Vacuum brazing of K465 superalloy was carried out by using Co45NiCrWB cobalt-base filler metal at 1220 ℃ for different holding time, and the joint clearance was 0.5 mm pre-filled with FGH95 nickel-base superalloy powder. The effect of the structural constitution of brazed different holding time of temperature on the brazed joint microstructure and properties. The results show that the brazing seam is composed of alloy powder particles and borides among them. It is two-phase structure of γ and γ' with a few small blocks of borides in the powder particles, and there exists phases rich in Cr, W and Nb elements. The powder particles are growing along the holding time during the brazing process, while their combination is expanded. It is good for stress rapture properties of joints that borides was fine in brazing seam with more superalloy powder and proper holding time. And the joints brazed for 30-60 min show higher stress rapture properties.
Microstructure and Mechanical Properties of Wide-gap Brazed Joints of K465 Alloy Using Cobalt-base Brazing Alloy
2017
Article (Journal)
Electronic Resource
Unknown
Metadata by DOAJ is licensed under CC BY-SA 1.0
SILVER AND COPPER ALLOY BRAZED JOINTS FOR AIRCRAFT POWERPLANTS
SAE Technical Papers | 1960
SILVER AND COPPER ALLOY BRAZED JOINTS FOR AEROSPACE PROPULSION SYSTEMS
SAE Technical Papers | 1969
BRAZING ALLOY Nickel Base - 4.5Si - 2.9B
SAE Technical Papers | 1960
BRAZING ALLOY Copper Base 39Mn - 9.5Ni
SAE Technical Papers | 1966
BRAZING ALLOY Nickel Base - 3.5Si - 1.8B
SAE Technical Papers | 1960