W–W brazed joints (tungsten block: 8 × 8 × 4 mm joined to an actively cooled copper heat sink) were exposed to steady state heat loads to study the effect of the thermal fatigue on their microstructure, mechanical integrity and heat transfer capability. Two different surface temperatures were tested (1000 °C and 1250 °C) varying the number of applied cycles (100 and 1000). The results indicated that a surface temperature of 1000 °C represents the limit condition for the joints to be used in the DEMO fusion reactor, which corresponds to a braze temperature in the range of 562–599 °C according to thermal simulation results. The use of that temperature caused a limited effect on the microstructure and heat transfer capability for both 100 and ...
Tungsten is the leading plasma-facing material (PFM) for nuclear fusion applications. It faces sever...
This paper summarises the challenges in accurately predicting stress states in dissimilar brazed joi...
To improve the efficiency of turbine aero engines, higher operating temperatures and weight savings ...
The qualification process of the materials and components for the next generation of fusion reactors...
To simulate the cyclic HHF operations of the divertor components, actively cooled, brazed joint mock...
Qualification of tungsten (W) and graphite (C) based brazed plasma facing components (PFCs) is an im...
In a future nuclear fusion reactor, the critical divertor component will require dissimilar material...
The preliminary conceptual design of both the blanket and the divertor of the future DEMO reactor en...
In nuclear fusion devices the surfaces directly facing the plasma are irradiated with high energy fl...
A duplex divertor component composed of dissimilar materials experiences considerable thermal stress...
Understanding the residual stress state in brazed joints is crucial for operational design and life ...
CX-2O02U and IG-430U coated by VPS-W were developed as a lighrweight high-Z plasma-facing material. ...
Wide gap brazing (WGB) is a cost effective and reliable means to repair gas turbine hot section comp...
In the braze repair of gas turbine components, substituting the parent metal with dissimilar metals ...
The conceptual designs of the blanket and the helium-cooled divertor of the DEMO reactor require joi...
Tungsten is the leading plasma-facing material (PFM) for nuclear fusion applications. It faces sever...
This paper summarises the challenges in accurately predicting stress states in dissimilar brazed joi...
To improve the efficiency of turbine aero engines, higher operating temperatures and weight savings ...
The qualification process of the materials and components for the next generation of fusion reactors...
To simulate the cyclic HHF operations of the divertor components, actively cooled, brazed joint mock...
Qualification of tungsten (W) and graphite (C) based brazed plasma facing components (PFCs) is an im...
In a future nuclear fusion reactor, the critical divertor component will require dissimilar material...
The preliminary conceptual design of both the blanket and the divertor of the future DEMO reactor en...
In nuclear fusion devices the surfaces directly facing the plasma are irradiated with high energy fl...
A duplex divertor component composed of dissimilar materials experiences considerable thermal stress...
Understanding the residual stress state in brazed joints is crucial for operational design and life ...
CX-2O02U and IG-430U coated by VPS-W were developed as a lighrweight high-Z plasma-facing material. ...
Wide gap brazing (WGB) is a cost effective and reliable means to repair gas turbine hot section comp...
In the braze repair of gas turbine components, substituting the parent metal with dissimilar metals ...
The conceptual designs of the blanket and the helium-cooled divertor of the DEMO reactor require joi...
Tungsten is the leading plasma-facing material (PFM) for nuclear fusion applications. It faces sever...
This paper summarises the challenges in accurately predicting stress states in dissimilar brazed joi...
To improve the efficiency of turbine aero engines, higher operating temperatures and weight savings ...