Ganesh Anantharaman
age ~56
from East Hartford, CT
- Also known as:
-
- Ga Anantharaman
- Ganesh N
- H Anantharaman
- Phone and address:
-
160 Ridgewood Rd, Hartford, CT 06118
8605683698
Ganesh Anantharaman Phones & Addresses
- 160 Ridgewood Rd, East Hartford, CT 06118 • 8605683698
- 200 Nutmeg Ln, East Hartford, CT 06118 • 8605683698
- 540 4Th St, Cookeville, TN 38501 • 9315208114
- 348 Firwood Dr, Dayton, OH 45419
Work
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Company:Pratt & whitneyAug 2018
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Position:Senior project manager
Education
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Degree:Master of Business Administration, Masters
-
School / High School:Rensselaer Polytechnic Institute at Hartford2001 to 2003
Skills
Cross Functional Team Leadership • Engineering • Aerospace • Earned Value Management • Engineering Management • Root Cause Analysis • Six Sigma • Project Planning • Continuous Improvement • Systems Engineering • Value Stream Mapping • Program Management • Aviation • Leadership • Lean Manufacturing • Ms Project • Product Development • Export Controls • Military • Propulsion • Aircraft • Project Engineering • Unigraphics • Itar • Process Improvement • Evms • Process Engineering • Pmp • Design of Experiments
Industries
Aviation & Aerospace
Resumes
Senior Project Manager
view sourceLocation:
Hartford, CT
Industry:
Aviation & Aerospace
Work:
Pratt & Whitney
Senior Project Manager
Pratt & Whitney May 2017 - Jul 2018
Deputy Cipt Manager, Ngpf 17K Program - Pratt and Whitney
Pratt & Whitney Oct 2009 - Dec 2011
Model Manager - Advance Engine Program
Pratt & Whitney Oct 2009 - Dec 2011
Program Manager, Ngpf Program - Global Services Engineering at Pratt and Whitney
Pratt & Whitney Jan 2008 - Oct 2009
Repair Development Engineer - Project Military Engines
Senior Project Manager
Pratt & Whitney May 2017 - Jul 2018
Deputy Cipt Manager, Ngpf 17K Program - Pratt and Whitney
Pratt & Whitney Oct 2009 - Dec 2011
Model Manager - Advance Engine Program
Pratt & Whitney Oct 2009 - Dec 2011
Program Manager, Ngpf Program - Global Services Engineering at Pratt and Whitney
Pratt & Whitney Jan 2008 - Oct 2009
Repair Development Engineer - Project Military Engines
Education:
Rensselaer Polytechnic Institute at Hartford 2001 - 2003
Master of Business Administration, Masters University of Dayton 1994 - 1996
Master of Science, Masters, Engineering Government College of Technology 1985 - 1989
Bachelors, Mechanical Engineering Carmel Garden Matriculation Hs 1983 - 1985
Master of Business Administration, Masters University of Dayton 1994 - 1996
Master of Science, Masters, Engineering Government College of Technology 1985 - 1989
Bachelors, Mechanical Engineering Carmel Garden Matriculation Hs 1983 - 1985
Skills:
Cross Functional Team Leadership
Engineering
Aerospace
Earned Value Management
Engineering Management
Root Cause Analysis
Six Sigma
Project Planning
Continuous Improvement
Systems Engineering
Value Stream Mapping
Program Management
Aviation
Leadership
Lean Manufacturing
Ms Project
Product Development
Export Controls
Military
Propulsion
Aircraft
Project Engineering
Unigraphics
Itar
Process Improvement
Evms
Process Engineering
Pmp
Design of Experiments
Engineering
Aerospace
Earned Value Management
Engineering Management
Root Cause Analysis
Six Sigma
Project Planning
Continuous Improvement
Systems Engineering
Value Stream Mapping
Program Management
Aviation
Leadership
Lean Manufacturing
Ms Project
Product Development
Export Controls
Military
Propulsion
Aircraft
Project Engineering
Unigraphics
Itar
Process Improvement
Evms
Process Engineering
Pmp
Design of Experiments
Us Patents
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Replacement Of Part Of Engine Case With Dissimilar Material
view source -
US Patent:8245399, Aug 21, 2012
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Filed:Jan 20, 2009
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Appl. No.:12/356321
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Inventors:Ganesh Anantharaman - East Hartford CT, US
David J. Bartholic - Avon CT, US -
Assignee:United Technologies Corporation - Hartford CT
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International Classification:B23P 6/00
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US Classification:298891, 2940203
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Abstract:A method of repairing a case for a gas turbine engine includes removing a first portion of the case from a second portion of the case and metallurgically joining a replacement material to the second portion of the case to form a repaired case. The first portion of the case includes a connection flange having a plurality of bolt holes formed therein. The replacement material has a different coefficient of thermal expansion than a parent material of the second portion of the case.
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Control Of Case Wall Growth During Repair And Method
view source -
US Patent:8281487, Oct 9, 2012
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Filed:Jan 20, 2009
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Appl. No.:12/356341
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Inventors:Ganesh Anantharaman - East Hartford CT, US
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Assignee:United Technologies Corporation - Hartford CT
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International Classification:B23P 6/00
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US Classification:298891, 2940219
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Abstract:A method for repairing a gas turbine engine component includes identifying a distorted feature located in a first portion of the component, identifying a second portion of the component that behaves as at least one of a heat sink or a stiffener, removing the second portion of the component from the first portion, cold working the first portion of the component to repair the distorted feature, heat treating the first portion of the component, and metallurgically joining the first portion of the component to the second portion of the component.
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Repair Of Case Flange With Bolt Holes
view source -
US Patent:20100183431, Jul 22, 2010
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Filed:Jan 20, 2009
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Appl. No.:12/356353
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Inventors:Ganesh Anantharaman - East Hartford CT, US
Gerard Dame - East Haddam CT, US -
Assignee:United Technologies Corporation - Hartford CT
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International Classification:F04D 29/40
B23P 6/00 -
US Classification:4151821, 2940201
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Abstract:A method for repairing damaged bolt holes in a flange having a plurality of circumferentially spaced bolt holes therein, with each bolt hole defining a center axis and the flange defining an outer diameter edge. The method includes removing parent material of the flange in a first pattern, and metallurgically joining a replacement detail to the parent material of the flange a location where the parent material of the flange was removed in the first pattern. The first pattern is bounded by first, second, third and fourth points. The first point corresponds to the center axis of a first of the plurality of bolt holes, the second point corresponds to center axis of a second of the plurality of bolt holes, and the third and fourth points are defined at the outer diameter edge of the flange circumferentially spaced from each other.
Ganesh Anantharaman
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Ganesh Anantharaman
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Ganesh Anantharaman
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Ganesh Anantharaman
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