Patents by Inventor Philipp Westphal

Philipp Westphal 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: 11096910
    Abstract: The present invention relates to compounds according to general formula (I) which are metabolically robust analogues of bioactive lipid mediators derived from omega-3 polyunsaturated fatty acids (n-3 PUFAs). The present invention further relates to compositions containing one or more of these compounds and to the use of these compounds or compositions for the treatment or prevention of cardiovascular diseases.
    Type: Grant
    Filed: July 22, 2016
    Date of Patent: August 24, 2021
    Assignees: Max Delbruck-Centrum Fur Molekulare Medizin, The Board of Regents of the University of Texas System, Omeicos Therapeutics GmbH
    Inventors: Robert Fischer, Anne Konkel, Tim Wesser, Philipp Westphal, Wolf-Hagen Schunk, Christina Westphal, John Russell Falck
  • Publication number: 20190133976
    Abstract: The present invention relates to compounds according to general formula (I) which are metabolically robust analogues of bioactive lipid mediators derived from omega-3 polyunsaturated fatty acids (n-3 PUFAs). The present invention further relates to compositions containing one or more of these compounds and to the use of these compounds or compositions for the treatment or prevention of cardiovascular diseases.
    Type: Application
    Filed: July 22, 2016
    Publication date: May 9, 2019
    Inventors: Robert FISCHER, Anne KONKEL, Tim WESSER, Philipp WESTPHAL, Wolf-Hagen SCHUNK, Christina WESTPHAL, John Russell FALCK
  • Patent number: 8439307
    Abstract: The present invention provides a fuselage structure for an aircraft or spacecraft with an outer skin. The fuselage structure comprises a rib element for stiffening the outer skin and ad cross member element. Here the rib element is bent in the shape of an arc to correspond to an inner contour of the outer skin. The cross member element connects two arc sections of the rib element transversely to each other. The cross member element has a higher strength than the rib element. From another point of view the invention provides an aircraft with such a fuselage structure.
    Type: Grant
    Filed: December 15, 2009
    Date of Patent: May 14, 2013
    Assignees: Airbus Operations GmbH, DLR-Deutsches Zentrum fuer Luft- und Raumfahrt e.V.
    Inventors: Philipp Westphal, Wolf-Dietrich Dolzinski, Thorsten Roming, Thorsten Schroeer, Dieter Kohlgrueber, Marius Luetzenburger
  • Publication number: 20130009008
    Abstract: The present invention provides a fuselage structure for an aircraft or spacecraft with an outer skin. The fuselage structure comprises a rib element for stiffening the outer skin and ad cross member element. Here the rib element is bent in the shape of an arc to correspond to an inner contour of the outer skin. The cross member element connects two arc sections of the rib element transversely to each other. The cross member element has a higher strength than the rib element. From another point of view the invention provides an aircraft with such a fuselage structure.
    Type: Application
    Filed: December 15, 2009
    Publication date: January 10, 2013
    Inventors: Philipp Westphal, Wolf-Dietrich Dolzinski, Thorsten Roming, Thorsten Schroeer, Dieter Kohlgrueber, Marius Luetzenburger