Patent ID: 8894011
Filing Date: 2014-11-25
Classification: B29C,B29L,B64C,B64F

Abstract:
1. An aircraft fuselage comprising: a first fuselage section, the first fuselage section having a length with a forward end and an opposite rearward end, a first screw thread on the first fuselage section adjacent the rearward end, the first screw thread spiraling around the first fuselage section; a second fuselage section, the second fuselage section having a length with a forward end and an opposite rearward end, a second screw thread on the second fuselage section adjacent the forward end, the second screw thread spiraling around the second fuselage section; a sleeve, the sleeve having a length with a forward end and an opposite rearward end, screw threading on the sleeve, the screw threading on the sleeve mating with the first screw thread on the first fuselage section and the screw threading on the sleeve mating with the second screw thread on the second fuselage section, the screw threading on the sleeve securing together the first and second fuselage sections.