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US 2016/0238248 A1Published application
Bonded combustor wall for a turbine engine
AssigneeUnited Technologies Corporation
InventorsGary D. Roberge, Grant O. Cook, III
Life of this patent
Estimating the term…
Abstract
A combustor wall is provided for a turbine engine. The combustor wall includes a shell, a heat shield and a combustion chamber. The heat shield is connected to the shell by a bonded connection, and defines a portion of the combustion chamber. A cooling cavity is defined between the shell and the heat shield.
Claims20
A combustor wall for a turbine engine, the combustor wall comprising:
- a combustor shell extending axially along a centerline;
- and
- a combustor heat shield extending axially along the centerline, the heat shield connected to the shell by a bonded connection;
- wherein a cooling cavity is defined radially between the shell and the heat shield.
1 more element
A combustor section for a turbine engine, comprising:
- a combustor including a shell, a heat shield and a combustion chamber;
- the heat shield connected to the shell by a bonded connection, and defining a portion of the combustion chamber;
- wherein a cooling cavity is defined between the shell and the heat shield.
Dependencies are inferred from the claim text.