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Anil Tolpadi Phones & Addresses

  • Liberty Township, OH
  • Cincinnati, OH
  • 57 Victoria Ct, Niskayuna, NY 12309 (518) 220-9339
  • Schenectady, NY
  • 2 Melissa Ct, Albany, NY 12205 (518) 452-8806
  • 1 Park 200, Clifton Park, NY 12065
  • Minneapolis, MN

Work

Company: Ge Feb 2015 Position: Technical leader, component cooling

Education

Degree: Doctorates, Doctor of Philosophy School / High School: University of Minnesota 1983 to 1987 Specialities: Mechanical Engineering

Skills

Gas Turbines • Heat Transfer • Cfd • Engineering • Turbomachinery • Turbines • Mechanical Engineering • Finite Element Analysis • Aerodynamics • Combustion • Fluid Dynamics • Ansys • Simulations • Thermodynamics • Thermal • Steam Turbines • Energy • Aerospace • Power Generation • Unigraphics • Engineering Management • Generators • Fluid Mechanics • Steam • Propulsion • Wind Turbines • Stress Analysis • Experimentation • Six Sigma • Product Development

Interests

Children • Environment • Education • Science and Technology • Disaster and Humanitarian Relief • Health

Emails

Industries

Aviation & Aerospace

Resumes

Resumes

Anil Tolpadi Photo 1

Technical Leader, Component Cooling

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Location:
Cincinnati, OH
Industry:
Aviation & Aerospace
Work:
Ge
Technical Leader, Component Cooling

Ge Aviation
Technical Leader, Component Cooling

Ge Aviation Sep 2013 - Jan 2015
Senior Staff Engineer and Technologist

Ge Global Research Jun 2003 - Dec 2007
Project Leader-Heat Transfer

Ge Global Research Dec 1989 - Apr 2000
Mechanical Engineer
Education:
University of Minnesota 1983 - 1987
Doctorates, Doctor of Philosophy, Mechanical Engineering
Iowa State University 1981 - 1983
Master of Science, Masters, Mechanical Engineering
Indian Institute of Technology, Kharagpur 1976 - 1981
Skills:
Gas Turbines
Heat Transfer
Cfd
Engineering
Turbomachinery
Turbines
Mechanical Engineering
Finite Element Analysis
Aerodynamics
Combustion
Fluid Dynamics
Ansys
Simulations
Thermodynamics
Thermal
Steam Turbines
Energy
Aerospace
Power Generation
Unigraphics
Engineering Management
Generators
Fluid Mechanics
Steam
Propulsion
Wind Turbines
Stress Analysis
Experimentation
Six Sigma
Product Development
Interests:
Children
Environment
Education
Science and Technology
Disaster and Humanitarian Relief
Health

Publications

Us Patents

Method And Apparatus To Facilitate Reducing Turbine Packing Leakage Losses

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US Patent:
6761530, Jul 13, 2004
Filed:
Mar 21, 2003
Appl. No.:
10/394126
Inventors:
Leonid Julievich Ginessin - Moscow, RU
Anil Kumar Tolpadi - Niskayuna NY
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D 1102
US Classification:
4151737, 4151745, 415230
Abstract:
A method for sealing between a rotary component and a stationary component. The method including positioning a seal assembly having a plurality of teeth adjacent the stationary component and positioning a packing surface to interface with the rotary component. The packing surface at the rotary component includes at least one step that has an axial width that is approximately equal to a distance the rotary component axially shifts relative to the stationary component during transition from startup to steady state operating conditions.

Variable Thickness Turbine Bucket Cover And Related Method

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US Patent:
6851926, Feb 8, 2005
Filed:
Mar 7, 2003
Appl. No.:
10/248999
Inventors:
Leonid Yulyevich Guinessine - Moscow, RU
Anil Kumar Tolpadi - Niskayuna NY, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D011/08
US Classification:
4151731, 4151734, 416195
Abstract:
A turbine bucket and cover assembly includes a bucket having a shank portion and an airfoil portion separated by a platform portion; and a bucket cover arranged on a sloped radially outer tip of the airfoil portion, the bucket cover having a radially inner surface matching the sloped edge and a radially outer surface lying in a plane parallel to a longitudinal axis of a rotor on which the bucket is adapted to be mounted. A related method includes the steps of a) providing a bucket cover having substantially parallel radially inner and outer surface; b) removing material from the bucket cover so as to form a new radially outer surface defining an acute angle relative to the radially inner surface; and c) securing the bucket cover on the sloped airfoil tip of the turbine bucket such that the radially outer surface is substantially parallel to the turbine rotor axis.

Covers For Turbine Buckets And Methods Of Assembly

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US Patent:
20030223872, Dec 4, 2003
Filed:
May 31, 2002
Appl. No.:
10/158229
Inventors:
Boris Frolov - Moscow, RU
Anil Tolpadi - Niskayuna NY, US
Gregory Landry - Glenburn ME, US
International Classification:
F01D005/22
US Classification:
416/191000, 029/889210
Abstract:
A bucket cover includes circumferentially disposed arcuate cover segments each having discrete arcuate inner, intermediate and outer cover elements for spanning the tips of a plurality of turbine buckets. Each segment includes circumferentially spaced radial openings through the elements for receiving the tenons at the bucket tips. The intermediate element has a cavity or recess formed between circumferentially spaced webs which define the openings through the intermediate element for weight reduction purposes. In final assembly, the tips of the tenons are automatically peened to retain the elements on the buckets and excess material is machined to provide a smooth, continuous arcuate, circumferentially extending outer surface. The cavities are bounded by the webs, forward and rear end walls and the inner and outer surfaces of the outer and inner elements, respectively.

Cooling Of Stator Core Flange

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US Patent:
20130169080, Jul 4, 2013
Filed:
Jan 3, 2012
Appl. No.:
13/342840
Inventors:
Samir Armando Salamah - Niskayuna NY, US
James Jonathan Grant - Niskayuna NY, US
Christopher Anthony Kaminski - Niskayuna NY, US
Rebinth Jose Robin - Bangalore, IN
Anil Kumar Tolpadi - Niskayuna NY, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
H02K 9/00
US Classification:
310 59
Abstract:
An approach for cooling a stator core flange is provided. In one aspect, a pair of stator flanges each disposed at opposing ends of a stator core assembly maintains a compressive load on the stator core assembly. Heat transport tubes may be located about at least one of the stator flanges at an end of the stator core assembly to redistribute heat therefrom.

Cooling Ducts In An Electro-Dynamic Machine

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US Patent:
20140070640, Mar 13, 2014
Filed:
Sep 13, 2012
Appl. No.:
13/613187
Inventors:
Anil Kumar Tolpadi - Niskayuna NY, US
Srinath Varadarajan Ekkad - Blacksburg VA, US
Christopher Anthony Kaminski - Niskayuna NY, US
Samir Armando Salamah - West Chester OH, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
H02K 1/20
US Classification:
310 59
Abstract:
A generator stator core assembly is disclosed. The assembly includes a plurality of packages of stacked laminations, each package including an outermost lamination having a plurality of radially extending spacer blocks. The plurality of radially extending spacer blocks and adjacent axially spaced laminations define a radial cooling duct, and the outermost lamination includes a plurality of recesses such that a flow through the cooling duct flows over the plurality of recesses. In one embodiment, at least one adjacent axially spaced lamination defining the radial cooling duct also includes a plurality of recesses.

Electric Machine

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US Patent:
20220231551, Jul 21, 2022
Filed:
Jan 21, 2021
Appl. No.:
17/154121
Inventors:
- Schenectady NY, US
Anil Kumar Tolpadi - Liberty Township OH, US
International Classification:
H02K 1/20
H02K 9/19
H02K 11/25
B64D 27/24
B64D 33/08
Abstract:
An electric machine is provided herein that includes a stator assembly. The stator assembly includes a stator core having one or more lamination packages. The stator core can define an outer ring and a plurality of teeth extending from the outer ring. A cooling plate may be positioned adjacent to at least one of the one or more lamination packages. The cooling plate can define one or more channels therethrough. One or more windings can be arranged around one or more of the plurality of teeth of the stator core. A rotor can be operably coupled with the stator assembly. A cooling system can be fluidly coupled with the one or more channels of the cooling plate. The cooling system provides a cryogenic fluid through the one or more channels to cool the electric machine.
Anil K Tolpadi from Liberty Township, OH, age ~64 Get Report