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:
Jul. 21, 2015

Filed:

Jan. 14, 2011
Applicants:

Christopher Payne, Bristol, GB;

Peter Griggs, Bristol, GB;

Antony C Peacock, Bristol, GB;

Raymond Bullock, Bristol, GB;

Glenn Watson, Bristol, GB;

Inventors:

Christopher Payne, Bristol, GB;

Peter Griggs, Bristol, GB;

Antony C Peacock, Bristol, GB;

Raymond Bullock, Bristol, GB;

Glenn Watson, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/00 (2006.01); B64C 3/20 (2006.01); B29C 70/08 (2006.01); B29C 70/86 (2006.01); B29C 70/88 (2006.01); B29D 99/00 (2010.01); B64C 3/26 (2006.01); B29K 105/04 (2006.01); B29L 31/30 (2006.01); B29L 31/60 (2006.01);
U.S. Cl.
CPC ...
B64C 3/20 (2013.01); B29C 70/086 (2013.01); B29C 70/088 (2013.01); B29C 70/865 (2013.01); B29C 70/887 (2013.01); B29D 99/0021 (2013.01); B64C 3/26 (2013.01); B29K 2105/043 (2013.01); B29L 2031/3085 (2013.01); B29L 2031/608 (2013.01); Y02T 50/433 (2013.01); Y10T 156/1074 (2015.01);
Abstract

An aircraft wing cover () comprising an integrally stiffened sandwich panel including first and second skins () sandwiching a core layer (), wherein at least one of the skins has a plurality of spanwise extending integral regions of increased thickness () accommodated by corresponding regions () of decreased thickness in the core. Also, a method of fabricating an aircraft wing cover, and a method of designing an aircraft wing.


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