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. 12, 2019

Filed:

Feb. 12, 2018
Applicant:

Rolls Royce Plc, London, GB;

Inventors:

Nigel H S Smith, Derby, GB;

Mark J. Wilson, Nottingham, GB;

Gabriel Gonzalez-Gutierrez, Derby, GB;

Marco Barale, Derby, GB;

Benedict Phelps, Derby, GB;

Kashmir S. Johal, Derby, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/38 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F04D 29/384 (2013.01); F02K 3/06 (2013.01); F04D 29/388 (2013.01); F05D 2220/32 (2013.01); F05D 2240/301 (2013.01); F05D 2240/303 (2013.01);
Abstract

A fan blade is provided with an aerofoil portion for which, at radii between 20% and 40% of the blade span, the location of the position of maximum thickness along the camber line is at less than a defined percentage of the total length of the camber line. For all cross-sections through the aerofoil portion at radii greater than 70% of the blade span, the location of the position of maximum thickness along the camber line is at more than a defined percentage of the total length of the camber line. The geometry of the fan blade may result in a lower susceptibility to flutter.


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