摘要:
In order to obtain crack-free, homogeneous welds in nickel-based superalloys, laser parameters in respect of the power, the beam diameter, in particular the beam diameter, the mass feed rate, and the speed of advancement, are specifically selected.
摘要:
The invention relates to the targeted selection of process parameters for laser welding, feeding, laser power beam diameter, and powder mass flow, wherein the temperature gradient substantially decisive for single crystal growth during laser application welding can be set deliberately.
摘要:
Welding methods are often carried out using a protective gas but the effect of said gas is often insufficient. According to the invention, the component (4) to be welded is arranged in a process chamber (31).
摘要:
The invention relates to a method for producing a component (1) for a turbomachine, comprising the additive build-up of the component by means of an additive production method from a base material (2) for the component (1) and the introduction of material fibers (3) into a construction for the component (1) during the additive build-up in such a way that the material fibers (3) are oriented in a circumferential direction (A) of the component (1) around a component axis and in such a way that a fiber composite material (4) is produced, comprising the material fibers (3) and a base material (2) that is solidified by means of the additive build-up. The invention further relates to a corresponding component (1) and to a corresponding device for producing the component (1).
摘要:
The invention relates to a method for repairing an airfoil (9) of an axial turbomachine in which material is deposited onto the airfoil (9) by means of deposition welding, and the airfoil (9) is cooled during the deposition welding. The invention further relates to a cooling collar (1) comprising at least one cooling channel (5) which has a coolant inlet (6) and a coolant outlet (7) and through which a coolant flows in the intended state. The cooling collar also comprises multiple cooling elements (8) which are arranged along an inner circumference of the cooling collar (1) and adjacently to the at least one cooling channel (5), said cooling elements resting against an object to be cooled, in particular an airfoil (9) to be cooled, in the intended state.