首页 | 本学科首页   官方微博 | 高级检索  
     检索      

钛合金耳片快速设计方法初探
引用本文:何,翔.钛合金耳片快速设计方法初探[J].民用飞机设计与研究,2013(3):49-52.
作者姓名:  
作者单位:上海飞机设计研究院,上海,201210
摘    要:为较快捷地得到以钛合金Ti-6Al-4V锻件为材料的耳片尺寸参数,同时获得合适的承载效率系数,依据相关文献中关于耳片的3种承载效率系数,并结合常规校核公式,将与耳片尺寸参数相关的关联参数由3种统一为1种、即统一为耳片最小径向截面宽度b与耳片内径D的比值,并拟合了对应的承载效率系数曲线。使用本文的3种拟合曲线,可快速、有效地得到耳片参数b/D与承载效率系数的对应关系,达到快速设计接头耳片的目的。

关 键 词:耳片  最小径向截面宽度  载荷效率系数  钛合金  快速设计

A Simple Approach for Fast Designing the Titanium Alloy Lug
He Xiang.A Simple Approach for Fast Designing the Titanium Alloy Lug[J].Civil Aircraft Design and Research,2013(3):49-52.
Authors:He Xiang
Institution:Shanghai Aircraft Design and Research Institute,Shanghai 201210,China
Abstract:For obtaining size parameter of Ti-6Al-4V forging lug quickly and obtaining suitable load efficiency factor, based on 3 load efficiency factors about the lug with related literature and general calculated formula ,3 associated parameters are united into 1 associated parameter ,that is a ratio of b (the minimum radial section width of lug)to D( the lug inner diameter). And 3 new curves are drew up. By using 3 curves of this paper ,The relationship between the size parameter of b/ D of lug and load efficiency factor can be obtained quickly and effectively. So we can achieve our purpose of fast designing a fitting lug.
Keywords:Lug  Minimum Radial Section Width  Load Efficiency Factor  Titanium Alloy  Fast Design
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《民用飞机设计与研究》浏览原始摘要信息
点击此处可从《民用飞机设计与研究》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号