Engine component assembly with a cooling aperture
An engine component assembly with a first substrate having a hot surface in thermal communication with a hot combustion gas flow and a cooling surface, with the cooling surface being different than the hot surface, a second substrate having a first surface in fluid communication with a cooling fluid supply and a second surface, different from the first surface, facing and spaced from the cooling surface to define at least one interior cavity. At least one cavity is provided within the first substrate defining a cavity surface where at least a portion of the cavity surface is directly opposite the second surface. At least one cooling aperture extending through the second substrate from the first surface to the second surface, and defining a streamline along which a cooling fluid passes from the cooling fluid supply to the at least one interior cavity.
1 . An engine component assembly, comprising:
a first substrate having a hot surface in thermal communication with a hot combustion gas flow and a cooling surface, with the cooling surface being different than the hot surface;
a second substrate having a first surface in fluid communication with a cooling fluid supply and a second surface, different from the first surface, facing and spaced from the cooling surface to define at least one interior cavity;
at least one cavity provided within the first substrate defining a cavity surface where at least a portion of the cavity surface is directly opposite the second surface; and
at least one cooling aperture extending through the second substrate from the first surface toward the cooling surface at a first non-orthogonal angle with respect to the first surface, and defining a streamline along which a cooling fluid passes from the cooling fluid supply to the at least one interior cavity, and where the at least one cooling aperture is located directly opposite the cooling surface;
wherein the at least one cooling aperture and the at least one cavity are arranged such that the at least one cooling aperture is directed toward the cavity surface and the at least one cavity is downstream from the at least one cooling aperture.
2 . The engine component assembly of claim 1 wherein the streamline extends into the at least one cavity at an angle near parallel with the cavity surface.
3 . The engine component assembly of claim 1 further comprising a line spaced from the cavity surface extending from and parallel to the cooling surface, wherein the streamline and the line form a second non-orthogonal angle.
4 . The engine component assembly of claim 3 wherein the second non-orthogonal angle is an acute angle.
5 . The engine component assembly of claim 1 wherein the at least one cavity comprises a plurality of cavities.
6 . The engine component assembly of claim 5 wherein the at least one cooling aperture comprises at least one cooling aperture for each of the plurality of cavities.
7 . The engine component assembly of claim 1 wherein the at least one cavity comprises a dimple or a channel.
8 . The engine component assembly of claim 1 wherein the at least one cavity has a leading edge and a trailing edge relative to a flow of the cooling fluid in the at least one interior cavity and a cooling feature is provided at or by the trailing edge.
9 . The engine component assembly of claim 8 wherein the streamline intersects the at least one cavity at the leading edge.
10 . The engine component assembly of claim 8 wherein the cooling feature has a leading edge and a trailing edge relative to the flow of the cooling fluid, and the cooling feature leading edge forms a transition with the at least one cavity.
11 . The engine component assembly of claim 1 wherein the at least one cooling aperture is defined by a louver in the second substrate.
12 . The engine component assembly of claim 1 wherein the first substrate defines a first engine component, the first engine component being at least one of a nozzle, a vane, a blade, a shroud, a combustor liner, or a combustor deflector.
13 . The engine component assembly of claim 12 wherein the second substrate comprises a wall located within an interior of the first engine component.
14 . The engine component assembly of claim 1 wherein the at least one cavity has a leading edge and a trailing edge relative to a flow of the cooling fluid in the at least one interior cavity and the cooling surface is parallel to the second surface at a location directly opposite the at least one cooling aperture and extending upstream from the leading edge.
15 . A method of cooling an engine component assembly, the method comprising:
flowing a cooling fluid through at least one cooling aperture from a cooling fluid supply toward a first substrate to define a cooling surface, the first substrate spaced from a second substrate to define an interior cavity, the at least one cooling aperture located within the second substrate, formed at a non-orthogonal angle with respect to the cooling surface, and defining a streamline;
directing the cooling fluid flow along the streamline toward at least one cavity provided within the first substrate downstream of the at least one cooling aperture;
impinging the cooling fluid flow on a cavity surface defining the at least one cavity; and
cooling the first substrate.
16 . The method of claim 15 , wherein impinging the cooling fluid flow comprises impinging the cooling fluid flow onto a leading edge of the at least one cavity.
17 . The method of claim 15 , further comprising flowing the cooling fluid flow through a louver, the louver defining the at least one cooling aperture.
18 . An engine component assembly, comprising:
a first engine component having a hot surface in thermal communication with a hot combustion gas flow and a cooling surface;
at least one cavity recessed within the cooling surface and having a cavity surface;
a second engine component having a first surface in fluid communication with a cooling fluid supply and a second surface facing and spaced from the cooling surface to define a space between the second surface and the cooling surface; and
at least one cooling aperture extending through the second engine component from the first surface toward the cooling surface at a non-orthogonal angle with respect to the first surface;
wherein the at least one cooling aperture and the at least one cavity are arranged such that the at least one cooling aperture is directed toward the cavity surface and the at least one cavity is downstream from the at least one cooling aperture.