | 2010-01-20 |
| 提出单位： | 中华人民共和国电子工业部科技与质量监督司 |
| 归口单位： | 电子工业部标准化研究所 |
| 起草单位： | 电子工业部华北计算技术研究所 |
| 起草人： | 丁成鹏 |
| 出版日期： | 1993-11-01 |
| 页数： | 3页 |
适用范围
本标准规定了微型数字电子计算机（以下简称微型机）、学习机及微型机极级产品（以下简称板级产品）质量分等和质量分等的技术要求。本标准适用于微型机、学习机及板级产品，是考核微型机、学习机及板级产品质量等级的依据。本标准必须与GB 9813或企业标准一起使用。
前言
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目录
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引用标准
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所属分类： 矿业 矿业综合 技术管理
Product Code:SAE AIR5766
Title:Using Aircraft Position Data to Estimate Aircraft Thrust
Issuing Committee:A-21 Aircraft Noise Measure Noise Aviation Emission Modeling
Scope: This SAE Aerospace Information Report (AIR) provides information and methods for using aircraft position data to estimate aircraft thrust. The thrust estimated using this AIR is intended to be used to estimate aircraft noise level and aircraft air pollution and greenhouse gas emissions. The method of estimating aircraft noise level using aircraft thrust is provided in AIR 1845. Aircraft noise and emissions are generally estimated using models that are based on standard sets of aircraft profiles that include aircraft thrust, speed, and altitude along the flight path. Potential uses of this AIR are to provide an experimental method of determining the adequacy of a standard profile or to develop a flight specific profile. Flight specific profiles may be used to develop or revise standard profiles or to model noise or emissions on a flight-by-flight basis. Potential users include: airport noise modelers, airport emission modelers, developers of airport noise and emission models, federal, state and local government agencies, equipment vendors and other public bodies and officials.The information included here is intended to apply to turbine powered aircraft operating at air carrier and general-aviation airports. The information and methods presented here do not apply rotorcraft or propeller driven aircraft.The primary topics addressed in this AIR include identifying sources of aircraft position data, processing aircraft position data into flight segments including data smoothing and dealing with incomplete or erroneous data, identifying flight segments of constant thrust, acquiring winds aloft data for use in computing aircraft airspeed, estimating aircraft bank angle, estimating aircraft weight when not available, and finally, using these data to estimate the aircraft thrust for each segment of constant thrust flight.
Rationale: This SAE Aerospace Information Report (AIR) provides information and methods for using aircraft position data to estimate aircraft thrust. The thrust estimated using this AIR is intended to be used to estimate aircraft noise level and aircraft air pollution and greenhouse gas emissions. The method of estimating aircraft noise level using aircraft thrust is provided in AIR 1845. Aircraft noise and emissions are generally estimated using models that are based on standard sets of aircraft profiles that include aircraft thrust, speed, and altitude along the flight path. Potential uses of this AIR are to provide an experimental method of determining the adequacy of a standard profile or to develop a flight specific profile. Flight specific profiles may be used to develop or revise standard profiles or to model noise or emissions on a flight-by-flight basis. Potential users include: airport noise modelers, airport emission modelers, developers of airport noise and emission models, federal, state and local government agencies, equipment vendors and other public bodies and officials.The information included here is intended to apply to turbine powered aircraft operating at air carrier and general-aviation airports. The information and methods presented here do not apply rotorcraft or propeller driven aircraft.The primary topics addressed in this AIR include identifying sources of aircraft position data, processing aircraft position data into flight segments including data smoothing and dealing with incomplete or erroneous data, identifying flight segments of constant thrust, acquiring winds aloft data for use in computing aircraft airspeed, estimating aircraft bank angle, estimating aircraft weight when not available, and finally, using these data to estimate the aircraft thrust for each segment of constant thrust flight.【英文标准名称】:Edisonscrewlampholders.
【原文标准名称】:爱迪生螺口灯座
【标准号】:NFC61-550-1999
【标准状态】:作废
【国别】:法国
【发布日期】:1999-08-01
【实施或试行日期】:1999-08-05
【发布单位】:法国标准化协会(AFNOR)
【起草单位】:
【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】:K74
【国际标准分类号】:29_140_10
【页数】:63P;A4
【正文语种】:其他
