HEAT SHIELD PANELS WITH OVERLAP JOINTS FOR A TURBINE ENGINE COMBUSTOR
A combustor wall is provided for a turbine engine. The combustor wall includes a combustor shell and a combustor heat shield that is attached to the shell. The heat shield includes a first panel and a second panel that sealingly engages the first panel in an overlap joint. A cooling cavity extends b...
Saved in:
Main Authors | , |
---|---|
Format | Patent |
Language | English French German |
Published |
15.05.2019
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | A combustor wall is provided for a turbine engine. The combustor wall includes a combustor shell and a combustor heat shield that is attached to the shell. The heat shield includes a first panel and a second panel that sealingly engages the first panel in an overlap joint. A cooling cavity extends between the shell and the heat shield and fluidly couples a plurality of apertures in the shell with a plurality of apertures in the heat shield. |
---|---|
Bibliography: | Application Number: EP20140851011 |