US Patent 10208765 Gas turbine axial compressor
Patent 10208765 was granted and assigned to MTU Aero Engines on February, 2019 by the United States Patent and Trademark Office.
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Patent abstract
The present invention relates to an axial compressor for a gas turbine, in particular an aircraft engine, having at least one rotor blade or guide vane having a blade or vane element, which is arranged in a flow duct, and a leading edge and a trailing edge, which are joined to each other through a pressure side and a suction side, wherein, a new and novel profile section of the blade or vane element is provided.
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Patent Inventor Names
Nina Wolfrum0
Sebastian Mann0
Sergio Elorza Gomez0
Tobias Froebel0
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Patent Applicant
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Patent Number
102087650
Date of Patent
February 19, 2019
0Patent Application Number
150002240
Date Filed
January 19, 2016
0Patent Citations Received
Patent Primary Examiner
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US Patent 10208765 Gas turbine axial compressor
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
10208765
Date of patent
February 19, 2019
Patent application number
15000224
Date Filed
January 19, 2016
Patent primary examiner
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