Daniel T Cushing, Age 509300 S Redwood Rd APT 1312, Taylorsville, UT 84088

8007620, Aug 30, 2011

Oct 12, 2009

12/577618

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

The Boeing Company - Chicago IL

B29C 65/18
B32B 27/04
B32B 27/12

156245, 1563082, 156311, 156312

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.

8043704, Oct 25, 2011

Apr 8, 2005

11/102401

Craig L. Berry - Sammamish WA, US
Daniel W. Cushing - Covington WA, US
Eugene A. Jackson - Renton WA, US

The Boeing Company - Chicago IL

B32B 27/36

428412, 4284111, 244117 R, 244133

A layered material for use in transparent, flame resistant components couples a thin, fire resistant outer polymeric film to a thicker, transparent inner polymeric material. The resultant transparent layered material meets FAA flammability requirements for OSU heat release, has excellent solvent resistance and cleanability, is scratch resistant, and is transparent enough for use in interior applications in the aerospace industry. The layered material is formed via a co-extrusion or co-lamination process.

2005014, Jun 30, 2005

Dec 24, 2003

10/707612

Daniel Cushing - Covington WA, US
Eugene Jackson - Renton WA, US
Keith Novak - Shoreline WA, US
David Dunn - Marysville WA, US
Gregory Bell - Renton WA, US

THE BOEING COMPANY - Chicago IL

B32B017/04

442136000, 442180000, 442239000, 442301000, 427164000, 427372200, 427374100

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.

2012015, Jun 21, 2012

Mar 15, 2011

13/048704

Daniel W. Cushing - Covington WA, US
Eugene A. Jackson - Deer Park WA, US
Keith H. Novak - Tukwila WA, US
David N. Dunn - Marysville WA, US
Gregory R. Bell - Renton WA, US

THE BOEING COMPANY - Chicago IL

B32B 3/00
B32B 7/02
B32B 5/26
D04H 13/00

4281951, 442416, 428212, 442391

A translucent composite material comprises a substrate and a plurality of glass fibers embedded within the substrate. The substrate may comprise a substantially continuous nonwoven, non-fabric, translucent thermoplastic polyphenylsulfone substrate. The plurality of glass fibers may substantially span across a length of the substrate and may have an orientation, a fiber thickness, and a fiber area density selected to provide the translucent composite material with a strength, a flame-resistance, and a light transmissivity.