EP 4359579 A1 20240501 - NICKEL-BASED SUPERALLOY, SINGLE-CRYSTAL BLADE AND TURBOMACHINE
Title (en)
NICKEL-BASED SUPERALLOY, SINGLE-CRYSTAL BLADE AND TURBOMACHINE
Title (de)
SUPERLEGIERUNG AUF NICKELBASIS, EINKRISTALLINE SCHAUFEL UND TURBOMASCHINE
Title (fr)
SUPERALLIAGE A BASE DE NICKEL, AUBE MONOCRISTALLINE ET TURBOMACHINE
Publication
Application
Priority
- FR 2106614 A 20210622
- FR 2022051112 W 20220610
Abstract (en)
[origin: WO2022269158A1] A nickel-based superalloy comprises in weight percentages: 5.4 to 6.0% of aluminium, 7.5 to 9.0% of tantalum, 0.10 to 0.25% of titanium, 5.5 to 7.5% of cobalt, 4.0 to 5.5% of chromium, 0.10 to 0.70% of molybdenum, 4.0 to 5.0% of tungsten, 4.8 to 6.2% of rhenium, 0.04 to 0.15% of hafnium, 0 to 0.15% of silicon, the remainder consisting of nickel and unavoidable impurities. The invention also relates to a single-crystal blade (20A, 20B) comprising such an alloy and to a turbomachine (10) comprising such a blade (20A, 20B).
IPC 8 full level
C22C 19/05 (2006.01); F01D 5/28 (2006.01)
CPC (source: EP US)
C22C 19/057 (2013.01 - EP US); C23C 28/347 (2013.01 - US); C30B 29/52 (2013.01 - US); F01D 5/28 (2013.01 - EP); C22C 2200/00 (2013.01 - US); F05D 2300/175 (2013.01 - EP); F05D 2300/611 (2013.01 - EP)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
Designated validation state (EPC)
KH MA MD TN
DOCDB simple family (publication)
FR 3124195 A1 20221223; FR 3124195 B1 20230825; CN 117651782 A 20240305; EP 4359579 A1 20240501; US 2024344180 A1 20241017; WO 2022269158 A1 20221229
DOCDB simple family (application)
FR 2106614 A 20210622; CN 202280047634 A 20220610; EP 22735212 A 20220610; FR 2022051112 W 20220610; US 202218573255 A 20220610