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Michael W Evens

from Renton, WA
Age ~61
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Also known as:
Mike W Evens, Mike Walter Evens, Michaelw Evens
Phone and address:
11621 19Th Ave SW, Seattle, WA 98146
(206) 244-5782
Related to:
Lieselotte M Mevens, 85Connie P Britt, 57Ronnie PerkinsJanis PerkinsBarbara Morgan, 77Archie Morgan, 41
Connected to:
Alice R Evens, 98Anita L Evens, 46Ann M Evens, 61Aubrey S Evens, 69Bob P Evens, 92Daniel L Evens, 56Joanne P Evens, 94Joe Evens, 39Kirsten Evens, 56Malarie S Evens, 38

Michael Evens Phones & Addresses

  • 11621 19Th Ave SW, Seattle, WA 98146 (206) 244-5782
  • 11661 19Th Ave SW, Seattle, WA 98146 (206) 244-5782
  • Renton, WA
  • Clements, MD
  • Cambridge, MA
  • Mill Creek, WA
  • 645 SW 149Th St, Burien, WA 98166

Work

Position: Clerical/White Collar

Education

Degree: High school graduate or higher

Professional Records

License Records

Michael C Evens

License #:
E003379 - Expired
Category:
Emergency medical services
Issued Date:
Feb 26, 2008
Expiration Date:
Feb 28, 2010
Type:
Los Angeles County EMS Agency

Business Records

Name / Title
Company / Classification
Phones & Addresses
Michael W Evens
President,Director
COMPOSITES INTERNATIONAL, INC
11621 19 Ave SW, Seattle, WA 98146

Publications

Us Patents

Gap Mapping For Fitting Composite Doublers

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US Patent:
8324911, Dec 4, 2012
Filed:
Dec 17, 2007
Appl. No.:
11/957767
Inventors:
Gary E. Georgeson - Federal Way WA, US
Michael W. Evens - Burien WA, US
Michael D. Fogarty - Auburn WA, US
Morteza Safai - Seattle WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G01R 27/26
US Classification:
324662
Abstract:
A non-conductive composite doubler is fabricated for application to an electrically conductive surface of a structure by: forming the composite doubler; placing an array of capacitive gap thickness sensors between the doubler and the structure surface; measuring the gap thickness between the doubler and the structure surface in a plurality of areas over the surface of the structure; using the gap thickness measurements to shape a layer of adhesive to essentially match the contour of the structure surface; and, applying the layer of adhesive to the doubler.

Method Of Repairing A Composite Structure

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US Patent:
8545650, Oct 1, 2013
Filed:
Dec 8, 2009
Appl. No.:
12/633753
Inventors:
Michael W. Evens - Burien WA, US
Megan N. Watson - Kent WA, US
Mary H. Vargas - Woodinville WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B32B 41/00
US Classification:
156 64, 156350, 156368, 156378, 156379
Abstract:
A surrogate patch assembly for a rework area of a structure comprises a surrogate patch body which may be formed of a material for drawing moisture from the rework area. The patch assembly may include a sensor mounted to the surrogate patch body. The sensor may comprise a thermal sensor for sensing the temperature of the rework area and the surrogate patch body. The sensor may comprise a moisture sensor for sensing moisture drawn into the surrogate patch body.

Fitting Doublers Using Gap Mapping

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US Patent:
20090154775, Jun 18, 2009
Filed:
Jul 30, 2008
Appl. No.:
12/183045
Inventors:
Scott W. Lea - Renton WA, US
Gary E. Georgeson - Federal Way WA, US
Michael D. Fogarty - Auburn WA, US
Michael W. Evens - Burien WA, US
Jeffrey M. Hansen - Newton WA, US
International Classification:
G06K 9/00
US Classification:
382108
Abstract:
A method and apparatus are used to fit a metallic or composite doubler on an uneven surface. A three dimensional digital map of the gap between the doubler and the uneven surface is generated by digitally scanning the uneven surface. The digital map is then used to fabricate a stack of adhesive plies tailored to substantially fill the gap between the doubler and the uneven surface.

Bond Line Control Process

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US Patent:
20100143722, Jun 10, 2010
Filed:
Dec 5, 2008
Appl. No.:
12/328903
Inventors:
David M. Anderson - Sammamish WA, US
Michael W. Evens - Burien WA, US
International Classification:
B32B 5/02
B32B 37/12
US Classification:
4284111, 156300
Abstract:
A method and apparatus for bonding parts. An adhesive and a plurality of beads may be applied onto a first surface of a first part to form a layer of adhesive and beads. The first surface of the first part with the layer of adhesive and beads may be placed in contact with a second surface of a second part to form a structure, wherein the structure may be cured.

Bonded Patches With Bond Line Control

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US Patent:
20100276065, Nov 4, 2010
Filed:
Nov 6, 2009
Appl. No.:
12/613810
Inventors:
Steve Blanchard - Issaquah WA, US
Aydin Akdeniz - Langley WA, US
John Spalding - Renton WA, US
David M. Anderson - Sammamish WA, US
Michael W. Evens - Burien WA, US
International Classification:
B32B 37/18
B32B 7/12
US Classification:
156 94, 428343
Abstract:
A patch is used to rework an area of a structure. The patch is bonded to the structure by a layer of adhesive. A spacer placed between the patch and the structure is used to control the thickness of the adhesive and/or a bondline.

Systems And Methods For On-Aircraft Composite Repair Using Double Vacuum Debulking

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US Patent:
20120080135, Apr 5, 2012
Filed:
Sep 30, 2010
Appl. No.:
12/894691
Inventors:
Michael W. Evens - Burien WA, US
Karl Edward Nelson - Shoeline WA, US
James D. Chanes - Auburn WA, US
Joel P. Baldwin - Seattle WA, US
Paul S. Rutherford - Maple Valley WA, US
Assignee:
THE BOEING COMPANY - Irvine CA
International Classification:
B32B 43/00
US Classification:
156 94, 156382
Abstract:
An in-situ double vacuum debulk (DVD) composite repair system designed to produce partially or fully cured autoclave-quality hot-bond composite repairs on contoured structures. The system provides vacuum pressure for hot bond repairs to be performed on flat and contoured structures using one set-up capable of debulking (partially curing) and then fully curing composite repairs on composite and metallic aircraft structures. The use of in-situ DVD also eliminates handling of the patch/adhesive when transferring from an off-aircraft DVD chamber to the repair site on the aircraft. This can increase the probability of successful repairs because the possibility of contaminating and misaligning the adhesive and repair patch are eliminated.

Methods And Apparatus For Void-Free Debulking Of Adhesive Bonded Joints

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US Patent:
20120125534, May 24, 2012
Filed:
Nov 24, 2010
Appl. No.:
12/953532
Inventors:
Megan Nicole Watson - Kent WA, US
Joseph L. Hafenrichter - Seattle WA, US
Mary H. Vargas - Woodinville WA, US
Michael W. Evens - Burien WA, US
Assignee:
THE BOEING COMPANY - Irvine CA
International Classification:
B29C 65/48
B32B 37/00
US Classification:
156285, 156580, 1565831
Abstract:
Methods and apparatus for fabricating adhesive bonded joints while minimizing the voids and/or porosity found in the cured bondline. In accordance with various embodiments, the apparatus comprises an evacuation chamber combined with a pressure inducing device to produce bonded joints that are both void free and thoroughly compacted. The surfaces to be bonded are continuously evacuated throughout the bonding process (pre-mating, mating, debulking and cure). Continuous evacuation is provided via standard vacuum, while the induced pressure can be pneumatically or mechanically provided.

Apparatus For Void-Free Debulking Of Adhesive Bonded Joints

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US Patent:
20120298311, Nov 29, 2012
Filed:
Jul 25, 2012
Appl. No.:
13/557269
Inventors:
Megan Nicole Watson - Kent WA, US
Joseph L. Hafenrichter - Seattle WA, US
Mary H. Vargas - Woodinville WA, US
Michael W. Evens - Burien WA, US
Assignee:
THE BOEING COMPANY - Seal Beach CA
International Classification:
B30B 15/34
B30B 15/00
US Classification:
1565831, 156580
Abstract:
Methods and apparatus for fabricating adhesive bonded joints while minimizing the voids and/or porosity found in the cured bondline. In accordance with various embodiments, the apparatus comprises an evacuation chamber combined with a pressure inducing device to produce bonded joints that are both void free and thoroughly compacted. The surfaces to be bonded are continuously evacuated throughout the bonding process (pre-mating, mating, debulking and cure). Continuous evacuation is provided via standard vacuum, while the induced pressure can be pneumatically or mechanically provided.
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Michael W Evens from Renton, WA, age ~61 Get Report