The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Feb. 19, 2019
Filed:
Jan. 19, 2016
Applicant:
Mtu Aero Engines Ag, Munich, DE;
Inventors:
Tobias Froebel, Siegertsbrunn, DE;
Sebastian Mann, Munich, DE;
Nina Wolfrum, Feldkirchen, DE;
Sergio Elorza Gomez, Munich, DE;
Assignee:
MTU Aero Engines AG, Munich, DE;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/32 (2006.01); F01D 9/04 (2006.01); F01D 5/14 (2006.01); F04D 29/54 (2006.01); F01D 9/06 (2006.01); F01D 19/02 (2006.01);
U.S. Cl.
CPC ...
F04D 29/324 (2013.01); F01D 5/141 (2013.01); F01D 5/145 (2013.01); F01D 9/041 (2013.01); F04D 29/544 (2013.01); F05D 2220/323 (2013.01); F05D 2240/303 (2013.01); F05D 2240/304 (2013.01); F05D 2250/70 (2013.01); F05D 2250/711 (2013.01); F05D 2250/712 (2013.01); Y02T 50/673 (2013.01);
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.