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:
Aug. 18, 2020

Filed:

Dec. 13, 2018
Applicant:

Mtu Aero Engines Ag, München, DE;

Inventors:

Guenter Ramm, Eichenau, DE;

Martin Hoeger, Erding, DE;

Irene Raab, Munich, DE;

Yavuz Guendogdu, Ismaning, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F02K 3/06 (2006.01); F01D 9/04 (2006.01); F01D 9/06 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); F01D 5/142 (2013.01); F01D 5/143 (2013.01); F01D 5/146 (2013.01); F01D 9/041 (2013.01); F01D 9/06 (2013.01); F01D 9/065 (2013.01); F01D 25/24 (2013.01); F05D 2240/12 (2013.01); F05D 2240/14 (2013.01); F05D 2250/37 (2013.01);
Abstract

The present invention relates to a turbine module for a turbomachine, comprising a first flow bypass structure and a second flow bypass structure, said flow bypass structures being arranged in a hot gas duct, which is bounded by the turbine module and is designed to convey a hot gas and, namely, being arranged in succession in relation to a longitudinal axis of the turbine module in a direction of rotation, wherein, in relation to the bypass flow in the hot gas duct, the flow bypass structures each have a leading edge, and, downstream thereto, a trailing edge, and the second flow bypass structure is provided as a deflecting blade, wherein the second flow bypass structure has a smaller profile thickness than the first flow bypass structure, and wherein the hot gas duct is enclosed by a radial width.


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