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:
May. 19, 2015

Filed:

Feb. 05, 2014
Applicant:

Rolls-royce Plc, London, GB;

Inventor:
Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); F01D 21/00 (2006.01); F01D 21/14 (2006.01); F01D 5/02 (2006.01); F02C 9/28 (2006.01); F01D 21/04 (2006.01); F01D 21/08 (2006.01);
U.S. Cl.
CPC ...
F02C 9/00 (2013.01); F02C 9/28 (2013.01); F01D 21/04 (2013.01); F01D 21/08 (2013.01); F01D 21/14 (2013.01); F01D 5/027 (2013.01); F01D 21/045 (2013.01); F05D 2270/11 (2013.01);
Abstract

This invention relates to the operation of gas turbine engines, and in particular to determining deterioration of components during operation. In a specific embodiment, the invention is concerned with determining the actions to be taken when a foreign body impact has been detected, for example on a fan blade. Accordingly, the invention provides a method to take one or more FOD detection apparatus, analyse the likely (probabilistic) outcome, and provide a system to determine subsequent action that assures safety whilst minimising operational disruption. This invention provides a method and apparatus to identify FOD or bird impact to gas turbine fan blades, assessing the damage that may have occurred whist still in flight and determining post impact actions, including replacement parts.


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