Gas turbine hot part and gas turbine

Patent metadata

Field	Value
Publication number	US-11085326-B2
Application number	US-201716345879-A
Country	US
Kind code	B2
Filing date	Nov 29, 2017
Priority date	Nov 30, 2016
Publication date	Aug 10, 2021
Grant date	Aug 10, 2021

Abstract

A gas turbine hot part includes: a body portion; a porous portion forming at least a part of the body portion or disposed on at least a part of the body portion and allowing a cooling gas to pass therethrough; and at least one filter disposed upstream of the porous portion in a flow direction of the cooling gas and capable of trapping foreign substances that cannot pass through the porous portion.

First claim

The invention claimed is:

1. A gas turbine hot part comprising:
a body portion;
a porous portion on at least a part of the body portion, the porous portion being configured to allow a cooling gas to pass therethrough; and
at least one filter upstream of the porous portion in a flow direction of the cooling gas, the at least one filter being capable of trapping substances that cannot pass through the porous portion,
wherein:
a cooling gas supply hole for supplying the cooling gas to the porous portion extends through the at least the part of the body portion from an inlet of the at least the part of the body portion to an outlet of the at least the part of the body portion;
a cross-sectional area of the cooling gas supply hole decreases toward the outlet of the at least the part of the body portion in the flow direction of the cooling gas; and
the at least one filter is inside the cooling gas supply hole at the inlet of the at least the part of the body portion in the flow direction of the cooling gas; and
the at least one filter does not extend to the outlet of the at least the part of the body portion in the flow direction of the cooling gas.

2. The gas turbine hot part according to claim 1 ,
wherein the body portion includes a cavity between the cooling gas supply hole and the porous portion, and the cavity has a cross-sectional area which is larger than the cross-sectional area of the cooling gas supply hole.

3. The gas turbine hot part according to claim 1 ,
wherein the body portion or the porous portion is at least a part of a rotor blade, a stator vane, a ring segment, or a combustor.

4. A gas turbine comprising the gas turbine hot part according to claim 1 .

5. The gas turbine hot part according to claim 1 ,
wherein a length of the at least one filter in the flow direction of the cooling gas is shorter than a length of the cooling gas supply hole in the flow direction of the cooling gas.

6. The gas turbine hot part according to claim 1 ,
wherein the porous portion is in contact with the body portion.

7. A gas turbine hot part comprising:
a body portion;
a porous portion on at least a part of the body portion, the porous portion being configured to allow a cooling gas to pass therethrough; and
at least one filter upstream of the porous portion in a flow direction of the cooling gas, the at least one filter being capable of trapping substances that cannot pass through the porous portion,
wherein:
the at least the part of the body portion includes a cooling gas supply hole for supplying the cooling gas to the porous portion;
the at least one filter is sandwiched between the porous portion and the at least the part of the body portion;
the at least one filter includes a first filter and a second filter, the second filter being downstream of the first filter in the flow direction of the cooling gas; and
the first filter is capable of trapping substances smaller than those which the second filter is capable of trapping.

8. The gas turbine hot part according to claim 7 ,
wherein the body portion or the porous portion is at least a part of a rotor blade, a stator vane, a ring segment, or a combustor.

9. A gas turbine comprising the gas turbine hot part according to claim 7 .

10. A gas turbine hot part comprising:
a body portion;
a porous portion on at least a part of the body portion, the porous portion being configured to allow a cooling gas to pass therethrough; and
at least one filter upstream of the porous portion in a flow direction of the cooling gas, the at least one filter being capable of trapping substances that cannot pass through the porous portion,
wherein:
the at least the part of the body portion includes a cooling gas supply hole for supplying the cooling gas to the porous portion;
the at least one filter is sandwiched between the porous portion and the at least the part of the body portion; and
the body portion includes a cavity between the cooling gas supply hole and the porous portion, and the cavity has a cross-sectional area which is larger than a cross-sectional area of the cooling gas supply hole.

11. The gas turbine hot part according to claim 10 ,
wherein the body portion or the porous portion is at least a part of a rotor blade, a stator vane, a ring segment, or a combustor.

12. A gas turbine comprising the gas turbine hot part according to claim 10 .

Assignees

• Mitsubishi Heavy Ind Ltd

Inventors

• Ishiguro Tatsuo

Classifications

• B33Y80/00

  Products made by additive manufacturing · CPC title

• F05D2300/514

  Porosity · CPC title

• B32B9/047

  made of fibres or filaments · CPC title

• B32B2260/046

  Synthetic resin · CPC title

• B32B9/041

  of metal · CPC title