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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.:

US 9932123 B1

PDFFull Text
Date of Patent:
Apr. 03, 2018

Filed:

Jun. 07, 2012

Monocoque helicopter fuselage with integral tail boom

Applicants:

Peter Maloney, Auckland, NZ;

Nina Heatley, Auckland, NZ;

Inventors:

Peter Maloney, Auckland, NZ;

Nina Heatley, Auckland, NZ;

Assignee:

COMPOSITE HELICOPTERS INTERNATIONAL HOLDINGS LTD, Albany, NZ;

Attorney:

Morrison & Foerster LLP

Primary Examiner:

Tien Q Dinh

Assistant Examiner:

Michael A Fabula

Int. Cl.
CPC ...
B64C 1/00 (2006.01); B64D 37/04 (2006.01); B60N 2/42 (2006.01); B60N 2/427 (2006.01); B60N 2/68 (2006.01); B64C 27/04 (2006.01); B64C 27/82 (2006.01); B64D 11/06 (2006.01); B29C 65/52 (2006.01); B29C 65/60 (2006.01); B29C 65/00 (2006.01); B29C 70/44 (2006.01); B29C 65/48 (2006.01); B29L 31/30 (2006.01); B29L 31/00 (2006.01);
U.S. Cl.
CPC ...
B64D 37/04 (2013.01); B29C 65/483 (2013.01); B29C 65/52 (2013.01); B29C 65/605 (2013.01); B29C 66/532 (2013.01); B29C 66/54 (2013.01); B29C 66/543 (2013.01); B29C 66/545 (2013.01); B29C 66/721 (2013.01); B29C 66/72141 (2013.01); B29C 70/443 (2013.01); B60N 2/4242 (2013.01); B60N 2/42709 (2013.01); B60N 2/686 (2013.01); B64C 1/00 (2013.01); B64C 27/04 (2013.01); B64C 27/82 (2013.01); B64D 11/0619 (2014.12); B64D 11/0689 (2013.01); B29C 66/61 (2013.01); B29C 66/71 (2013.01); B29C 66/727 (2013.01); B29C 66/7212 (2013.01); B29L 2031/3082 (2013.01); B29L 2031/3088 (2013.01); B29L 2031/771 (2013.01); B64C 2027/8254 (2013.01); Y02T 50/433 (2013.01);
Abstract

A composite structure forming a load bearing composite shell for a helicopter, with a shell which defines the exterior of a fuselage and includes a central fuselage section and tail boom, a fuselage which is adapted house an engine or drive train, a layered composite crashworthy seat and support structure and a fastening and a method of fastening by providing an adhesive between two layers which is allowed to flow through opposing holes in the layers to provide a chemical and mechanical attachment between the layers.

Find Patent Forward Citations

Maloney, Peter. (2018). Monocoque helicopter fuselage with integral tail boom (U.S. Patent No. 9932123). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9932123

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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