Patents by Inventor Björn Anders

Björn Anders 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: 12345176
    Abstract: A turbine rotor having an improved rotor tip, which has at least one cooling channel in the rotor blade, the cooling channel, in the region of its cuspidal point, having at least one locally limited constriction that is caused by a thickened portion at the end of a partition of the cooling channel.
    Type: Grant
    Filed: April 5, 2022
    Date of Patent: July 1, 2025
    Assignee: Siemens Energy Global GmbH & Co. KG
    Inventors: Björn Anders, Constantin Garske, Kay Krabiell, Heiko Lammers, Markus Lempke, Ricardo Nilsson, Daniel Vöhringer
  • Publication number: 20240229650
    Abstract: A turbine rotor having an improved rotor tip, which has at least one cooling channel in the rotor blade, the cooling channel, in the region of its cuspidal point, having at least one locally limited constriction that is caused by a thickened portion at the end of a partition of the cooling channel.
    Type: Application
    Filed: April 5, 2022
    Publication date: July 11, 2024
    Applicant: Siemens Energy Global GmbH & Co. KG
    Inventors: Björn Anders, Constantin Garske, Kay Krabiell, Heiko Lammers, Markus Lempke, Ricardo Nilsson, Daniel Vöhringer
  • Patent number: 11958150
    Abstract: A method for repairing a damaged leading or trailing edge region of a metallic turbine blade, which has a suction-side blade wall, a pressure-side blade wall and a leading edge and a trailing edge, includes: removing the damaged leading or trailing edge region, with a cutout being formed; providing a replacement part which can be inserted in form-fitting fashion into the cutout and which restores the intended geometry of the turbine blade; inserting the replacement part in form-fitting fashion into the cutout in a predetermined insertion direction, and cohesively connecting the replacement part to the turbine blade, wherein mechanical connection of the replacement part and turbine blade using separate fastening elements is performed in addition to the cohesive connection.
    Type: Grant
    Filed: August 6, 2021
    Date of Patent: April 16, 2024
    Assignee: Siemens Energy Global GmbH & Co. KG
    Inventors: Björn Anders, Reiner Anton, Constantin Garske, Kay Krabiell, Heiko Lammers, Ricardo Nilsson, Daniel Vöhringer, Jörg Ziege
  • Patent number: 11859510
    Abstract: A turbine blade tip, turbine blade and method where improved cooling is made possible by an improved cooling structure with cooling air holes inside a depression in a blade tip and a special arrangement of multiple cooling air holes which are supplied by a single cooling air channel inside a wall.
    Type: Grant
    Filed: February 8, 2021
    Date of Patent: January 2, 2024
    Assignee: Siemens Energy Global GmbH & Co. KG
    Inventors: Björn Anders, Reiner Anton, Kay Krabiell, Christian Lerner
  • Publication number: 20230347457
    Abstract: A method for repairing a damaged leading or trailing edge region of a metallic turbine blade, which has a suction-side blade wall, a pressure-side blade wall and a leading edge and a trailing edge, includes: removing the damaged leading or trailing edge region, with a cutout being formed; providing a replacement part which can be inserted in form-fitting fashion into the cutout and which restores the intended geometry of the turbine blade; inserting the replacement part in form-fitting fashion into the cutout in a predetermined insertion direction, and cohesively connecting the replacement part to the turbine blade, wherein mechanical connection of the replacement part and turbine blade using separate fastening elements is performed in addition to the cohesive connection.
    Type: Application
    Filed: August 6, 2021
    Publication date: November 2, 2023
    Applicant: Siemens Energy Global GmbH & Co. KG
    Inventors: Björn Anders, Reiner Anton, Constantin Garske, Kay Krabiell, Heiko Lammers, Ricardo Nilsson, Daniel Vöhringer, Jörg Ziege
  • Publication number: 20230127843
    Abstract: A turbine blade tip, turbine blade and method where improved cooling is made possible by an improved cooling structure with cooling air holes inside a depression in a blade tip and a special arrangement of multiple cooling air holes which are supplied by a single cooling air channel inside a wall.
    Type: Application
    Filed: February 8, 2021
    Publication date: April 27, 2023
    Applicant: Siemens Energy Global GmbH & Co. KG
    Inventors: Björn Anders, Reiner Anton, Kay Krabiell, Christian Lerner