Pin in Double Shear (Mechanics of Materials)

In summary: The left hand side is the mass (10,000 lbs) divided by the width of the lug (0.250"). In summary, the homework statement is trying to determine the loads P1 and P2 in the lugs on the opposite side of the pin. However, they need another equation to generate another variable in terms of P1 or P2. No material is given (all must be same), nor width, nor diameter of pin. Only thicknesses are given. Hint says use stiffness information.
  • #1
michael page
11
0

Homework Statement


Knowing the left lug is carrying 10,000 lbs, determine the loads P1 and P2 in the lugs on the opposite side of the pin.

Homework Equations


Force Balance (ΣF=0)
Another equation needed

The Attempt at a Solution


10000 = P1 + P2
This is where I need another equation to generate another variable in terms of P1 or P2. No material is given (all must be same), nor width, nor diameter of pin. Only thicknesses are given. Hint says use stiffness information. I tried to put everything in terms of distributed load w but still got stuck.
 

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  • #2
michael page said:
Hint says use stiffness information.
I don't see how to use stiffness since we know nothing about the pin. Try torque.
 
  • #3
You are correct, another equation is needed. The diagram does not give the information necessary to find another equation. If we assume that the elongation of the two links loaded by P1 and P2 have identical strain and that the 0.250" lug is perfectly rigid, then it is possible to get the second equation.

Since your background is aerospace engineering, you should be able to appreciate that no good engineer would want to design a lug with an unbalanced load.
 
  • #4
jrmichler said:
The diagram does not give the information necessary to find another equation.
Yes it does. See post #2.
 
  • #5
OOPS, yes now I see it (where's that thumps head with palm emoji when I need it?). Forces do not prevent rotation, so getting the second equation is a sum of moments problem.
 
  • #6
Ok the hint says "Stiffness governs distribution of load".
I put everything in terms of distributed loads, w.

Based on area of rectangles I tried to say:
since t2 = 1.24*t1
w2 = 1.24*w1

But then when I solve for w1 and w2 from this method they don't add up to 10,000 (upon converting back to force).

Still trying things.
 
  • #7
jrmichler said:
OOPS, yes now I see it (where's that thumps head with palm emoji when I need it?). Forces do not prevent rotation, so getting the second equation is a sum of moments problem.

It's not a beam there are no fixed ends.
 
  • #8
michael page said:
Ok the hint says "Stiffness governs distribution of load".
I put everything in terms of distributed loads, w.

Based on area of rectangles I tried to say:
since t2 = 1.24*t1
w2 = 1.24*w1

But then when I solve for w1 and w2 from this method they don't add up to 10,000 (upon converting back to force).

Still trying things.
As I posted, I don't think you can use stiffness, despite the hint.

The diagram shows P1 and P2 as being central in their respective lugs. If that is correct you can use torque.

If that is not to be trusted then P1 and P2 could be equal. Nothing in the real world is perfectly stiff or fits perfectly snugly, so suppose e.g. that the pin flexes but fits relatively loosely within the lug holes. In this case, the principal contact between pin and lugs is at the face adjacent to the left-hand lug. Correspondingly, P1 and P2 would be adjacent to that face and equal. The thicknesses of the two right hand lugs becomes irrelevant.

We could make all sorts of alternative assumptions about stiffness and fit, consistent with the diagram, to arrive at different conclusions.
 
  • #9
haruspex said:
As I posted, I don't think you can use stiffness, despite the hint.

The diagram shows P1 and P2 as being central in their respective lugs. If that is correct you can use torque.

If that is not to be trusted then P1 and P2 could be equal. Nothing in the real world is perfectly stiff or fits perfectly snugly, so suppose e.g. that the pin flexes but fits relatively loosely within the lug holes. In this case, the principal contact between pin and lugs is at the face adjacent to the left-hand lug. Correspondingly, P1 and P2 would be adjacent to that face and equal. The thicknesses of the two right hand lugs becomes irrelevant.

We could make all sorts of alternative assumptions about stiffness and fit, consistent with the diagram, to arrive at different conclusions.

What if I just said the deflection of the right is the opposite of the deflection of the left would that get me anywhere?
 
  • #10
michael page said:
What if I just said the deflection of the right is the opposite of the deflection of the left would that get me anywhere?
What deflections, exactly?
 
  • #11
michael page said:
It's not a beam there are no fixed ends.
So?
 
  • #12
haruspex said:
So?
They all have the same width. It's not shown as a variable though.
If kL = AL * EL / LL for the single element on the left what's the right hand side of this equation?
Like how do you superimpose the two stiffnesses in parallel like that again, for the right two bars?
 
  • #13
michael page said:
They all have the same width. It's not shown as a variable though.
If kL = AL * EL / LL for the single element on the left what's the right hand side of this equation?
Like how do you superimpose the two stiffnesses in parallel like that again, for the right two bars?
You seem to be thinking of stiffness purely in regard to elongation of the three lugs. Assuming the right hand two are independently secured at the far end, this cannot be relevant. The only way stiffness could come into it is in terms of flexing of the pin and/or lugs.
 
  • #14
jrmichler said:
You are correct, another equation is needed. The diagram does not give the information necessary to find another equation. If we assume that the elongation of the two links loaded by P1 and P2 have identical strain and that the 0.250" lug is perfectly rigid, then it is possible to get the second equation.

Since your background is aerospace engineering, you should be able to appreciate that no good engineer would want to design a lug with an unbalanced load.

I guess this will have to work. I did what you said. w and E cancelled, you generate the second equation, has to be it am I right??!
Thank you,
Michael
 
  • #15
michael page said:
I guess this will have to work. I did what you said. w and E cancelled, you generate the second equation, has to be it am I right??!
Thank you,
Michael
As I posted, there is no indication that the two right hand lugs are anchored to the same (rigid) support at the far end. Without that, there is no basis for saying they have the same strain.
Why will you not consider torque?
 
  • #16
haruspex said:
As I posted, there is no indication that the two right hand lugs are anchored to the same (rigid) support at the far end. Without that, there is no basis for saying they have the same strain.
Why will you not consider torque?

There's also nothing to say from the diagram that they aren't both fixed to the same thing.
Unless you mean a force-couple, torsion was not covered yet in any section of the book. If you could show me something with a force-couple I'm 100% open to looking into that.
 
  • #17
I could have drawn it better but I sketched it in like 2 mins. The ends of the bar go on indefinitely on my handout, on both sides.
They also show a top view where it can be seen that each lug has same width but it's not given a variable name so it's not something to really consider I don't think.
Michael
 
  • #18
michael page said:
There's also nothing to say from the diagram that they aren't both fixed to the same thing.
If the solution depends on such anchorage then it should surely be shown in the diagram. Also it would depend on that distant anchorage, and the left hand lug, being rigid.
michael page said:
torsion was not covered yet in any section of the book.
It is not a matter of torsion in the sense of strain, simply a static balance. The net torque on the pin must be zero. If you assume P1 and P2 act exactly as show, along the centre lines of the lugs, this gives you the ratio between them.

Now, I am not at all certain that this is the intended solution, especially in view of the hint. But if we take the information as given it is the most reasonable approach I can see. It could be just a poorly posed question.
 
  • #19
There is an old engineering adage that says, "Load follows stiffness." The displacements of the upper and lower members wil be the same by virtue of the pin joint. This means that both see the same strain. The load in each member is proportional to the strain in the member.
 
  • #20
Dr.D said:
There is an old engineering adage that says, "Load follows stiffness." The displacements of the upper and lower members wil be the same by virtue of the pin joint. This means that both see the same strain. The load in each member is proportional to the strain in the member.
You are making the assumption that the far ends of the two right-hand lugs have not undergone any relative displacement in going from a state of no tension to the current state. The only evidence I see for that assumption is the hint. Other than that, the tensions could have been applied by tightening two nuts independently, e.g.
So, yes, this may be how the problem setter expects it to be solved, but if so it is very poorly specified.
 
  • #21
haruspex said:
So, yes, this may be how the problem setter expects it to be solved, but if so it is very poorly specified.

I would not dare to argue with such an august, magisterial personage as haruspex, so there can be no doubt that it is my fault if the problem does not measure up to his grand standards.

This is rather like the difference between second moment of area and area moment of inertia. The statement of this problem, along with the hint, is simply the way that engineers communicate. If you say to a structural engineer, "the problem with your design is an inadequate second moment of area" he is almost certain to look at you like you have grown several extra heads. In that case, there is one term that is correct, and a different term that communicates meaning. Exactly the same thing is happening in this problem, even if it distresses those who demand correct terminology.
 
  • #22
Dr.D said:
distresses those who demand correct terminology.
In this thread it is not a question of terminology but one of problem specification. Were it not for the hint there would be no basis whatsoever for supposing the strain is the same in both lugs.
 
  • #23
haruspex said:
Were it not for the hint there would be no basis whatsoever for supposing the strain is the same in both lugs.

Ah, but the hint was there. That makes all the difference in the world!
 
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  • #24
Dr.D said:
Ah, but the hint was there. That makes all the difference in the world!
The difference it makes is that it allows one to guess what it is the problem setter forgot to specify. It does not make the problem well specified.
"Two spheres roll down an incline. Which reaches the bottom first?
Hint: hollow and solid spheres have different moments of inertia"
 
  • #25
haruspex said:
You are making the assumption that the far ends of the two right-hand lugs have not undergone any relative displacement in going from a state of no tension to the current state. The only evidence I see for that assumption is the hint. Other than that, the tensions could have been applied by tightening two nuts independently, e.g.
So, yes, this may be how the problem setter expects it to be solved, but if so it is very poorly specified.

Thanks. It makes sense to me that both lug's strains can't be known simultaneously without more information. So I set the left one equal to zero.
I also read into the next chapter and I am confident this is the method he wanted us to take (in hindsight).
 

Related to Pin in Double Shear (Mechanics of Materials)

1. What is double shear in mechanics of materials?

Double shear occurs when a pin or bolt is subjected to a force that is applied in two planes, along the length of the pin and perpendicular to it. This type of loading creates a stress state that is known as double shear, where the pin is effectively being cut into two pieces.

2. How does the pin in double shear affect the strength of a joint?

The pin in double shear provides greater resistance to forces compared to a single shear pin. This is because the load is distributed across two planes, reducing the amount of stress on each plane and increasing the overall strength of the joint.

3. What is the difference between single shear and double shear?

In single shear, the force is applied in one plane and the pin is loaded along its length. In double shear, the force is applied in two planes and the pin is loaded along its length and perpendicular to it. Double shear provides greater strength and resistance to forces compared to single shear.

4. What are the factors that affect the strength of a pin in double shear?

The strength of a pin in double shear is influenced by several factors, including the material properties of the pin and the joint, the size and shape of the pin, and the applied load. The geometry and surface conditions of the pin and the joint also play a role in determining the strength of the pin in double shear.

5. How can the strength of a pin in double shear be calculated?

The strength of a pin in double shear can be calculated using the formula τ = (F/2)/(A*sin(θ)), where τ is the shear stress, F is the applied force, A is the cross-sectional area of the pin, and θ is the angle between the applied force and the pin. This formula takes into account the double shear effect and can be used to determine the maximum load a pin can withstand before failing.

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