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David Carbery Phones & Addresses

  • 27731 99Th Ave SW, Vashon, WA 98070 (206) 463-2553
  • 22509 Deppman Rd, Vashon, WA 98070 (206) 463-2553
  • McCleary, WA
  • Ann Arbor, MI

Resumes

Resumes

David Carbery Photo 1

Royal Navy Mine Warfare And Survey

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Location:
Vashon, WA
Industry:
Military
Work:
Royal Navy
Royal Navy Mine Warfare and Survey
Education:
Northumbria University
David Carbery Photo 2

David Carbery

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Location:
Stevensville, MI
Industry:
Aviation & Aerospace
Work:
Boeing
Retired

Environmental Dynamics International 1975 - 1986
Engineer
Education:
University of Michigan 1973 - 1986
Lakeshore High School
University of Michigan
Skills:
Composites

Publications

Us Patents

Composite Material Placement Method And System

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US Patent:
7867352, Jan 11, 2011
Filed:
Feb 13, 2006
Appl. No.:
11/352274
Inventors:
Brice A. Johnson - Federal Way WA, US
David J. Carbery - Vashon WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B32B 38/04
US Classification:
156250, 156256, 156193
Abstract:
To apply a course on a layup mold, a ply boundary that defines a ply area on the layup mold is determined and a tape of composite material is applied on the ply area at an oblique angle relative to the ply boundary. In addition, a leading edge of the tape is butt cut and the leading edge, and the ply boundary essentially converge. Furthermore, a trailing edge is generated. The trailing edge is a butt cut and the trailing edge and the ply boundary essentially converge.

Composite Material Placement Method And System

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US Patent:
20110073238, Mar 31, 2011
Filed:
Dec 6, 2010
Appl. No.:
12/961066
Inventors:
Brice A. Johnson - Federal Way WA, US
David J. Carbery - Vashon WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B32B 37/02
US Classification:
156 60, 156538
Abstract:
To apply a course on a layup mold, a ply boundary that defines a ply area on the layup mold is determined and a tape of composite material is applied on the ply area at an oblique angle relative to the ply boundary. In addition, a leading edge of the tape is butt cut and the leading edge, and the ply boundary essentially converge. Furthermore, a trailing edge is generated. The trailing edge is a butt cut and the trailing edge and the ply boundary essentially converge.

Lightweight Honeycomb Panel Structure

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US Patent:
54458617, Aug 29, 1995
Filed:
Sep 4, 1992
Appl. No.:
7/940501
Inventors:
Jefferson F. Newton - Seattle WA
Thomas D. Martin - Bellevue WA
Willard N. Westre - Bellevue WA
David J. Carbery - Vashon Island WA
Roy Ikegami - Seattle WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B32B 312
US Classification:
428116
Abstract:
Disclosed is a lightweight honeycomb structure that comprises a top panel (34) and bottom panel (32) and a large-celled honeycomb layer (36) disposed between the top and bottom panels. The honeycomb panel structure according to the present invention can be used in such applications as a sound-absorbing payload shroud for launch vehicles, flooring and walls in aerospace applications, aircraft wings and in structures that will be exposed to high heat. Additionally, a method of making a honeycomb structure of thermoplastic material is disclosed.
David John Carbery from Vashon, WA, age ~70 Get Report