Is a
Patent attributes
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Joachim Bamberg0
Axel Rossmann0
Franz Heitmeir0
Date of Patent
July 26, 2011
Patent Application Number
10590868
Date Filed
February 26, 2005
Patent Primary Examiner
Patent abstract
A gas turbine vane, especially a vane pertaining to an aircraft engine, comprising a blade and a vane footing. The blade is defined by a flow inlet edge or a front edge, a flow outlet edge or a rear edge, and a blade surface extending between the front edge and the rear edge and forming a suction side and a pressure side. The suction side of the blade includes at least one microprofiled or microstructured region for optimizing the flow around the blade.
Timeline
No Timeline data yet.
Further Resources
No Further Resources data yet.
