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:
Nov. 30, 2021

Filed:

Feb. 15, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Robert C Backhouse, Wells, GB;

Vincent Gill, Bristol, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B29C 70/30 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); B29C 70/36 (2006.01); B29C 70/54 (2006.01); B29C 70/70 (2006.01); B29L 31/08 (2006.01); B32B 1/00 (2006.01); B32B 5/06 (2006.01); B32B 5/26 (2006.01); B32B 38/00 (2006.01); B32B 38/18 (2006.01); B29C 70/08 (2006.01); B29C 70/12 (2006.01); B29C 70/34 (2006.01); B29C 70/68 (2006.01); B29D 99/00 (2010.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); F01D 5/282 (2013.01); B29C 70/081 (2013.01); B29C 70/12 (2013.01); B29C 70/30 (2013.01); B29C 70/345 (2013.01); B29C 70/36 (2013.01); B29C 70/54 (2013.01); B29C 70/682 (2013.01); B29C 70/70 (2013.01); B29D 99/0025 (2013.01); B29L 2031/08 (2013.01); B29L 2031/082 (2013.01); B32B 1/00 (2013.01); B32B 5/06 (2013.01); B32B 5/26 (2013.01); B32B 38/0012 (2013.01); B32B 38/1808 (2013.01); B32B 2250/20 (2013.01); B32B 2255/02 (2013.01); B32B 2255/26 (2013.01); B32B 2305/076 (2013.01); B32B 2603/00 (2013.01); F05D 2220/32 (2013.01); F05D 2230/40 (2013.01); F05D 2300/44 (2013.01); F05D 2300/603 (2013.01); F05D 2300/6034 (2013.01); F05D 2300/611 (2013.01);
Abstract

A method of manufacturing a fan blade for a gas turbine engine. The method includes providing a compression mould having an internal mould surface corresponding to an outer profile of a fan blade, providing opposing first and second laminates to form a shell corresponding to the mould surface, each laminate comprising a lay-up of plies of fibre reinforcement material, applying a core material comprising quasi-isotropic short fibre reinforced resin in the compression mould so that with the compression mould in a moulding configuration the core material is enclosed by the shell, the core material and the shell forming a pre-form for the fan blade, applying pressure to compress the pre-form so that it conforms to the mould surface, and applying heat to cure the pre-form.


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