Wide gap brazing (WGB) is a cost effective and reliable means to repair gas turbine hot section components with defect sizes exceeding 0.3 mm. However, it has been shown that WGB joints of nickel-based superalloys suffer from reduced ductility and thermal fatigue life due to the presence of brittle intermetallics and porosities in the brazed joint. In order to disperse the brittle intermetallic compounds, potentially increase the ductility of the repaired region, and reduce the risk of the thermo-mechanical fatigue failure, elemental tungsten (W) was added to the braze additive filler alloy IN738 by mechanical alloying. The alloyed IN738 was then brazed with the addition of 30, 50 and 80 wt% of braze alloy (BNi-9). After brazing at 1200\ub0...
Tungsten is a promising armour material for plasma facing components of nuclear fusion reactors (NFR...
In the developing DEMO divertor, the design of joints between tungsten to other fusion related mater...
Gas turbine engines for future subsonic transports will probably have higher pressure ratios which w...
Wide gap brazing (WGB) of X-40 cobalt based superalloy was conducted in this study using BNi-9 braze...
In the braze repair of gas turbine components, substituting the parent metal with dissimilar metals ...
In this work, nickel-based braze reservoirs embedded in single crystal nickel-based superalloy subst...
In this study, the third-generation rhenium containing single crystal superalloy was brazed by mixed...
Both aviation and land based turbine components such as vanes/nozzles, combustion chambers, liners, ...
Fractures in blade sections of Inconel 725 were impregnated with tungsten nanoparticles and jointed ...
peer-reviewedTo emulate combined welding and brazing techniques, frequently used during the rejuvena...
One of the most promising structural materials in gas turbine engineering is the alloys based on an ...
Metallurgical joining is a common repair process in the aviation industry involving nickel superallo...
W–W brazed joints (tungsten block: 8 × 8 × 4 mm joined to an actively cooled copper heat sink) were ...
The qualification process of the materials and components for the next generation of fusion reactors...
Research article with tables, illustrations, and graphs.Many industrial components such as heat exch...
Tungsten is a promising armour material for plasma facing components of nuclear fusion reactors (NFR...
In the developing DEMO divertor, the design of joints between tungsten to other fusion related mater...
Gas turbine engines for future subsonic transports will probably have higher pressure ratios which w...
Wide gap brazing (WGB) of X-40 cobalt based superalloy was conducted in this study using BNi-9 braze...
In the braze repair of gas turbine components, substituting the parent metal with dissimilar metals ...
In this work, nickel-based braze reservoirs embedded in single crystal nickel-based superalloy subst...
In this study, the third-generation rhenium containing single crystal superalloy was brazed by mixed...
Both aviation and land based turbine components such as vanes/nozzles, combustion chambers, liners, ...
Fractures in blade sections of Inconel 725 were impregnated with tungsten nanoparticles and jointed ...
peer-reviewedTo emulate combined welding and brazing techniques, frequently used during the rejuvena...
One of the most promising structural materials in gas turbine engineering is the alloys based on an ...
Metallurgical joining is a common repair process in the aviation industry involving nickel superallo...
W–W brazed joints (tungsten block: 8 × 8 × 4 mm joined to an actively cooled copper heat sink) were ...
The qualification process of the materials and components for the next generation of fusion reactors...
Research article with tables, illustrations, and graphs.Many industrial components such as heat exch...
Tungsten is a promising armour material for plasma facing components of nuclear fusion reactors (NFR...
In the developing DEMO divertor, the design of joints between tungsten to other fusion related mater...
Gas turbine engines for future subsonic transports will probably have higher pressure ratios which w...