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:
May. 05, 2020

Filed:

Aug. 06, 2018
Applicant:

Rolls-royce Plc, London, GB;

Inventor:

Leo V. Lewis, Kenilworth, GB;

Assignee:

ROLLS-ROYCE PLC, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/24 (2006.01); F01D 5/02 (2006.01); F01D 5/12 (2006.01); F01D 25/24 (2006.01); F01D 25/10 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 11/24 (2013.01); F01D 5/02 (2013.01); F01D 5/12 (2013.01); F01D 25/10 (2013.01); F01D 25/12 (2013.01); F01D 25/24 (2013.01); F05D 2220/32 (2013.01); F05D 2260/201 (2013.01);
Abstract

An arrangement for a gas turbine engine that includes a turbine blade configured to rotate about an axis, a casing radially outside of the turbine blade, and a carrier segment mounted to the casing so as to define a first impingement space therebetween. The carrier segment is positioned radially outside the turbine blade and includes a first impingement carrier wall, a main carrier wall, and a cooling chamber. The first impingement carrier wall is adjacent to and radially inside of the first impingement space, and the first impingement carrier wall includes a first aperture. The main carrier wall is radially inside of the first impingement carrier wall. The cooling chamber is radially inside of the main carrier wall. Additionally, an intermediate chamber is disposed radially between the cooling chamber and the first impingement space. A second aperture is configured to allow ingress of air into the intermediate chamber.


Find Patent Forward Citations

Lewis, Leo. (2020). Tip clearance control for turbine blades (U.S. Patent No. 10641122). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10641122

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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