US12448057 - Folding cabin assembly for low velocity air drop

The patent describes a military vehicle cabin featuring a bottom assembly that can connect with various top assemblies and a foldable top assembly designed for low velocity aerial drops. The top assembly incorporates a torsional spring to facilitate its transition from a folded to a deployed position.
Claim 1
- A military vehicle comprising: a cabin comprising: a bottom assembly configured to receive and removably couple with a plurality of different top assemblies; a foldable top assembly configured to transition between a folded position for a low velocity aerial drop (LVAD) and a deployed position, wherein the foldable top assembly comprises a torsional spring configured to provide a torque to assist transitioning of the foldable top assembly from the folded position to the deployed position. a cabin comprising: a bottom assembly configured to receive and removably couple with a plurality of different top assemblies; a foldable top assembly configured to transition between a folded position for a low velocity aerial drop (LVAD) and a deployed position, wherein the foldable top assembly comprises a torsional spring configured to provide a torque to assist transitioning of the foldable top assembly from the folded position to the deployed position. a bottom assembly configured to receive and removably couple with a plurality of different top assemblies; a foldable top assembly configured to transition between a folded position for a low velocity aerial drop (LVAD) and a deployed position, wherein the foldable top assembly comprises a torsional spring configured to provide a torque to assist transitioning of the foldable top assembly from the folded position to the deployed position.
Google Patents
https://patents.google.com/patent/US12448057
USPTO PDF
https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/12448057