Ronald S Denmark from 1109 River Walk Dr, Simpsonville, SC 29681, age 62, Phone: (864)7579379

Resumes

Consulting Engineer - Compressor Airfoils

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Location:

Brownsville, TX

Industry:

Oil & Energy

Work:

Ge Power Jul 2003 - Feb 2011
Technical Leader - Compressor Airfoil Design
Ge Power Jul 2003 - Feb 2011
Consulting Engineer - Compressor Airfoils
Ge Power Apr 2002 - Jul 2003
Senior Mechanical Design Engineer - Hot Gas Path
Ge Power Nov 1999 - Apr 2002
Mechanical Design Engineer - Compressor
Pratt & Whitney Feb 1996 - Nov 1999
Technical Leader - F119 Fan

Education:

Penn State University 1981 - 1985
Bachelors, Mechanical Engineering

Skills:

Mechanical Engineering
Engineering
Gas Turbines
Power Generation
Energy
Six Sigma
Project Engineering
Turbines
Engineering Management
Product Development
Root Cause Analysis
Engineering Design
Design Engineering
Gas
Compressor
Power Systems
Process Engineering
Team Leadership
Jet Engines
Project Management

Consulting Engineer - Compressor

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Location:

Simpsonville, SC

Work:

Ge Power
Consulting Engineer - Compressor

Education:

Penn State University
Bachelors

Us Patents

Compressor Stator Floating Tip Shroud And Related Method
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US Patent:

7195453, Mar 27, 2007
Filed:

Aug 30, 2004
Appl. No.:

10/928735
Inventors:

Nicholas Francis Martin - Simpsonville SC, US
John David Memmer - Simpsonville SC, US
Ronald Stuart Denmark - Greenville SC, US
Assignee:

General Electric Company - Schenectady NY
International Classification:

F01D 9/00
US Classification:

415138, 4152093
Abstract:

A stator blade segment for a compressor includes an inner ring segment and an outer ring segment and a plurality of stator blades extending radially between the inner and outer ring segments, the stator blade secured to the outer ring at a shank portion of the blade and loosely held in a slot in the inner ring segment at a tip portion of the blade, the slot formed to substantially match a cross-sectional profile of the tip portion of the blade but sized to create a clearance between the tip portion and the slot.

Stator Ring Configuration
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US Patent:

8429816, Apr 30, 2013
Filed:

Feb 24, 2009
Appl. No.:

12/391856
Inventors:

David R. Spracher - Simpsonville SC, US
Michael T. Hudson - Greenville SC, US
Ronald Stuart Denmark - Simpsonville SC, US
Assignee:

General Electric Company - Schenectady NY
International Classification:

B21K 25/00
US Classification:

2988922, 29889, 298892
Abstract:

A stator ring for use in a compressor of a gas turbine engine and a method of assembling the stator ring are provided. The stator ring includes a first plurality of segments that includes a first segment including a first circumferential end formed with a first cut and a second circumferential end formed with a second cut that is complementary to the first cut, wherein the first plurality of segments are configured to be circumferentially-coupled together, and a second plurality of segments that includes a second segment including a first circumferential end with a third cut and a second circumferential end with a fourth cut that is complementary to the third cut, wherein the second plurality of segments are configured to be circumferentially-coupled together.

Method And Apparatus To Repair A Turbomachine Rotor Wheel
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US Patent:

8601689, Dec 10, 2013
Filed:

Jun 17, 2011
Appl. No.:

13/163312
Inventors:

Yagnesh Dalpatbhai Hathiwala - Karnataka, IN
Ronald Stuart Denmark - Simpsonville SC, US
Ashok Kumar Haveri Murigeppa - Karnataka, IN
Srinivas Ravi - Simpsonville SC, US
Paul Anthony Santos - Simpsonville SC, US
Assignee:

General Electric Company - Schenectady NY
International Classification:

B23P 6/00
US Classification:

298891, 2940211, 416219 R
Abstract:

A method of repairing a turbomachine rotor wheel including a first outer circumferential edge extending to a second outer circumferential edge through a circumferential surface, a dovetail interface extending across the outer circumferential surface between the first and second outer circumferential edges, and a bucket mounted to the dovetail interface includes identifying a defect on one of the first and second outer circumferential edges of the rotor wheel adjacent the bucket, securing the bucket in the dovetail interface to substantially constrain axial movement, and removing a portion of the one of the first and second outer circumferential edges to remove the defect.

Air Foil Shape For A Compressor Blade
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US Patent:

20060073014, Apr 6, 2006
Filed:

Nov 12, 2004
Appl. No.:

10/986162
Inventors:

Steven Tomberg - Simpsonville SC, US
Roger Beharrysingh - Simpsonville SC, US
Timothy DeJoris - Mauldin SC, US
William Miller - Simpsonville SC, US
Paul Deivernois - Greer SC, US
Venkata Siva Chaluvadi - Mauldin SC, US
Adrian Mistreanu - Greenville SC, US
Michael Dutka - Simpsonville SC, US
Nathan Race - Pendleton SC, US
Jeffrey Boyd - Greenville SC, US
Christopher McGowan - Greenville SC, US
Peter Cleveland - Greenville SC, US
Jason Harrell - Centerville MA, US
Carl Schott - Simpsonville SC, US
John Stampfli - Greer SC, US
Ronald Denmark - Greenville SC, US
Steven Schirle - Anderson SC, US
Jennifer Michenfelder - Fountain Inn SC, US
John Ryman - Taylors SC, US
Assignee:

General Electric Company - Schenectady NY
International Classification:

F01D 5/18
US Classification:

41609600R
Abstract:

An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a table. The table selected from the group of tables consisting of TABLES 1S-16S, 1R-17R, and IGV. Wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.

Airfoil Shroud Assembly Using Tenon With Externally Threaded Stud And Nut
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US Patent:

20200088049, Mar 19, 2020
Filed:

Sep 18, 2018
Appl. No.:

16/134344
Inventors:

- Schenectady NY, US
Ronald Denmark - Greenville SC, US
Prem Navin Dhayanandam - Bengaluru, IN
Richard Gutta - Greenville SC, US
Sanjeev Kumar Jha - Bengaluru, IN
International Classification:

F01D 9/04
F01D 25/28
Abstract:

An airfoil and shroud assembly includes an airfoil including a root end, a free end and a tenon extending from the free end, the tenon including a base and an externally threaded stud extending from the base. A shroud includes an opening configured to receive the base of the tenon. A nut is configured to be threadably coupled to the externally threaded stud on the tenon on the airfoil to couple the shroud to the airfoil.