Effusion plate using additive manufacturing methods
Additive manufacturing techniques may be utilized to construct effusion plates. Such additive manufacturing techniques may include defining a configuration for an effusion plate having one or more internal cooling channels. The manufacturing techniques may further include depositing a powder into a chamber, applying an energy source to the deposited powder, and consolidating the powder into a cross-sectional shape corresponding to the defined configuration. Such methods may be implemented to construct an effusion plate having one or more channels with a curved cross-sectional geometry.
1. A turbine combustor, comprising:
a combustion chamber;
a head end portion; and
an effusion plate positioned between the combustion chamber and the head end portion, the effusion plate comprising:
a proximal face;
a distal face; and
one or more channels extending between the proximal face and the distal face, wherein the one or more channels comprise a serpentine cross-sectional geometry, wherein the cross-section is taken along a plane extending between the proximal face and distal face.
2. The turbine combustor of claim 1 , wherein the one or more channels comprise a radially expanded outlet.
3. The turbine combustor of claim 1 , wherein the one or more channels comprise a radially expanded inlet.
4. The turbine combustor of claim 1 , wherein the one or more channels have curves oriented in multiple planes within the effusion plate.
5. The turbine combustor of claim 1 , wherein a length of the one or more channels is at least 50 percent larger than a thickness of the effusion plate.
6. The turbine combustor of claim 1 , wherein a first channel of the one or more channels comprises a first outlet oriented at a first angle of less than 90 degrees with respect to the distal face of the effusion plate, a second channel of the one or more channels comprises a second outlet oriented at a second angle of less than 90 degrees with respect to the distal face of the effusion plate, and the first angle and the second angle are different from one another.
7. The turbine combustor of claim 1 , wherein an interior wall of the one or more channels is striated.
8. The turbine combustor of claim 1 , wherein the head end portion is upstream from the combustion chamber and comprises one or more fuel nozzles configured to provide fuel to the combustion chamber.
9. A system, comprising:
an effusion plate configured to be attached to a turbine combustor and positioned between a combustion chamber and a head end portion of the turbine combustor, comprising:
a proximal face;
a distal face; and
one or more channels extending between the proximal face and the distal face, wherein the one or more channels comprise a curved cross-sectional geometry such that the one or more channels intersect a plane extending between the proximal face and distal face multiple times, wherein the plane is perpendicular to the proximal face or the distal face.
10. The system of claim 9 , wherein the one or more channels comprise a radially expanded outlet.
11. The system of claim 9 , wherein the one or more channels comprise an outlet oriented at an angle of less than 90 degrees with respect to the distal face of the effusion plate.
12. The system of claim 9 , wherein the one or more channels have curves oriented in multiple planes within the effusion plate.
13. The system of claim 9 , wherein a length of the one or more channels is at least 50 percent larger than a thickness of the effusion plate.
14. The system of claim 9 , wherein a first channel of the one or more channels comprises a first outlet oriented at a first angle of less than 90 degrees with respect to the distal face of the effusion plate, a second channel of the one or more channels comprises a second outlet oriented at a second angle of less than 90 degrees with respect to the distal face of the effusion plate, and the first angle and the second angle are different from one another.
15. The system of claim 9 , wherein the one or more channels are concentrated in a central portion of the effusion plate.