High-reliability turbine metal sealing material
View Patent ↗A metal sealing material used in a sealing device which can reduce a gap between a stator and a rotor of a turbine. The metal sealing material used in a sealing device for a stator and a rotor of a turbine includes a surface layer and a lower layer composed of a porous metal layer, wherein the porosity of the surface layer is smaller than the porosity of the lower layer; the porosity of the surface layer is 60 to 65% and the porosity of the lower layer is 67 to 75% or less; and the porous metal layer has a thickness of 0.3 to 3.0 mm and may include, as a main component, an MCrAlY alloy where M is either one of Ni and Co or both thereof, and h-BN as a solid lubricant.
1. A turbine metal sealing material used in a sealing device for reducing a fluid leaking from a gap between a stator and a rotor of a turbine,
wherein the metal sealing material comprises a porous metal layer and the porous metal layer comprises a surface layer directly coming into contact with a working fluid and a lower layer lying thereunder,
wherein the porosity of the surface layer is smaller than the porosity of the lower layer,
wherein the porous metal layer comprises, as a main component, an MCrAlY alloy where M is either one of Ni and Co or both thereof, and the MCrAlY alloy comprises 15% to 30% of Cr, 6 to 15% of Al and 0.3 to 1.0% of Y, the balance comprising either one of Ni and Co or both thereof, and
wherein a thickness of the porous metal layer is in the range of 0.3 to 3.0 mm, and a ratio of the surface layer to the lower layer is in the range of 0.1 to 1.0.
2. The turbine metal sealing material according to claim 1 , wherein the porosity of the surface layer is 60 to 65% and the porosity of the lower layer is 67 to 75%.
3. The turbine metal sealing material according to claim 1 , wherein the porous metal layer further comprises hexagonal boron nitride (h-BN).
4. A steam turbine comprising a sealing device for reducing a fluid leaking from a gap between a stator and a rotor of the turbine, a metal sealing material being used in the sealing device,
wherein the metal sealing material comprises a porous metal layer and the porous metal layer comprises a surface layer directly coming into contact with a working fluid and a lower layer lying thereunder,
wherein the porosity of the surface layer is smaller than the porosity of the lower layer,
wherein the porous metal layer comprises, as a main component, an MCrAlY alloy where M is either one of Ni and Co or both thereof, and the MCrAlY alloy comprises 15% to 30% of Cr, 6 to 15% of Al and 0.3 to 1.0% of Y, the balance comprising either one of Ni and Co or both thereof, and
wherein a thickness of the porous metal layer is in the range of 0.3 to 3.0 mm, and a ratio of the surface layer to the lower layer is in the range of 0.1 to 1.0.