Combustor with particle collection panel having a plurality of particle collection chambers
A combustor may include a combustor shell, a particle collection panel, and a combustor panel. The combustor shell may define a plurality of first impingement holes, the particle collection panel may include a plurality of particle collection chambers and may define a plurality of second impingement holes, and the combustor panel may define a plurality of effusion holes. The particle collection panel may be disposed inward of the combustor shell and the combustor panel may be disposed inward of the particle collection panel. Each particle collection chamber may have a closed inward end and an opening defined in an outward end. The particle collection chambers may be configured to entrap particulates.
1. A combustor comprising:
a combustor shell defining a plurality of first impingement holes;
a particle collection panel comprising a plurality of particle collection chambers and defining a plurality of second impingement holes, wherein the particle collection panel is disposed inward of the combustor shell; and
a combustor panel defining a plurality of effusion holes, wherein the combustor panel is disposed inward of the particle collection panel;
wherein each particle collection chamber of the plurality of particle collection chambers comprises a closed inward end and an opening defined in an outward end;
wherein a centerline axis of the opening of each particle collection chamber of the plurality of particle collection chambers intersects a respective first impingement hole of the plurality of first impingement holes; and
wherein a space is defined between the opening defined in the outward end of each particle collection chamber of the plurality of particle collection chambers and the combustor shell.
2. The combustor of claim 1 , wherein a first quantity of the first impingement holes corresponds to a second quantity of the particle collection chambers.
3. The combustor of claim 2 , wherein the first quantity equals the second quantity.
4. The combustor of claim 1 , wherein a first cumulative cross-sectional area of the plurality of first impingement holes is equal to a sum of a second cumulative cross-sectional area of the plurality of second impingement holes and a third cumulative cross-sectional area of the plurality of effusion holes.
5. The combustor of claim 1 , wherein each first impingement hole of the plurality of first impingement holes has a first diameter, wherein a distance between the combustor shell and the opening defined in the outward end of each particle collection chamber of the plurality of particle collection chambers is more than 0.5 times the first diameter.
6. The combustor of claim 1 , wherein each first impingement hole of the plurality of first impingement holes has a first diameter, wherein a distance between the combustor shell and the opening defined in the outward end of each particle collection chamber of the plurality of particle collection chambers is greater than 0.5 times the first diameter and less than 2.0 times the first diameter.
7. The combustor of claim 1 , wherein each first impingement hole of the plurality of first impingement holes has a first diameter and the opening of each particle collection chamber has a second diameter, wherein the second diameter is at least 0.2 times the first diameter.
8. A gas turbine engine comprising:
a combustor shell defining a plurality of first impingement holes;
a particle collection panel comprising a plurality of particle collection chambers and defining a plurality of second impingement holes, wherein the particle collection panel is disposed inward of the combustor shell; and
a combustor panel defining a plurality of effusion holes, wherein the combustor panel is disposed inward of the particle collection panel;
wherein each particle collection chamber of the plurality of particle collection chambers comprises a closed inward end and an opening defined in an outward end;
wherein a centerline axis of the opening of each particle collection chamber of the plurality of particle collection chambers intersects a respective first impingement hole of the plurality of first impingement holes; and
wherein a space is defined between the opening defined in the outward end of each particle collection chamber of the plurality of particle collection chambers and the combustor shell.
9. The gas turbine engine of claim 8 , wherein each first impingement hole of the plurality of first impingement holes has a first diameter, wherein the opening of each particle collection chamber of the plurality of particle collection chambers is offset in the aft direction about 0.5 times the first diameter.