×

COMBUSTOR DOME TILES

  • US 20200132303A1
  • Filed: 10/26/2018
  • Published: 04/30/2020
  • Est. Priority Date: 10/26/2018
  • Status: Active Grant
First Claim
Patent Images

1. A tile for a combustor dome of a gas turbine engine comprising:

  • a tile body defining an upstream surface and an axially opposed downstream surface with at least one injection orifice defined through the tile body from the upstream surface to the downstream surface,wherein the tile body extends in a radial direction from a radially inner surface to a radially outer surface, wherein the radially inner and outer surfaces define circular arcs that are concentric with one another, andwherein the tile body extends circumferentially from a first end face to a second end face, wherein the first end face follows a sigmoid profile and wherein the second end face follows a sigmoid profile configured to interlock with the sigmoid profile of the first end face of another identical tile body.

View all claims
  • 2 Assignments
Timeline View
Assignment View
    ×
    ×