Patents by Inventor Anton Bergmann

Anton Bergmann 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).

  • Patent number: 8328138
    Abstract: A supporting strut for supporting an intermediate deck (2) that is arranged in an aircraft fuselage (1), includes a hollow cylindrical rod body (3) that includes a fiber reinforced material, with the two ends of the rod body (3) being designed as attachment sections for detachable attachment to the aircraft fuselage (1) or to the intermediate deck (2), wherein the rod body (3) includes at least one first reinforcement layer (10a) made from a carbon fiber fabric with an identical number of warp- and weft threads in 45° alignment or 90° alignment, as well as at least one second reinforcement layer (10b, 10c) made from a carbon fiber fabric including a higher number of warp threads than weft threads in 0° alignment, as well as a final layer including glass fiber, which together with artificial resin form a compact fiber reinforced material.
    Type: Grant
    Filed: May 5, 2009
    Date of Patent: December 11, 2012
    Assignee: Eurocopter Deutschland GmbH
    Inventors: Anton Bergmann, Marinus Sedlmeier
  • Publication number: 20090277995
    Abstract: A supporting strut for supporting an intermediate deck (2) that is arranged in an aircraft fuselage (1), includes a hollow cylindrical rod body (3) that includes a fibre reinforced material, with the two ends of the rod body (3) being designed as attachment sections for detachable attachment to the aircraft fuselage (1) or to the intermediate deck (2), wherein the rod body (3) includes at least one first reinforcement layer (10a) made from a carbon fibre fabric with an identical number of warp- and weft threads in 45° alignment or 90° alignment, as well as at least one second reinforcement layer (10b, 10c) made from a carbon fibre fabric including a higher number of warp threads than weft threads in 0° alignment, as well as a final layer including glass fibre, which together with artificial resin form a compact fibre reinforced material.
    Type: Application
    Filed: May 5, 2009
    Publication date: November 12, 2009
    Applicant: EUROCOPTER DEUTSCHLAND GMBH
    Inventors: Anton BERGMANN, Marinus SEDLMEIER
  • Patent number: 6886779
    Abstract: An impact-absorbing, load-limiting connection device includes a first connection structure, a second connection structure, a guiding mechanism, and at least one impact-absorbing, load-limiting sacrificial element disposed between the first and second connection structure. At least one of the first and second connection structures is moveable with respect to the other in a predetermined direction of movement corresponding to an anticipated main impact direction. The guiding mechanism is configured to guide at least one of the first and second connection structures along the direction of movement and includes at least one transverse force-absorbing guide element configured to absorb a force in a direction transverse to the direction of movement.
    Type: Grant
    Filed: October 22, 2003
    Date of Patent: May 3, 2005
    Assignee: Eurocopter Deutschland GmbH
    Inventors: Horst Bansemir, Jyrki Majamaeki, Walter Oefner, Anton Bergmann
  • Patent number: 6835263
    Abstract: An undercritical drive shaft and a method of producing the undercritical drive shaft from fiber composite material is disclosed. The drive shaft, which is produced of fiber composite material and is to be used as an undercritically operating shaft, has a high damage tolerance with respect to resistance to torsion and the manufacturing process requires lower expenditures. For the drive shaft, the fiber composite material consists of several successively individually wound-up webs of prepreg. For the method of producing the drive shaft from fiber composite material, as the fiber material, the web-shaped prepreg is wound onto the winding spindle and this prepreg is deaerated and simultaneously compressed by the winding-on of a thermoplastic woven band which is prestressed in a defined manner. The thermoplastic woven band is unwound again and additional prepreg layers are then wound up which are then deaerated and compressed in the same manner by a thermoplastic woven band.
    Type: Grant
    Filed: April 2, 2002
    Date of Patent: December 28, 2004
    Assignee: Eurocopter Deutschland GmbH
    Inventors: Anton Bergmann, Marinus Sedlmeier
  • Publication number: 20040135029
    Abstract: An impact-absorbing, load-limiting connection device includes a first connection structure, a second connection structure, a guiding mechanism, and at least one impact-absorbing, load-limiting sacrificial element disposed between the first and second connection structure. At least one of the first and second connection structures is moveable with respect to the other in a predetermined direction of movement corresponding to an anticipated main impact direction. The guiding mechanism is configured to guide at least one of the first and second connection structures along the direction of movement and includes at least one transverse force-absorbing guide element configured to absorb a force in a direction transverse to the direction of movement.
    Type: Application
    Filed: October 22, 2003
    Publication date: July 15, 2004
    Applicant: Eurocopter Deutschland GmbH
    Inventors: Horst Bansemir, Jyrki Majamaeki, Walter Oefner, Anton Bergmann
  • Publication number: 20020160138
    Abstract: An undercritical drive shaft and a method of producing the undercritical drive shaft from fiber composite material is disclosed. The drive shaft, which is produced of fiber composite material and is to be used as an undercritically operating shaft, has a high damage tolerance with respect to resistance to torsion and the manufacturing process requires lower expenditures. For the drive shaft, the fiber composite material consists of several successively individually wound-up webs of prepreg. For the method of producing the drive shaft from fiber composite material, as the fiber material, the web-shaped prepreg is wound onto the winding spindle and this prepreg is deaerated and simultaneously compressed by the winding-on of a thermoplastic woven band which is prestressed in a defined manner. The thermoplastic woven band is unwound again and additional prepreg layers are then wound up which are then deaerated and compressed in the same manner by a thermoplastic woven band.
    Type: Application
    Filed: April 2, 2002
    Publication date: October 31, 2002
    Inventors: Anton Bergmann, Marinus Sedlmeier