US Patent 11396812 Flow channel for a turbomachine
Patent 11396812 was granted and assigned to MTU Aero Engines on July, 2022 by the United States Patent and Trademark Office.
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
113968120
Date of Patent
July 26, 2022
0Patent Application Number
162049540
Date Filed
November 29, 2018
0Patent Citations
Patent Primary Examiner
Edits on 27 Sep, 2022
Golden AI
Infobox
Is a
Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
113968120
Date of Patent
July 26, 2022
0Patent Application Number
162049540
Date Filed
November 29, 2018
0Patent Citations
Patent Primary Examiner
Edits on 26 Sep, 2022
Golden AI
Edits on 27 Jul, 2022
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Article (+559 characters)
US Patent 11396812 Flow channel for a turbomachine
Article
The present invention relates to a method for designing a flow channel for a turbomachine, in particular a gas turbine that comprises a guide vane cascade having a plurality of guide vanes, which are distributed in the peripheral direction, and flow passages, each of which is bounded by two successive guide vanes, and a support rib arrangement having at least one support rib, wherein a design of one of the flow passages is adapted to this support rib, that it is situated downstream of, in order to reduce a pressure loss and/or a vibrational stimulation.
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
11396812
Date of patent
July 26, 2022
Patent application number
16204954
Date Filed
November 29, 2018
Patent citations
Patent primary examiner
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