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:
Feb. 14, 2017

Filed:

Jul. 24, 2013
Applicant:

Rohr, Inc., Chula Vista, CA (US);

Inventors:

Michael J. Layland, Bonita, CA (US);

Norman J. James, San Diego, CA (US);

David Forsey, Poway, CA (US);

Christian Soria, La Mesa, CA (US);

Assignee:

Rohr, Inc., Chula Vista, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16M 13/00 (2006.01); F16M 1/00 (2006.01); B64D 27/26 (2006.01); B64D 29/06 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 29/06 (2013.01);
Abstract

A hybrid beam for support of a nacelle panel of a jet engine is disclosed. The beam is comprised of a first longitudinal composite panel and a second longitudinal composite panel, wherein the first longitudinal composite panel is integrally affixed to the second longitudinal composite panel along a longitudinal edge. The composite panels form a composite beam structure that is substantially open with a cross-section that is generally 'L-shaped'. A plurality of hinge stations are affixed to a first side of the first longitudinal composite panel and at least one track guide is disposed on a second side of the first longitudinal composite panel. The track guides receive a head portion of a slider that is fixed to the translating jet engine nacelle panel. Each hinge station further comprises a bushing for defining a center of rotation for the jet engine nacelle panel relative to the beam.


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