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An improved mixing tube design and fuel nozzle that allows for a more uniform and thorough mixing of fuel and air being fed to the combustor of a gas turbine engine, wherein each of a plurality of mixing tubes comprises a pair of concentric hollow cylinders that define a ring-like, annular path for

An improved mixing tube design and fuel nozzle that allows for a more uniform and thorough mixing of fuel and air being fed to the combustor of a gas turbine engine, wherein each of a plurality of mixing tubes comprises a pair of concentric hollow cylinders that define a ring-like, annular path for the flow of fuel between the two hollow cylinders in each mixing tube, a plurality of air injection slots formed in the concentric hollow cylinders defining corresponding air flow paths from the outside into the interior of each mixing tube, and one or more fuel injection ports formed in selected ones of the plurality of air injection slots that allow for the flow of fuel from the annular path formed by the hollow cylinders into the air flow path, resulting in significantly better mixing and improved thermodynamic behavior of the fuel and air mixture downstream of the nozzle and upstream of the combustor.

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1. A mixing tube for combining gas fuel and air fed to the combustor of a gas turbine engine, comprising: a pair of concentric hollow cylinders defining a ring-like annular path for the flow of gas fuel between said hollow cylinders;a plurality of air injection slots formed in said concentric hollow

1. A mixing tube for combining gas fuel and air fed to the combustor of a gas turbine engine, comprising: a pair of concentric hollow cylinders defining a ring-like annular path for the flow of gas fuel between said hollow cylinders;a plurality of air injection slots formed in said concentric hollow cylinders that define a plurality of corresponding air flow paths from the outside substantially tangentially through said ring-like annular path into the interior of said mixing tube; said air injection slots arranged in axially-spaced, circumferential rows, andat least one fuel injection port extending through a wall at least partially defining a respective one of said plurality of air injection slots in one or more of said axially-spaced, circumferential rows to allow for the flow of fuel from said annular path into said air flow path. 2. A mixing tube according to claim 1, wherein said at least one fuel injection port comprises plural fuel injection ports in said air injection slots of some but not all of said axially-spaced circumferential rows. 3. A mixing tube according to claim 1, wherein said fuel injection ports comprise two or more small diameter openings through one side of said plurality of air injection slots to thereby define a fuel injection flow path. 4. A mixing tube according to claim 1, wherein said plurality of air injection slots include a first portion along the longitudinal axis having fuel injection ports and a second portion downstream of said first portion that do not include fuel injection ports. 5. A mixing tube according to claim 1, wherein said plurality of air injection slots are oriented to cause a clockwise or counter-clockwise flow of air into said mixing tube. 6. A mixing tube according to claim 1, further comprising a liquid fuel/compressed air injector disposed inside said mixing tube upstream of selected ones of said plurality of air injection slots to provide a supplemental atomized fuel and air feed to said combustor. 7. A mixing tube according to claim 6, wherein said liquid fuel/compressed air injector comprises a fuel injection nozzle having a plurality of pinhole openings discharging liquid fuel that becomes atomized by said compressed air before the mixture is discharged into said mixing tube. 8. A mixing tube according to claim 1, further comprising a perforated cylindrical screen disposed outside said plurality of hollow cylinders. 9. A fuel nozzle for providing an air and gas fuel mixture to the combustor of a gas turbine engine, comprising: a plurality of fuel and air mixing tubes disposed at equidistant radial positions about the longitudinal axis of said fuel nozzle, wherein each mixing tube comprises a pair of concentric hollow cylinders defining a ring-like, annular flow path for fuel between said hollow cylinders, a plurality of air injection slots formed in said hollow cylinders to define a plurality of corresponding air flow paths from the outside substantially tangentially through the ring-like annular flow path into the interior of the mixing tube, and one or more fuel injection ports formed in selected ones of said plurality of air injection slots; andan end plate for securing each of said mixing tubes at one end thereof at corresponding equidistant radial positions about the longitudinal axis of said fuel nozzle. 10. A fuel nozzle according to claim 9, further comprising a cylindrical end cap sized to enclose the discharge ends of said plurality of mixing tubes at one end and open at the other end. 11. A fuel nozzle according to claim 9, wherein said plurality of air injection slots in each of said mixing tubes are disposed in rows along the longitudinal axis of each mixing tube. 12. A fuel nozzle according to claim 9, wherein said fuel injection ports in each mixing tube comprise two or more small diameter openings through one side of said air injection slots to thereby define corresponding fuel injection flow paths. 13. A fuel nozzle according to claim 9, wherein said air injection slots of each mixing tube include a first portion along the longitudinal axis having fuel injection ports and a second portion downstream of said first portion that do not include fuel injection ports. 14. A fuel nozzle according to claim 9, wherein each of said mixing tubes further comprises a perforated cylindrical screen disposed outside said hollow cylinders. 15. A distributed gas fuel and air combustion system for a gas turbine engine, comprising: a combustor;a fuel supply system for providing hydrocarbon fuel to said combustor;a compressed air supply to said combustor; anda fuel nozzle for providing a distributed mixture of gas fuel and air to said combustor, said fuel nozzle comprising a plurality of fuel and air mixing tubes disposed about the longitudinal axis of said fuel nozzle, wherein each mixing tube comprises a pair of concentric hollow cylinders defining an annular flow path for fuel between the hollow cylinders, a plurality of air injection slots formed in said hollow cylinders extending substantially tangentially through said annular flow path and into an inner one of said pair of hollow-concentric cylinders, and one or more fuel injection ports formed in selected ones of said plurality of air injection slots.