BLADE FOR A GAS TURBINE, METHOD FOR MANUFACTURING A TURBINE BLADE, AND GAS TURBINE WITH A BLADE
First Claim
1. A blade for a gas turbine having a rotor shaft, the blade comprising:
- an airfoil extending along a longitudinal direction, and a blade root configured and arranged to mount said blade on the rotor shaft, wherein said blade root includes a cooling air supply arranged within said blade root and said airfoil comprises interior cooling channels, which cooling channels extend along the longitudinal direction and can be supplied with cooling air through the blade root cooling air supply;
wherein said blade root comprises a blade channel running transversely through said blade root and being connected to said cooling channels, and an insert positioned in said blade channel and including fluid connections between said blade channel and said cooling channels.
2 Assignments
0 Petitions
Accused Products
Abstract
A blade (30′) for a gas turbine has an airfoil (31) and a blade root (32) for mounting the blade (30) on a rotor shaft of the gas turbine. The airfoil (31) is provided with cooling channels (33, 35) in the interior thereof, which cooling channels (33, 35) preferably extend along the longitudinal direction and can be supplied with cooling air (45) through cooling air supply passages (40-43() within the blade root (32). The blade root (32) includes a blade channel (40) running transversely through the blade root (32) and is connected to the cooling channels (33, 35), and an insert (41) is inserted into the blade channel (40) for determining the final configuration and characteristics of the connections between the blade channel (40) and the cooling channels (33, 35).
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Citations
16 Claims
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1. A blade for a gas turbine having a rotor shaft, the blade comprising:
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an airfoil extending along a longitudinal direction, and a blade root configured and arranged to mount said blade on the rotor shaft, wherein said blade root includes a cooling air supply arranged within said blade root and said airfoil comprises interior cooling channels, which cooling channels extend along the longitudinal direction and can be supplied with cooling air through the blade root cooling air supply; wherein said blade root comprises a blade channel running transversely through said blade root and being connected to said cooling channels, and an insert positioned in said blade channel and including fluid connections between said blade channel and said cooling channels. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 15)
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11. A method for manufacturing a blade, the method comprising:
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forming a blade including casting and using a core to form cooling channels within an airfoil of the blade; machining a blade channel into a blade root of said blade; removing said core from an interior of said airfoil; and inserting an insert into said blade channel. - View Dependent Claims (12, 13, 14, 16)
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Specification