Determine Force for inclining platform

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SUMMARY

The discussion focuses on calculating the force required for an inclining platform with a load of 12,000 kg. The calculated moment is 36,000 kg⋅m, and the load at a distance of 1.906 m from the fulcrum results in a force of 185,100 newtons. Participants express concerns about the safety and implications of using such a load, questioning whether it is a real scenario or a mockup. The thread was ultimately closed due to safety concerns regarding dangerous discussions.

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TL;DR
A hydraulic actuator force, F is 3000m from the right is lifting the platform upwards. The load 12000kg is UDL. How do I calculate for F?
inclined_beam.jpg
 
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Is it accelerating the load? ##F## will also be a function of the cylinder geometry.
 
No it's not accelerating the load. The cylinder geometry will be depending on the calculated force.
 
Moment: 12,000 kg at 3.000 m = 36,000 kg⋅m .
If one lift cylinder is located at 1.906 m from the fulcrum,
the load will be; 36,000 / 1.906 = 18,888. kg .
18,888 kg * 9.8 = 185,100 newton.
Have you included the mass of the tilting platform?
 
jr5 said:
The load 12000kg is UDL. How do I calculate for F?
The load is 12,000 kg, and you are asking for advice on an Internet forum? Can you provide a link to your buisiness insurance company please?
 
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berkeman said:
The load is 12,000 kg, and you are asking for advice on an Internet forum? Can you provide a link to your buisiness insurance company please?
It's not for company, it's a mockup.
 
jr5 said:
It's not for company, it's a mockup.
I don't understand. Is the load really 12,000 kg, or is that mocked up too? If it's real, what happens if/when the support fails?
 
berkeman said:
I don't understand. Is the load really 12,000 kg, or is that mocked up too? If it's real, what happens if/when the support fails?
Jeopardy.
 
DeBangis21 said:
Jeopardy.
You are not helping your case to keep this thread open; thread is now closed per the "no dangerous discussions" clause in the PF Rules (see INFO at the top of the page).
 

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