Is a
Patent attributes
Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Sergio Elorza Gomez0
Nina Wolfrum0
Sebastian Mann0
Tobias Froebel0
Date of Patent
February 19, 2019
0Patent Application Number
150002240
Date Filed
January 19, 2016
0Patent Citations Received
Patent Primary Examiner
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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