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. 24, 2015

Filed:

Mar. 04, 2008
Applicants:

Jonathan Meyer, Bristol, GB;

Daniel Johns, Bristol, GB;

Andrew Henstridge, Bristol, GB;

Inventors:

Jonathan Meyer, Bristol, GB;

Daniel Johns, Bristol, GB;

Andrew Henstridge, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B22F 3/105 (2006.01); B22F 3/24 (2006.01); B22F 7/04 (2006.01); B29C 65/00 (2006.01); B29C 65/64 (2006.01); B23K 15/00 (2006.01); B23K 26/34 (2014.01); C09J 5/02 (2006.01); F16B 5/07 (2006.01); B23K 26/32 (2014.01); B22F 5/00 (2006.01);
U.S. Cl.
CPC ...
B22F 3/1055 (2013.01); B22F 3/24 (2013.01); B22F 5/00 (2013.01); B22F 7/04 (2013.01); B23K 15/0086 (2013.01); B23K 26/322 (2013.01); B23K 26/3206 (2013.01); B23K 26/328 (2013.01); B23K 26/3246 (2013.01); B23K 26/34 (2013.01); B29C 65/64 (2013.01); B29C 66/30321 (2013.01); B29C 66/742 (2013.01); C09J 5/02 (2013.01); F16B 5/07 (2013.01); B22F 2005/005 (2013.01); Y10T 428/24008 (2015.01); Y10T 428/24521 (2015.01);
Abstract

A method of preparing a component () to be joined to another component (). The method comprises growing an array of projections () on a bond region of the component () in a series of layers, each layer being grown by directing energy and/or material from a head to selected parts of the bond region. The joint may be used to join a pair of structural components, for instance in an aerospace application. For instance the joint may be used to join a reinforcing plate, floating rib foot, or stringer to a panel such as a wing or fuselage cover. Alternatively the joint may be used to join adjacent layers in a laminate structure.


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