An inversion-formed double-walled tube includes an outer tube having an outer wall thickness, an inner tube disposed inside the outer tube and having an inner wall thickness, and a transition portion connecting the inner tube and the outer tube. In this arrangement, at least one of the inner and outer wall thicknesses varies along a length of the double-walled tube. The inversion-formed double-walled tube may be configured as an inversion tube type energy absorber and as an energy absorbing inversion tube assembly.
INVERSION-FORMED DOUBLE-WALLED TUBE AND ENERGY ABSORBING INVERSION TUBE ASSEMBLY
01.06.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
INVERSION-FORMED DOUBLE-WALLED TUBE AND ENERGY ABSORBING INVERSION TUBE ASSEMBLY
Europäisches Patentamt | 2025
|Inversion-formed double-walled tube and energy absorbing inversion tube assembly
Europäisches Patentamt | 2025
|