http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-20160130991-A

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classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01L3-02
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C22C19-053
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C22C19-055
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C22C19-058
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C22C19-05
filingDate 2015-01-12-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a031388eae130e8bb0b50683983281c2
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f86d60173e469b2a4df9ba21ca854103
publicationDate 2016-11-15-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber KR-20160130991-A
titleOfInvention Hardened nickel-chromium-titanium-aluminum alloy with good wear resistance, creep resistance, corrosion resistance and workability
abstract The present invention relates to a nickel-chromium-titanium alloy having very excellent wear resistance and at the same time having excellent corrosion resistance, excellent creep strength and good processability. - Aluminum alloying alloy comprising 25 to 35 mass% of chromium, 1.0 to 3.0 mass% of titanium, 0.6 to 2.0 mass% of aluminum, 0.005 to 0.10 mass% of carbon, 0.0005 to 0.050 mass% of nitrogen, 0.0005 to 0.030 mass At most 0.010 mass% sulfur, at most 0.020 mass% oxygen, at most 0.70 mass% silicon, at most 2.0 mass% manganese, at most 0.05 mass% magnesium, at most 0.05 mass% calcium, at most 2.0 mass% Up to 0.5 mass% copper, up to 0.5 mass% vanadium, if necessary, from 0 to 20 mass% Fe, and optionally from 0 to 15 mass% cobalt , Phil If a range of 0 to 0.20% by weight Zr, necessary relates to alloy with nickel and conventional processes associated (process-related) of a boron impurity, the remaining amount of 0.0001 to 0.008 mass%. The nickel content is more than 35 mass%. The following relationship is satisfied: Cr + Fe + Co? 26 mass% (1) to obtain excellent abrasion resistance; And fh ≥ 0 (2a), where fh = 6.49 + 3.88 Ti + 1.36 Al - 0.301 Fe + (0.759 - 0.0209 Co) Co - 0.428 Cr - 28.2 to obtain sufficient solidness at higher temperatures C (2); Here, Ti, Al, Fe, Co, Cr and C are the mass% concentration of the element, and fh is expressed in%.
priorityDate 2014-02-04-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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