Diffusing hole for rail effusion
A heat shield panel for use in a gas turbine engine combustor is disclosed. The heat shield panel includes a hot side defining a first surface having an outer perimeter, a cold side defining a second surface spaced from the first surface, a rail member disposed on the cold side proximate a first portion of the outer perimeter, the rail member having an outer wall and an inner wall, and an orifice extending through the rail member, from the inner wall to the outer wall, the orifice having a cross sectional area that increases from the inner wall to the outer wall.
1. A heat shield panel for use in a gas turbine engine combustor, comprising:
a hot side defining a first surface having an outer perimeter;
a cold side defining a second surface spaced from the first surface;
a rail member disposed on the cold side proximate a first portion of the outer perimeter, the rail member having an outer wall and an inner wall; and
an orifice extending through the rail member, from the inner wall to the outer wall, the orifice having a cross sectional area that increases from the inner wall to the outer wall,
wherein the orifice includes an inner opening positioned on the inner wall, the inner opening having a portion in contact with and tangent to the second surface.
2. The heat shield panel of claim 1 , wherein the orifice includes an outer opening positioned on the outer wall, the outer opening positioned to direct a flow of air through the orifice toward an engine component positioned adjacent the rail member.
3. The heat shield panel of claim 2 , wherein the engine component is a second panel positioned adjacent the rail member.
4. The heat shield panel of claim 1 , wherein the inner opening positioned on the inner wall includes a circular cross section and the orifice includes an outer opening positioned on the outer wall that includes an oval cross section.
5. The heat shield panel of claim 1 , wherein the outer perimeter has a rectangular shape and the first surface and the second surface have an arcuate shape.
6. The heat shield panel of claim 5 , wherein the rail member extends entirely about the rectangular shape of the outer perimeter.
7. The heat shield panel of claim 5 , wherein the outer perimeter includes a first side and a second side spaced in a circumferential direction from the first side, the first side including the rail member and the second side including a second rail member, the second rail member having a second orifice extending therethrough, the second orifice having a second cross sectional area that increases from a second inner wall to a second outer wall.
8. The heat shield panel of claim 5 , wherein the outer perimeter includes a first side and a second side spaced in an axial direction from the first side, the first side including the rail member and the second side including a second rail member, the second rail member having a second orifice extending therethrough, the second orifice having a second cross sectional area that increases from a second inner wall to a second outer wall.
9. The heat shield panel of claim 8 , wherein the outer perimeter includes a third side and a fourth side spaced in a circumferential direction from the third side, the third side including a third rail member and the fourth side including a fourth rail member, the third rail member having a third orifice extending therethrough, the third orifice having a third cross sectional area that increases from a third inner wall to a third outer wall and the fourth rail member having a fourth orifice extending therethrough, the fourth orifice having a fourth cross sectional area that increases from a fourth inner wall to a fourth outer wall.
10. A heat shield panel for use in a gas turbine engine combustor, comprising:
a hot side defining a first surface having an outer perimeter;
a cold side defining a second surface spaced from the first surface;
a rail member disposed on the cold side proximate a first portion of the outer perimeter, the rail member having an outer wall and an inner wall; and
a diffusing hole extending through the rail member, from the inner wall to the outer wall,
wherein the diffusing hole includes an inner opening positioned on the inner wall, the inner opening having a portion in contact with and tangent to the second surface.
11. The heat shield panel of claim 10 , wherein the diffusing hole includes an outer opening positioned on the outer wall, the outer opening positioned to direct a flow of air through the diffusing hole toward an engine component positioned adjacent the rail member.
12. The heat shield panel of claim 10 , wherein the inner opening positioned on the inner wall includes a circular cross section and the diffusing hole includes an outer opening positioned on the outer wall that includes an oval cross section.
13. The heat shield panel of claim 12 , wherein the diffusing hole includes a cross sectional area that increases in size continuously from the inner opening to the outer opening.