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. 01, 2019

Filed:

Jul. 13, 2017
Applicant:

Rolls-royce Deutschland Ltd & CO KG, Blankenfelde-Mahlow, DE;

Inventor:

Marcel Schmidt, Berlin, DE;

Assignee:

ROLLS-ROYCE DEUTSCHLAND LTD & CO KG, Blankenfelde-Mahlow, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/14 (2006.01); F01D 25/16 (2006.01); F01D 25/24 (2006.01); F02C 7/24 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 25/145 (2013.01); F01D 9/04 (2013.01); F01D 25/162 (2013.01); F01D 25/24 (2013.01); F01D 25/246 (2013.01); F02C 7/24 (2013.01); F05D 2220/32 (2013.01); F05D 2230/642 (2013.01); F05D 2240/12 (2013.01); F05D 2240/15 (2013.01); F05D 2250/75 (2013.01); F05D 2260/231 (2013.01);
Abstract

A subassembly of a gas turbine engine includes a heat shield and carrier subassembly for a turbine section are disclosed. The carrier includes support features to couple to an engine casing. The upstream end of the carrier includes a radially inward arm extending toward to an engine axis. The outer end of the radially floating heat shield is coupled to the radially inward arm via a pin-and-slot joint configured to allow movement of the heat shield relative to the radially inward arm of the carrier. In response to thermal expansion and contraction of the vane, the heat shield is configured to move radially outward and inward, respectively, relative to the radially inward arm to maintain contact with the outer platform of the vane.


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