Patents by Inventor Martin LAZAK

Martin LAZAK 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).

  • Radome cover shell and opening kinematic
    Patent number: 11697488
    Abstract: An aircraft with an aircraft structure that comprises a radome cover opening kinematic and a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position. The radome cover opening kinematic may enable movements of the radome cover shell between the closed position and an opened position and vice versa. The radome cover opening kinematic may include a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller are arranged on opposing sides of the guiding rail, and wherein the second and a third roller are arranged on the same side of the guiding rail. The radome shell opening kinematic further comprises a radome cover shell rotation stopper that can stop movement of the radome cover shell at the completely opened position.
    Type: Grant
    Filed: December 3, 2020
    Date of Patent: July 11, 2023
    Assignee: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
    Inventors: Jan Boehme, Yann Le Cadet, Martin Lazak
  • Radome cover shell and opening kinematic
    Patent number: 11643182
    Abstract: An aircraft with an aircraft structure that comprises a radome cover opening kinematic and a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position. The radome cover opening kinematic may enable movements of the radome cover shell between the closed position and an opened position and vice versa. The radome cover opening kinematic may include a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller are arranged on opposing sides of the guiding rail, and wherein the second and a third roller are arranged on the same side of the guiding rail.
    Type: Grant
    Filed: October 22, 2020
    Date of Patent: May 9, 2023
    Assignee: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
    Inventors: Jan Boehme, Yann Le Cadet, Martin Lazak
  • RADOME COVER SHELL AND OPENING KINEMATIC
    Publication number: 20220126976
    Abstract: An aircraft with an aircraft structure that comprises a radome cover opening kinematic and a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position. The radome cover opening kinematic may enable movements of the radome cover shell between the closed position and an opened position and vice versa. The radome cover opening kinematic may include a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller are arranged on opposing sides of the guiding rail, and wherein the second and a third roller are arranged on the same side of the guiding rail.
    Type: Application
    Filed: October 22, 2020
    Publication date: April 28, 2022
    Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
    Inventors: Jan BOEHME, Yann LE CADET, Martin LAZAK
  • RADOME COVER SHELL AND OPENING KINEMATIC
    Publication number: 20220126977
    Abstract: An aircraft with an aircraft structure that comprises a radome cover opening kinematic and a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position. The radome cover opening kinematic may enable movements of the radome cover shell between the closed position and an opened position and vice versa. The radome cover opening kinematic may include a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller are arranged on opposing sides of the guiding rail, and wherein the second and a third roller are arranged on the same side of the guiding rail. The radome shell opening kinematic further comprises a radome cover shell rotation stopper that can stop movement of the radome cover shell at the completely opened position.
    Type: Application
    Filed: December 3, 2020
    Publication date: April 28, 2022
    Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
    Inventors: Jan BOEHME, Yann LE CADET, Martin LAZAK