Hot part of gas turbine, gas turbine including the same, and manufacturing method of hot part of gas turbine
View Patent ↗A hot part ( 450 ) of a gas turbine includes a planar member having a gas path surface ( 451 ) that faces at least one of an inner side and an outer side in a radial direction of the rotor in a combustion gas flow path. A cooling flow path is formed in an interior of the planar member along an outer peripheral surface ( 452 ) that intersects the gas path surface ( 451 ). The planar member has an outer peripheral surface side turbulator ( 482 ) that protrudes from an inner surface on an outer peripheral surface ( 452 ) side of the cooling flow path.
1. A hot part of a gas turbine that defines a ring-shaped combustion gas flow path around a rotor, the combustion gas flow path having combustion gas flowing therethrough, the hot part comprising:
a planar member that includes a gas path surface, the gas path surface facing at least one of an inner side and an outer side in a radial direction of the rotor in the combustion gas flow path,
wherein the planar member includes a cooling flow path that is formed in an interior of the planar member along an outer peripheral surface that intersects the gas path surface, and an outer peripheral surface side turbulator that protrudes from an inner surface on the outer peripheral surface side of the cooling flow path, and
wherein the hot part further comprises a gas path surface side turbulator that protrudes from an inner surface on the gas path surface side of the cooling flow path.
2. The hot part of a gas turbine according to claim 1 , wherein
the cooling flow path is formed by a channel portion recessed from the outer peripheral surface of the planar member, and a cover portion that blocks an opening of the channel portion; and
the outer peripheral surface side turbulator is provided on the cover portion.
3. The hot part of a gas turbine according to claim 1 , wherein
the cooling flow path is formed by a channel portion recessed from the outer peripheral surface of the planar member, and a cover portion that blocks an opening of the channel portion;
the outer peripheral surface side turbulator is provided on the cover portion; and
the gas path surface side turbulator is provided on the channel portion.
4. The hot part of a gas turbine according to claim 1 , wherein
the cooling flow path is formed by a channel portion recessed from the outer peripheral surface of the planar member, and a cover portion that blocks an opening of the channel portion; and
the outer peripheral surface side turbulator and the gas path surface side turbulator are provided on the cover portion.
5. A gas turbine comprising the hot part of a gas turbine according to claim 1 .
6. A manufacturing method of a hot part of a gas turbine that defines a ring-shaped combustion gas flow path around a rotor, the combustion gas flow path having combustion gas flowing therethrough, the method comprising:
a channel portion forming step of forming a channel portion recessed from an outer peripheral surface that intersects a gas path surface along the outer peripheral surface in a planar member, the planar member including the gas path surface that faces at least one of an inner side and an outer side in a radial direction of the rotor in the combustion gas flow path;
a cover portion forming step of forming a cover portion that blocks an opening of the channel portion; and
a cover portion fixing step of fixing the cover portion to the channel portion;
the cover portion forming step forming an outer peripheral surface side turbulator that protrudes from the cover portion; and
the cover portion fixing step fixing the outer peripheral surface side turbulator toward the channel portion, wherein
the channel portion forming step forms a gas path surface side turbulator that protrudes from an inner surface on the gas path surface side of the channel portion by performing machining from the outer peripheral surface side.