Increasing Cantilever Beam Stiffness

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SUMMARY

This discussion focuses on optimizing the stiffness of cantilever beams for prosthetic applications, specifically using a carbon fiber material with a Young's modulus of 3.8E10 Pa. The user is experimenting with various shapes and profiles, aiming to achieve maximum stiffness while adhering to specific constraints such as a cross-section of 6 x 25 mm and a length of 100 mm under a maximum load of 1200 N. Key equations for angular deflection and vertical displacement are employed to analyze the stiffness, with a particular interest in finding the optimal shape that maximizes stiffness without exceeding material limits.

PREREQUISITES
  • Understanding of cantilever beam mechanics
  • Familiarity with material properties, specifically carbon fiber
  • Knowledge of structural analysis equations, including angular deflection and vertical displacement
  • Experience with optimization techniques in engineering design
NEXT STEPS
  • Research the principles of cantilever beam optimization
  • Explore advanced composite material properties and their applications
  • Study the effects of varying cross-sectional shapes on beam stiffness
  • Investigate software tools for structural analysis and optimization, such as ANSYS or SolidWorks
USEFUL FOR

Engineers and designers in the prosthetics field, structural analysts, and anyone involved in optimizing cantilever beam designs for enhanced performance and stiffness.

Jeffrey Lee
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Is it possible to create a cantilever beam with constant or increasing stiffness. I've been experimenting with several different shapes and profiles, and have not had any luck.

I know that there are shapes with constant stress throughout, but I'm hoping to find a shape with constant or increasing stiffness, or the shape of a cantilever beam that has maximum stiffness throughout.
 
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There are many ways of making cantilever beams stiffer but any practical solution depends very much on what you are actually trying to do .

What is basic requirement ?

Leading dimensions and applied loads ?

Class of job - basic plate and girder type construction or something more sophisticated ?

Deflection limits ?

Clear diagram would very useful .
 
Hi, thanks for you reply. This is for applications in the prosthetics field, so geometry and construction is dependent upon what can be contained within a biological form factor.

Basic dimensions:
Cross Section: 6 x 25 mm
Length: 100 mm

Material:
Carbon Fiber with E = 3.8E10 Pa

Maximum applied load is around 1200 N

Attached is a picture of the general setup, please let me know if you have any other questions.

Thanks!
 

Attachments

We can work out what you want from first principles if needs be but in general terms is this the sort of thing you have in mind ? :

http://waset.org/publications/10000410/design-and-development-of-constant-stress-composite-cantilever-beam
 
Somewhat, but that is designing for constant stress. I am hoping to find the optimum shape for stiffness. What I have been trying to do is using the equations for angular deflection, vertical displacement in order to find a shape that maximizes stiffness (F/displacement). These are the equations I have been using.

$$\theta (x) = \frac{1}{E} \int \frac{M(x)}{I(x)} dx$$
$$\delta (x) = \int \theta(x) dx$$

I have varied the equation for I(x) based on different profiles, but am wondering what the optimal shape for k(x) would be.
 
Maximum stiffness as such is open ended - for a simple parallel or tapering down cantilever beam the deeper the sections used the stiffer it gets .

Need some constraints for a meaningful analysis .

Would it be useful for your purpose if we try to find shape of a cantilever beam with best stiffness compared to stiffness of your existing parallel one and using same amount of material ?
 
Last edited:
Yes, that would be helpful. Finding the max stiffness of a cantilever beam at its tip with the same amount of material, and both being the same length would be of use to me.

Thank you
 
Jeffrey Lee - please contact me .
 

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