WO2025214648 - A LOW DENSITY NICKEL BASE GAMMA PRIME STRENGTHENED SUPERALLOY, A COMPONENT AND METHOD

National phase entry is expected:
Publication Number WO/2025/214648
Publication Date 16.10.2025
International Application No. PCT/EP2025/055221
International Filing Date 26.02.2025
Title **
[English] A LOW DENSITY NICKEL BASE GAMMA PRIME STRENGTHENED SUPERALLOY, A COMPONENT AND METHOD
[French] SUPERALLIAGE RENFORCÉ PAR GAMMA PRIME À BASE DE NICKEL À FAIBLE DENSITÉ, COMPOSANT ET PROCÉDÉ
Applicants **
SIEMENS ENERGY GLOBAL GMBH & CO. KG
Inventors
HASSELQVIST, Magnus
Priority Data
2405225.0   12.04.2024   GB
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Quotation for National Phase entry

Country StagesTotal
China Filing, Examination, Granting2143
EPO Filing, Examination, Granting10345
Japan Filing, Examination, Granting2325
South Korea Filing, Examination, Granting2276
USA Filing, Examination, Granting13140
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Abstract[English] The invention is a Nickel base gamma prime strengthened superalloy with a composition (in wt%) comprising (in wt%) 3.0 - 13.0 Cobalt (Co), 11.5% - 13.5% Chromium (Cr), 1.5% - 2.0% Molybdenum (Mo), 1.7% - 2.7% Tungsten (W), 3.8% - 4.8% Aluminum (Al), 1.7 - 2.7 Titanium (Ti), 3.8 - 5.5 Niobium (Nb), 0.005 - 0.20 Carbon (C), up to 0.03 Boron (B), up to 0.05 Zirconium (Zr), 0.005 - 0.50 Silicon (Si), up to 2.0 Hafnium (Hf), up to 5.0 Iron (Fe). The rest being Nickel (Ni) and unavoidable impurities. Use of this alloy for conventional, directional solidification or single crystal casting of components, especially later stage blades, in land based gas turbines.[French] L'invention est un superalliage renforcé par gamma prime à base de nickel avec une composition (% en poids) comprenant (en % en poids) entre 3,0 et 13,0 de cobalt (Co), entre 11,5 % et 13,5 % de chrome (Cr), entre 1,5 % et 2,0 % de molybdène (Mo), entre 1,7 % et 2,7 % de tungstène (W), entre 3,8 % et 4,8 % d'aluminium (Al), entre 1,7 et 2,7 de titane (Ti), entre 3,8 et 5,5 de niobium (Nb), entre 0,005 et 0,20 de carbone (C), jusqu'à 0,03 de bore (B), jusqu'à 0,05 de zirconium (Zr), entre 0,005 et 0,50 de silicium (Si), jusqu'à 2,0 d'hafnium (Hf), jusqu'à 5,0 de fer (Fe). Le reste est du nickel (Ni) et des impuretés inévitables. Utilisation de cet alliage pour la solidification dirigée classique ou le coulage monocristallin de composants, notamment de pales d'étape ultérieure, dans des turbines à gaz terrestres.

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