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Gurmohan S Baveja

from West Palm Beach, FL
Age ~57

Gurmohan Baveja Phones & Addresses

  • 8761 Wellington View Dr, West Palm Bch, FL 33411 (925) 785-5874
  • West Palm Beach, FL
  • Tampa, FL
  • 799 Pradera Way, San Ramon, CA 94583 (925) 362-8335
  • 8051 Hackberry Dr, Mentor, OH 44060 (440) 255-4499
  • 8309 Browning Ct, Mentor, OH 44060 (440) 354-4602
  • Englewood, CO
  • Wickliffe, OH
  • Dublin, CA
  • Eastlake, OH
  • 8051 Hackberry Dr, Mentor, OH 44060

Work

Position: Food Preparation and Serving Related Occupations

Education

Degree: High school graduate or higher

Business Records

Name / Title
Company / Classification
Phones & Addresses
Gurmohan Baveja
President
Afb Resources
Metal Injection Molding Consulting Manufacturers Sales Representative · Administrative Management and General Management Consulting
4404 Bangor Ct, Pleasanton, CA 94568
PO Box 302, Willowick, OH 44092
(925) 785-5874
Gurmohan Singh Baveja
President
AFB RESOURCES
8309 Browning Ct, Mentor, OH 44060

Publications

Us Patents

Truncated Chamfer Turbine Blade

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US Patent:
61589616, Dec 12, 2000
Filed:
Oct 13, 1998
Appl. No.:
9/170173
Inventors:
Richard E. Kehl - Niskayuna NY
Gurmohan S. Baveja - Mentor OH
Assignee:
General Electric Compnay - Cincinnati OH
International Classification:
F01D 530
US Classification:
416193A
Abstract:
A gas turbine blade includes an airfoil, platform, and dovetail. The blade is cast with a chamfer along one edge of the platform thereof. The platform edge is then machined to truncate the chamfer in a simple and precise method.

Method And Apparatus For Use In Predicting Flow Of Fluid Through Passages In A Proposed Airfoil

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US Patent:
53580290, Oct 25, 1994
Filed:
Jul 29, 1993
Appl. No.:
8/098969
Inventors:
Gurmohan S. Baveja - Lakewood OH
Robert M. Brozier - Mentor OH
Albert C. Hoekenga - North Canton OH
Francis J. O'Connor - Barrington RI
Assignee:
PCC Airfoils, Inc. - Cleveland OH
International Classification:
B22C 900
B22D 2300
US Classification:
164516
Abstract:
To predict the rate of flow of cooling fluid (gas) through a passage system in a proposed airfoil during operation of a Jet engine, a full size model of the passage system is prepared. The flow of air or other gas is conducted through the model of the passage system. The characteristics of the flow of air or gas through the model of the passage system is determined to enable the characteristics of the flow of cooling fluid through the passage system in the proposed airfoil to be predicted. The model of the cooling fluid passage system in the proposed airfoil is formed by covering the pattern with a layer of metal. The pattern is removed from the covering to form a passage system having a configuration corresponding to the configuration of the cooling fluid passage system in the proposed airfoil.
Gurmohan S Baveja from West Palm Beach, FL, age ~57 Get Report