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Ronald A Jeroszko

from Colchester, CT
Age ~78

Ronald Jeroszko Phones & Addresses

  • 26 Village Ct, Colchester, CT 06415 (860) 531-9180
  • Glastonbury, CT
  • Hampton, NH
  • 351 Charlemagne Blvd, Naples, FL 34112 (239) 793-4785 (239) 331-8393
  • Bristol, CT
  • Hebron, CT

Business Records

Name / Title
Company / Classification
Phones & Addresses
Ronald Jeroszko
Treasurer, Director
Riviera Golf Estates Condominium Unit #2, Inc
Nonclassifiable Establishments
351 Charlemagne Blvd, Naples, FL 34112

Publications

Us Patents

Combustor Employing Serially Staged Pilot Combustion, Fuel Vaporization, And Primary Combustion Zones

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US Patent:
39733904, Aug 10, 1976
Filed:
Dec 18, 1974
Appl. No.:
5/533921
Inventors:
Ronald A. Jeroszko - Hebron CT
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 322
F02M 2300
US Classification:
60 3906
Abstract:
A low emission combustion chamber in which a premixed, fuel rich-air mixture is discharged uniformly into the hot products of combustion of a pilot combustion zone to be vaporized thereby and to flow therewith as a non-autoignitable, vaporized, fuel rich-air mixture into the main combustion zone where combustion air is added thereto in swirling form for rapid mixing, autocombustion and burning therewith for low emission results.

Burner Construction For Gas Turbines

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US Patent:
43898483, Jun 28, 1983
Filed:
Jan 12, 1981
Appl. No.:
6/224408
Inventors:
Stanley J. Markowski - East Hartford CT
Ronald A. Jeroszko - Hebron CT
Robert P. Lohmann - South Windsor CT
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 722
US Classification:
60738
Abstract:
A burner construction for low emission burners in which the primary fuel is injected with air in an annulus into the upstream end of the burners so as to cause a significant recirculation of the fuel and air mixture adjacent to the end cap, the secondary fuel is injected into the burner in a small angle spray at a point substantially spaced from the end cap and large combustion and/or dilution holes in the burner wall a small distance upstream of the secondary nozzle are sized to produce an additional recirculation in the primary fuel and air around the secondary nozzle with this additional recirculation in the direction opposite to the first recirculation.

High-Performance Burner Construction

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US Patent:
45907692, May 27, 1986
Filed:
Jan 12, 1981
Appl. No.:
6/224406
Inventors:
Robert P. Lohmann - South Windsor CT
Ronald A. Jeroszko - Hebron CT
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02C 300
US Classification:
60752
Abstract:
A burner construction for gas turbine engines in which the conventional throat is replaced by a plurality of tubes extending radially into the burner downstream of the end cap, the inner ends being spaced apart to provide a clear axial passage and the tubes being spaced apart circumferentially to leave axial passages therebetween.
Ronald A Jeroszko from Colchester, CT, age ~78 Get Report