Abstract: An aircraft structure component (1) for laminar flow including an outer skin (3) having an aerodynamic surface (5), wherein the aerodynamic surface (5) has a leading edge portion (7) and a downstream portion (11) adjacently downstream from the leading edge portion (7), wherein the downstream portion (11) of the aerodynamic surface (5) comprises a paint layer (13) or a foil layer that is not present in the leading edge portion (7), so that a border line (15) is formed between the leading edge portion (7) and the downstream portion (11) by the beginning paint layer (13) or foil layer, and wherein the outer skin (3) comprises an attachment surface (17) to which the paint layer (13) or the foil layer is attached.

Abstract: A wing for an aircraft is disclosed having a main wing, a high lift body, and a connection assembly movably connecting the high lift body to the main wing, such that the high lift body can be moved between a retracted position and at least one extended position. The connection assembly includes a drive system having a first drive unit and a second drive unit, wherein the first drive unit has a first input section coupled to a drive shaft, a first gear unit and a first output section drivingly coupled to a first connection element. The second drive unit has a second input section coupled to the drive shaft, a second gear unit, and a second output section drivingly coupled to a second connection element. The first output section includes a first output wheel and the second output section includes a second output wheel.

Abstract: A wing for an aircraft is disclosed having a main wing, a high lift body, and a connection assembly movably connecting the high lift body to the main wing, such that the high lift body can be moved between a retracted position and at least one extended position. The connection assembly includes a drive system having a first drive unit and a second drive unit, wherein the first drive unit has a first input section coupled to a drive shaft, a first gear unit and a first output section drivingly coupled to the high lift body. The second drive unit has a second input section coupled to the drive shaft, a second gear unit, and a second output section drivingly coupled to the high lift body.

Abstract: A wing for an aircraft including a fixed wing and a high-lift device movable between a retracted position and an extended position. The high-lift device includes a movable fence. The fence is movable between a first position in which the fence does not protrude beyond an outer surface of the high-lift device and a second position in which the fence protrudes beyond the outer surface of the high-lift device. The fence is in the first position when the high-lift device is in the retracted position and in the second position when the high-lift device is in the extended position. Further, an aircraft with such a wing, a high-lift device and a fence as well as use of a high-lift device and a fence are provided.

Abstract: A wing for an aircraft is disclosed having a main wing, a high lift body, and a connection assembly movably connecting the high lift body to the main wing, such that the high lift body can be moved between a retracted position and at least one extended position. The connection assembly includes a drive system having a first drive unit and a second drive unit, wherein the first drive unit has a first input section coupled to a drive shaft, a first gear unit and a first output section drivingly coupled to a first connection element. The second drive unit has a second input section coupled to the drive shaft, a second gear unit, and a second output section drivingly coupled to a second connection element. The first output section includes a first output wheel and the second output section includes a second output wheel.

Abstract: A wing for an aircraft is disclosed having a main wing, a high lift body, and a connection assembly movably connecting the high lift body to the main wing, such that the high lift body can be moved between a retracted position and at least one extended position. The connection assembly includes a drive system having a first drive unit and a second drive unit, wherein the first drive unit has a first input section coupled to a drive shaft, a first gear unit and a first output section drivingly coupled to the high lift body. The second drive unit has a second input section coupled to the drive shaft, a second gear unit, and a second output section drivingly coupled to the high lift body. The first output section includes a first drive arm drivingly coupled to the high lift body via at least one first link element rotatably coupled to the first drive arm and mounted to the high lift body.

Abstract: A wing for an aircraft including a fixed wing and a high-lift device movable between a retracted position and an extended position. The high-lift device includes a movable fence. The fence is movable between a first position in which the fence does not protrude beyond an outer surface of the high-lift device and a second position in which the fence protrudes beyond the outer surface of the high-lift device. The fence is in the first position when the high-lift device is in the retracted position and in the second position when the high-lift device is in the extended position.

Abstract: A collection of data values is divided into plural bins, wherein a number of the bins is dependent upon a change feature of the data values. Parameter values associated with respective bins are determined. Based on the parameter values, visualization of the plural bins is provided in corresponding plural display screen partitions of a display screen, wherein at least one of the display screen partitions has a resolution that is different from another of the display screen partitions.

Abstract: A method for displaying a time-series data set. The method may include determining a number of data intervals for the data set, determining a data resolution for each data interval, partitioning a display space into a number of substantially equally sized partitions equal to the number of data intervals, partitioning the dataset into a number of time-relevance-based subsets equal to the number of partitions based on the currentness of the data and the desired data resolution for each partition, determining a data layout for each partition, and associating the data values for each subset with the corresponding layout. Furthermore, the first subset may consist of more current data at a first resolution and the second subset may consist of data that is less current than the first subset at a lower resolution than the first resolution.

Abstract: A collection of data values is divided into plural bins, wherein a number of the bins is dependent upon a change feature of the data values. Parameter values associated with respective bins are determined. Based on the parameter values, visualization of the plural bins is provided in corresponding plural display screen partitions of a display screen, wherein at least one of the display screen partitions has a resolution that is different from another of the display screen partitions.

Abstract: An arrangement for printing flat workpieces is provided and includes an application roller which rolls on the workpiece surface 6 to be printed and thereby applies a printed image to the workpiece surface 8, the application roller forming a printing cylinder 5 or a transfer roller 1 cooperating with a printing cylinder 5, a counter-roller 2 which forms in cooperation with the application roller a printing gap 3, through which the workpiece 4 passes during the printing process, and a transport device 7 for feeding the workpiece 4 into and out of the printing gap 3 formed by the application roller and the counter-roller 2.

Abstract: An arrangement for printing flat workpieces is provided and includes an application roller which rolls on the workpiece surface 6 to be printed and thereby applies a printed image to the workpiece surface 8, the application roller forming a printing cylinder 5 or a transfer roller 1 cooperating with a printing cylinder 5, a counter-roller 2 which forms in cooperation with the application roller a printing gap 3, through which the workpiece 4 passes during the printing process, and a transport device 7 for feeding the workpiece 4 into and out of the printing gap 3 formed by the application roller and the counter-roller 2.