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David E Gideon

from Everett, WA
Age ~39
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Also known as:
David Eli Gideon
Related to:
Nsf Nrc GideonDanielle Lawson, 46Garrett AcostaChelsea Acosta, 41Ann Acosta, 73John Acosta, 77
Connected to:
Adam L Gideon, 36Andrea H Gideon, 51Anthony T Gideon, 58Bayta T Gideon, 49Ben Gideon, 77Blinda S Gideon, 60Cheryl D Gideon, 50Deanna G Gideon, 86Eileen O Gideon, 70Elizabeth A Gideon, 58

David Gideon Phones & Addresses

  • Everett, WA
  • Sedro Woolley, WA
  • 36708 146Th St SE, Sultan, WA 98294
  • Snohomish, WA

Resumes

Resumes

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David Gideon

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Location:
United States
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David Gideon

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Location:
United States
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David Gideon

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Location:
United States

Publications

Us Patents

Compression Molding Of Composite Material Quasi-Isotropic Flakes

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US Patent:
8529809, Sep 10, 2013
Filed:
Sep 22, 2011
Appl. No.:
13/240620
Inventors:
Aaron William Bartel - Mountlake Terrace WA, US
David Eric Gideon - Edmonds WA, US
Gregg Robert Bogucki - Saint Charles MO, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B29C 43/02
B27N 3/00
US Classification:
264115, 264126
Abstract:
Concepts and technologies are disclosed herein for compression molding of composite material quasi-isotropic flakes. According to some embodiments disclosed herein, a first layer formed from a composite component material and a second layer formed from a composite component material are consolidated together to form a quasi-isotropic panel. Composite material flakes having quasi-isotropic properties (“quasi-flakes”) are obtained from the quasi-isotropic panel. A compression mold is filled with the quasi-flakes, and heat is applied to the compression mold to form a part.

Molding Apparatus And Method

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US Patent:
7267542, Sep 11, 2007
Filed:
Nov 13, 2003
Appl. No.:
10/705873
Inventors:
Mark L. Younie - Snohomish WA, US
David E. Gideon - Seattle WA, US
Eugene A. Jackson - Renton WA, US
David A. Vaughan - Stanwood WA, US
Michael Kuntz - Snohomish WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B29C 33/00
US Classification:
425389, 4254051, 425456, 425470
Abstract:
An apparatus and method for making a mold or mold face includes a container having at least one opening. The apparatus also includes a flexible membrane that is retained to the container that extends across the opening of the container. The apparatus for making a mold further includes support media that is disposed within the container along with a vacuum valve that is connected to the container.

Molding Apparatus And Method

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US Patent:
20070290389, Dec 20, 2007
Filed:
Jul 23, 2007
Appl. No.:
11/878219
Inventors:
Mark Younie - Snohomish WA, US
David Gideon - Seattle WA, US
Eugene Jackson - Renton WA, US
David Vaughan - Stanwood WA, US
Michael Kuntz - Snohomish WA, US
International Classification:
B28B 1/08
US Classification:
264069000, 264101000, 264220000, 264511000
Abstract:
An apparatus and method for making a mold or mold face includes a container having at least one opening. The apparatus also includes a flexible membrane that is retained to the container that extends across the opening of the container. The apparatus for making a mold further includes support media that is disposed within the container along with a vacuum valve that is connected to the container.

Compression Molding Method And Reinforced Thermoplastic Parts Molded Thereby

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US Patent:
20110111172, May 12, 2011
Filed:
Nov 6, 2009
Appl. No.:
12/613842
Inventors:
David E. Gideon - Edmonds WA, US
International Classification:
B32B 3/10
B29C 43/18
C08G 73/04
C08G 75/02
C08G 75/20
C08G 65/00
C08K 3/04
US Classification:
428138, 264257, 524612, 524609, 524592
Abstract:
A fiber reinforced part is formed from a compression molded thermoplastic resin reinforced with individual fibers of differing lengths randomly oriented substantially throughout the part.

Method Of Creating Large Complex Composite Panels Using Co-Consolidation Of Thermoplastic Material Systems

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US Patent:
20180345591, Dec 6, 2018
Filed:
May 30, 2017
Appl. No.:
15/608245
Inventors:
- Chicago IL, US
Trevor Shane McCrea - Everett WA, US
David Eric Gideon - Edmonds WA, US
Bernhard Dopker - Bellevue WA, US
Paul Diep - Bothell WA, US
Julie Frances Murphy - Puyallup WA, US
Jordan Seth Erickson - Federal Way WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B29C 65/00
Abstract:
A method of constructing a large, complex composite panel involves connecting smaller compression molded thermoplastic subpanels, edge to edge using a thermoplastic co-consolidation method. The edges of adjacent subpanels are given complementary surface configurations. The surface configurations are overlapped and heat and pressure are applied to the overlapping surface constructions to co-consolidate the surface constructions in forming a large, composite panel of two or more subpanels.

Thermoplastic Composite Part And Method Of Fabrication

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US Patent:
20160339611, Nov 24, 2016
Filed:
May 22, 2015
Appl. No.:
14/720645
Inventors:
- Chicago IL, US
Wallace Chan - Bothell WA, US
Paul B. Diep - Bothell WA, US
Bernhard Dopker - Bellevue WA, US
David Gideon - Edmonds WA, US
International Classification:
B29C 43/18
Abstract:
An assembly of thermoplastic parts for forming a final composite part is presented where the assembly includes at least two prefabricated shells fabricated of thermoplastic. Each prefabricated shell has substantially the same shape as the final composite part and where the shapes of the prefabricated shells have dimensions that allow the prefabricated shells to be assembled into a nest for placement into a mold.

Fabrication Of Reinforced Thermoplastic Composite Parts

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US Patent:
20140183784, Jul 3, 2014
Filed:
Jan 2, 2013
Appl. No.:
13/732624
Inventors:
The Boeing Company - , US
David E. Gideon - Edmonds WA, US
Michael H. Larson - Mercer Island WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B29C 51/02
US Classification:
264258, 425508
Abstract:
A method of fabricating a reinforced thermoplastic composite part comprises moving a laminate of reinforcing fibers embedded in a thermoplastic matrix for sequential operations through a heating station and then a forming station. The heating station is used to soften the thermoplastic matrix in a portion of the laminate while the forming station is used to impart a geometry to a portion of the laminate whose thermoplastic matrix had just been softened. The softening and the forming are performed simultaneously on different portions of the laminate.
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David E Gideon from Everett, WA, age ~39 Get Report