US Patent 12018584 Airfoil for a compressor of a turbomachine
Patent 12018584 was granted and assigned to MTU Aero Engines on June, 2024 by the United States Patent and Trademark Office.
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US Patent 12018584 Airfoil for a compressor of a turbomachine
Article
Patent abstract
The invention relates to an airfoil for a compressor of a turbomachine, which extends starting from a blade root between a leading edge and a trailing edge to a blade tip, wherein the leading edge has a leading-edge thickness and the airfoil has a maximum profile thickness, the ratio of which to each other represents a relative leading-edge thickness, and the airfoil has a leading-edge wedge angle.
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Astrid Kraus0
Benjamin Hanschke0
Francesca Storti0
Michael Junge0
Date of Patent
June 25, 2024
0Patent Application Number
179300120
Date Filed
September 6, 2022
0Patent Citations
Patent Primary Examiner
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