Hot gas path component cooling system having a particle collection chamber
A cooling system for a hot gas path component includes a substrate having an outer surface and an inner surface. The inner surface defines at least one interior space. A passage is formed in the substrate between the outer surface and the inner surface. An access passage is formed in the substrate and extends from the outer surface to the inner space. The access passage is formed at a first acute angle to the passage and includes a particle collection chamber. The access passage is configured to channel a cooling fluid to the passage. Furthermore, the passage is configured to channel the cooling fluid therethrough to cool the substrate.
1. A cooling system for a hot gas path component, said cooling system comprising:
a substrate comprising an outer surface and an inner surface, said inner surface defining at least one interior space;
an outer passage that extends along said outer surface of said substrate;
an access passage formed in said substrate and extending from said outer surface to said at least one inner space, said access passage formed at a first acute angle to said outer passage; and
a metering passage extending between said outer passage and said access passage, said metering passage coupling said outer passage in fluid communication with said access passage at an intermediate location along said access passage,
wherein said access passage comprises a particle collection chamber between said intermediate location and said outer surface.
2. The cooling system in accordance with claim 1 , wherein said metering passage is formed at a second acute angle to said access passage, and wherein said first acute angle is larger than said second acute angle.
3. The cooling system in accordance with claim 1 , wherein said metering passage intersects said access passage at a distance below said outer surface of said substrate.
4. The cooling system in accordance with claim 3 , wherein said particle collection chamber is defined between said outer surface of said substrate and the intersection distance of said metering passage.
5. The cooling system in accordance with claim 1 , wherein said metering passage comprises a first diameter, and said access passage comprises a second diameter larger than said first diameter.
6. The cooling system in accordance with claim 5 , wherein a ratio of said second diameter to said first diameter is between 1.14 and 2.4.
7. The cooling system in accordance with claim 5 , wherein said metering passage comprises a circular cross-section having a diameter between about 0.025 inches (0.6 mm) and about 0.035 inches (0.9 mm).
8. The cooling system in accordance with claim 5 , wherein said access passage comprises a circular cross-section having a diameter between about 0.040 inches (1.0 mm) and about 0.060 inches (1.5 mm).
9. The cooling system in accordance with claim 1 further comprising an exit passage coupled in fluid communication with said particle collection chamber.
10. A gas turbine engine comprising:
a compressor;
a turbine coupled to said compressor; and
a hot gas path component disposed in a least one of said compressor and said turbine, said hot gas path component comprising:
a substrate comprising an outer surface and an inner surface, said inner surface defining at least one interior space;
an outer passage that extends along said outer surface of said substrate;
an access passage formed in said substrate and extending from said outer surface to said at least one inner space, said access passage formed at a first acute angle to said outer passage; and
a metering passage extending between said outer passage and said access passage, said metering passage coupling said outer passage in fluid communication with said access passage at an intermediate location along said access passage,
wherein said access passage comprises a particle collection chamber between said intermediate location and said outer surface.
11. The gas turbine engine in accordance with claim 10 further comprising a casing comprising a cooling fluid supply conduit.
12. The gas turbine engine in accordance with claim 11 , wherein said cooling fluid supply conduit is coupled in fluid communication to said at least one interior space.
13. The gas turbine engine in accordance with claim 10 , wherein said hot gas path component further comprises a coating disposed along at least a portion of said outer surface of said substrate.
14. The gas turbine engine in accordance with claim 13 further comprising an exit passage formed through said coating and coupled in fluid communication with said particle collection chamber.
15. The gas turbine engine in accordance with claim 10 , wherein said metering passage is formed at a second acute angle to said access passage, and wherein said first acute angle is larger than said second acute angle.
16. The gas turbine engine in accordance with claim 10 , wherein said metering passage intersects said access passage at a distance below said outer surface of said substrate.
17. The gas turbine engine in accordance with claim 16 , wherein said particle collection chamber is defined between said outer surface of said substrate and the intersection distance of said metering passage.
18. The gas turbine engine in accordance with claim 10 , wherein said metering passage comprises a first diameter, and said access passage comprises a second diameter larger than said first diameter.