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. 08, 2019

Filed:

Sep. 13, 2016
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Sylvain Tessier, Fassett, CA;

Richard Gingras, Montreal, CA;

Jacques Dionne, Saint-André-d'Argenteuil, CA;

Felix Bednar, Laval, CA;

Assignee:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 33/48 (2006.01); B29C 70/32 (2006.01); B29C 33/38 (2006.01); B29K 105/08 (2006.01); B29K 63/00 (2006.01); B29K 307/04 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B29C 33/485 (2013.01); B29C 33/3807 (2013.01); B29C 70/32 (2013.01); B29K 2063/00 (2013.01); B29K 2105/0872 (2013.01); B29K 2307/04 (2013.01); B29K 2863/00 (2013.01); B29K 2903/00 (2013.01); B29K 2907/04 (2013.01); B29K 2995/0013 (2013.01); B29K 2995/0015 (2013.01); B29L 2031/3082 (2013.01);
Abstract

A method of manufacturing a self-supporting, monolithic fuselage body, including engaging peripheral mandrel sections around at least one central mandrel section, placing uncured composite material on the mold surface, curing the composite material on the mold surface, and sliding the central mandrel section(s) out of engagement with the peripheral mandrel sections and disengaging the peripheral mandrel sections from the cured composite material without collapsing the mandrel sections. The peripheral mandrel sections each include a shape-retaining core of a thermally insulating material and an outer layer on an outer surface of the shape-retaining core. The outer layer has a coefficient of thermal expansion within the range of variation of that of the coefficient of thermal expansion of the composite material. A mandrel for layup and cure of a predetermined composite material in the manufacture of a monolithic fuselage is also discussed.


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