Turbine blades
First Claim
1. A cast turbine blade comprising:
- a blade root and a blade tip;
at least one internal cooling passage that passes from an inlet in the blade root to an outlet in the blade tip, the cooling passage having a zone that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured along the cooling passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line;
a supplementary passage that extends between the zone and the inlet through an internal wall of the cooling passage, wherein the supplementary passage is elongate and passes in a straight line from an aperture in an external surface of a base of the blade root, through the blade root, the inlet and the internal wall, to the zone; and
a plug which obturates the supplementary passage, wherein the plug is elongate and substantially co-extensive with the supplementary passage.
3 Assignments
0 Petitions
Accused Products
Abstract
A cast turbine blade is disclosed and includes an internal cooling passage that passes (e.g., zig-zags or meanders) through the blade from an inlet in the blade root to an outlet in the blade tip. The cooling passage can have a zone at a bend that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured around the passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line. During casting of the blade, the cooling passage can be defined by a core or cores having a leachable material, the cores being removed after casting by a chemical leaching process. A supplementary passage is also provided for connecting the remote zone to the inlet during the leaching process. The supplementary passage can likewise be defined by a leachable core, or it may be machined into the blade after casting. During the service life of the blade, a plug can be used to obturate the supplementary passage to prevent leakage of cooling air from the cooling passage through the supplementary passage.
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Citations
13 Claims
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1. A cast turbine blade comprising:
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a blade root and a blade tip; at least one internal cooling passage that passes from an inlet in the blade root to an outlet in the blade tip, the cooling passage having a zone that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured along the cooling passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line; a supplementary passage that extends between the zone and the inlet through an internal wall of the cooling passage, wherein the supplementary passage is elongate and passes in a straight line from an aperture in an external surface of a base of the blade root, through the blade root, the inlet and the internal wall, to the zone; and a plug which obturates the supplementary passage, wherein the plug is elongate and substantially co-extensive with the supplementary passage. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. A method of manufacturing a turbine blade using the lost wax casting process, the method comprising:
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casting a cooling passage that extends from an inlet in a root portion of the blade to an outlet in a tip portion of the blade, the cooling passage having a zone that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured along the passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line; casting a supplementary passage for connecting the zone to the inlet during the manufacture of the blade, wherein the supplementary passage extends from an external surface of a base of the blade root, through the blade root, the inlet and an internal wall defining the cooling passage, to the zone, and wherein the cooling passage and the supplementary passage are defined by at least one core comprising a leachable material; and obturating the supplementary passage after removal of the core material by inserting a metallic plug into the supplementary passage to prevent leakage of cooling air through the supplemental passage, from the zone into the inlet, and leakage of cooling air through supplemental passage blade root portion from the inlet to an exterior. - View Dependent Claims (9, 10, 11, 12)
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13. A method of manufacturing a turbine blade using the lost wax casting process, the method comprising:
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casting a cooling passage that extends from an inlet in a root portion of the blade to an outlet in a tip portion of the blade, the cooling passage having a zone that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured along the passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line; machining a supplementary passage for connecting the zone to the inlet during the manufacture of the blade, wherein the supplementary passage extends from an external surface of a base of the blade root, through the blade root, the inlet and an internal wall defining the cooling passage, to the zone, and wherein the cooling passage and the supplementary passage are defined by at least one core comprising a leachable material; and obturating the supplementary passage after removal of the core material by inserting a metallic plug into the supplementary passage to prevent leakage of cooling air through the supplemental passage, from the zone into the inlet, and leakage of cooling air through supplemental passage blade root portion from the inlet to an exterior.
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Specification