Search

Gregory L Fillman

from Pueblo, CO
Age ~71
Get Report
Also known as:
Gregory Lee Fillman, Greg L Fillman, Gregg Fillman
Phone and address:
2001 Bronquist Rd, Pueblo, CO 81005
(425) 271-9986
Related to:
Lucy M Cammisa, 97Mary Beth Howells, 68Tess A Fillman
Connected to:
Angela Fillman, 33Gary S Fillman, 80Joanne M Fillman, 64Kellie R Fillman, 65Matt W Fillman, 40Michael P Fillman, 61Mitchell A Fillman, 68Rebecca L Fillman, 47Stephanie A Fillman, 50Steve R Fillman, 53

Gregory Fillman Phones & Addresses

  • 2001 Bronquist Rd, Pueblo, CO 81005 (425) 271-9986
  • Seattle, WA

Work

Company: Fillman design 2008 Position: Consulting engineer

Education

School / High School: Renton Technical College 2010

Resumes

Resumes

Gregory Fillman Photo 1

Gregory Fillman Renton, WA

View page
Work:
Fillman Design

2008 to 2009
Consulting Engineer
Nova Composites Inc

1997 to 2008
Senior Engineer
PDS, Boeing Commercial Airplane Company

1996 to 1996
Contract Stress Analysis Engineer
Heath Tecna Aerospace Company
Kent, WA
1985 to 1995
Material & Process Engineer/Research & Development Engineer
The Boeing Company

1982 to 1985
Stress Analysis Engineer
Boeing Commercial Airplane Company

1979 to 1982
Aerodynamic Configuration Engineer
NASA Langley
Center, Kansas, US
1976 to 1979
Graduate Research Engineer

Publications

Us Patents

Attachment Fitting For Composite Material Structures

View page
US Patent:
6379763, Apr 30, 2002
Filed:
Aug 19, 1999
Appl. No.:
09/378563
Inventors:
Gregory L. Fillman - Renton WA
Assignee:
Nova Composites, Inc. - Mukilteo WA
International Classification:
B32B 512
US Classification:
428 369, 428 363, 428 3691, 138121, 138122, 138125, 138153
Abstract:
A load bearing attachment fitting for a composite material structure. The fitting includes an elongate body having a plurality of undulations formed along its longitudinal sides. The undulations engage the fibers in the fiber-resin matrix so as to transmit loads from the fitting into the body of the structure. To form the connection between the fitting and the composite material structure, longitudinal strips of fiber-resin tape are laid over the fitting and an adjacent form which defines the body of the structure. Crosswise fibers are then wound over the longitudinal tape to force and hold the longitudinal fibers in conformity with the undulations along the fitting, so that the longitudinal fibers transmit loads from the fitting into the composite material structure. A fluidizable form may be used to form the body of the structure, and after curing the forms may be removed by washing this out through a threaded bore in the attachment fitting. The threaded bore then provides a mounting point for attaching the assembly to other structures in load bearing engagement.

Fitting Assembly For A Composite Structure

View page
US Patent:
51042517, Apr 14, 1992
Filed:
Apr 17, 1990
Appl. No.:
7/510013
Inventors:
Gregory L. Fillman - Renton WA
Richard W. Randall - Seattle WA
Assignee:
Heath Tecna Aerospace Company - Kent WA
International Classification:
F16B 708
US Classification:
403191
Abstract:
An apparatus and method for securing fittings to composite structures such as those composites formed out of resin-embedded fibers is disclosed. The invention includes the use of support structures wrapped around the fittings such that the support prevents the fitting from movement when a compression load is applied thereto. The support serves to transfer the force of the compression load into the entire body of the composite structure so that the force will be absorbed by the structure. In one embodiment of the invention, the support structure comprises a composite fiber tow formed of high tensile strength fibers impregnated with a matrix material. The composite fiber tow is fibers wrapped around the fittings to form suspension strands. As the matrix material cures the composite fiber stiffens to hold the fitting in place against the composite structure.
Control profile
Gregory L Fillman from Pueblo, CO, age ~71 Get Report