AIRCRAFT FUSELAGE CONFIGURATIONS FOR UPWARD DEFLECTION OF ART FUSELAGE
AIRCRAFT FUSELAGE CONFIGURATIONS FOR UPWARD DEFLECTION OF ART FUSELAGE
- Neue Suche nach: REWERTS SCOTT DAVID
- Neue Suche nach: BELL JASON C
- Neue Suche nach: LUNDSTROM MARK EMIL
- Neue Suche nach: REWERTS SCOTT DAVID
- Neue Suche nach: BELL JASON C
- Neue Suche nach: LUNDSTROM MARK EMIL
A fixed-wing cargo aircraft having a kinked fuselage is disclosed. The fuselage contains a continuous interior cargo bay, and includes a forward portion, an aft portion, and a kinked portion forming a junction in the fuselage between the forward and aft portions. The kinked portion contains a transition region of the cargo bay and defines a bend between a forward centerline and an aft centerline. The kinked portion is formed with a forward transverse frame section, a separate aft transverse frame section, and a plurality of longitudinal frame elements extending between the forward and aft frame sections, the forward frame being coupled to an aft end of the forward portion and the aft frame section being coupled to a forward end of the aft portion such that the aft frame section is angled with respect to the forward frame section about a lateral axis of the cargo aircraft.
Dokumentinformationen
AIRCRAFT FUSELAGE CONFIGURATIONS FOR UPWARD DEFLECTION OF ART FUSELAGE
2024-04-18
Patent
Elektronische Ressource
Englisch
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