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:
Sep. 10, 2019

Filed:

Mar. 30, 2016
Applicant:

Rolls-royce Plc, London, GB;

Inventor:
Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); B23P 15/02 (2006.01); F01D 11/00 (2006.01); B22D 15/02 (2006.01); B22D 25/02 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); B22D 15/02 (2013.01); B22D 25/02 (2013.01); B23P 15/02 (2013.01); F01D 5/18 (2013.01); F01D 5/188 (2013.01); F01D 11/00 (2013.01); B23P 2700/06 (2013.01); F01D 5/186 (2013.01); F05D 2220/32 (2013.01); F05D 2230/00 (2013.01); F05D 2230/10 (2013.01); F05D 2230/12 (2013.01); F05D 2230/21 (2013.01); F05D 2240/30 (2013.01); F05D 2250/14 (2013.01); F05D 2260/20 (2013.01); F05D 2260/202 (2013.01); Y10T 29/49341 (2015.01);
Abstract

A turbine blade having a labyrinth of internal channels for circulation of coolant received through an inlet formed in a terminal portion of a blade root. A labyrinth geometry includes: (i) the inlet arranged on an axially upstream face of the terminal portion leading to an upstream duct portion having a first section adjacent the inlet and a second section having a reduced cross-section compared to the first section, (ii) a leading edge passage intersecting with the first section and extending through a blade body towards a tip of the blade, where a proximal end of the leading edge passage is angled towards a direction of incoming air flow, (iii) a main blade passage intersecting with a downstream duct portion arranged in axial alignment with, and separate from, the upstream duct portion, and (iv) a restrictor passage intersecting with a mid-blade passage and extending towards a mid-blade duct portion.


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