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Jeffrey H Boy

from Wilmington, DE
Age ~68
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Also known as:
Jeffrey A Boy, Hermes Boy, Jffrey Boy
Phone and address:
2638 Sherwood Dr, Wilmington, DE 19808
(302) 994-4144
Related to:
Doris F Boy, 99Steven G Boy, 70George L Boy
Connected to:
Betty W Boy, 96Brandon D Boy, 38Harry H Boy, 97Jeremy J Boy, 38Joey Boy, 43Justin M Boy, 35Katherine L Boy, 32Megan E Boy, 35Ramiz Boy, 40Robert J Boy, 38

Jeffrey Boy Phones & Addresses

  • 2638 Sherwood Dr, Wilmington, DE 19808 (302) 994-4144
  • Middletown, NY
  • Bristol, VA
  • 1061 Teviot Rd, Schenectady, NY 12308
  • Edison, NJ
  • Champaign, IL

Resumes

Resumes

Jeffrey Boy Photo 1

Senior Engineer

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Location:
Mantua, NJ
Industry:
Aviation & Aerospace
Work:
Ge Aviation
Senior Product Manager
Ge
Senior Engineer
Education:
University of Illinois at Urbana - Champaign
Doctorates, Doctor of Philosophy, Engineering, Philosophy Rutgers University
Bachelors, Bachelor of Science, Engineering University of Illinois at Urbana - Champaign
Master of Science, Masters, Engineering
Skills:
Aerospace
Composites
Engineering
Continuous Improvement
Manufacturing
Engineering Management
Languages:
English
Portuguese
Jeffrey Boy Photo 2

Jeffrey Boy

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Location:
Wilmington, DE
Work:
Ge Aviation Jun 2001 - 2018
Senior Product Manager
Education:
Rutgers University

Publications

Us Patents

Method For Modifying Composite Articles

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US Patent:
20130062000, Mar 14, 2013
Filed:
Sep 9, 2011
Appl. No.:
13/228927
Inventors:
Paul Edward Gray - North East MD, US
Roger Lee Ken Matsumoto - Newark DE, US
Jeffrey H. Boy - Wilmington DE, US
Philip Harold Monaghan - Hockessin DE, US
Joseph Halada - Newark DE, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
B32B 37/06
B32B 37/14
B32B 38/10
B32B 37/02
B32B 38/16
US Classification:
156 735
Abstract:
In certain embodiments of the present disclosure a method for modifying a composite article is described. The method includes positioning a plug made from composite material at a site on the composite article. The method further includes rotating at least one of the plug and the article at a rate of speed sufficient to form an inertia bond between the plug and the site of the composite article. The plug and the site are engaged to effect an inertia bond therebetween.

Methods For Repairing A Turbine Airfoil Constructed From Cmc Material

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US Patent:
20130022471, Jan 24, 2013
Filed:
Jul 22, 2011
Appl. No.:
13/188755
Inventors:
Paul Edward Gray - North East MD, US
Roger Lee Ken Matsumoto - Newark DE, US
Jeffrey H. Boy - Wilmington DE, US
Philip Harold Monaghan - Hockessin DE, US
Joseph Halada - Newark DE, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
F01D 5/14
B05D 3/00
B05D 1/38
B05D 7/22
B05D 3/02
US Classification:
416229 R, 427140
Abstract:
Methods for repairing a turbine airfoil constructed from a CMC material are provided via filling a cavity located in the turbine airfoil with a ceramic paste (e.g., including a ceramic powder and a binder), heating the ceramic paste in the cavity to remove the binder, thereby forming a porous ceramic material, and adding a molten ceramic material to the porous ceramic material. The cavity can be defined in an airfoil of the turbine airfoil (e.g., on a tip or cap of the airfoil). Intermediates formed during the repair of a turbine airfoil are also provided. The intermediate can generally include an airfoil comprising a CMC material, a cavity defined in the airfoil, and a porous ceramic material filling the cavity.

Methods For Repairing A Turbine Airfoil Constructed From Cmc Material

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US Patent:
20140241900, Aug 28, 2014
Filed:
May 5, 2014
Appl. No.:
14/269240
Inventors:
- Schenectady NY, US
Paul Edward Gray - North East MD, US
Roger Lee Ken Matsumoto - Newark DE, US
Jeffrey H. Boy - Wilmington DE, US
Philip Harold Monaghan - Hockessin DE, US
Joseph Halada - Newark DE, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D 5/00
F01D 5/14
US Classification:
416241 B, 298891
Abstract:
Methods for repairing a turbine airfoil constructed from a CMC material are provided via filling a cavity located in the turbine airfoil with a ceramic paste (e.g., including a ceramic powder and a binder), heating the ceramic paste in the cavity to remove the binder, thereby forming a porous ceramic material, and adding a molten ceramic material to the porous ceramic material. The cavity can be defined in an airfoil of the turbine airfoil (e.g., on a tip or cap of the airfoil). Intermediates formed during the repair of a turbine airfoil are also provided. The intermediate can generally include an airfoil comprising a CMC material, a cavity defined in the airfoil, and a porous ceramic material filling the cavity.
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Jeffrey H Boy from Wilmington, DE, age ~68 Get Report