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US Patent 10041353 Blade cascade and turbomachine

Patent 10041353 was granted and assigned to MTU Aero Engines on August, 2018 by the United States Patent and Trademark Office.

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Patent abstract

A blade cascade of a turbomachine whose at least one side wall is configured to be circumferentially undulated and which has at least two elevations and at least one depression or at least two depressions having at least one elevation, as well as a turbomachine having a blade cascade of this kind.

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Patent Inventor Names
Jochen Gier0
Karl Engel0
Yavuz Guendogdu0
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Patent Citations Received
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US Patent 11629608 Axial flow turbine
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Patent citations received
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US Patent 10968748 Non-axisymmetric end wall contouring with aft mid-passage peak
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US Patent 10876411 Non-axisymmetric end wall contouring with forward mid-passage peak
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US Patent 10458248 Blade channel, blade cascade and turbomachine
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 US Patent 10041353 Blade cascade and turbomachine

Infobox
Is a
Patent
Patent
Patent applicant
MTU Aero Engines
MTU Aero Engines
Current assignee
MTU Aero Engines
MTU Aero Engines
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10041353
Date of patent
August 7, 2018
Patent application number
14452594
Date Filed
August 6, 2014
Patent primary examiner
‌
Eldon Brockman

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