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.

Date of Patent:
Dec. 16, 2014

Filed:

Aug. 10, 2010
Applicants:

Christian Cornelius, Sprockhövel, DE;

Georg Kröger, Köln, DE;

Eberhard Nicke, Köln, DE;

Inventors:

Christian Cornelius, Sprockhövel, DE;

Georg Kröger, Köln, DE;

Eberhard Nicke, Köln, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F04D 29/324 (2013.01); F05D 2250/711 (2013.01); F01D 5/141 (2013.01); F05D 2250/712 (2013.01); Y10S 416/05 (2013.01); Y10S 416/02 (2013.01);
Abstract

A compressor blade for an axially permeated compressor, preferably of a stationary gas turbine is provided. The camber line of the blade tip side profile of the blade of the compressor blade includes at least two inflection points for reducing radial gap losses. By means of two inflection points, there is a concavely designed suction side contour segment in a segment from 35% to 50% for the suction side contour, and a convexly implemented pressure side contour segment for the pressure side contour. It is possible by means of the geometry to generate low-loss gap vortices, in order to increase the overall efficiency of an axial compressor including the compressor blades.


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