JBee
Well-known member
- First Name
- JB
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- Nov 22, 2019
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- Cybertruck
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I think the closest the CT gets to a stressed skin is me pulling my hair out trying to describe how there's not many parts of it that are a load carrying exoskeleton! 
But on a more serious note the structural battery pack is a lot closer to a stressed skin element than the exoskeleton type fender. The trick why it works for an airliner though is that the stressed skins are in a tube shape, that are capable of transferring loads over a large area, without creating load hot spots that need reinforcement. The CT square box shape is less than optimal for that in comparison.
But the biggest difference to an aircraft is that the CT won't be designed to incorporate as much deflection as an aircraft has (that is to say t won't bend as much), and of course won't have fuel laden wings. The wheels are the only place the loads are carried, and the CT will want to be stiff to keep it agile for on road handling.
on CT Suspension
There is another factor to consider when it comes to the CT air suspension, that will also affect the CT structural design. That is that unlike common steel springs, air suspension can be "cross-linked". This can be done mechanically or electronically.
This means you can have one side front and rear airspring linked together by a hose connection, and the other side too by its own connection, you end up with a system where the front wheel compression pushes the rear wheel up to compensate, and the rear the front when the bump passes underneath. In cornering because both airsprings are compressed on the outside of the vehicle it will also have less body roll in corners. This is similar to a local manufacture that make the Kinetic Suspension for Toyota, that uses a hydraulic roll bar.
The reason this becomes important for the structure (and traction offroad too) is that in nearly all normal driving conditions the load on each spring can remain the same, regardless of the wheel articulation position. That means unlike a steel spring, the more tighlty compressed spring does not have the most load, and the most traction, rather all wheels can have the same amount of load at the same time and equal traction because of it.
This works up until the CT suspension travel is maxed out, and the airspring can no longer compensate for articulation.
Now being able to monitor load on each airspring also allows for the traction control system to predict available traction, which means better motivation in difficult terrain. Obviously, being and active air suspension there's a heap of other features that could be mentioned here, but for the structure the primary benefit is that torsional loads could be greatly reduced in all driving conditions, until the airsprings hit their stops. This along with the rear F1 style pushrod suspension, would mean the torsion loads would be near zero, because the rear assembly and pushrod geometry essentially make the CT a tripod for suspension load, which does not have a longitudinal torsional element.
But on a more serious note the structural battery pack is a lot closer to a stressed skin element than the exoskeleton type fender. The trick why it works for an airliner though is that the stressed skins are in a tube shape, that are capable of transferring loads over a large area, without creating load hot spots that need reinforcement. The CT square box shape is less than optimal for that in comparison.
But the biggest difference to an aircraft is that the CT won't be designed to incorporate as much deflection as an aircraft has (that is to say t won't bend as much), and of course won't have fuel laden wings. The wheels are the only place the loads are carried, and the CT will want to be stiff to keep it agile for on road handling.
on CT Suspension
There is another factor to consider when it comes to the CT air suspension, that will also affect the CT structural design. That is that unlike common steel springs, air suspension can be "cross-linked". This can be done mechanically or electronically.
This means you can have one side front and rear airspring linked together by a hose connection, and the other side too by its own connection, you end up with a system where the front wheel compression pushes the rear wheel up to compensate, and the rear the front when the bump passes underneath. In cornering because both airsprings are compressed on the outside of the vehicle it will also have less body roll in corners. This is similar to a local manufacture that make the Kinetic Suspension for Toyota, that uses a hydraulic roll bar.
The reason this becomes important for the structure (and traction offroad too) is that in nearly all normal driving conditions the load on each spring can remain the same, regardless of the wheel articulation position. That means unlike a steel spring, the more tighlty compressed spring does not have the most load, and the most traction, rather all wheels can have the same amount of load at the same time and equal traction because of it.
This works up until the CT suspension travel is maxed out, and the airspring can no longer compensate for articulation.
Now being able to monitor load on each airspring also allows for the traction control system to predict available traction, which means better motivation in difficult terrain. Obviously, being and active air suspension there's a heap of other features that could be mentioned here, but for the structure the primary benefit is that torsional loads could be greatly reduced in all driving conditions, until the airsprings hit their stops. This along with the rear F1 style pushrod suspension, would mean the torsion loads would be near zero, because the rear assembly and pushrod geometry essentially make the CT a tripod for suspension load, which does not have a longitudinal torsional element.
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