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Jerald C Cammer

from Sauquoit, NY
Age ~64
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Also known as:
Jerald J Cammer, Jernca C Cammer, Jerald C Crammer, Gerald C Cammer, Jerry Cammer
Phone and address:
9100 Paris Hill Rd, Paris, NY 13456
(315) 737-0197
Related to:
Joseph J CammerJarrod CammerJack L Adkisson, 76Linda R Adkisson, 73Janet A Adkisson, 53Jodi K Cammer, 60James A Cammer, 67Carol C Cammer, 64Stephen P Adkisson, 54
Connected to:
David S Cammer, 33Marc C Cammer, 60Maureen K Cammer, 60Lori Cammett, 50Mena A Cammett, 37Richard N Cammett, 36Arnold Cammeyer, 83Michael A Cammeyer, 46Robert Cammidge, 48Crystal S Cammile, 35

Jerald Cammer Phones & Addresses

  • 9100 Paris Hill Rd, Sauquoit, NY 13456 (315) 737-0197
  • Paris, NY
  • 104 Utica St, Clinton, NY 13323 (315) 853-2445
  • Georgetown, DE

Work

Company: Tect corporation 1979 to 2014 Position: Chief engineer

Education

Degree: Associate degree or higher

Skills

Aerospace • Engineering Management • Engineering • Lean Manufacturing • Manufacturing • Manufacturing Engineering • Process Improvement • Root Cause Analysis • Six Sigma • Value Stream Mapping • Continuous Improvement • Process Engineering • Product Development • Project Management

Industries

Aviation & Aerospace

Resumes

Resumes

Jerald Cammer Photo 1

Jerald Cammer

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Location:
9100 Paris Hill Rd, Sauquoit, NY 13456
Industry:
Aviation & Aerospace
Work:
Tect Corporation 1979 - 2014
Chief Engineer
Skills:
Aerospace
Engineering Management
Engineering
Lean Manufacturing
Manufacturing
Manufacturing Engineering
Process Improvement
Root Cause Analysis
Six Sigma
Value Stream Mapping
Continuous Improvement
Process Engineering
Product Development
Project Management

Publications

Us Patents

Method Of Manufacturing A Turbine Fan Blade

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US Patent:
8256118, Sep 4, 2012
Filed:
Sep 27, 2010
Appl. No.:
12/890806
Inventors:
Jerald C. Cammer - Sauquoit NY, US
Assignee:
Turbine Engine Components Technologies Corporation - Thomasville GA
International Classification:
B21D 53/78
US Classification:
298897, 29557
Abstract:
A metal leading edge of a turbine fan blade is manufactured by cutting and shaping an elongated metal part. The metal part has front and rear edges extending lengthwise of the part, and has a generally wedge-shaped transverse cross-section with opposite sides diverging from the front edge toward the rear edge. A cavity is cut inward from the rear edge toward the front edge. This provides the part with a generally V-shaped transverse cross-section having opposite side walls diverging rearwardly from the front edge. A mandrel is inserted into the cavity, and the side walls of the V-shaped part are deflected toward each other to constrict the cavity into the configuration of the mandrel. The part is then mounted as a metal leading edge by inserting a turbine fan blade component into the constricted cavity and fastening the part to the component.

Method Of Manufacturing A Turbine Fan Blade

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US Patent:
20090165299, Jul 2, 2009
Filed:
Dec 31, 2007
Appl. No.:
11/967484
Inventors:
Jerald C. Cammer - Sauquoit NY, US
International Classification:
B23P 15/04
US Classification:
298897
Abstract:
A metal leading edge of a turbine fan blade is manufactured by cutting and shaping an elongated metal part. The metal part has front and rear edges extending lengthwise of the part, and has a generally wedge-shaped transverse cross-section with opposite sides diverging from the front edge toward the rear edge. A cavity is cut inward from the rear edge toward the front edge. This provides the part with a generally V-shaped transverse cross-section having opposite side walls diverging rearwardly from the front edge. A mandrel is inserted into the cavity, and the side walls of the V-shaped part are deflected toward each other to constrict the cavity into the configuration of the mandrel. The part is then mounted as a metal leading edge by inserting a turbine fan blade component into the constricted cavity and fastening the part to the component.
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Jerald C Cammer from Sauquoit, NY, age ~64 Get Report