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Jerome Wojtalik Phones & Addresses

  • Lincolnwood, IL
  • 7237 N Kedvale Ave, Lincolnwood, IL 60712

Work

Position: Executive, Administrative, and Managerial Occupations

Education

Degree: Bachelor's degree or higher

Publications

Us Patents

Low Drag Ducted Ram Air Turbine Generator And Cooling System

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US Patent:
62703099, Aug 7, 2001
Filed:
Dec 14, 1999
Appl. No.:
9/461551
Inventors:
Richard Ghetzler - Buffalo Grove IL
Jerome F. Wojtalik - Hoffman Estates IL
Neils Kruse - Cary IL
Kendal R. Stephens - Fox River Grove IL
Harold Schmulenson - Buffalo Grove IL
Assignee:
Ghetzler Aero-Power Corporation - Buffalo Grove IL
International Classification:
F01D 1706
F01D 1714
US Classification:
415 35
Abstract:
A low drag ducted ram air turbine generator and cooling system is provided. The ducted ram air turbine generator and cooling system has reduced drag while extracting dynamic energy from the air stream during the complete range of intended flight operating regimes. A centerbody/valve tube having an aerodynamically shaped nose is slidably received in a fairing and primary structure to provide a variable inlet area. An internal nozzle control mechanism attached to the valve tube positions nozzle control doors to provide variable area nozzles directing air flow to the turbine stator and rotor blades to maintain optimum generator efficiency. An alternate embodiment includes an annular internal nozzle having interleaved panels to modulate the air flow to the turbine.

Low Drag Ducted Ram Air Turbine Generator And Cooling System

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US Patent:
20020122717, Sep 5, 2002
Filed:
Aug 6, 2001
Appl. No.:
09/923649
Inventors:
Richard Ghetzler - Buffalo Grove IL, US
Jerome Wojtalik - Hoffman Estates IL, US
Neils Kruse - Cary IL, US
Kendal Stephens - Fox River Grove IL, US
Harold Schmulenson - Buffalo Grove IL, US
International Classification:
F01D017/06
US Classification:
415/035000
Abstract:
A low drag ducted ram air turbine generator and cooling system is provided. The ducted ram air turbine generator and cooling system has reduced drag with respect to prior ram air turbine generator systems while extracting dynamic energy from the air stream during the complete range of intended flight operating regimes. A centerbody/valve tube having an aerodynamically shaped nose is slidably received in a fairing and primary structure to provide a variable inlet area. An internal nozzle control mechanism attached to the valve tube positions nozzle control doors to provide variable area nozzles directing air flow to the turbine stator and rotor blades to maintain optimum generator efficiency. An alternate embodiment includes an annular internal nozzle having interleaved panels to modulate the air flow to the turbine.
Jerome Wojtalik from Lincolnwood, IL, age ~83 Get Report