TURBINE ROTOR BLADES WITH TIP PORTION PARAPET WALL CAVITIES
First Claim
1. A turbine rotor blade for a turbine section of an engine, the turbine rotor blade comprising:
- a platform; and
an airfoil extending from the platform into a mainstream gas path of the turbine section, the airfoil comprisinga first side wall;
a second side wall joined to the first side wall at a leading edge and a trailing edge;
a tip cap extending between the first side wall and the second side wall;
a first parapet wall extending from the first side wall;
a first parapet wall cavity formed at least partially within the first parapet wall; and
a first cooling hole extending between the first parapet wall cavity and a first surface of the first parapet wall such that cooling air flows through the first parapet wall cavity, through the first cooling hole, and out of the first parapet wall.
1 Assignment
0 Petitions
Accused Products
Abstract
In accordance with an exemplary embodiment, a turbine rotor blade is provided for a turbine section of an engine. The turbine rotor blade includes a platform and an airfoil extending from the platform into a mainstream gas path of the turbine section. The airfoil includes a first side wall; a second side wall joined to the first side wall at a leading edge and a trailing edge; a tip cap extending between the first side wall and the second side wall; a first parapet wall extending from the first side wall; a first parapet wall cavity formed at least partially within the first parapet wall; and a first cooling hole extending between the first parapet wall cavity and a first surface of the first parapet wall such that cooling air flows through the first parapet wall cavity, through the first cooling hole, and out of the first parapet wall.
9 Citations
20 Claims
-
1. A turbine rotor blade for a turbine section of an engine, the turbine rotor blade comprising:
-
a platform; and an airfoil extending from the platform into a mainstream gas path of the turbine section, the airfoil comprising a first side wall; a second side wall joined to the first side wall at a leading edge and a trailing edge; a tip cap extending between the first side wall and the second side wall; a first parapet wall extending from the first side wall; a first parapet wall cavity formed at least partially within the first parapet wall; and a first cooling hole extending between the first parapet wall cavity and a first surface of the first parapet wall such that cooling air flows through the first parapet wall cavity, through the first cooling hole, and out of the first parapet wall. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17)
-
-
18. An airfoil for a turbine blade, the airfoil comprising
a first side wall; -
a second side wall joined to the first side wall at a leading edge and a trailing edge; a tip cap extending between the first side wall and the second side wall; a first parapet wall extending from the first side wall; a first parapet wall cavity formed at least partially within the first parapet wall; and a first cooling hole extending between the first parapet wall cavity and a first surface of the first parapet wall such that cooling air flows through the first parapet wall cavity, through the first cooling hole, and out of the first parapet wall. - View Dependent Claims (19, 20)
-
Specification