几何尺寸与公差论坛------致力于产品几何量公差标准GD&T (GDT:ASME)|New GPS(ISO)研究/CAD设计/CAM加工/CMM测量  


返回   几何尺寸与公差论坛------致力于产品几何量公差标准GD&T (GDT:ASME)|New GPS(ISO)研究/CAD设计/CAM加工/CMM测量 » 三维空间:产品设计或CAX软件使用 » CAD设计 » 产品功能分析
用户名
密码
注册 帮助 会员 日历 银行 搜索 今日新帖 标记论坛为已读


 
 
主题工具 搜索本主题 显示模式
旧 2009-09-08, 04:56 PM   #1
huangyhg
超级版主
 
huangyhg的头像
 
注册日期: 04-03
帖子: 18592
精华: 36
现金: 249466 标准币
资产: 1080358888 标准币
huangyhg 向着好的方向发展
默认 deflection of beam in x and y

deflection of beam in "x" and "y"
i am trying to figure out how much the end of a cantilevered beam will displace if loaded at the end. i know the equation that will give me the displacement in the "y" direction, but how do i figure the displacement in the "x" direction?

you can compute it in same manner as for the y-direction. however, use the proper moment in inertia (i). to get a final resultant displacement:
r = ((dx)^2+(dy)^2)^0.5
in other words, square both deflections, add them and then take the square root.
good luck.
follow up,
i am assuming that you would have a load applied in the other direction. otherwise, your deflection would be zero!
lutfi,
the beam is horizontal and the (point) load is acting vertical. every equation that i have only solves for the deflection in the "y" direction. in reality as the cantilevered beam deflects down, the end of the beam will move toward the wall support.
i am trying to determine how much is moved toward the support.
thanks
i think in general beam theory is based upon small deflections so the deflection into the support is negigible. the forumla for deflection is y = (f * x^2)/(6 * e * i) * (x - 3 * l) which gives the maximum at x=l and not at a point x<l. you'd have to look at large deformation theory to get the correct answer.
alternatively you could integrate along the length of the curve to equate the original length of the beam to the curve length to evaluate x, ie. integrate from 0 to x the curve length [root(1 + f'(x)^2)]=l to find x.
the deflection equations noted above are based on a "model" of the beam. the model has the load applied perfectly concentric with the cg of the beam, the beam is perfectly prismatic, the compression flange is braced against rotation, etc. thus there is no lateral displacement or rotation.
in reality, of course, the conditions are not perfect, and there is a lateral displacement and/or rotation.
depending on why you need to know there are a couple of different approaches. if it's a matter of allowable stress and/or displacement you could assume a horizontal load of say 0.1 of gravity load and/or apply the load eccentric.
if it has to do with needing to know "exactly" what the lateral displacement is you may have a bigger problem on your hands. load testing is a possibility. another choice would be to brace the tip of the cantilever back to the support, thus greatly reducing any lateral motion.
hope this helps.
steve,
"if it has to do with needing to know "exactly" what the lateral displacement is you may have a bigger problem on your hands."
that is exactly what i need.
this is what i am going to have to figure. i am interested in the amount the center of the circle shown here moves.
thanks
karthur,
you had us all confused. we thought you were looking for displacement "into" the page.
your problem is really quite simple.
if you have access to an analysis program, simply model it.
if you're doing hand calcs, and i haven't done a problem like this by hand in a while, you can use the slope deflection equations to solve. unfortunately i'm in transit and my books are in temporary storage or i'd give you a better reference.
you can approximate the displacement by noting that it's due to the rotation at the end of the long cantilever. there are published equations for calculating this. from the end rotation (and dispacement y) you use trig to get the displacement at the point you want.
sorry i don't have the equations you need at hand. i'm sure someone else will provide them.
now we can see your problem in its context, it is apparent that the formula you need is not the one for the x displacement of the cantilever's tip, but the one for its rotation:
fl^2/(2ei)
where l is the length of your horizontal member.
your required x displacement at the top of your vertical member is then the product of this rotation and the length of the vertical
karthur, how did you paste that picture in your post?
karthur
i was confused as well. i think you solve it by simple trig as well, once you determined the vertical deflection. you may have to exaggerate the deflection and by simple triangulations, you should be able to be to compute the "x" movement.
how did you paste the image, i never tried before, but i think this could be helpful for the future posts.
__________________
借用达朗贝尔的名言:前进吧,你会得到信心!
[url="http://www.dimcax.com"]几何尺寸与公差标准[/url]
huangyhg离线中   回复时引用此帖
GDT自动化论坛(仅游客可见)
 


主题工具 搜索本主题
搜索本主题:

高级搜索
显示模式

发帖规则
不可以发表新主题
不可以回复主题
不可以上传附件
不可以编辑您的帖子

vB 代码开启
[IMG]代码开启
HTML代码关闭



所有的时间均为北京时间。 现在的时间是 04:38 AM.


于2004年创办,几何尺寸与公差论坛"致力于产品几何量公差标准GD&T | GPS研究/CAD设计/CAM加工/CMM测量"。免责声明:论坛严禁发布色情反动言论及有关违反国家法律法规内容!情节严重者提供其IP,并配合相关部门进行严厉查处,若內容有涉及侵权,请立即联系我们QQ:44671734。注:此论坛须管理员验证方可发帖。
沪ICP备06057009号-2
更多