Lucky_3838
Roller Poster
Thanks both for taking the time to read it!Am I understanding correctly? As I say, I’m not an engineer by any means, so please correct me if I’m spouting rubbish!
Matt, the force scaling makes sense for that simplified, purely upward loading example. The part I'd be careful with is turning it into a body weight needed to break the restraint. The 4.66 kN is where a calculated nominal stress in one sampled pawl section reaches an assumed yield strength of 355 MPa. It isn't an established breaking load for the real assembly, so it doesn't give us a minimum rider weight that could cause failure. Upward loading during airtime is also only one way the bar can be loaded.
And bratcurry, assessing the locking paths doesn't cover every possible failure of the complete assembly, or establish the condition of any individual restraint. My study can't identify or exclude a cause of the incident. That's a separate question from what loads this reconstructed model carries under its stated assumptions.
Update: the clamshell study is now 67 pages
I got a bit carried away expanding this last night and ended up getting rather less sleep than planned
The revised PDF is here: Read or download the full study.
Thanks again to Nicky for the CoasterStats recommendation. I went through their Mako recording and used the displayed motion readings to explore what forces they might imply for the seat and lap bar, with different assumptions about how the rider contacts both. These are forces calculated from the displayed readings, not measured forces on the restraint.
A few things came out of it:
- The timing matters. The recovered longitudinal and vertical minima occur 9.5 seconds apart. Combining those separate extremes would create a load vector that wasn't observed in the recovered record.
- The seat and bar can both be loaded during braking. The pad can push backwards and downwards on the rider while the rider pushes forwards and upwards on the bar. The seat remains loaded, so positive vertical loading doesn't automatically mean zero bar load.
- Direction and contact position matter. I've compared seven closing configurations and three assumed contact positions. The earlier purely upward result doesn't describe every combination of forces on the bar.
At an assumed 200 kg, the force becomes 3.34 kN, slightly above the same threshold. That threshold again marks the first included nominal section stress reaching the assumed yield strength, not a prediction of fracture or release. The masses are calculation inputs, not statements about who fits. The 3.25 kN also concerns a different direction and contact position from the earlier 4.66 kN upward reference.
One correction to my earlier video comment: its overview gives a longitudinal minimum of −1.50g, while the onride minimum indicator and confirmed readings give −0.85g. I've documented that disagreement rather than treating −1.50g as a recovered event.
The new analysis, diagrams and limitations are in Section 15. The original CAD reconstruction and mechanism study are still there too.
My overall impression of the clamshell's locking mechanism is very positive. From what I've been able to reconstruct, it looks like a well thought-out and mechanically robust arrangement. That is my assessment of the reconstructed mechanism, rather than verification of the real assembly's strength or the condition of any particular restraint.
Hopefully it gives anyone interested in the engineering a bit more to get their teeth into. Corrections and additional documented information are very welcome!

