Article and manifold for thermal adjustment of a turbine component
An article is disclosed including a manifold, an article wall having at least one external aperture, and a post-impingement cavity disposed between the manifold and the article wall. The manifold includes an impingement plate defining a plenum having a plenum surface, and at least one impingement aperture. The at least one impingement aperture interfaces with the plenum at an intake aperture having a flow modification structure, which, together with the at least one impingement aperture, defines an exhaust aperture. The manifold exhausts a fluid from the plenum into the intake aperture, through the at least one impingement aperture, out the exhaust aperture, into the post-impingement cavity, and through the at least one external aperture.
1. An article, comprising:
a manifold including an impingement plate, the impingement plate defining a plenum and at least one impingement aperture, the plenum having a plenum surface and the at least one impingement aperture interfacing with the plenum at an intake aperture;
an article wall including at least one external aperture; and
a post-impingement cavity disposed between the manifold and the article wall, the post-impingement cavity arranged to receive a fluid from the plenum through the at least one impingement aperture and pass the fluid through the at least one external aperture,
wherein the at least one impingement aperture includes:
a flow modification structure in contact with the impingement plate; and
an exhaust aperture, and
wherein the exhaust aperture is defined by:
the flow modification structure; or
the at least one impingement aperture and the flow modification structure.
2. The article of claim 1 , wherein the intake aperture includes an intake area, the exhaust aperture includes at least one exhaust area, and the at least one exhaust area is between 10% to 500% of the intake area.
3. The article of claim 1 , wherein the at least one impingement aperture defines an impingement angle relative to the plenum surface between 30° and 90°.
4. The article of claim 3 , wherein the exhaust aperture deflects from the impingement angle by a deflection angle of up to 60°.
5. The article of claim 1 , wherein the exhaust aperture is defined by the at least one impingement aperture and the flow modification structure, and the exhaust aperture is annular.
6. The article of claim 1 , wherein the exhaust aperture is defined by the at least one impingement aperture and the flow modification structure, and the flow modification structure includes a turbulator.
7. The article of claim 6 , wherein the turbulator includes at least one vane.
8. The article of claim 7 , wherein the at least one vane includes a torsional conformation.
9. The article of claim 1 , wherein the exhaust aperture is defined by the flow modification structure, and the flow modification structure includes a plurality of flow distribution apertures.
10. The article of claim 1 , wherein the exhaust aperture is defined by the flow modification structure, and the flow modification structure includes a directional nozzle.
11. The article of claim 1 , wherein the article is a turbine component selected from the group consisting of an airfoil, a bucket, a nozzle, a shroud, a combustor, and combinations thereof.
12. A manifold, comprising an impingement plate, the impingement plate defining a plenum and at least one impingement aperture, wherein:
the plenum includes a plenum surface;
the at least one impingement aperture interfaces with the plenum at an intake aperture;
the at least one impingement aperture includes a flow modification structure in contact with the impingement plate;
the at least one impingement aperture includes an exhaust aperture;
the exhaust aperture is annular;
the exhaust aperture is defined by the at least one impingement aperture and the flow modification structure; and
the manifold is arranged to exhaust a cooling fluid from the plenum into the intake aperture, through the at least one impingement aperture, and out the exhaust aperture.
13. A manifold, comprising an impingement plate, the impingement plate defining a plenum and at least one impingement aperture, wherein:
the plenum includes a plenum surface;
the at least one impingement aperture interfaces with the plenum at an intake aperture;
the at least one impingement aperture includes a flow modification structure in contact with the impingement plate;
the flow modification structure includes a directional nozzle;
the at least one impingement aperture includes an exhaust aperture;
the exhaust aperture is defined by the flow modification structure; and
the manifold is arranged to exhaust a cooling fluid from the plenum into the intake aperture, through the at least one impingement aperture, and out the exhaust aperture.