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Richard Andera Ghetzler

from Vernon Hills, IL
Age ~82
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Also known as:
Richard A Ghetzler, Andrea B Ghetzler, Hetzer G Andrea, Richard R
Phone and address:
26 Manchester Ln, Indian Creek, IL 60061
(224) 513-5894
Related to:
Lila Ghetzler, 92Aeropower GhetzlerMarni C Rotblut, 59Leslie Ghetzler
Connected to:
Arash Gheytanchi, 45Susanne G Ghez, 87Ann M Ghezzi, 76Katherine W Ghezzi, 42Megan A Ghezzi, 33Paul G Ghezzi, 60Piero S Ghezzi, 56Ginny C Ghezzo, 54Achal D Ghia, 45Amit P Ghia, 44

Richard Ghetzler Phones & Addresses

  • 26 Manchester Ln, Vernon Hills, IL 60061 (224) 513-5894
  • Arlington Heights, IL
  • Buffalo Grove, IL
  • Los Angeles, CA
  • Lake Zurich, IL
  • Rolling Meadows, IL
  • Palatine, IL
  • Lake Zurich, IL
  • 26 Manchester Ln, Vernon Hills, IL 60061 (847) 691-0781

Work

Company: Ghetzler aerospace -energy consultants 2001 Address: USA Position: Engineering consultant

Education

Degree: PhD Mechanical Engineering School / High School: University of Illinois at Urbana-Champaign 1974 to 1981 Specialities: Fluid and Thermal Sciences

Skills

Aerospace • Energy • Heat Transfer • Fluid Mechanics • Optics • Electronics • Engineering • Aerospace Engineering • Power Generation • Engineering Management

Languages

English

Interests

Casinos • Exercise • Sweepstakes • Nascar • Engineering Consultant • Home Improvement • Reading • Gourmet Cooking • Sports • Golf • Home Decoration • Health • Cooking • Energy and Aerospace Systems • Cruises • Outdoors • Sewing • Electronics • Crafts • Fitness • Music • Camping • Dogs • Family Values • Movies • Collecting • Christianity • Kids • Medicine • Diet • Travel • Boating • Investing • Traveling • International Traavel • Tennis

Industries

Aviation & Aerospace

Resumes

Resumes

Richard Ghetzler Photo 1

Engineering Consultant

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Location:
26 Manchester Ln, Vernon Hills, IL 60061
Industry:
Aviation & Aerospace
Work:
Ghetzler Aerospace -Energy Consultants - USA since 2001
Engineering Consultant
Northrop Grumman Corporation - Rolling Meadows, Illinois 1980 - 2001
Senior Technical Advisor
Education:
University of Illinois at Urbana-Champaign 1974 - 1981
PhD Mechanical Engineering, Fluid and Thermal Sciences Illinois Institute of Technology
Bachelor of Science (BS), Mechanical Engineering University of California, Berkeley
Master of Science (MS) Mechanical Engineering - Aeronautics, Aeronautical Science,Rocket Propulson, Rocket Flight Dynamics
Skills:
Aerospace
Energy
Heat Transfer
Fluid Mechanics
Optics
Electronics
Engineering
Aerospace Engineering
Power Generation
Engineering Management
Interests:
Casinos
Exercise
Sweepstakes
Nascar
Engineering Consultant
Home Improvement
Reading
Gourmet Cooking
Sports
Golf
Home Decoration
Health
Cooking
Energy and Aerospace Systems
Cruises
Outdoors
Sewing
Electronics
Crafts
Fitness
Music
Camping
Dogs
Family Values
Movies
Collecting
Christianity
Kids
Medicine
Diet
Travel
Boating
Investing
Traveling
International Traavel
Tennis
Languages:
English

Business Records

Name / Title
Company / Classification
Phones & Addresses
Richard Ghetzler
President
Ghetzler Aero Power
Other Professional Equip Merchant Whols
1405 Busch Pkwy, Buffalo Grove, IL 60089
(847) 215-0520, (847) 215-0445
Richard Ghetzler
President
Ghetzler Aero-Power Corp
Mfg Motors/Generators Engineering Services Whol Professional Equipment
26 Manchester Ln, Indian Creek, IL 60061

Publications

Us Patents

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.

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.

Molding Device And Method For Measuring The Bonding Strength Of Elastomers

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US Patent:
62897411, Sep 18, 2001
Filed:
May 20, 1999
Appl. No.:
9/315562
Inventors:
Richard Ghetzler - Buffalo Grove IL
Michael A. Mast - Palatine IL
Neil E. Hodge - Evanston IL
Nate Newman - Winnetka IL
Jeff Browning - Chicago IL
Assignee:
Northrop Grumman Corporation - Los Angeles CA
International Classification:
G01N 308
US Classification:
73827
Abstract:
A novel device and method for the injection and molding of a body of elastomeric composition within a mold cavity, around a core member and against the prepared surface of a test substrate, such as a ceramic or metallic disk, at the base of the mold cavity. The molded elastomeric composition is molded as an axial-symmetrical frustro-conical body which tapers down to a uniformly thin layer between the test substrate surface and the flat undersurface of the core member, and the core member supporting the molded elastomeric body bonded to the test substrate are separable from the mold cavity for attachment to a conventional tension test machine for measuring the interfacial bond strength between the elastomer and the prepared surface of the test substrate.

Ram Air Turbine Generating Apparatus

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US Patent:
55055877, Apr 9, 1996
Filed:
Jan 5, 1995
Appl. No.:
8/369065
Inventors:
Richard Ghetzler - Buffalo Grove IL
Assignee:
Northrop Grumman Corporation - Los Angeles CA
International Classification:
F01D 1700
US Classification:
415 49
Abstract:
A ram air turbine generator comprises a cylindrical external fairing having bypass exhaust orifices adjacent the leading end and external exhaust ports adjacent the aft end. A central flow guide is coaxially mounted and has a contoured outer surface spaced from the external fairing. A valve tube is coaxial with, and intermediate, the external fairing and the central flow guide and extends between a nose end with openings nearest the leading end of the external fairing and an aft plate. The valve tube also has a plurality of aft internal exhaust ports generally coextensive with the aft external exhaust ports in the external fairing. The valve tube is spring biased to a first position at which its nose end is proximate the leading end of the fairing and blocks the bypass exhaust orifices such that air is caused to flow through an annular nozzle defined between the valve tube and the central flow guide, through a turbine wheel, then out to the surrounding region through the aft internal and external exhaust ports. Ram air is effective to move the valve tube to a second position so as to expose the bypass exhaust orifices enabling substantial flow of bleed air therethrough. Additionally, a nozzle flow control mechanism is operable in response to movement of the valve tube between the first and second positions.

Apparatus To Simulate Aerodynamic Cooling And Heating Effects On Aircraft/Missile Equipment

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US Patent:
59426829, Aug 24, 1999
Filed:
Feb 2, 1998
Appl. No.:
9/017429
Inventors:
Richard Ghetzler - Buffalo Grove IL
Kim D. Volendorf - Cary IL
Donald A. Sofia - Sheboygan WI
Terrance W. Mollison - Wheeling IL
Assignee:
Northrop Grumman Corporation - Los Angeles CA
International Classification:
G01M 900
G01N 1700
US Classification:
73147
Abstract:
Apparatus for simulating aerodynamic heating and cooling on the outer surface of equipment externally mounted on an aircraft or missile as if airborne and exposed to an air stream. A first proximately spaced enclosure substantially uniformly conforms to the outer surface of the equipment and defines a low pressure chamber. A second enclosure envelops the first enclosure and defines a high pressure chamber. An adjustable flow producing mechanism directs flow of pressurized inlet air into the high pressure chamber. A temperature control mechanism selectively heats and cools the inlet air. Vents in the second enclosure exhaust the air from the low pressure chamber to the ambient region and a plurality of spaced orifices in the first enclosure direct jets of the pressurized air from the high pressure chamber into the low pressure chamber which vigorously impinge on the outer surface of the equipment. A first sensor measures the temperature of the air in the high pressure chamber and generates a first proportional signal and a second sensor measures the heat transfer coefficient at a plurality of locations on the outer surface of the equipment and generates a second proportional signal. A processor containing known information concerning the temperature and heat transfer properties of the equipment if airborne and exposed to an air stream under specified operating flight conditions compares the first and second signals with the known information and operates the flow producing and temperature control mechanisms until the signals conform to the known information.
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Richard Andera Ghetzler from Vernon Hills, IL, age ~82 Get Report