Manufacturing of hot structural components for aero engines requires the materials being used to beweldable. The high demands on strength and temperature resistance make nickel based superalloys thematerial of choice for this application. Alloy 718 has been the standard grade for several years,providing high strength at elevated temperatures while being weldable due to the relatively slowprecipitation kinetics of its hardening phase gamma double prime. Increasing operating temperaturesas well as intermittent cycling of land-based gas and steam turbines motivate research on highlytemperature stable alloys such as nickel based superalloys. Increased temperature stability ofprecipitation hardening superalloys is generally achieved via the gamm...
The nickel-base superalloy Rene 80 is considered very susceptible to liquation and strain-age crack...
An extensive experimental study on a nickel-based superalloy, Rene 80 using autogenous laser weldin...
Hot cracking susceptibility of fillers 52 and 82 in 800H and 825 nickel-base superalloys was discuss...
High temperature resistance and strength requirements make nickel-based superalloys the material of ...
Usable weldability data is desired in the manufacturing industry, especially within the aerospace in...
This paper reviews the literature with emphasis on strain age cracking, a cracking phenomenon that c...
Precipitation hardened Ni- and Ni-Fe- based superalloys, used in hot structural components for aero ...
HAYNES ® 282 ® alloy is a wrought gamma-prime (γ') strengthened Ni-base superalloy that was develope...
This paper reviews the inherent weldability of precipitation hardening Ni-based superalloys commonly...
The electron beam welding process is used to investigate the weldability of the Ni-based superalloy ...
Superalloys and in particular the precipitation hardened Ni-based superalloys have always been used ...
Precipitation-hardened nickel-based superalloys find wide applications in aero engines and land-base...
The aim of this study was to present the hot cracking behavior of a blade originating from a turbine...
[[abstract]]Superalloys Haynes 230 is one of several high strength precipitated hardened Ni-base sup...
Nickel based superalloys are an integral material for gas turbines, where their excellent high temp...
The nickel-base superalloy Rene 80 is considered very susceptible to liquation and strain-age crack...
An extensive experimental study on a nickel-based superalloy, Rene 80 using autogenous laser weldin...
Hot cracking susceptibility of fillers 52 and 82 in 800H and 825 nickel-base superalloys was discuss...
High temperature resistance and strength requirements make nickel-based superalloys the material of ...
Usable weldability data is desired in the manufacturing industry, especially within the aerospace in...
This paper reviews the literature with emphasis on strain age cracking, a cracking phenomenon that c...
Precipitation hardened Ni- and Ni-Fe- based superalloys, used in hot structural components for aero ...
HAYNES ® 282 ® alloy is a wrought gamma-prime (γ') strengthened Ni-base superalloy that was develope...
This paper reviews the inherent weldability of precipitation hardening Ni-based superalloys commonly...
The electron beam welding process is used to investigate the weldability of the Ni-based superalloy ...
Superalloys and in particular the precipitation hardened Ni-based superalloys have always been used ...
Precipitation-hardened nickel-based superalloys find wide applications in aero engines and land-base...
The aim of this study was to present the hot cracking behavior of a blade originating from a turbine...
[[abstract]]Superalloys Haynes 230 is one of several high strength precipitated hardened Ni-base sup...
Nickel based superalloys are an integral material for gas turbines, where their excellent high temp...
The nickel-base superalloy Rene 80 is considered very susceptible to liquation and strain-age crack...
An extensive experimental study on a nickel-based superalloy, Rene 80 using autogenous laser weldin...
Hot cracking susceptibility of fillers 52 and 82 in 800H and 825 nickel-base superalloys was discuss...