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:
Aug. 30, 2011

Filed:

Oct. 12, 2009
Applicants:

Daniel W. Cushing, Covington, WA (US);

Eugene A. Jackson, Renton, WA (US);

Keith H. Novak, Shoreline, WA (US);

David N. Dunn, Marysville, WA (US);

Gregory R. Bell, Renton, WA (US);

Inventors:

Daniel W. Cushing, Covington, WA (US);

Eugene A. Jackson, Renton, WA (US);

Keith H. Novak, Shoreline, WA (US);

David N. Dunn, Marysville, WA (US);

Gregory R. Bell, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 65/18 (2006.01); B32B 27/04 (2006.01); B32B 27/12 (2006.01);
U.S. Cl.
CPC ...
Abstract

A translucent composite material that can be used in various airplane interior applications that allows sufficient light transmissivity while preferably meeting Federal Aviation Administration (FAA) flammability requirements for overhead materials in the cabin of a commercial aircraft. The material also meets FAA standards regarding vertical burn, smoke emissions tests, and toxic fume emissions tests. The composite material is formed by laminating long glass fibers and (PPSU) into a composite sheet under controlled heat and pressure. The composite sheet is then cut, bent or thermoformed to form the desired part. The parts formed are available for a wide variety of uses within the passenger cabin of a commercial aircraft. The long glass fibers may be unidirectional or weaved into a glass cloth like material. While preferably formed for airplane interior applications, these components may also be used in other aerospace or non-aerospace applications.


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