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:
Jan. 11, 2022

Filed:

Jul. 18, 2019
Applicant:

Airbus Operations S.l., Madrid, ES;

Inventors:
Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 5/10 (2017.01); B64C 1/26 (2006.01); B64C 3/26 (2006.01); B64C 5/02 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64F 5/10 (2017.01); B64C 1/26 (2013.01); B64C 3/26 (2013.01); B64C 5/02 (2013.01); B64C 2001/0072 (2013.01);
Abstract

A method for manufacturing a composite rear section assembly having a continuous skin solution including obtaining a vertical tail plane tooling that has intermediate tooling for tooling intermediate preforms of a vertical tail plane (), obtaining a fuselage barrel tooling (), (), () and () the fuselage barrel tooling having a cut-out (), (), () and longitudinal cavities (), (), () and (), attaching the vertical tail plane tooling to the fuselage barrel tooling by the cut-out of the fuselage barrel tooling, performing a composite skin lay-up () over the fuselage barrel tooling and the vertical tail plane tooling to obtain a continuous skin, curing the composite skin lay-up, the vertical tail plane tooling and the fuselage barrel tooling and demolding the tools to obtain the composite assembly with a continuous skin (), ().


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