Abstract: A networking device (e.g. edge gateway), configured to host containers to provide application services, for converting data between an IP-Port of the networking device and a serial communication link to enable serial communication between the networking device and a serial interface of a device (e.g. controller, actor, sensor).

Abstract: A photovoltaic apparatus is provided including a first photovoltaic module and a second photovoltaic module. Each photovoltaic module includes a front sheet having an outer portion and an inner portion. The outer portion is disposed around a core to form a keder. Each photovoltaic module further includes a back sheet and a photovoltaic device disposed between the front sheet and the back sheet. Each photovoltaic device includes an array of photovoltaic cells.

Abstract: A photovoltaic apparatus is provided including a first photovoltaic module and a second photovoltaic module. Each photovoltaic module includes a front sheet having an outer portion and an inner portion. The outer portion is disposed around a core to form a keder. Each photovoltaic module further includes a back sheet and a photovoltaic device disposed between the front sheet and the back sheet. Each photovoltaic device includes an array of photovoltaic cells.

Abstract: Embodiments of the present disclosure generally relate to an apparatus and method of forming a photovoltaic module assembly that contains a plurality of interconnected photovoltaic modules that are used to generate an amount of power when exposed to electromagnetic radiation. The formed photovoltaic module assembly will generally include two or more photovoltaic modules that can generate and deliver power to an external grid, external network or external device. The photovoltaic module assembly can be a stand alone power generating device or be disposed within an array of interconnected photovoltaic devices.

Abstract: A flexible photovoltaic apparatus is provided including a photovoltaic device that includes an array of photovoltaic cells having a first end and a second end. The array extends in a first direction from the first end to the second end. The photovoltaic apparatus further includes a first fabric that includes an insulating fabric, a first conductor disposed in the insulating fabric and connected to the first end of the array, and a second conductor disposed in the insulating fabric and connected to the second end of the array.

Abstract: Embodiments of the present disclosure generally relate to an apparatus and method of forming a photovoltaic module assembly that contains a plurality of interconnected photovoltaic modules that are used to generate an amount of power when exposed to electromagnetic radiation. The formed photovoltaic module assembly will generally include two or more photovoltaic modules that can generate and deliver power to an external grid, external network or external device. The photovoltaic module assembly can be a stand alone power generating device or be disposed within an array of interconnected photovoltaic devices.

Abstract: A flexible photovoltaic apparatus is provided including a photovoltaic device that includes an array of photovoltaic cells having a first end and a second end. The array extends in a first direction from the first end to the second end. The photovoltaic apparatus further includes a first fabric that includes an insulating fabric, a first conductor disposed in the insulating fabric and connected to the first end of the array, and a second conductor disposed in the insulating fabric and connected to the second end of the array.

Abstract: A tip material for a turbine blade or for repairing a damaged tip of a turbine blade having a metallic coating, the material used for the tip is equivalent in composition to the metallic coating material used for the turbine blade. Also disclosed is a method of manufacturing or repairing a tip of a turbine blade having a metallic coating by reforming the blade tip with a material equivalent in composition to the metallic coating material used for the turbine blade by bonding the material to the damaged tip.

Abstract: A tip material for a turbine blade or for repairing a damaged tip of a turbine blade having a metallic coating, the material used for the tip is equivalent in composition to the metallic coating material used for the turbine blade. Also disclosed is a method of manufacturing or repairing a tip of a turbine blade having a metallic coating by reforming the blade tip with a material equivalent in composition to the metallic coating material used for the turbine blade by bonding the material to the damaged tip.

Abstract: A tip material for a turbine blade or for repairing a damaged tip of a turbine blade having a metallic coating, the material used for the tip is equivalent in composition to the metallic coating material used for the turbine blade. Also disclosed is a method of manufacturing or repairing a tip of a turbine blade having a metallic coating by reforming the blade tip with a material equivalent in composition to the metallic coating material used for the turbine blade by bonding the material to the damaged tip.

Abstract: In a soldering process for treating tears, recesses, or other material defects in the surface of thermally and mechanically highly stressed components of gas turbines, a nickel foam is applied together with the soldering powder, which can also be mixed with another filler. After this, a heat treatment of the soldering process is performed.

Abstract: A process for treating the surface of a component prior to coating. The component is made from a Ni based superalloy designed for high temperature service. Both the component and the coating include the elements Al and/or Cr. The process includes depleting the outer surface of the component of any one or a combination of Al, Ti or Cr and thereafter applying the coating directly on the depleted surface. The process minimizes the formation of a brittle gamma prime phase within the interdiffusion zone during service of the component. The process can also be used to renew old damaged coatings.

Abstract: In a soldering process for treating tears, recesses, or other material defects in the surface of thermally and mechanically highly stressed components of gas turbines, a nickel foam is applied together with the soldering powder, which can also be mixed with another filler. After this, a heat treatment of the soldering process is performed.

Abstract: A tip material for a turbine blade or for repairing a damaged tip of a turbine blade having a metallic coating, the material used for the tip is equivalent in composition to the metallic coating material used for the turbine blade.

Abstract: Process of plugging cooling holes (4) of a gas turbine component (1) with an external surface (7), having a cavity (2) and a plurality of cooling holes (4) before coating the gas turbine component (4), characterised in that mask material (6) is applied to the external surface (7) of the component (1) while a fluid is forced through the cooling holes (4), the mask material (6) is thickened while the fluid is forced through the cooling holes (4), the cooling holes (4) are plugged with plug material (6b), the mask material (6a) is removed from the external surface (7) of the component (1), the component (1) and the plugged cooling holes (4) are coated and the plug material (6b) is removed from the cooling holes (4).