Patents by Inventor Philipp WENG

Philipp WENG 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-seat assembly
    Patent number: 12515798
    Abstract: An aircraft seat arrangement includes a first aircraft seat device and a second aircraft seat device. The second aircraft seat device has an enclosure which forms a backrest wall in a subregion of the enclosure of the second aircraft seat device. The second aircraft seat device includes in an aircraft seat region a seat bottom which has a seat bottom front edge, a main extension axis of the seat bottom front edge being oriented at an angle of at least 5 degrees with respect to an aircraft seat device transversal axis of the second aircraft seat device. A lying-down direction of the aircraft seat region is oriented at an angle of at least 30 degrees with respect to an aircraft seat device longitudinal axis of the second aircraft seat device, the lying-down direction being directed away from an access region of the aircraft seat region.
    Type: Grant
    Filed: July 12, 2022
    Date of Patent: January 6, 2026
    Assignee: RECARO Aircraft Seating GmbH & Co. KG
    Inventors: Maik Thiele, Christopher Chilcott, Hermann Hoffmann, Heiko Minzer, Violina Mikova, Philipp Weng
  • AIRCRAFT-SEAT ASSEMBLY
    Publication number: 20240367796
    Abstract: An aircraft seat arrangement includes a first aircraft seat device and a second aircraft seat device, wherein the second aircraft seat device has an enclosure which forms a backrest wall in a subregion of the enclosure of the second aircraft seat device, wherein the second aircraft seat device comprises in an aircraft seat region a seat bottom which has a seat bottom front edge, a main extension axis of the seat bottom front edge being oriented at an angle of at least 5 degrees with respect to an aircraft seat device transversal axis of the second aircraft seat device, wherein a lying-down direction of the aircraft seat region is oriented at an angle of at least 30 degrees with respect to an aircraft seat device longitudinal axis of the second aircraft seat device, the lying-down direction being directed away from an access region of the aircraft seat region.
    Type: Application
    Filed: July 12, 2022
    Publication date: November 7, 2024
    Inventors: Maik THIELE, Christopher CHILCOTT, Hermann HOFFMANN, Heiko MINZER, Violina MIKOVA, Philipp WENG