Patents by Inventor Franziskus Mayer

Franziskus Mayer has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Aircraft with an integrated energy-absorbing deformation structure and aircraft with such a fuselage
    Patent number: 9162745
    Abstract: An aircraft fuselage has an integrated energy-absorbing deformation structure. The fuselage includes annular frames, longitudinal fuselage beams interconnecting the annular frames, and a covering forming a fuselage skin. A lower floor structure is disposed in an interior of the fuselage. The lower floor structure includes a plurality of transverse beams connected to an assigned frame and longitudinal floor beams which interconnect said transverse beams. The deformation structure is formed in a lower fuselage region disposed below the lower floor structure. The deformation structure includes a first inelastically deformable central region and, on a left-hand side and a right-hand side, respective second inelastically deformable regions of greater stiffness in the vertical direction than the central region.
    Type: Grant
    Filed: April 9, 2011
    Date of Patent: October 20, 2015
    Assignee: PREMIUM AEROTEC GMBH
    Inventors: Franziskus Mayer, Christoph Meisner, Peter Starke
  • AIRCRAFT WITH AN INTEGRATED ENERGY-ABSORBING DEFORMATION STRUCTURE AND AIRCRAFT WITH SUCH A FUSELAGE
    Publication number: 20130112811
    Abstract: An aircraft fuselage has an integrated energy-absorbing deformation structure. The fuselage includes annular frames, longitudinal fuselage beams interconnecting the annular frames, and a covering forming a fuselage skin. A lower floor structure is disposed in an interior of the fuselage. The lower floor structure includes a plurality of transverse beams connected to an assigned frame and longitudinal floor beams which interconnect said transverse beams. The deformation structure is formed in a lower fuselage region disposed below the lower floor structure. The deformation structure includes a first inelastically deformable central region and, on a left-hand side and a right-hand side, respective second inelastically deformable regions of greater stiffness in the vertical direction than the central region.
    Type: Application
    Filed: April 9, 2011
    Publication date: May 9, 2013
    Applicant: PREMIUM AEROTEC GMBH
    Inventors: Franziskus Mayer, Christoph Meisner, Peter Starke