Film hole with protruding flow accumulator

A gas turbine engine component, comprising:

• an internal flow path defined by an internal surface and extending from an upstream direction to a downstream direction;
• a component wall including a film hole comprising:
• an inlet defined by the internal surface,
• an outlet defined by an external surface, wherein the film hole extends from the inlet at least partially in the upstream direction,
• a flow accumulator extending from the component wall adjacent the inlet, wherein the flow accumulator is configured to direct fluid into the inlet, through the film hole, and through the outlet, wherein the flow accumulator is at least partially defined by a first surface extending from a sidewall of the film hole in the upstream direction, wherein the first surface is spaced from, faces, and at least partially overlaps the inlet in the upstream direction.