Patents by Inventor Patricia Parlevliet

Patricia Parlevliet 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: 10737463
    Abstract: A method for producing a sandwich panel with a reinforced foam core includes inserting rod-shaped, thermoplastic reinforcing elements into a thermoplastic foam material such that the reinforcing elements extend through the foam material. End regions of the reinforcing elements project out of the foam material. The foam material is thermoformed to form a reinforced foam core, wherein the end regions of the reinforcing elements are integrally formed by applying temperature and pressure to the cover surfaces of the foam material and are bonded to the foam material in a fused connection. A thermoplastic cover layer is laminated on either side by applying temperature and pressure to the reinforced foam core on the cover surfaces of the foam material in order to form the sandwich panel, wherein the cover layers are bonded to the reinforced foam core in a fused connection.
    Type: Grant
    Filed: June 28, 2017
    Date of Patent: August 11, 2020
    Assignee: Airbus Defence and Space GmbH
    Inventors: Tilman Orth, Jonas Gruenewald, Patricia Parlevliet
  • Patent number: 10414116
    Abstract: A sandwich component has a first cover layer, a second cover layer, and a core disposed therebetween. In the sandwich component, the cover layers are each formed from an outer layer made of a fiber-reinforced thermoplast material having greater resistance to a certain solvent and, fused therewith, an inner layer made of a thermoplast material having lower resistance to the solvent. The core has outer layers, each of which is formed from a thermoplast material having lower resistance to the solvent, and an inner structure, which is formed entirely or partially from a thermoplast material having greater resistance to the solvent. The inner layers of the cover layers were each fused with one of the outer layers of the core with the use of the solvent.
    Type: Grant
    Filed: May 22, 2015
    Date of Patent: September 17, 2019
    Assignee: Airbus Defence and Space GmbH
    Inventors: Jonas Gruenewald, Patricia Parlevliet, Thomas Meer
  • Patent number: 10399299
    Abstract: A sandwich component and method of producing the sandwich component are provided wherein the sandwich component has a first cover layer, a second cover layer, and a core disposed therebetween. In the sandwich component, the cover layers are each formed from an outer layer made of a fiber-reinforced high-melting-point thermoplast material and, fused therewith, an inner layer made of a low-melting-point thermoplast material. The core has outer layers, each of which is formed from a low-melting-point thermoplast material, and an inner structure, which is formed entirely or partially from a high-melting-point thermoplast material. The inner layers of the cover layers were each fused with one of the outer layers of the core.
    Type: Grant
    Filed: May 22, 2015
    Date of Patent: September 3, 2019
    Assignee: Airbus Defence and Space GmbH
    Inventors: Jonas Gruenewald, Patricia Parlevliet
  • Publication number: 20190002685
    Abstract: The embodiments relate to a polymerisable thermoset composition having improved flame retardant properties, a polymerised thermoset having improved flame retardant properties, a process for manufacturing the polymerised thermoset, and use of the polymerisable thermoset composition to produce lightweight construction components, preferably carbon fibre composites (CFRP), and a lightweight construction component, preferably carbon fibre composite (CFRP), containing the polymerised thermoset.
    Type: Application
    Filed: August 21, 2018
    Publication date: January 3, 2019
    Inventors: Christoph MEIER, Patricia PARLEVLIET, Manfred DOERING
  • Patent number: 10077359
    Abstract: The embodiments relate to a polymerizable thermoset composition having improved flame retardant properties, a polymerized thermoset having improved flame retardant properties, a process for manufacturing the polymerized thermoset, and use of the polymerizable thermoset composition to produce lightweight construction components, preferably carbon fiber composites (CFRP), and a lightweight construction component, preferably carbon fiber composite (CFRP), containing the polymerized thermoset.
    Type: Grant
    Filed: June 30, 2016
    Date of Patent: September 18, 2018
    Assignee: AIRBUS DEFENCE AND SPACE GMBH
    Inventors: Christoph Meier, Patricia Parlevliet, Manfred Doering
  • Patent number: 10040906
    Abstract: A polymerizable thermoset composition including a polymerizable organic cyanate ester resin and a polymerizable aryl ethynyl-terminated polyimide, a polymerized thermoset, a process for the production of the polymerized thermoset as well as the use of the polymerizable thermoset composition for the production of lightweight construction components, preferably carbon fiber composite materials (CFC), and a lightweight construction component, preferably carbon fiber composite material (CFC), containing the polymerized thermoset are described.
    Type: Grant
    Filed: July 1, 2016
    Date of Patent: August 7, 2018
    Assignee: Airbus Defence and Space GmbH
    Inventors: Christoph Meier, Patricia Parlevliet, Manfred Doering
  • 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
  • Publication number: 20180001593
    Abstract: A method for producing a sandwich panel with a reinforced foam core includes inserting rod-shaped, thermoplastic reinforcing elements into a thermoplastic foam material such that the reinforcing elements extend through the foam material. End regions of the reinforcing elements project out of the foam material. The foam material is thermoformed to form a reinforced foam core, wherein the end regions of the reinforcing elements are integrally formed by applying temperature and pressure to the cover surfaces of the foam material and are bonded to the foam material in a fused connection. A thermoplastic cover layer is laminated on either side by applying temperature and pressure to the reinforced foam core on the cover surfaces of the foam material in order to form the sandwich panel, wherein the cover layers are bonded to the reinforced foam core in a fused connection.
    Type: Application
    Filed: June 28, 2017
    Publication date: January 4, 2018
    Inventors: Tilman ORTH, Jonas GRUENEWALD, Patricia PARLEVLIET
  • Publication number: 20170002191
    Abstract: The embodiments relate to a polymerisable thermoset composition having improved flame retardant properties, a polymerised thermoset having improved flame retardant properties, a process for manufacturing the polymerised thermoset, and use of the polymerisable thermoset composition to produce lightweight construction components, preferably carbon fibre composites (CFRP), and a lightweight construction component, preferably carbon fibre composite (CFRP), containing the polymerised thermoset.
    Type: Application
    Filed: June 30, 2016
    Publication date: January 5, 2017
    Inventors: Christoph MEIER, Patricia PARLEVLIET, Manfred DOERING
  • Publication number: 20170002147
    Abstract: A polymerizable thermoset composition including a polymerizable organic cyanate ester resin and a polymerizable aryl ethynyl-terminated polyimide, a polymerized thermoset, a process for the production of the polymerized thermoset as well as the use of the polymerizable thermoset composition for the production of lightweight construction components, preferably carbon fibre composite materials (CFC), and a lightweight construction component, preferably carbon fibre composite material (CFC), containing the polymerized thermoset are described.
    Type: Application
    Filed: July 1, 2016
    Publication date: January 5, 2017
    Applicant: Airbus Defence and Space GmbH
    Inventors: Christoph Meier, Patricia Parlevliet, Manfred Doering
  • Publication number: 20150336350
    Abstract: A sandwich component and method of producing the sandwich component are provided, wherein the sandwich component has a first cover layer, a second cover layer, and a core disposed therebetween. In the sandwich component, the cover layers are each formed from an outer layer made of a fiber-reinforced thermoplast material having greater resistance to a certain solvent and, fused therewith, an inner layer made of a thermoplast material having lower resistance to the solvent. The core has outer layers, each of which is formed from a thermoplast material having lower resistance to the solvent, and an inner structure, which is formed entirely or partially from a thermoplast material having greater resistance to the solvent. The inner layers of the cover layers were each fused with one of the outer layers of the core with the use of the solvent.
    Type: Application
    Filed: May 22, 2015
    Publication date: November 26, 2015
    Inventors: Jonas GRUENEWALD, Patricia PARLEVLIET, Thomas MEER
  • Publication number: 20150336352
    Abstract: A sandwich component and method of producing the sandwich component are provided wherein the sandwich component has a first cover layer, a second cover layer, and a core disposed therebetween. In the sandwich component, the cover layers are each formed from an outer layer made of a fiber-reinforced high-melting-point thermoplast material and, fused therewith, an inner layer made of a low-melting-point thermoplast material. The core has outer layers, each of which is formed from a low-melting-point thermoplast material, and an inner structure, which is formed entirely or partially from a high-melting-point thermoplast material. The inner layers of the cover layers were each fused with one of the outer layers of the core.
    Type: Application
    Filed: May 22, 2015
    Publication date: November 26, 2015
    Inventors: Jonas GRUENEWALD, Patricia PARLEVLIET
  • Publication number: 20150158280
    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: Application
    Filed: December 5, 2014
    Publication date: June 11, 2015
    Inventors: Christian WEIMER, Patricia PARLEVLIET
  • Patent number: 8790487
    Abstract: The present invention relates to a method of fabricating a composite part presenting an integral structure of composite material comprising at least one reinforcing layer based on reinforcing fibers, fabrics, or textiles, and at least one impregnation matrix, the method consisting in assembling the integral structure, in placing said integral structure in a mold, in impregnating said integral structure with the impregnation matrix by injection or infusion, and in solidifying said impregnated integral structure by raising it to a determined temperature, the method being characterized in that it consists in: using at least two distinct primary parts for making up the integral structure; placing a thermoplastic sheet on at least one of the primary parts so as to make the interface between said primary parts once they are assembled together.
    Type: Grant
    Filed: January 17, 2011
    Date of Patent: July 29, 2014
    Assignees: Airbus Helicopters Deutschland GmbH, EADS Deutschland GmbH
    Inventors: Christian Weimer, Nikolaus Bätge, Hans Luinge, Georg Wachinger, Patricia Parlevliet
  • Publication number: 20110174426
    Abstract: The present invention relates to a method of fabricating a composite part presenting an integral structure of composite material comprising at least one reinforcing layer based on reinforcing fibers, fabrics, or textiles, and at least one impregnation matrix, the method consisting in assembling the integral structure, in placing said integral structure in a mold, in impregnating said integral structure with the impregnation matrix by injection or infusion, and in solidifying said impregnated integral structure by raising it to a determined temperature, the method being characterized in that it consists in: using at least two distinct primary parts for making up the integral structure; placing a thermoplastic sheet on at least one of the primary parts so as to make the interface between said primary parts once they are assembled together.
    Type: Application
    Filed: January 17, 2011
    Publication date: July 21, 2011
    Applicants: EUROCOPTER DEUTSCHLAND GMBH, EADS DEUTSCHLAND GMBH
    Inventors: Christian Weimer, Nikolaus Bätge, Hans Luinge, Georg Wachinger, Patricia Parlevliet
  • Publication number: 20110151179
    Abstract: A semi-finished product used to mold a composite part including at least one dry laminar reinforcing layer that is designed to be impregnated with an impregnation matrix by liquid injection/infusion. The semi-finished product includes a thermoplastic layer, at least locally, where the properties of the component materials provide the future molded part, at least locally, with the required properties; since the thermoplastic layer has been stitched to at least one reinforcing layer using at least one yarn crossing through the perforations in said thermoplastic layer and in at least one reinforcing layer.
    Type: Application
    Filed: December 20, 2010
    Publication date: June 23, 2011
    Applicant: EUROCOPTER DEUTSCHLAND GMBH
    Inventors: Nikolaus Bätge, Patricia Parlevliet, Christian Weimer