Fuel nozzle for turbine combustion engines having...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S740000

Reexamination Certificate

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06883332

ABSTRACT:
A fuel nozzle for dispensing an atomized fluid spray into the combustion chamber of a gas turbine engine. The nozzle includes a body assembly with an inner fuel passage and an annular outer atomizing air passage. An array of turning vanes is disposed within the outer fuel passage. Each of the vanes is configured generally in the shape of an airfoil in having a pressure side and an opposing suction side, the suction side of each vane being spaced-apart from a juxtaposing pressure side of an adjacent vane to define a corresponding one of a plurality of aligned air flow channels therebetween. Fuel is directed through the fuel flow channels to be issued from the nozzle as a generally helical flow having a substantial uniform velocity profile.

REFERENCES:
patent: 2526410 (1950-10-01), Price
patent: 3013732 (1961-12-01), Webster et al.
patent: 3024045 (1962-03-01), Cleminshaw et al.
patent: 3029029 (1962-04-01), Webster
patent: 3159971 (1964-12-01), Hoebius et al.
patent: 3201050 (1965-08-01), Simmons et al.
patent: 3474970 (1969-10-01), Simmons et al.
patent: 3638865 (1972-02-01), McEneny et al.
patent: 3675853 (1972-07-01), Lapera
patent: 3685741 (1972-08-01), O'Sickey
patent: 3866413 (1975-02-01), Sturgess
patent: 3899884 (1975-08-01), Ekstedt
patent: 3912164 (1975-10-01), Lefebvre et al.
patent: 3979069 (1976-09-01), Garofalo
patent: 3980233 (1976-09-01), Simmons et al.
patent: 4134606 (1979-01-01), Menti, Jr.
patent: 4139157 (1979-02-01), Simmons
patent: 4168803 (1979-09-01), Simmons et al.
patent: 4246757 (1981-01-01), Heberling
patent: 4258544 (1981-03-01), Gebhart et al.
patent: 4365753 (1982-12-01), Harding et al.
patent: 4425755 (1984-01-01), Hughes
patent: 4600151 (1986-07-01), Bradley
patent: 4613079 (1986-09-01), Mains
patent: 4701124 (1987-10-01), Maghon et al.
patent: 4735044 (1988-04-01), Richey et al.
patent: 4845940 (1989-07-01), Beer
patent: 4854127 (1989-08-01), Vinson et al.
patent: 4941617 (1990-07-01), Russell
patent: 4977740 (1990-12-01), Madden et al.
patent: 5062792 (1991-11-01), Maghon
patent: 5078324 (1992-01-01), DuBell et al.
patent: 5174504 (1992-12-01), Halvorsen
patent: 5228283 (1993-07-01), Sciocchetti
patent: 5251447 (1993-10-01), Joshi et al.
patent: 5299909 (1994-04-01), Wulf
patent: 5351477 (1994-10-01), Joshi et al.
patent: 5394688 (1995-03-01), Amos
patent: 5423178 (1995-06-01), Mains
patent: 5435884 (1995-07-01), Simmons et al.
patent: 5484107 (1996-01-01), Holmes
patent: 5511375 (1996-04-01), Joshi et al.
patent: 5570580 (1996-11-01), Mains
patent: 5588824 (1996-12-01), McMillan
patent: 5605287 (1997-02-01), Mains
patent: 5615555 (1997-04-01), Mina
patent: 5622054 (1997-04-01), Tingle
patent: 5673552 (1997-10-01), Idleman et al.
patent: 5697553 (1997-12-01), Stotts
patent: 5735117 (1998-04-01), Toelle
patent: 5737921 (1998-04-01), Jones et al.
patent: 5740967 (1998-04-01), Simmons et al.
patent: 5761907 (1998-06-01), Pelletier et al.
patent: 5782626 (1998-07-01), Joos et al.
patent: 6460340 (2002-10-01), Chauvette et al.
patent: 20020134084 (2002-09-01), Mansour et al.
patent: 20040040310 (2004-03-01), Prociw et al.
Vincini et al., “Inverse and Direct Airfoil Design Using a Multiobjective Genetic Algorithm,” AIAA Journal, vol. 35, No. 9, Sep. 1997.
Trosset et al., “Numerical Optimization Using Computer Experiments,” ICASE Report No. 97-38, Aug. 1997.
Ta'asan, “Introduction to Shape Design and Control,” Carnegie Mellon University; and Sanz, “On the impact of Inverse Design Methods to Enlarge the Aero Design Envelope for Advanced Turbo-Engines,” NASA Lewis Research Center.
Sanz, “Lewis Inverse Design Code (LINDES),” NASA Technical Paper 2676, Mar. 1987.
Sanz, “On the Impact of Inverse Design Methods to Enlarge the Aero Design Envelope for Advanced Turbo-Engines,” NASA Lewis Research Center.
Sanz et al., “The Engine Design Engine: A Clustered Computer Platform for the Aerodynamic Inverse Design and Analysis of a Full Engine,” NASA Technical Memorandum 105838, 1992.
Reuther et al., “Constrained Multipoint Aerodynamic Shape Optimization Using and Adjoint Formulation and Parallel Computers,” American Institute of Aeronautics and Astrounautics, 1997.
Prandtl and Tletjens in “Applied Hydro- and Aerodynamics,” Dover Publ., Inc. (1957).
Oyama et al., “Transonic Wing Optimization Using Genetic Algorithim,” AIAA 97-1854, 13thComputational Fluid Dynamics Conference, American Institute of Aeronautics and Astronautics, Jun. 1997, Snowmass Village, Co.
Jameson et al., “Optimum Aerodynamic Design Using the Navier-Stokes Equations,” AIAA 97-0101, 35thAerospace Sciences Meeting & Exhibit, American Institute of Aeronautics and Astronautics, Jan. 1997, Reno, NV.
Goldstein in “Modern Developments in Fluid Dynamics,” vol. II, Dover Publ., Inc. (1965).
Elliot et al., “Aerodynamic Optimization on Unstructured Meshes with Viscous Effects.” AIAA 97-1849, 13thAIICFD Conference, American Institute of Aeronautics and Astronautics, Jun. 1997, Snowmass Village, Co.
Dang et al., “Development of an Advanced 3-Dimensional & Viscous Aerodynamic Design Method for Turbomachine Components in Utility & Industrial Gas Turbine Applications,” South Carolina Energy Research & Development Center (1997).
GTFS BR Nozzle.
NASA Technical Menorandum 101968 dated Mar. 1989 authored by Dr. Jose Sanz of NASA entitled “A Compendium of Controlled Diffusion Blades Generated by an Automated Inverse Design Procedure”.
Reprint from Oct. 1988, vol. 110, Journal of Turbomachinery, authored by Dr. Jose Sanz of NASA entitled “Automated Design of Controlled-Diffusion Blades”.

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