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. 26, 2017

Filed:

Aug. 29, 2014
Applicant:

Rolls-royce Plc, London, GB;

Inventor:

Steven Aleksy Radomski, Nottingham, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); B23P 15/04 (2006.01); B23K 13/01 (2006.01); B23K 20/00 (2006.01); B23K 20/02 (2006.01); B23K 20/16 (2006.01); F01D 5/14 (2006.01); B23K 101/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/18 (2013.01); B23K 13/01 (2013.01); B23K 20/002 (2013.01); B23K 20/02 (2013.01); B23K 20/16 (2013.01); B23P 15/04 (2013.01); F01D 5/147 (2013.01); B23K 2201/001 (2013.01); F05D 2220/32 (2013.01); F05D 2230/10 (2013.01); F05D 2230/236 (2013.01); F05D 2230/51 (2013.01); F05D 2230/60 (2013.01); F05D 2230/90 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01); Y10T 29/49337 (2015.01);
Abstract

A method of manufacturing a hollow aerofoil component () for a gas turbine engine () comprises using a capping panel () to cover a pocket () in a pocketed aerofoil body (). During manufacture, a mandrel () is provided to support the capping panel () in the correct position. This ensures that the outer surface of the capping panel () is located as accurately as possible. This means that the capping panel () can be made to be as thin as possible, which in turn reduces weight and material wastage. Remotely detectable elements () may be provided to the mandrel () to enable the location of the pocket () to be accurately determined from outside the aerofoil ().


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