Turbine engine component with deflector

1. An airfoil for a turbine engine, the airfoil comprising:

an outer wall having an outer surface and an inner surface bounding an interior space, the outer wall defining a pressure side and a suction side extending axially between a leading edge and a trailing edge defining a chord-wise direction and extending radially between a root and a tip defining a span-wise direction;

a first rib extending between the outer wall on the pressure side and the suction side, and defining a corner at a junction between the first rib and the outer wall;

a cooling passage located in the interior space and at least partially defining a cooling circuit and defining a flow direction;

a second rib extending from the outer wall and at least partially defining the cooling passage, the second rib spaced from the first rib;

multiple film holes extending through the outer wall, each film hole having an inlet provided on the inner surface and an outlet provided on the outer surface; and

multiple deflectors, with each deflector of the multiple deflectors positioned at the corner such that a portion of each deflector of the multiple deflectors is provided along the outer wall at the first rib, with each having a deflector height provided in the cooling passage, and with each deflector of the multiple deflectors positioned upstream of spaced from each film hole of the multiple film holes by a spacing distance within ten deflector heights of the nearest film hole of the multiple film holes relative to the flow direction;

wherein each deflector of the multiple deflectors is provided at the first rib but spaced from the second rib.

2. The airfoil of claim 1 wherein there is one deflector for every film hole, and the multiple deflectors and the multiple film holes are arranged in an alternating manner.

3. The airfoil of claim 1 wherein the multiple deflectors each includes a ramp facing the flow direction.

4. The airfoil of claim 1 wherein the multiple deflectors are rounded.

5. The airfoil of claim 1 wherein the multiple deflectors mount to the inner surface of the outer wall and includes a fillet at a junction between the multiple deflectors and the outer wall.

6. A component for a turbine engine, the component comprising:

an outer wall having an outer surface and an inner surface at least partially bounding an interior space;

a first rib extending from the outer wall into the interior space, the first rib defining a first corner at a junction between the first rib and the outer wall;

a second rib extending from the outer wall into the interior space, the second rib defining a second corner at the junction between the second rib and the outer wall;

a cooling passage located in the interior space along the inner surface of the outer wall, the first rib, and the second rib, and at least partially defining a cooling circuit and defining a flow direction for a fluid passing along the cooling passage;

multiple film holes extending through the outer wall with each film hole of the multiple film holes having an inlet provided on the inner surface at the first corner, and an outlet provided on the outer surface; and

multiple deflectors, with each deflector of the multiple deflectors having a deflector height and positioned at the first corner and spaced from the second corner, with each deflector of the multiple deflectors spaced from the film hole along the flow direction by a spacing distance being no more than ten deflector heights.

7. The component of claim 6 wherein the deflector includes a fillet at the junction between each deflector of the multiple deflectors and the outer wall.

8. The component of claim 7 wherein the multiple film holes extend through the fillet.