US Patent 12123419 Compressor for an engine
Patent 12123419 was granted and assigned to MTU Aero Engines on October, 2024 by the United States Patent and Trademark Office.
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US Patent 12123419 Compressor for an engine
Article
Patent abstract
The invention relates to a compressor for an engine, wherein the compressor has compressor stages arranged in succession in a flow direction of the compressor and each compressor stage has a rotating blade cascade and a guide vane cascade arranged downstream of the rotating blade cascade and the rotating blade cascade and the guide vane cascade each have an aspect ratio.
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Roland Matzgeller0
Sergio Elorza Gomez0
Werner Humhauser0
Date of Patent
October 22, 2024
0Patent Application Number
183453190
Date Filed
June 30, 2023
0Patent Primary Examiner
CPC Code
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