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. 08, 2022

Filed:

Jun. 10, 2019
Applicant:

B/e Aerospace, Inc., Winston Salem, NC (US);

Inventors:

Peter J. L. Burd, Burry Port, GB;

Venkata P. S. Neti, Milton Keynes, GB;

Nicholas J. W. Pearce, Mukilteo, WA (US);

Hayley L. Campbell, Bedfordshire, GB;

Assignee:

B/E Aerospace, Inc., Winston-Salem, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 11/04 (2006.01); B32B 3/12 (2006.01); B32B 5/02 (2006.01); B32B 5/24 (2006.01); B32B 5/26 (2006.01); B64D 11/00 (2006.01);
U.S. Cl.
CPC ...
B64D 11/04 (2013.01); B32B 3/12 (2013.01); B32B 5/02 (2013.01); B32B 5/245 (2013.01); B32B 5/26 (2013.01); B32B 2262/106 (2013.01); B32B 2605/18 (2013.01); B64D 2011/0046 (2013.01);
Abstract

An ultra light weight aircraft composite galley architecture system and method comprises composite construction of a partially molded aircraft monument structure based on embedded load bearing hoops and beams used in conjunction with pre formed composite flat panel construction. An upper L shaped structural section mates with a lower inverted L shaped structural section forming a structure upon which additional panels are joined to form the complete composite galley. This system and method of construction produces a high strength aircraft monument capable of maintaining aircraft structural flight and crash load requirements without external monument extrusions for support. This galley architecture system and method of construction creates an aircraft monument with desirable reduction in weight with no loss of required structural strength.


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