GB/T 5316-1985 Ni-Cr-B-Si系自熔合金粉
作者:标准资料网 时间:2024-05-13 09:42:36 浏览:9445
来源:标准资料网
基本信息
| 标准名称： | Ni-Cr-B-Si系自熔合金粉 |
| 英文名称： | Metallic powder material; Self-fluxing Ni-Cr-B-Si alloy powder |
| 中标分类： |
冶金 >>
粉末冶金 >>
金属与合金粉末 |
| ICS分类： |
机械制造 >>
焊接、钎焊和低温焊 >>
焊接消耗品
|
| 替代情况： | 调整为YS/T 527-2006 |
| 发布部门： | 中国有色金属工业协会 |
| 发布日期： | 1985-08-24 |
| 实施日期： | 1986-07-01 |
| 首发日期： | 1985-08-24 |
| 作废日期： | 2007-09-29 |
| 主管部门： | 中国有色金属工业协会 |
| 归口单位： | 全国有色金属标准化技术委员会 |
| 起草单位： | 钢铁研究总院 |
| 出版日期： | 1900-01-01 |
| 页数： | 4页 |
适用范围
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前言
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目录
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引用标准
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所属分类： 冶金 粉末冶金 金属与合金粉末 机械制造 焊接 钎焊和低温焊 焊接消耗品
【英文标准名称】:Ergonomicsofthethermalenvironment-Evaluationofthermalenvironmentsinvehicles-Part1:Principlesandmethodsforassessmentofthermalstress(ISO/TS14505-1:2007)
【原文标准名称】:热环境的人类工效学.车内热环境的评定.第1部分:评估热应力的原理和方法
【标准号】:DINISO/TS14505-1-2007
【标准状态】:现行
【国别】:德国
【发布日期】:2007-12
【实施或试行日期】:
【发布单位】:德国标准化学会(DIN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:基础;气候;气候条件;气候荷载;座舱;舒适;起重机;定义;虚线;人类工效学;评定;热负载;人体;车内;判断尺度;负载限度;载荷试验;汽车;理解;专用的;应力;温度;热环境;热应力;牵引车;运载工具
【英文主题词】:
【摘要】:
【中国标准分类号】:A25
【国际标准分类号】:13_180
【页数】:15P;A4
【正文语种】:德语
Product Code:SAE AIR1494
Title:Verification of Landing Gear Design Strength (Cancelled Apr 2010)
Issuing Committee:A-5b Gears, Struts And Couplings Committee
Scope: Verification of landing gear design strength is accomplished by dynamic and static test programs. This is essentially a verification of the analytical procedures used to design the gear. An industry survey was recently conducted to determine just what analysis and testing are currently being applied to landing gear. Timing in relation to first flight of new aircraft was also questioned. Opinions were solicited from designers of the following categories and/or types of aircraft: a. military - large land based (bomber);b. mililtary - small land based (fighter);c. military - carrier based (Navy); d. military - helicopter (large);e. military - helicopter (small-attack); f. commercial - large (airliner); g. commercial - small (business); and h. USAF (WPAFB) - recommendations. It is the objective of this AIR to present a summary of these responses. It is hoped that this summary will be useful to designers as a guide and/or check list in establishing criteria for landing gear analysis and test.
