Pre-mixing apparatus for a turbine engine

1. A pre-mixing apparatus for a turbine engine comprising:

a main body having an inlet portion, an outlet portion and an exterior wall that collectively establish at least one fluid delivery plenum; and

a plurality of fluid delivery tubes extending through at least a portion of the at least one fluid delivery plenum, each of the plurality of fluid delivery tubes including an inlet end section, an outlet end section, and at least one fluid delivery opening disposed between the inlet end section and the outlet end section and fluidly connected to the at least one fluid delivery plenum wherein, a first fluid is selectively delivered to the at least one fluid delivery plenum, passed through the at least one fluid delivery opening and mixed with a second fluid flowing through the plurality of fluid delivery tubes prior to being combusted in a combustion chamber of a turbine engine.

2. The pre-mixing apparatus according to claim 1 , wherein the at least one fluid delivery opening being located proximate to the outlet end section so as to define a lean direct injection opening.

3. The pre-mixing apparatus according to claim 1 , wherein the at least one fluid delivery opening being located slightly spaced from the inlet end section so as to define a partially pre-mixed lean direct injection opening.

4. The pre-mixing apparatus according to claim 1 , wherein each of the plurality of fluid delivery tubes includes an outlet end section exposed at the outlet portion of the main body, an inlet end section exposed at the inlet portion of the main body and an intermediate section, the at least one fluid delivery opening is substantially spaced from the inlet end section so as to define a fully pre-mixed opening.

5. The pre-mixing apparatus according to claim 1 , wherein the at least one fluid delivery plenum constitutes a plurality of fluid delivery plenums including a first plenum, a second plenum and a third plenum.

6. The pre-mixing apparatus according to claim 5 , wherein the at least one fluid delivery opening in each of the plurality of fluid delivery tubes constitutes a plurality of fluid delivery openings including a first fluid delivery opening fluidly connected to the first fuel plenum, a second fluid delivery opening fluidly connected to the second plenum and a third fluid delivery opening fluidly connected to the third plenum.

7. The pre-mixing apparatus according to claim 6 , wherein each of the plurality of fluid delivery tubes includes an inlet end section, the first fluid delivery opening is arranged proximate to the inlet end section.

8. The pre-mixing apparatus according to claim 7 , wherein each of the plurality of fluid delivery tubes includes an inlet end section, the third fluid delivery opening is substantially spaced from the inlet end section.

9. The pre-mixing apparatus according to claim 8 , wherein second fluid delivery opening is arranged between the first and third fluid delivery openings.

10. The pre-mixing apparatus according to claim 1 , wherein at least one of the plurality of fluid delivery tubes includes an angled portion.

11. The pre-mixing apparatus according to claim 1 , wherein, the inlet portion is fluidly connected to the at least one fluid delivery plenum.

12. The pre-mixing apparatus according to claim 1 , wherein each of the plurality of fluid delivery tubes includes at least one of a substantially circular cross section and a rectangular cross section.

13. The pre-mixing apparatus according to claim 1 , wherein each of the plurality of fluid delivery tubes includes at least one thin wall portion that establishes a plurality of fluid delivery passages.

14. The pre-mixing apparatus according to claim 1 , wherein each of the plurality of fluid delivery tubes includes at least one of an oval cross-section having a serpentine wall member that establishes a plurality of internal passages, and a spiral section that facilitates mixing of the combustible mixture.

15. A turbine engine comprising:

at least one first fluid source containing a first fluid;

at least one second fluid source containing a second fluid; and

an apparatus for mixing the at least one first fluid and the at least one second fluid including:

a main body having an inlet portion, an outlet portion and an exterior wall that collectively establish at least one fluid delivery plenum; and

a plurality of fluid delivery tubes extending through the at least one fluid delivery plenum, each of the plurality of fluid delivery tubes including a first end section exposed at the inlet portion of the main body, a second end section exposed at the outlet portion of the main body and an intermediate section, and at least one fluid delivery opening disposed between the first end section and the second end section and fluidly connected to the at least one fluid delivery plenum, wherein the first fluid is selectively delivered to the at least one fluid delivery plenum, passed through the at least one fluid delivery opening and mixed with the second fluid flowing through at least a portion of the plurality of fluid delivery tubes prior to being combusted in a combustion chamber of the turbine engine.