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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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Patent attributes

Patent Applicant

MTU Aero Engines

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Current Assignee

MTU Aero Engines

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Patent Jurisdiction

United States Patent and Trademark Office

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Patent Number

Patent Inventor Names

Astrid Kraus0

Michael Junge0

Francesca Storti0

Benjamin Hanschke0

Date of Patent

June 25, 2024

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Patent Application Number

179300120

Date Filed

September 6, 2022

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Patent Citations

US Patent 9340277 Airfoils for use in rotary machines

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US Patent 7179058 Aerodynamically wide range applicable cylindrical blade profiles

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US Patent 9879539 Engine airfoils and methods for reducing airfoil flutter

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Patent Primary Examiner

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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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