Patents by Inventor Christian Weimer

Christian Weimer 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: 9970814
    Abstract: A device for processing items, in particular items in a production sequence, in different processing steps, has at least one sensor arrangement having a plurality of sensors, wherein at least one item is measured in a detection mode by at least a partial quantity of the sensors as the detection means, wherein an impacting of the at least one item with an irradiation means is determined by a control means while considering a result of the measuring procedure of the at least one item; and wherein the at least one item is irradiated in an irradiation mode by at least a further partial quantity of the plurality of sensors as the irradiation means. If appropriate, at least part of the method is repeated with a renewed measuring, determination and/or irradiation.
    Type: Grant
    Filed: July 6, 2017
    Date of Patent: May 15, 2018
    Assignee: Airbus Defence and Space GmbH
    Inventors: Tilman Orth, Jonas Gruenewald, Christian Weimer
  • Patent number: 9937692
    Abstract: A method for the manufacture of reinforced core composites, comprises: inserting of a pin into a foamed core material or a filled honeycomb-shaped core material, wherein the pin and the core material contain a thermoplastic polymer, or a mixture of thermoplastic polymers; the pin is heated such that as the pin is inserted the core material softens or melts at the point of insertion; and/or the core material is heated at the point of insertion such that the core material softens or melts.
    Type: Grant
    Filed: December 5, 2014
    Date of Patent: April 10, 2018
    Assignee: AIRBUS DEFENCE AND SPACE GMBH
    Inventors: Christian Weimer, Patricia Parlevliet
  • Patent number: 9942670
    Abstract: A method operates a system of a hearing aid device and a communication device. The hearing aid device has an acousto-electrical transducer, a signal processing device and an electro-acoustic transducer. The communication device has a controller and an electro-acoustic transducer. The method includes the steps of: receiving of an incoming call by the communication device, signaling of the incoming call by the communication device by a first acoustic signal via the electro-acoustic transducer, receiving of the first acoustic signal by the acousto-electrical transducer of the hearing aid device, identifying of the first acoustic signal and carrying out of a first change of adjustment on the hearing aid device when the first acoustic signal has been identified.
    Type: Grant
    Filed: August 27, 2015
    Date of Patent: April 10, 2018
    Assignee: Sivantos Pte. Ltd.
    Inventors: Thomas Dickel, Matthias Froehlich, Uwe Harich, Carlo Christian Weimer
  • Patent number: 9879987
    Abstract: A positioning system for detecting a spatial position of a laying head of a device for automatically laying reinforcing fiber strips in relation to a base on which the reinforcing fiber strips can be laid by the laying head includes at least two laser lines which extend substantially in parallel at a spacing A from one another and substantially transversely to a laying direction can be projected on the laid reinforcing fiber strips by at least one laser source. The elevation profiles of the projected laser lines which occur on account of an irregular surface of the laid reinforcing fiber strips are able to be recorded by a camera and supplied to an evaluation unit.
    Type: Grant
    Filed: November 18, 2015
    Date of Patent: January 30, 2018
    Assignee: Airbus Defence and Space GmbH
    Inventors: Franz Engel, Christian Weimer
  • Publication number: 20180017440
    Abstract: A device for processing items, in particular items in a production sequence, in different processing steps, has at least one sensor arrangement having a plurality of sensors, wherein at least one item is measured in a detection mode by at least a partial quantity of the sensors as the detection means, wherein an impacting of the at least one item with an irradiation means is determined by a control means while considering a result of the measuring procedure of the at least one item; and wherein the at least one item is irradiated in an irradiation mode by at least a further partial quantity of the plurality of sensors as the irradiation means. If appropriate, at least part of the method is repeated with a renewed measuring, determination and/or irradiation.
    Type: Application
    Filed: July 6, 2017
    Publication date: January 18, 2018
    Applicant: Airbus Defence and Space GmbH
    Inventors: Tilman Orth, Jonas Gruenewald, Christian Weimer
  • Publication number: 20170297745
    Abstract: In order to provide a simplified inspection of an aircraft for the pilot, an aircraft inspection system is provided which includes at least one movable inspection unit, a position detection arrangement, and at least one data transfer interface. The at least one moveable inspection unit is moveable relative to an aircraft to be inspected. The at least one movable inspection unit includes at least one sensor for detecting a characteristic value, for verifying a characteristic and/or for determining a defect of an aircraft. The movable inspection unit is configured to generate monitoring data. When a defect or a characteristic value is detected, the position detection arrangement detects position data of the movable inspection unit in relation to the aircraft to be inspected, and assigns the position data to the monitoring data. The data transfer interface provides the position data with the assigned monitoring data as inspection data.
    Type: Application
    Filed: November 28, 2016
    Publication date: October 19, 2017
    Applicant: Airbus Defence and Space GmbH
    Inventors: Franz Engel, Daniel Bauer, Tilman Orth, Christian Weimer
  • Publication number: 20170297277
    Abstract: A method for producing a fiber composite laminate, including the steps of applying pressure and/or heat to a first preform, which has one or more dry fiber layers and a thermoplastic elastomer, such that the thermoplastic portion of the thermoplastic elastomer completely impregnates the dry fiber layers of the first preform in at least one first region and only partially impregnates the dry fiber layers in at least one second region and, in a thermosetting polymer matrix, impregnating and curing the fiber layers of the second region of the first preform that are still dry and have not been impregnated with the thermoplastic portion of the thermoplastic elastomer.
    Type: Application
    Filed: April 4, 2017
    Publication date: October 19, 2017
    Inventors: Christopher Buchmann, Christian Weimer, Christoph Meier, Jonas Gruenewald
  • Publication number: 20170144384
    Abstract: A laying unit for producing a fiber composite component includes a drive device which is formed for magnetic cooperation with a running face, which provides a magnetic field and/or is ferromagnetic, to advance the laying unit on the running face. A device for producing a fiber composite component comprising a laying unit of this type and a method for producing a fiber composite component comprising a device of this type are disclosed.
    Type: Application
    Filed: November 22, 2016
    Publication date: May 25, 2017
    Inventors: Franz ENGEL, Christian WEIMER, Tilman ORTH
  • Publication number: 20170144387
    Abstract: An apparatus for producing a fiber composite component. The apparatus includes a shaping tool and a plurality of laying units which are mechanically independent of one another and are each configured to lay a fiber material on the shaping tool, wherein the laying units each include a control device which is configured to actuate each laying unit to automatically interact with at least one other laying unit to lay a predetermined fiber arrangement together.
    Type: Application
    Filed: November 22, 2016
    Publication date: May 25, 2017
    Inventors: Franz ENGEL, Christian WEIMER, Tilman ORTH
  • Publication number: 20170144386
    Abstract: A laying unit for producing a fibre composite component is provided. The laying unit includes a housing and a plurality of fibre coils which are designed so as to be able to be unwound during a movement of the laying unit, wherein the fibre coils are provided in a movably mounted manner inside the housing.
    Type: Application
    Filed: November 15, 2016
    Publication date: May 25, 2017
    Applicant: Airbus Defence and Space GmbH
    Inventors: Franz Engel, Christian Weimer, Tilman Orth
  • Publication number: 20170095982
    Abstract: A method to produce a fibrous body that includes structures crosslinked in a fluid-permeable manner. The method includes constructing the fibrous body in layers by alternately applying a fiber-matrix material to a layer substrate and fusing each applied layer of the fiber-matrix material. The fiber-matrix material contains a matrix material and a plurality of short fibers and/or fiber particles.
    Type: Application
    Filed: October 4, 2016
    Publication date: April 6, 2017
    Inventors: Christian WEIMER, Franz ENGEL
  • Publication number: 20170095985
    Abstract: An activation device used for binder activation during the production of a fiber-reinforced plastic laminate. The activation device has at least one light-emitting diode for heating a portion of at least one semi-finished fiber ribbon. A method is used for producing a fiber-reinforced plastic laminate. It comprises automatically laying at least one semi-finished fiber ribbon on a laying support, heating at least one portion of the semi-finished fiber ribbon by means of one or more light-emitting diode(s) of an activation device, and pressing the heated portion of the semi-finished fiber ribbon on the laying support.
    Type: Application
    Filed: October 3, 2016
    Publication date: April 6, 2017
    Inventors: Franz Engel, Tilman Orth, Christian Weimer, Katharina Schlegel
  • Publication number: 20170015070
    Abstract: A testing arrangement serves for controlling the manufacturing of a fiber reinforced component. The testing arrangement includes an inspection device with a sensor system, with the inspection device being configured to move on and/or above one or more material layer(s) and/or a surface of the component and to examine the material layer(s) or the surface with the sensor system. A device serves for automated manufacturing of a fiber reinforced plastic laminate. The device includes a forming tool, a laying head for automated laying of material layers in the forming tool as well as a testing arrangement.
    Type: Application
    Filed: July 12, 2016
    Publication date: January 19, 2017
    Applicant: Airbus Defence and Space GmbH
    Inventors: Daniel Bauer, Franz Engel, Tilman Orth, Christian Weimer
  • Publication number: 20170001389
    Abstract: A method for repairing a component which contains fiber-reinforced plastics material. For curing a deformable material introduced into and/or applied to a repair point of the component, the material is heated by irradiation with light from a light-emitting device. The disclosure herein further relates to a light-emitting device for heating a material that is deformable at least in part, in a method according to the disclosure herein, and to a repair device which comprises a light-emitting device.
    Type: Application
    Filed: June 29, 2016
    Publication date: January 5, 2017
    Inventors: Franz ENGEL, Tilman ORTH, Christian WEIMER
  • Publication number: 20170001384
    Abstract: Devices and methods are disclosed for depositing reinforcing fiber tapes and detecting laying errors. Automatic depositing of reinforcing fiber tapes on a support can occur by a laying head and at least one roller assigned to the laying head. At least one radiation source and/or at least one sensor is integrated into the at least one roller for the detection of laying errors, and this roller is transmissive at least by region for a radiation emitted by the radiation source.
    Type: Application
    Filed: June 30, 2016
    Publication date: January 5, 2017
    Inventors: Christian EITZINGER, Franz ENGEL, Tilman ORTH, Christian WEIMER
  • Publication number: 20160368586
    Abstract: In order to simplify a system integration in a fuselage of an aircraft, the disclosure herein provides a production method for producing a load-bearing fuselage panel for a fuselage section of an aircraft fuselage in an area of an aircraft cabin, including manufacturing the fuselage panel to have a sandwich construction with an inner panel and an outer skin as shells and a filling panel embedded between the shells as a core, while configuring the outer skin as a part of a fuselage structure and the outer delimitation of the aircraft fuselage, configuring the inner panel for an interior space delimitation of the cabin, and integrating functional elements of the fuselage structure and the cabin and/or the aircraft into the filling panel. Preferably, the shells and the filling panel are connected to each other by a joining process while producing covalent bonds.
    Type: Application
    Filed: June 17, 2016
    Publication date: December 22, 2016
    Inventors: Christian Weimer, Rainer Rauh
  • Publication number: 20160183327
    Abstract: A light emitting unit comprises at least one lighting means for emitting light (L) for heating a composite material, e.g. resin of a carbon fiber reinforced plastic, wherein the composite material can be fused and/or softened and/or cured, and/or be hold in a liquid state by the heating and wherein the emission of light (L) of the lighting means can be controlled differently in several areas. Furthermore, this relates to a method for producing a component made of the composite material as well as a method for producing the light emitting unit.
    Type: Application
    Filed: December 22, 2015
    Publication date: June 23, 2016
    Inventors: Franz Engel, Tilman Orth, Christian Weimer, Wolfgang Rehm
  • Publication number: 20160176100
    Abstract: A device for consolidating a thermoplastic preform, in particular a carbon fiber thermoplastic preform includes a heating element, e.g., an LED array, for heating the preform and a consolidation element, e.g., a consolidation roller, for exposing the preform to pressure and for cooling the preform. In order to consolidate the preform, the heating element and consolidation element are arranged and movable relative to each other in such a way that the preform can be exposed to pressure and cooled by the consolidation element after heated by means of the heating element.
    Type: Application
    Filed: December 21, 2015
    Publication date: June 23, 2016
    Applicant: Airbus Defence and Space GmbH
    Inventors: Christian Weimer, Franz Engel, Tilman Orth
  • Publication number: 20160146598
    Abstract: A positioning system for detecting a spatial position of a laying head of a device for automatically laying reinforcing fiber strips in relation to a base on which the reinforcing fiber strips can be laid by the laying head includes at least two laser lines which extend substantially in parallel at a spacing A from one another and substantially transversely to a laying direction can be projected on the laid reinforcing fiber strips by at least one laser source. The elevation profiles of the projected laser lines which occur on account of an irregular surface of the laid reinforcing fiber strips are able to be recorded by a camera and supplied to an evaluation unit.
    Type: Application
    Filed: November 18, 2015
    Publication date: May 26, 2016
    Inventors: Franz Engel, Christian Weimer
  • Publication number: 20160121559
    Abstract: A deposition device for depositing fibrous structures in an automated manner on a workpiece includes a plurality of support elements each having at least one deposition head, wherein the at least one deposition head is designed to deposit fibrous structures on the workpiece, and wherein the plurality of support elements and the workpiece are arranged so as to be movable relative to one another in a circumferential direction of the workpiece and in a longitudinal direction of the workpiece.
    Type: Application
    Filed: October 30, 2015
    Publication date: May 5, 2016
    Applicant: AIRBUS DEFENCE AND SPACE GMBH
    Inventor: Christian WEIMER