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:
Feb. 06, 2024

Filed:

Sep. 12, 2022
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Dharun Vadugappatty Srinivasan, Singapore, SG;

Sridhar Idapalapati, Singapore, SG;

Assignee:

Rolls-Royce PLC, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23P 6/00 (2006.01); F01D 5/00 (2006.01); B29C 73/10 (2006.01); B29C 73/26 (2006.01); F01D 5/28 (2006.01); B23P 6/04 (2006.01); B29L 31/08 (2006.01);
U.S. Cl.
CPC ...
F01D 5/005 (2013.01); B23P 6/002 (2013.01); B23P 6/045 (2013.01); B29C 73/10 (2013.01); B29C 73/26 (2013.01); F01D 5/282 (2013.01); B29C 2073/264 (2013.01); B29L 2031/082 (2013.01); F05D 2230/10 (2013.01); F05D 2230/23 (2013.01); F05D 2230/80 (2013.01); F05D 2300/603 (2013.01);
Abstract

A method of repairing a composite blade. The composite blade includes a metal work bonded to a composite part through an adhesive layer. The method includes determining a locally damaged portion of the metal work, and removing a bullet portion corresponding to the locally damaged portion. The method further includes detaching, debonding, and removing a first wing portion from the composite part to obtain a first exposed surface portion. The method further includes detaching, debonding, and removing a second wing portion from the composite part to obtain a second exposed surface portion. The method further includes reconditioning the first and second exposed surface portions to obtain first and second reconditioned surface portions, respectively, and applying first and second adhesive layers to the first and second reconditioned surface portions respectively. The method further includes bonding a metal work patch to the first and second adhesive layers.


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