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Oleg B Dubitsky

from Hanover, NH
Age ~62

Oleg Dubitsky Phones & Addresses

  • 17 Hollenbeck Ln, Hanover, NH 03755 (603) 643-6561
  • West Lebanon, NH
  • Lebanon, NH

Resumes

Resumes

Oleg Dubitsky Photo 1

Director - Corporate Technology, Software At Concepts Nrec, Inc

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Location:
109 Rose Dr, Palm Coast, FL 32164
Industry:
Mechanical Or Industrial Engineering
Work:
Concepts Nrec
Director - Corporate Technology, Software at Concepts Nrec, Inc
Education:
Dartmouth College 1995 - 1998
Doctorates, Doctor of Philosophy
Dartmouth College 1992 - 1994
Master of Science, Masters
National Technical University of Ukraine 'Kyiv Polytechnic Institute'​ 1986 - 1989
National Technical University of Ukraine 'Kyiv Polytechnic Institute'​ 1979 - 1985
Skills:
Cfd
Engineering
Mechanical Engineering
Finite Element Analysis
Simulations
Gas Turbines
Cad
Product Development
Manufacturing
Numerical Analysis
Fortran
Multidisciplinary Design
Multidisciplinary Optimization
Steam Turbines
Centrifugal Compressors
Axial Compressors
Heat Transfer
Matlab
Energy
Renewable Energy
Algorithms
Visual C++
Power Plants
Fluid Mechanics
Multiphase Flow
Power Generation
Nuclear Power Plants
Heat Exchangers
Pre Sales
International Sales
Technical Training
Consulting Engineering
Languages:
English
Ukrainian
Russian
Oleg Dubitsky Photo 2

Oleg Dubitsky

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Oleg Dubitsky Photo 3

Oleg Dubitsky

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Publications

Us Patents

Turbocompressor And System For A Supercritical-Fluid Cycle

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US Patent:
20120034067, Feb 9, 2012
Filed:
Apr 27, 2010
Appl. No.:
13/265505
Inventors:
Elia P. Demetri - Westford MA, US
Oleg Dubitsky - Hanover NH, US
Louis Larosiliere - Quechee VT, US
Robert Pelton - Lebanon NH, US
Karl Wygant - Pearland TX, US
Assignee:
CONCEPTS ETI, INC. - White River Junction VT
International Classification:
F04D 29/046
F04D 29/06
F04D 29/08
US Classification:
415111, 415229
Abstract:
A turbocompressor for use with a process fluid and including an axial expansion turbine for expanding the process fluid and a centrifugal compressor for compressing the process fluid. The turbine and compressor share a common shaft, all of which can be housed by a common housing that encloses sealed spaces. The axial expansion turbine has a rotor located between two main bearings, and the centrifugal compressor includes an impeller mounted to one end of the shaft. In one embodiment, the main bearings are lubricated by a portion of the process fluid so that the only fluid in the sealed spaces is the process fluid. The turbocompressor can be used in a power-cycle system that includes a heat source and, optionally, an electrical generator.
Oleg B Dubitsky from Hanover, NH, age ~62 Get Report