Patents by Inventor Hans-Peter Wentzel

Hans-Peter Wentzel 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).

  • FUSELAGE OF AN AIRCRAFT OR SPACECRAFT OF CRP/METAL HYBRID CONSTRUCTION WITH A METAL FRAMEWORK
    Publication number: 20100090061
    Abstract: The present invention provides an inherently rigid fuselage of an aircraft or spacecraft comprising shell elements or fuselage barrels of CRP construction, wherein the shell elements or fuselage barrels each have an outer skin and an inner skin, which each at least partially or completely consist of a CRP material, wherein a composite core element is provided between the outer skin and the inner skin, and wherein the fuselage in the interior has a metal framework which is connected to the shell elements or fuselage barrels.
    Type: Application
    Filed: January 18, 2008
    Publication date: April 15, 2010
    Applicant: AIRBUS DEUTSCHLAND GMBH
    Inventors: Michael Kolax, Wolf-Dietrich Dolzinski, Hans-Peter Wentzel, Ralf Herrmann
  • FUSELAGE STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT, WITH A FOAM LAYER AS THERMAL INSULATION
    Publication number: 20100038487
    Abstract: The present invention creates a fuselage structural component of an aircraft or spacecraft, with a non-load-bearing outer skin and a load-bearing inner framework structure, wherein a foam layer which effects heat insulation and/or impact protection is arranged between the outer skin and the inner framework structure.
    Type: Application
    Filed: January 18, 2008
    Publication date: February 18, 2010
    Applicant: AIRBUS DEUTSCHLAND GmbH
    Inventors: Michael Kolax, Wolf-Dietrich Dolzinski, Hans-Peter Wentzel, Ralf Herrmann
  • SHELL ELEMENT AS PART OF AN AIRCRFAFT FUSELAGE
    Publication number: 20100025532
    Abstract: The present invention provides a shell element as part of an aircraft fuselage, wherein the shell element is formed as a curved sheet-like element and is at least partially or completely of CRP construction.
    Type: Application
    Filed: January 23, 2008
    Publication date: February 4, 2010
    Applicant: AIRBUS DEUTSCHLAND GMBH
    Inventors: Ralf Herrmann, Wolf-Dietrich Dolzinski, Hans-Peter Wentzel, Michael Kolax