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:
Jul. 05, 2016

Filed:

Jan. 16, 2012
Applicants:

Martin Hoeger, Erding, DE;

Inga Mahle, Munich, DE;

Jochen Gier, Karlsfeld, DE;

Inventors:

Martin Hoeger, Erding, DE;

Inga Mahle, Munich, DE;

Jochen Gier, Karlsfeld, DE;

Assignee:

MTU Aero Engines GmbH, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 25/14 (2006.01); F01D 25/24 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 5/143 (2013.01); F01D 25/14 (2013.01); F01D 25/24 (2013.01); F05D 2240/11 (2013.01); F05D 2270/17 (2013.01);
Abstract

Intermediate housing (), in particular of turbines () of a gas turbine engine, having a radially inner bounding wall () and having a radially outer bounding wall ('), having a crossflow channel (), which is formed by the bounding walls (′) and within which at least one supporting rib () is positioned that has a leading edge (), a trailing edge (), as well as side walls () extending between the leading edge () and the trailing edge () that direct a gas flow traversing the crossflow channel (); the radially outer bounding wall () having a contour that changes in the circumferential direction at least in one section upstream of the supporting rib ().


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