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Constantin A Dinu

from Katy, TX
Age ~66
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Also known as:
Suzanne Drummond, Constanti L Dinu, Constandin Dinu, Constantina Dinu
Related to:
Gerald TroidlNiculina Dinu, 61Hiculina DinuMichael P Troidl, 35Graham Drummond, 45Alexandra Dinu, 34Migulina Dinu
Connected to:
Ioana C Dinu, 68Mircea M Dinu, 59Paul C Dinu, 86Bernice M Dinubile, 96Brandon T Dinucci, 37David P Dinuccio, 82Viviana Dinucci, 55Carl M Dinunno, 62Joseph N Dinunno, 68Debra M Dinunzio, 56

Constantin Dinu Phones & Addresses

  • Katy, TX
  • 125 Hammett Pond Ct, Greer, SC 29650 (864) 469-9295
  • 3 Shadetree Ct, Greer, SC 29651
  • 245 Rock Rd, Greer, SC 29651 (864) 329-1807
  • Clemson, SC
  • Greenville, SC
  • Seneca, SC
  • Marietta, GA
  • 1519 Lago Vista Ln, Katy, TX 77494 (864) 329-1807

Work

Position: Healthcare Support Occupations

Education

Degree: High school graduate or higher

Public records

Vehicle Records

Constantin Dinu

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Address:
2211 Hudson Rd APT 1211, Greer, SC 29650
VIN:
4A3AK24FX7E024454
Make:
MITSUBISHI
Model:
ECLIPSE
Year:
2007

Resumes

Resumes

Constantin Dinu Photo 1

Electrician At Samsung C&T

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Position:
Electrician at Samsung C&T
Location:
Dambovita County, Romania
Industry:
Industrial Automation
Work:
Samsung C&T
Electrician
Constantin Dinu Photo 2

Physician At Ssonoclar

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Position:
Physician at sSonoclar
Location:
Galati County, Romania
Industry:
Health, Wellness and Fitness
Work:
sSonoclar
Physician

Publications

Us Patents

Flow Controller For Gas Turbine Combustors

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US Patent:
6996990, Feb 14, 2006
Filed:
Aug 27, 2003
Appl. No.:
10/648203
Inventors:
Constantin Alexandru Dinu - Greer SC, US
Assignee:
General Electric Company - Schnectady NY
International Classification:
F23R 3/40
US Classification:
60723, 60749, 431170
Abstract:
A flow controller is disposed between a preburner section in a diffuser and prior to the main fuel injector and catalytic sections in a turbine combustor. The flow from the burner section is typically not uniform in temperature and velocity and the flow splitter renders the flow substantially uniform at the fuel injector and catalyst inlet. The flow splitter comprises substantially equal mass annular flow areas defined by a first outer frustoconical element and the diffuser wall, a second element defining with the first element a second annular area and a central bluff disk defining with the second element the interior annular area. Vanes are provided on the flow splitter to enhance turbulent flow and substantially preclude swirling flow. As a result, flow uniformity at the catalyst inlet and main fuel injection is achieved.

Multi-Sided Diffuser For A Venturi In A Fuel Injector For A Gas Turbine

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US Patent:
7003958, Feb 28, 2006
Filed:
Jun 30, 2004
Appl. No.:
10/879102
Inventors:
Constantin Alexandru Dinu - Greer SC, US
Iris Ziqin Hu - Greer SC, US
James Michael Storey - Taylors SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/00
F02G 3/00
US Classification:
60737, 60723, 60 39822
Abstract:
A combustor for a gas turbine includes a main fuel injector for receiving compressor discharge air and mixing the air with fuel for flow to a downstream catalytic section. The main fuel injector includes an array of venturis each having an inlet, a throat and a diffuser. A main fuel supply plenum between forward and aft plates supplies fuel to secondary annular plenums having openings for supplying fuel into the inlets of the venturis upstream of the throats. Each diffuser transitions from a circular cross-section at the throat to multiple discrete angularly related side walls at the diffuser exit. Gaps between circumferentially and radially spaced diffusers at their exits are eliminated. With this arrangement, uniform flow distribution of the fuel/air, velocity and temperature is provided at the catalyst inlet.

Multi-Venturi Tube Fuel Injector For A Gas Turbine Combustor

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US Patent:
7007478, Mar 7, 2006
Filed:
Jun 30, 2004
Appl. No.:
10/879059
Inventors:
Constantin Alexandru Dinu - Greer SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/00
F02G 3/00
US Classification:
60737, 60723, 60 39822
Abstract:
A combustor for a gas turbine includes a main fuel injector for receiving compressor discharge air and mixing the air with fuel for flow to a downstream catalytic section. The main fuel injector includes an array of venturis each having an inlet, a throat and a diffuser. A main fuel supply plenum between forward and aft plates supplies fuel to secondary annular plenums having openings for supplying fuel into the inlet of the venturis upstream of the throat. The diffusers transition from a circular cross-section at the throat to multiple discrete angularly related side walls at the diffuser exits without substantial gaps therebetween. With this arrangement, uniform flow distribution of the fuel/air, velocity and temperature is provided at the catalyst inlet.

Multiple Venture Tube Gas Fuel Injector For A Combustor

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US Patent:
7093438, Aug 22, 2006
Filed:
Jan 17, 2005
Appl. No.:
10/905686
Inventors:
Constantin Dinu - Greer SC, US
Thomas Raymond Farrell - Simpsonville SC, US
Kevin M. Gordon - Greer SC, US
James Michael Storey - Taylors SC, US
Krishna Kumar Venkataraman - Simpsonville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/00
F02G 3/00
US Classification:
60737, 60723, 60 39822
Abstract:
A gas fuel injector includes a first header plate; a second header plate spaced downstream from the upstream header plate; and a plurality of venturi tubes arranged in rows and sealably secured to the first and second header plates. Each of the venturi tubes includes an inlet section, a throat section and an exit. The exit is shaped into a pattern that reduces space between each of the venturi tubes at the exit of each of the plurality of venturi tubes.

Apparatus Having Thermally Isolated Venturi Tube Joints

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US Patent:
7509808, Mar 31, 2009
Filed:
Mar 25, 2005
Appl. No.:
10/907248
Inventors:
James M Storey - Taylors SC, US
Constantin Dinu - Greer SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/00
F02G 3/00
US Classification:
60740, 60747
Abstract:
A gas fuel injector includes a first header plate, a second header plate, and a plurality of venturi tubes. The second header plate is spaced downstream from the first header plate. The plurality of venturi tubes is sealably secured to the first and second header plates. Each venturi tube of the plurality of venturi tubes is defined by a plurality of fixable components.

Re-Heat Combustor For A Gas Turbine Engine

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US Patent:
8006477, Aug 30, 2011
Filed:
Apr 1, 2008
Appl. No.:
12/060481
Inventors:
Constantin Dinu - Greer SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/06
US Classification:
60 3917, 60791
Abstract:
A turbine engine includes a turbine section having a first turbine portion and a second turbine portion arranged along a central axis. A re-heat combustor is arranged between the first and second turbine portions. The re-heat combustor includes a combustion duct having a curvilinear flow portion. The curvilinear flow portion provides an increased residence time of combustion products passing through the re-heat combustor.

Control Systems And Method For Controlling A Load Point Of A Gas Turbine Engine

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US Patent:
8127557, Mar 6, 2012
Filed:
Apr 7, 2008
Appl. No.:
12/098906
Inventors:
Constantin Dinu - Greer SC, US
Assignee:
General Electric Company - Schenetady NY
International Classification:
F02C 9/00
US Classification:
60773, 60 395
Abstract:
Control systems and a method for controlling a load point of a gas turbine engine are provided. A control system includes a controller that receives a temperature signal and a pressure signal associated with exhaust gases from the gas turbine engine. The controller is further configured to generate the fuel control signal. The controller is further configured to generate an actuator control signal such that flow restriction member is moved from the first operational position to the second operational position to restrict the flow path such that the exhaust gases have a temperature level within a desired turndown temperature range, the pressure level in the exhaust gases is less than a threshold pressure level, and the load point of the gas turbine engine is adjusted to toward a target load point.

Turbine Fuel Nozzle Having Heat Control

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US Patent:
8186165, May 29, 2012
Filed:
Mar 16, 2009
Appl. No.:
12/405195
Inventors:
Constantin Dinu - Katy TX, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/00
US Classification:
60743, 60736, 60740, 431 11, 431208, 431214, 239 5
Abstract:
In one embodiment, a system includes a turbine engine fuel nozzle having an air path, a fuel path, and a surface along the air path. The fuel path may be directed toward the surface. The turbine engine fuel nozzle also may include a heating element configured to heat the surface.
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Constantin A Dinu from Katy, TX, age ~66 Get Report