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:
Jan. 18, 2022

Filed:

Jan. 23, 2018
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventor:

Lothar Albers, Munich, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/14 (2006.01); F01D 11/18 (2006.01); F04D 29/58 (2006.01); F04D 29/52 (2006.01); F04D 29/16 (2006.01); B33Y 80/00 (2015.01); F01D 25/24 (2006.01); F01D 11/12 (2006.01); F01D 9/04 (2006.01); F01D 25/26 (2006.01); F01D 25/12 (2006.01); F01D 11/08 (2006.01); F01D 11/24 (2006.01);
U.S. Cl.
CPC ...
F01D 25/145 (2013.01); B33Y 80/00 (2014.12); F01D 9/04 (2013.01); F01D 11/08 (2013.01); F01D 11/122 (2013.01); F01D 11/127 (2013.01); F01D 11/18 (2013.01); F01D 11/24 (2013.01); F01D 25/12 (2013.01); F01D 25/14 (2013.01); F01D 25/24 (2013.01); F01D 25/246 (2013.01); F01D 25/26 (2013.01); F04D 29/164 (2013.01); F04D 29/526 (2013.01); F04D 29/5853 (2013.01); F05D 2220/32 (2013.01); F05D 2230/31 (2013.01); F05D 2260/231 (2013.01);
Abstract

A turbomachine housing element, having a flow channel for accommodating a rotor blade assembly and a first cavity at least partially produced by primary shaping; the first cavity being adapted for passive thermal insulation and/or the assemblable turbomachine housing element not being adapted for the active circulation of fluid through the first cavity; and/or, between the first cavity and the flow channel, a separate seal being attached to turbomachine housing element; and/or the first cavity extending in the axial direction of the flow channel over at least 20% of a minimum axial length of the turbomachine housing element at the level of the cavity and/or over a minimum axial length of the separate seal and/or being filled with air or a thermally insulating fluid, whose specific thermal conductivity λ is at least 10% lower than the specific thermal conductivity λ of air.


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