US2014064939A1PendingUtilityA1
High-reliablity turbine metal sealing material
Est. expiryJun 29, 2029(~3 yrs left)· nominal 20-yr term from priority
C22C 19/00C23C 28/02Y10T428/249981F01D 11/001C22C 19/058Y10T428/249989C23C 30/00F05D 2300/509F01D 11/122F05D 2220/31Y10T428/249961C23C 4/073F01D 11/02C22C 19/07Y10T428/249974
57
PatentIndex Score
0
Cited by
0
References
0
Claims
Abstract
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.
Claims
exact text as granted — not AI-modified1 - 7 . (canceled)
8 . A turbine metal sealing material arranged in 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 60 to 65% and the porosity of the lower layer is 67 to 75%.
9 . The turbine metal sealing material according to claim 8 , wherein the porous metal layer comprises, as a main component, an MCrAlY alloy where M is either one of the Ni and Co or both thereof, and hexagonal boron nitride (h-BN).
10 . The turbine metal sealin material according to claim 9 , wherein the MCrAl 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.
11 . The turbine metal sealing material according to claim 8 , 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.
12 . The turbine metal sealing material according to claim 8 , wherein the metal sealing material is used in a steam turbine.
13 . A steam turbine, comprising a metal sealing material according to claim 8 .Cited by (0)
No later patents cite this yet.
References (0)
No backward citations on record.