Abstract: The invention relates to a method for determining a damage state of components, wherein damage states are determined for a component on the basis of operating states of an overall system that comprises the component by determining time-normalised stress collectives and/or load collectives for each operating state (ZBB), wherein, by means of the time-normalised stress collectives and/or load collectives for each operating state (ZBB) the damage state is determined for the component on the basis of operating states of the overall system that have occurred, and/or the prospective damage state is determined on the basis of predicted prospectively occurring operating states of the overall system that comprises the component, and/or the damage state is determined for a further component, designed similarly to the aforementioned component, depending on operating states that have occurred of a further overall system, which comprises the further component and is designed similarly to the aforementioned overall system,

Abstract: An apparatus for machining a component is provided. The apparatus includes a fixation mechanism, wherein the fixation mechanism includes a first fixation member with a first fixation face and a second fixation member with a second fixation face, wherein the first fixation face and the second fixation face are arranged and configured such that different bearing surfaces of a plurality of different components can be fixed between the first fixation member and the second fixation member, wherein the apparatus further includes a machining device, and wherein the apparatus is configured to machine a machining surface of the respective component by means of the machining device and according to a predetermined accuracy. Further, a method of machining the component is presented.

Abstract: A crane system having a gas turbine that has a manhole on the outer housing thereof, the manhole being designed to open up a maintenance access to hot gas parts of the gas turbine in the open state of the manhole, which is provided with a fastening section; the crane system further has a hoisting mechanism that includes a mating fastening section which is connected to the fastening section of the manhole in such a way that the hoisting mechanism introduces weights that same has to lift into the outer housing of the gas turbine.

Abstract: An apparatus for machining a component is provided. The apparatus includes a fixation mechanism, wherein the fixation mechanism includes a first fixation member with a first fixation face and a second fixation member with a second fixation face, wherein the first fixation face and the second fixation face are arranged and configured such that different bearing surfaces of a plurality of different components can be fixed between the first fixation member and the second fixation member, wherein the apparatus further includes a machining device, and wherein the apparatus is configured to machine a machining surface of the respective component by means of the machining device and according to a predetermined accuracy. Further, a method of machining the component is presented.

Abstract: A crane system having a gas turbine that has a manhole on the outer housing thereof, the manhole being designed to open up a maintenance access to hot gas parts of the gas turbine in the open state of the manhole, which is provided with a fastening section; the crane system further has a hoisting mechanism that includes a mating fastening section which is connected to the fastening section of the manhole in such a way that the hoisting mechanism introduces weights that same has to lift into the outer housing of the gas turbine.

Abstract: A device for installing and removing a component, preferably a burner or a transition pipe of a gas turbine, on or in a stationary gas turbine, is provided. The device includes a rail system having a frame carriage that can be moved along the rail system, on which frame carriage an insertion unit having a carrier unit for the component that can be moved along a movement axis is arranged. In order to specify an especially space-saving and especially rigid design, by means of which components of a gas turbine can be installed and removed relatively simply and quickly, the rail system is designed as a two-track rail system and the movement axis extends between the two rails transversely to an area that extends between the rails.

Abstract: A device for installing and removing a component, preferably a burner or a transition pipe of a gas turbine, on or in a stationary gas turbine, is provided. The device includes a rail system having a frame carriage that can be moved along the rail system, on which frame carriage an insertion unit having a carrier unit for the component that can be moved along a movement axis is arranged. In order to specify an especially space-saving and especially rigid design, by means of which components of a gas turbine can be installed and removed relatively simply and quickly, the rail system is designed as a two-track rail system and the movement axis extends between the two rails transversely to an area that extends between the rails.