Systems and methods for preventing flashback in a combustor assembly
Embodiments of the present application include a combustor assembly. The combustor assembly may include a combustion chamber, a first plenum, a second plenum, and one or more elongate air/fuel premixing injection tubes. Each of the elongate air/fuel premixing injection tubes may include a first length at least partially disposed within the first plenum and configured to receive a first fluid from the first plenum. Moreover, each of the elongate air/fuel premixing injection tubes may include a second length disposed downstream of the first length and at least partially disposed within the second plenum. The second length may be formed of a porous wall configured to allow a second fluid from the second plenum to enter the second length and create a boundary layer about the porous wall.
1. A combustor assembly, comprising:
a combustion chamber;
a first plenum;
a second plenum; and
one or more elongate air/fuel premixing injection tubes, each of the one or more elongate air/fuel premixing injection tubes comprising:
a first length at least partially disposed within the first plenum and configured to receive a first fluid from the first plenum, wherein the first length is defined between a forward plate and a mid-plate; and
a second length disposed downstream of the first length and at least partially disposed within the second plenum, wherein the second length is defined between the mid-plate and an aft plate, wherein the second length is formed of a porous wall comprising a dense open cell material configured to allow a second fluid from the second plenum to uniformly effuse along the second length and create a boundary layer about the porous wall.
2. The combustor assembly of claim 1 , wherein the one or more elongate air/fuel premixing injection tubes each comprise:
a first end open to a flow of compressed air; and
a second end open to the combustion chamber.
3. The combustor assembly of claim 1 , wherein the first length comprises one or more apertures configured to receive the first fluid from the first plenum.
4. The combustor assembly of claim 1 , wherein the first plenum and the second plenum are disposed adjacent to each other.
5. The combustor assembly of claim 1 , wherein the porous wall is formed of one of a ceramic, metallic, or cera-metallic material.
6. The combustor assembly of claim 1 , wherein the first fluid is a high reactivity fuel.
7. The combustor assembly of claim 1 , wherein the second fluid is a low reactivity fuel.
8. The combustor assembly of claim 1 , wherein the second fluid is a no reactivity fluid.
9. The combustor assembly of claim 1 , wherein the second fluid is nitrogen.
10. The combustor assembly of claim 1 , wherein the lean boundary layer is incombustible due to the second fluid having no reactivity.
11. The combustor assembly of claim 1 , wherein a velocity of the air/fuel mixture at a center of the one or more elongate air/fuel premixing injection tubes is greater than a velocity of the boundary layer.
12. The combustor assembly of claim 1 , wherein the second fluid entering the one or more elongate air/fuel premixing injection tubes via the porous wall forces the air/fuel mixture away from the porous wall.
13. The combustor assembly of claim 1 , wherein the dense open cell material comprises a dense open cell metal.
14. A combustor assembly, comprising:
a combustion chamber;
a first fuel plenum defined by a forward plate, a mid-plate, and an outer sleeve;
a second fuel plenum defined by an aft plate, the mid-plate, and the outer sleeve; and
one or more elongate air/fuel premixing injection tubes, each of the one or more elongate air/fuel premixing injection tubes comprising:
a first length at least partially disposed within the first fuel plenum and configured to receive a first fuel from the first fuel plenum to create a first air/fuel mixture, wherein the first length is defined between the forward plate and the mid-plate; and
a second length disposed downstream of the first length and at least partially disposed within the second fuel plenum, wherein the second length is defined between the mid-plate and the aft plate, wherein the second length is formed of a porous wall comprising a dense open cell material configured to allow a second fuel from the second fuel plenum to uniformly effuse along the second length and create a boundary layer of a second air/fuel mixture about the porous wall.
15. The combustor assembly of claim 14 , wherein the one or more elongate air/fuel premixing injection tubes each comprise:
a first end open to a flow of compressed air; and
a second end open to the combustion chamber.
16. The combustor assembly of claim 14 , wherein the first fuel is a high reactivity fuel and the second fuel is a low reactivity fuel.
17. The combustor assembly of claim 14 , wherein the second fuel is nitrogen.
18. The combustor assembly of claim 14 , wherein a velocity of the first air/fuel mixture at a center of the one or more elongate air/fuel premixing injection tubes is greater than a velocity of the second air/fuel mixture at the boundary layer.
19. The combustor assembly of claim 14 , wherein the second fluid entering the one or more elongate air/fuel premixing injection tubes via the porous wall forces the first air/fuel mixture away from the porous wall.
20. A method for air/fuel premixing in a combustor, comprising:
directing a flow of air into one or more elongate air/fuel premixing injection tubes;
directing a first fuel from a first fuel plenum into the one or more elongate air/fuel premixing injection tubes along a first length defined between a forward plate and a mid-plate; and
uniformly effusing a second fuel from a second fuel plenum along a second length defined between the mid-plate and an aft plate into the one or more elongate air/fuel premixing injection tubes through a porous wall comprising a dense open cell material to create a boundary layer about the porous wall downstream of the first length.