Sorry, but now guests are starting to arrive for dinner. Will continue tomorrow.
 
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Derbyboy
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D
Have a nice time :)
 
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Huggedugge1
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Huggedugge1 Huggedugge1 said:
yes. But about 850cm free. To the terrace that the deck goes under. Had to weld together two IPE beams and box them in with 4 mm corten steel. It deflects 3.5 cm despite that.
That's because you need to increase the mass on the top and bottom of the beam to counteract the deflection, not on the sides..

(Sounds crazy, I know, but that's how it is)
 
D
Yes, that really sounds strange.
 
It may sound as strange as it wants. But that's how it is if you calculate with steel and most other metallic materials.

Then, of course, there must be something that holds the top and bottom together (like a web in an I-beam or the sides of a tube), but the further from the center of the cross-section (in the load direction) you can increase the area of the cross-section, the better...
 
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Derbyboy
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An interesting and challenging problem at least for those of us who do not live with it and need to solve it. I have read through the thread but may have missed the answer to the obvious question. How much does the midpoint need to be raised for it to work, i.e., how much must the deflection be reduced?
 
In total, it’s about 15 cm, but "only" 5 cm from the position where the tire is now..
 
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hlph
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Violina Violina said:
May sound as strange as it wants. But that's how it is anyway when you calculate with steel and most other metallic materials...

Then, of course, there must be something that holds the top and bottom together (like a web in an I-beam or the sides of a tube) but the further from the center of the cross-section (in the load direction) you can increase the area of the cross-section, the better...
It's really quite intuitive that you should have a lot of material with a large lever arm to the neutral plane. It's not about the material but applies to all materials.
 
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richardtenggren
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Bernieberg Bernieberg said:
It is quite intuitive that you should have a lot of material with a large lever arm to the neutral axis. It doesn't have to do with the material but applies to all materials.
Since I don't work with many materials other than metals, I don't want to comment on it either.

But yes, I agree that I also (intuitively) think it should apply to "all other" materials as well, but since I'm not sure that is the case, I won't say anything about it.

Then I don't know what you mean by "lever arm to the neutral axis" because it's based on the cross-section that you calculate the resistance to deflection and the force has no lever arm with this type of load..
If it were a matter of twisting then yes, but not when calculating deflection.
 
Violina Violina said:
Since I don't work with many other materials than metals, I don't want to comment on them either.

But yes, I agree that I also (intuitively) think it should apply to "all other" materials as well, but since I'm not sure if that's the case, I won't say anything about it.

Also, I don't know what you mean by "lever arm to the neutral plane" because it's from the cross-section that you calculate resistance to deflection and the force has no lever arm in this type of load.
If it had been about twisting, then yes, but not when calculating deflection.
The neutral plane is the plane where there is neither tension nor compression. This plane lies in the centroid of the cross-section during pure bending.
 
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richardtenggren
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Bernieberg Bernieberg said:
The neutral plane is the plane where there is neither tension nor compression. This plane is located at the cross-section's center of gravity during pure bending.
Absolutely, but where is your lever arm??
 
Violina Violina said:
Absolutely, but where is your lever arm??
I am talking about the lever arm in the cross-section, not the lever arm for any external load. The distance between a point in the cross-section and the neutral plane. The coordinate y in the figure below.

Cross-section diagrams of a beam showing lever arm, neutral axis, and stress distribution along the y-coordinate, ranging from -12 ksi to 12 ksi.
 
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richardtenggren and 1 other
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Well… now you have REALLY lost me!!!

Self-supporting sheet metal is probably a good way to go, I think. I found a Plannja variant that didn't add much height. Then my idea is to lay the decking and screw it into the self-supporting sheet. (I haven't checked which screws etc, but I'll figure it out.)

When it comes to the frame, I've looked at Montano.se and found KKR tubes. I was thinking of VKR or KKR square tubes. Since VKR is insanely expensive, I'm more interested in KKR, which should be rust-protected and then painted black or clad with wood. I was thinking of KKR 120*60 with 5 mm thickness. 840 cm + 420 cm will be the frame. The weight of the frame will then be approximately 320 kg.

The self-supporting sheet from Plannja is 7 cm in height and has a span of 480 cm. Then the covering width is 750 cm (unsure what happens when it has to cover 840 cm…) The weight of the entire roof sheet will then be about 100 kg depending on thickness. The decking weighs approximately 1000 kg, the frame 320 kg. So 1.5 tons in total.

So my question is... Is KKR 120*60 with 5 mm thickness a reasonable solution as a frame that will work? How much will the open part that goes over the pool sag when it closes???

Or can someone suggest something else suitable to make it work?

Can someone help me…
 
  • Technical specification for KKR rectangular tube S355J2H, showing dimensions, welding suitability, and treatment options from montano.se website.
  • Screenshot of Montano.se showing technical specifications for KKR square tubes, including dimensions, area, and mass in a tabular format.
  • Screenshot of Montano website table showing specifications for KKR square tubes, including strength and chemical composition for S355J2H steel.
  • Table showing KKR and VKR steel pipe dimensions, weights, and thicknesses from Montano.se. Values include 120x60 and 120x120 sizes in various thicknesses.
Bernieberg Bernieberg said:
I'm talking about the lever arm in the cross-section, not the lever arm for any external load. The distance between a point in the cross-section and the neutral plane. The coordinate y in the figure below.

[image]
Hello! Do you have the opportunity to check my latest post?
 
Violina Violina said:
Absolutely, but where is your leverage??
Hi! Can you take a look at my last post? Am I completely off track?
 
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