Patent ID: 11959641
Assignee: RTX CORPORATION
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  Y | IPC F

Claim 0:
1. A combustor for use in a gas turbine engine, the combustor comprises:
a heat shield panel having a first surface and a second surface opposite the first surface of the heat shield panel, the heat shield panel having a plurality of effusion apertures extending from the second surface to the first surface; and
a combustor shell having an inner surface and an outer surface opposite the inner surface, the inner surface of the combustor shell and the second surface of the heat shield panel being in a facing spaced relationship defining an impingement cavity therebetween,
wherein the combustor shell further comprises a plurality of impingement apertures each of the plurality of impingement apertures having a nonaxisymmetric shape that has a comma shape, the comma shape being defined by one curved wall and one linear wall, the one linear wall extending from a first end of the one curved wall to a second end of the one curved wall, and
wherein each of the plurality of impingement apertures perpendicularly extend from the outer surface to the inner surface through the combustor shell and each of the plurality of impingement apertures are configured to disperse particulate on the second surface of the heat shield panel.