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:
Apr. 07, 2015

Filed:

Jun. 19, 2009
Applicants:

Robert Clive Fews, Beaconsfield, CA;

Bijan Derisi, Montreal, CA;

Suong Van Hoa, Brossard, CA;

Mehdi Hojjati, Dollard-des-Ormeaux, CA;

Inventors:

Robert Clive Fews, Beaconsfield, CA;

Bijan Derisi, Montreal, CA;

Suong Van Hoa, Brossard, CA;

Mehdi Hojjati, Dollard-des-Ormeaux, CA;

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/52 (2006.01); B64C 25/32 (2006.01);
U.S. Cl.
CPC ...
B64C 25/52 (2013.01); B64C 2025/325 (2013.01);
Abstract

A fiber-reinforced, organic matrix, composite structural member includes a plurality of layers of fiber-reinforced, organic matrix, composite material in which adjacent layers are bonded to one another, wherein the structural member exhibits a non-linear stress-strain response when mechanically loaded to failure. A helicopter landing gear includes a pair of skids and one or more cross members extending between the pair of skids. The one or more cross members includes a plurality of layers of fiber-reinforced, organic matrix, composite material in which adjacent layers are bonded to one another, wherein the cross members exhibit non-linear stress-strain responses when mechanically loaded to failure.


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