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:
Jun. 09, 2020

Filed:

May. 02, 2018
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Dale E. Evans, Derby, GB;

Steven A. Radomski, Nottingham, GB;

Clive Grafton-Reed, Leicester, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B23K 31/02 (2006.01); F01D 5/18 (2006.01); F01D 9/04 (2006.01); B23P 15/04 (2006.01); F01D 25/28 (2006.01); B23K 101/00 (2006.01);
U.S. Cl.
CPC ...
B23K 31/02 (2013.01); B23P 15/04 (2013.01); F01D 5/18 (2013.01); F01D 9/042 (2013.01); F01D 9/044 (2013.01); B23K 2101/001 (2018.08); F01D 25/285 (2013.01); F05D 2230/232 (2013.01); F05D 2230/236 (2013.01); F05D 2240/11 (2013.01); F05D 2240/12 (2013.01);
Abstract

A method of manufacturing a vane arrangement for a gas turbine engine comprises providing an aerofoil having a hollow cavity with an open end and providing a support member having a stub with a through hole extending therethrough. The method comprises welding the aerofoil to the stub such that the open end of the hollow cavity of the aerofoil is aligned with the through hole of the stub so as to define a hollow region extending through the support member and stub to the cavity of the aerofoil. During welding a tool is positioned within the through hole and cavity and is aligned with an interface between the stub and aerofoil, the tool being configured to prevent weld splatter onto a surface of the cavity or through hole.


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