Patents by Inventor Bengt Abel

Bengt Abel 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: 9316562
    Abstract: The invention relates to a structural component, to a system and to a method for monitoring the integrity of a structure or a structural component. The structural component according to the invention has at least one elongated air duct which can be connected to a vacuum source and to a device for detecting the volumetric flow of air and/or the air pressure in the air duct, wherein, when the structure is intact in the region of the air duct, the air pressure in the air duct essentially corresponds to the air pressure of the vacuum source and there is essentially no volumetric flow of air through the air duct but, when a structural defect occurs in the region of the air duct, air from the region surrounding the structure or structural component enters the air duct and increases the air pressure and volumetric flow of air in the air duct in an identifiable manner.
    Type: Grant
    Filed: April 18, 2008
    Date of Patent: April 19, 2016
    Assignee: Airbus Operations GmbH
    Inventors: Jens Telgkamp, Holger Speckmann, Bengt Abel
  • Patent number: 8783609
    Abstract: A movable storage compartment for a passenger cabin comprises a housing and fixing structures on the side walls of the housing, the housing being open on one side and being able to be moved back and forth between an open and a closed position, that is to say being able to be opened and closed. The fixing structures are formed in such a way that during a movement from the open position to the closed position the housing can be moved first predominantly rotationally and then predominantly translationally upwards.
    Type: Grant
    Filed: June 19, 2012
    Date of Patent: July 22, 2014
    Assignee: Airbus Operations GmbH
    Inventors: Uwe Schneider, Bengt Abel, Peter Bielik, Raj Kotian
  • Publication number: 20120318917
    Abstract: A movable storage compartment for a passenger cabin comprises a housing and fixing structures on the side walls of the housing, the housing being open on one side and being able to be moved back and forth between an open and a closed position, that is to say being able to be opened and closed. The fixing structures are formed in such a way that during a movement from the open position to the closed position the housing can be moved first predominantly rotationally and then predominantly translationally upwards.
    Type: Application
    Filed: June 19, 2012
    Publication date: December 20, 2012
    Applicant: Airbus Operations GmbH
    Inventors: Uwe Schneider, Bengt Abel, Peter Bielik, Raj Kotian
  • Patent number: 8245975
    Abstract: The invention relates to a vehicle window consisting of a transparent composite material, wherein the composite material comprises fibers and a matrix material such that the vehicle window is capable of withstanding structural loads occurring in the window region and can substantially provide the window function even in spite of damage to the vehicle window (damage-tolerant), the fibers and the matrix material being transparent and substantially having the same refractive index. The invention proposes vehicle windows which are damage-tolerant, load bearing, cost-saving, easy to handle and require less installation space than conventional vehicle windows.
    Type: Grant
    Filed: July 20, 2010
    Date of Patent: August 21, 2012
    Assignee: Airbus Operations GmbH
    Inventors: Bengt Abel, Klaus Edelmann, Arne Hartwig, Klaus Hoppmann, Jens Wleting
  • Publication number: 20110071770
    Abstract: The invention relates to a structural component, to a system and to a method for monitoring the integrity of a structure or a structural component. The structural component according to the invention has at least one elongated air duct which can be connected to a vacuum source and to a device for detecting the volumetric flow of air and/or the air pressure in the air duct, wherein, when the structure is intact in the region of the air duct, the air pressure in the air duct essentially corresponds to the air pressure of the vacuum source and there is essentially no volumetric flow of air through the air duct but, when a structural defect occurs in the region of the air duct, air from the region surrounding the structure or structural component enters the air duct and increases the air pressure and volumetric flow of air in the air duct in an identifiable manner.
    Type: Application
    Filed: April 18, 2008
    Publication date: March 24, 2011
    Applicant: AIRBUS OPERATIONS GMBH
    Inventors: Jens Telgkamp, Holger Speckmann, Bengt Abel
  • Publication number: 20110017871
    Abstract: The invention relates to a vehicle window consisting of a transparent composite material, wherein the composite material comprises fibres and a matrix material such that the vehicle window is capable of withstanding structural loads occurring in the window region and can substantially provide the window function even in spite of damage to the vehicle window (damage-tolerant), the fibres and the matrix material being transparent and substantially having the same refractive index. The invention proposes vehicle windows which are damage-tolerant, load bearing, cost-saving, easy to handle and require less installation space than conventional vehicle windows.
    Type: Application
    Filed: July 20, 2010
    Publication date: January 27, 2011
    Inventors: Bengt Abel, Klaus Edelmann, Arne Hartwig, Klaus Hoppmann, Jens Wieting
  • Publication number: 20090159749
    Abstract: A connector element for connecting two component parts which can be for example a fuselage skin which is connected to a ring frame segment. Alternatively the connector element can also serve as a frame coupling for connecting two ring frame segments. The component parts can be formed with the same materials or with different materials. According to the disclosed embodiments the connector element in the ideal case completely compensates a temperature-conditioned change in length of at least one of the component parts by varying a connector element length of the connector elements. Thus two component parts can be connected together with different materials such as for example a fuselage skin 6 of an aluminium alloy to a ring frame segment which is formed by carbon fibre reinforced epoxy resin. The different coefficients of thermal expansion in this design lead to different changes in length of the component parts which are compensated by a corresponding variation in the length of the connector element.
    Type: Application
    Filed: November 4, 2008
    Publication date: June 25, 2009
    Inventors: Achim Etzkorn, Bengt Abel, Herwig Assler