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.
Patent No.:
Date of Patent:
Nov. 06, 2018
Filed:
May. 12, 2016
Applicant:
Airbus Operations Limited, Bristol, GB;
Inventors:
Jonathan Price, Bristol, GB;
Chetan Korya, Bristol, GB;
Peter Baker, Bristol, GB;
Stephen Williams, Bristol, GB;
Assignee:
AIRBUS OPERATIONS LIMITED, Bristol, GB;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/00 (2006.01); B29C 70/34 (2006.01); B29C 70/08 (2006.01); B29C 70/38 (2006.01); B32B 3/04 (2006.01); B32B 37/06 (2006.01); B32B 37/10 (2006.01); B64C 1/06 (2006.01); B64C 3/00 (2006.01); B64C 3/18 (2006.01); B64C 5/02 (2006.01); B32B 27/12 (2006.01); B29C 70/30 (2006.01); B29C 53/38 (2006.01); C08J 5/24 (2006.01); B32B 3/00 (2006.01); B32B 27/00 (2006.01); B32B 27/06 (2006.01); C08J 5/04 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B29C 70/34 (2013.01); B29C 53/382 (2013.01); B29C 70/08 (2013.01); B29C 70/30 (2013.01); B29C 70/382 (2013.01); B32B 3/00 (2013.01); B32B 3/04 (2013.01); B32B 27/00 (2013.01); B32B 27/06 (2013.01); B32B 27/12 (2013.01); B32B 37/06 (2013.01); B32B 37/10 (2013.01); B64C 1/06 (2013.01); B64C 3/00 (2013.01); B64C 3/18 (2013.01); B64C 5/02 (2013.01); C08J 5/042 (2013.01); C08J 5/24 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/3085 (2013.01); B32B 2305/00 (2013.01); B32B 2305/72 (2013.01); B32B 2307/50 (2013.01); B32B 2405/00 (2013.01); B32B 2597/00 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01); C08J 2300/22 (2013.01); C08J 2300/24 (2013.01); C08J 2363/00 (2013.01); Y02T 50/433 (2013.01);
Abstract
A method of manufacturing an aircraft component, the component comprising a pair of covers joined by a pair of spars. The covers and spars form a closed box structure with four corners, each corner providing a transition between one of the covers and one of the spars. The method comprises: laying up a laminated sheet of fiber plies; and after the sheet has been laid up, folding the sheet to form the four corners and then joining the sheet to itself to provide the closed box structure.