Patents by Inventor Peer KONITZER

Peer KONITZER 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 FUSELAGE, BALLISTIC SHIELD FOR USE ON AN INNER SURFACE OF AN AIRCRAFT FUSELAGE, BALLISTIC SHIELD ASSEMBLY AND AIRCRAFT HAVING A FUSELAGE
    Publication number: 20260103284
    Abstract: An aircraft fuselage, in particular of an open fan propeller aircraft, includes a primary structure having frame members extending in a circumferential direction of the fuselage and stringers extending in a longitudinal direction of the fuselage and a ballistic shield covering an inner surface of a longitudinal section of the fuselage. The ballistic shield is inserted between adjacent frame members of the primary structure and extends in a longitudinal direction and a circumferential direction of the fuselage section. A ballistic shield for use on an inner surface of an aircraft fuselage, a ballistic shield assembly and aircraft are disclosed.
    Type: Application
    Filed: September 26, 2025
    Publication date: April 16, 2026
    Applicant: Airbus Operations GmbH
    Inventors: Peer Konitzer, Manuel Schweers
  • Antenna assembly, vertical tail, horizontal tail, wing, aircraft, and method
    Patent number: 11843164
    Abstract: An elongate antenna assembly (1) for an aircraft including a structural section (3) and an antenna element (5), wherein the structural section (3) includes an elongate leading edge section (7) extending in a longitudinal direction (13) of the antenna assembly, a first lateral section (9), and a second lateral section (11), wherein the leading edge section (7) is curved such that the leading edge section (7) comprises a convex outer surface (15) extending in the longitudinal direction (13) of the antenna assembly (1) on a convex side (19) of the antenna assembly.
    Type: Grant
    Filed: June 23, 2020
    Date of Patent: December 12, 2023
    Assignee: Airbus Operations GmbH
    Inventor: Peer Konitzer
  • ANTENNA ASSEMBLY, VERTICAL TAIL, HORIZONTAL TAIL, WING, AIRCRAFT, AND METHOD
    Publication number: 20220115777
    Abstract: An elongate antenna assembly (1) for an aircraft including a structural section (3) and an antenna element (5), wherein the structural section (3) includes an elongate leading edge section (7) extending in a longitudinal direction (13) of the antenna assembly, a first lateral section (9), and a second lateral section (11), wherein the leading edge section (7) is curved such that the leading edge section (7) comprises a convex outer surface (15) extending in the longitudinal direction (13) of the antenna assembly (1) on a convex side (19) of the antenna assembly.
    Type: Application
    Filed: June 23, 2020
    Publication date: April 14, 2022
    Inventor: Peer KONITZER