Patents by Inventor Florian HESSELBACH

Florian HESSELBACH 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).

  • Publication number: 20200164958
    Abstract: A cladding element having a heating layer in a sandwich construction. In the case of a cladding element in a sandwich construction for an interior space of an aircraft, the cladding element includes a core layer and a first cover layer. The first cover layer forms a visible side of the cladding element. An electrically heating layer extends at least across a sub-face of the first cover layer and serves for generating heat for emission through the first cover layer is disposed between the core layer and the first cover layer.
    Type: Application
    Filed: November 22, 2019
    Publication date: May 28, 2020
    Inventors: Rainer Müller, Andreas Baatz, Dietmar Voelkle, Florian Hesselbach, Tobias Lechner, Norbert Staudigel, Benjamin Joemann
  • Publication number: 20200023974
    Abstract: The invention relates to a cabin air inlet module (16). The cabin air inlet module (16) comprises a streaming channel body (8). The streaming channel body (8) comprises at least one wall which limits a streaming channel wherein incoming air (5) is supplied to a zone (2) of a cabin (3). The cabin air inlet module (16) comprises an electric heating element (9) which is used for heating the incoming air (5). According to the invention it is proposed that the electric heating element (9) is embodied as a two-dimensional heating element (in particular as a heating paper, a heating web, a heating foil or a heating varnish). The two-dimensional heating element extends along a wall of the streaming channel body (8). The inventive cabin air inlet module (16) is arranged upstream with a small distance (25) from an inlet opening (6) into the zone (2) of the cabin (3). The inventive cabin air inlet module (16) is used for a tempering zones (2) of a cabin (3) of an airplane according to the needs.
    Type: Application
    Filed: September 18, 2019
    Publication date: January 23, 2020
    Inventors: Johannes Bosbach, Tobias Dehne, Felix Werner, Florian Hesselbach, Norbert Staudigel, Sven Utikal
  • Publication number: 20190061286
    Abstract: In a method for producing a pipe made of a fiber-reinforced thermoplastic material, two workpieces of the material are provided. The workpieces are introduced into a tool having a core and two part molds surrounding the core. The workpieces are heated and shaped between the core and the part molds to give a structural part of the pipe. The core is removed from the structural parts, the structural parts being held on the part molds, and joining regions of the structural parts are oriented towards one another. The structural parts are joined to one another in the joining regions to form the pipe. The pipe is released from the part molds, wherein the part molds are moved away from one another after shaping in order to remove the core, and are then moved back together in order to orient the structural parts towards one another.
    Type: Application
    Filed: August 21, 2018
    Publication date: February 28, 2019
    Inventors: STEFAN GIEHL, SVEN UTIKAL, FLORIAN HESSELBACH, MARTIN ZABOR
  • Patent number: 8747957
    Abstract: A coating method wherein in order to simplify the coating method and increase the flexibility thereof with respect to respective desired coatings, provision is made that a powder lacquer layer (3) is applied to a surface (2) of the component (1), and an imprint (4) is applied to the powder lacquer layer (3), preferably by an inkjet method.
    Type: Grant
    Filed: October 18, 2010
    Date of Patent: June 10, 2014
    Assignee: Diehl Aircabin GmbH
    Inventors: Mathias Gruen, Dietmar Voelkle, Benedict Michelis, Florian Hesselbach
  • Publication number: 20120040599
    Abstract: To implement replenished-air ventilation of a passenger cabin of, for example, an aircraft, an inner wall cladding (12) with integrated replenished-air inlets (18) is proposed. For this purpose, the inner wall cladding (12) has sandwich boards (30) which are constructed from a first top layer (32) facing the passenger cabin (10), a second top layer (34) facing away from the passenger cabin (10) and a sandwich core (36) arranged between the first top layer (32) and the second top layer (34), the sandwich core (36) being designed to be at least partially air-permeable, and the first top layer (32) having at least one air-permeable portion (38).
    Type: Application
    Filed: August 11, 2011
    Publication date: February 16, 2012
    Inventors: Florian HESSELBACH, Dietmar VÖLKLE
  • Publication number: 20110284689
    Abstract: The present invention relates to an aircraft cabin panel for sound reduction in an interior space. The invention in particular also relates to an aircraft comprising an interior lining with sound-absorbing and sound-reducing panels. In order to provide a panel that is optimized in terms of the design space required by it and in terms of its weight, for use in aircraft, which panel provides improved sound reduction and sound absorption characteristics, an aircraft cabin panel for sound reduction in an interior space is provided, which aircraft cabin panel in at least one region comprises a sandwich construction with a core layer, a first covering layer and a second covering layer. The core layer comprises sound absorbing open-pore core material. The first and the second covering layer are connected to the core layer in a planar fashion. The first covering layer is arranged towards the sound waves to be absorbed and the second covering layer is arranged opposite the first covering layer.
    Type: Application
    Filed: December 17, 2009
    Publication date: November 24, 2011
    Applicant: Airbus Operations GmbH
    Inventors: Christian Thomas, Florian Hesselbach, Stephan Hoetzeldt, Wilfried Michaelis, Uwe Schneider, Ralph Sturm, Arno Berger
  • Publication number: 20110097544
    Abstract: A coating method wherein in order to simplify the coating method and increase the flexibility thereof with respect to respective desired coatings, provision is made that a powder lacquer layer (3) is applied to a surface (2) of the component (1), and an imprint (4) is applied to the powder lacquer layer (3), preferably by an inkjet method.
    Type: Application
    Filed: October 18, 2010
    Publication date: April 28, 2011
    Applicant: DIEHL AIRCABIN GmbH
    Inventors: Mathias GRÜN, Dietmar VÖLKLE, Benedict MICHELIS, Florian HESSELBACH