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:
Oct. 22, 2019

Filed:

Jun. 23, 2015
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventor:

Alexander Boeck, Kottgeisering, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 9/04 (2006.01); F01D 17/16 (2006.01); F04D 29/56 (2006.01); F01D 11/00 (2006.01); F01D 25/28 (2006.01); F04D 29/64 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 9/04 (2013.01); F01D 11/005 (2013.01); F01D 17/162 (2013.01); F01D 25/28 (2013.01); F04D 29/563 (2013.01); F04D 29/644 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2240/12 (2013.01); Y02T 50/671 (2013.01); Y10T 29/49323 (2015.01);
Abstract

The invention relates to a guide means () for a gas turbine, in particular for an aircraft engine, having at least one casing element (); having at least one first duct segment (), which is arranged in the radial direction on the inside of the casing element (), by means of which at least one duct (), through which gas can flow, is at least partially delimited outward in the radial direction; having at least one second duct segment (), which is arranged in the radial direction on the inside of the first duct segment (), by means of which the duct () is at least partially delimited inward in the radial direction; and having at least one guide vane ().


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