SAE AS85049/94 Connector Accessories, Electrical, Mounting Device Flange Type, Full Mounting Perimeter Device, Type I (
作者:标准资料网 时间:2024-05-15 14:22:22 浏览:9464
来源:标准资料网
Product Code:SAE AS85049/94
Title:Connector Accessories, Electrical, Mounting Device Flange Type, Full Mounting Perimeter Device, Type I (Heavy Duty)
Issuing Committee:Ae-8c1 Connectors Committee
Scope:No scope available.
上一篇:
SAE AS85049/9 Connector Accessories, Electrical, Backshell, Environmental, Cable Sealing, 90Md, Category 1a (For Mil-C-下一篇:
SAE AS85049/96 Connector Accessories, Electrical, Mounting Device Flange Type, 1/4 Mounting Perimeter Device, Type Iii 【英文标准名称】:StandardSpecificationforGeneralRequirementsforRolledStructuralSteelBars,Plates,Shapes,andSheetPiling
【原文标准名称】:轧制结构钢棒材、板材、型材和打板桩一般要求的标准规范
【标准号】:ASTMA6/A6Mb-2002
【标准状态】:作废
【国别】:美国
【发布日期】:2002
【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】:钢;结构钢
【英文主题词】:steels;structuralsteels
【摘要】:
【中国标准分类号】:H44
【国际标准分类号】:77_140_60
【页数】:64P;A4
【正文语种】:英语
Product Code:SAE AIR4003
Title:Report on Aircraft Engine Containment
Issuing Committee:Engine Containment Ad Hoc Committee
Scope:To gather and analyze service data on aircraft propulsion turbine engine rotating part non-containment failures on record, assess the resulting aircraft damage, and determine the rate of past occurrences based on these data. In addition, to classify incidents by cause and consequence, to identify areas of greatest concern, and to recommend areas for greatest potential improvement. While the previous SAE Committee report, AIR 1537, focused solely on fixed wing commercial engine experience, the current Committee decided that the scope should be expanded to collect the data relating to helicopter and general aviation operations. The inclusion of helicopter experience was prompted by the FAA request to anticipate the projected substantial increase in commercial use of helicopters within the next decade. For completeness, general aviation experience, including commuter airlines, was considered significant enough to include in the current committee's activities. At the direction of the Aerospace Council, all three classes of engines have been treated in a single report. It is expected that the data, conclusions and recommendations of this report will be accepted as a standard reference by anyone dealing with turbine engine rotor non-containment
