Multiple venture tube gas fuel injector for a combustor

1. A gas fuel injector comprising:

a first header plate;

a second header plate spaced downstream from said first header plate;

a plurality of venturi tubes arranged in straight rows and sealably secured to said first header plate and said second header plate,

wherein each of said venturi tubes includes an inlet section, a throat section and an exit, said exit is shaped into a pattern that reduces space between each of said venturi tubes at said exit of each of said plurality of venturi tubes.

2. The injector of claim 1 , wherein said venturi tubes further includes a body section that transitions between a circular shape of said throat and a different shape of said exit.

3. The injector of claim 1 , wherein said plurality of venturi tubes are arranged in a hexagonal pattern.

4. The injector of claim 1 , wherein said exit is shaped so as to match an arrangement of said venturi tubes.

5. The injector of claim 1 , wherein said exit is shaped as a hexagon.

6. The injector of claim 1 , wherein said exit has a plurality of pointed ends formed from a conical interior and hexagonal perimeter.

7. The injector of claim 1 , further comprising a manifold that is sealed about a perimeter of said first and second header plates.

8. The injector of claim 7 , wherein said manifold, a perimeter of said first and second head plates, and a perimeter of each of said plurality of venturi tubes forms a plenum space and a fuel line is in fluid communication with said plenum space via an external manifold which acts to evenly distribute fluid around perimeter of said plenum.

9. The injector of claim 1 , wherein each of said plurality of venturi tubes includes at least one hole for receiving fuel, said at least one hole is disposed at either said inlet section or said throat.

10. The injector of claim 1 , further comprising an exit diffuser surrounding said plurality of venturi tubes.

11. The injector of claim 1 , wherein said exit diffuser has a first end that is shaped to match the arrangement of said plurality of venturi tubes and a second end that is circular.

12. A combustor for a gas turbine engine comprising:

a preburner;

a fuel injector downstream of said preburner, and

wherein said fuel injector includes a plurality of venturi tubes arranged in straight rows, each of said venturi tubes includes an inlet section, a throat section and an exit, said exit is shaped into a pattern that minimizes space between eting flow area of each of said plurality of venturi tubes at said exit of each of said plurality of venturi tubes.

13. The combustor of claim 12 , further comprising a catalyst bed downstream of said fuel injector passing through said catalyst bed and experiencing a combustion reaction while passing therethrough wherein energetic gases are emitted downstream of said catalyst bed.

14. The combustor of claim 12 , wherein said injector further comprises:

a first header plate;

a second header plate spaced downstream from said first header plate,

wherein said plurality of parallel venturi tubes are sealably secured to said first header plate and said second header plate.

15. The combustor of claim 12 , further comprising a manifold that is sealed about a perimeter of said first and second header plates.

16. The combustor of claim 15 , wherein said manifold, a perimeter of said first and second head plates, and a perimeter of each of said plurality of venturi tubes forms a plenum space and a fuel line is in fluid communication with said plenum space via an external manifold which acts to evenly distribute fluid around perimeter of said plenum.

17. The combustor of claim 12 , wherein said venturi tubes are arranged in a hexagonal pattern.

18. The combustor of claim 12 , wherein said exit is shaped so as to match an arrangement of said venturi tubes.

19. The combustor of claim 12 , wherein said exit is shaped as a hexagon.

20. The combustor of claim 12 , wherein said exit has a plurality of pointed ends.

21. The combustor of claim 12 , wherein each of said plurality of venturi tubes includes at least one hole for receiving fuel, said at least one hole is disposed at either said inlet section or said throat.

22. The combustor of claim 12 , wherein said injector further comprises an exit diffuser surrounding said plurality of venturi tubes.

23. The combustor of claim 22 , wherein said exit diffuser has a first end that is shaped to match the arrangement of said plurality of venturi tubes and a second end that is circular.