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. 01, 2018

Filed:

Oct. 01, 2015
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Paul A Hucker, Bristol, GB;

Stephen C Harding, Bristol, GB;

Alan P Geary, Bristol, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/00 (2006.01); F01D 5/18 (2006.01); F01D 9/06 (2006.01); F23R 3/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); F01D 5/188 (2013.01); F01D 9/065 (2013.01); F23R 3/002 (2013.01); F23R 3/005 (2013.01); F05B 2260/202 (2013.01); F05D 2240/81 (2013.01); F05D 2260/202 (2013.01); F23R 2900/00018 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03042 (2013.01); F23R 2900/03043 (2013.01);
Abstract

A cooled gas turbine engine component comprises a wall having first and second surfaces. The second surface has a plurality of recesses and each recess has a planar upstream end surface arranged so that it hangs over the upstream end of the recess. Each recess has a depth equal to the required depth plus the thickness of the thermal barrier coating to be deposited. The wall has a plurality of angled effusion cooling apertures extending from the first surface towards the second surface. Each effusion cooling aperture has an inlet in the first surface and an outlet in the end surface of a corresponding one of the recesses in the second surface. Each recess has smoothly curved transitions from the end surface and side surfaces to the second surface. Blocking of the effusion cooling apertures by thermal barrier coating is reduced.


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