Abstract: The present disclosure relates to a method for parameterizing an automation field device which is communicatively connected to a server, having the following steps: initiating the method by transmitting a command to parameterize the field device on the server; transmitting identification information of the field device to the server; ascertaining a digital image of the field device stored on the server using the transmitted identification information, said digital image containing configuration settings of the field device and measurement location-relevant information and being designed to reproduce the behavior of the field device in a simulated or emulated manner; generating and proposing a parameter set for the field device using the field device information; selecting and confirming the proposed parameter set by a user; and transmitting the confirmed parameter set to the field device and parameterizing the field device using the transmitted parameter set.

Abstract: The present disclosure relates to a method for parameterizing an automation field device which is communicatively connected to a server, having the following steps: initiating the method by transmitting a command to parameterize the field device on the server; transmitting identification information of the field device to the server; ascertaining a digital image of the field device stored on the server using the transmitted identification information, said digital image containing configuration settings of the field device and measurement location-relevant information and being designed to reproduce the behavior of the field device in a simulated or emulated manner; generating and proposing a parameter set for the field device using the field device information; selecting and confirming the proposed parameter set by a user; and transmitting the confirmed parameter set to the field device and parameterizing the field device using the transmitted parameter set.

Abstract: An arcuate spring having a plurality of coils which are configured and dimensioned to provide an arcuate shape to the spring and being substantially free of internal stresses which would tend to urge the coils into linear alignment. The spring is designed to function under load conditions while maintaining its natural arcuate shape. The spring is can be heated by use of an induction heating process.

Abstract: A spaceplane suitable for aeronautical flight comprising a body and a wing defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters disposed under the lower airfoil surface of same and maneuverable between a stowed position and an inclined extended position for aerodynamic braking during the transition from a phase of space flight to a phase of aeronautical flight of the aircraft.

Abstract: A method for displaying an attitude of an aircraft includes receiving a roll angle, a pitch angle and a yaw angle of the aircraft, generating a display image indicating the roll angle, the pitch angle and the yaw angle, and displaying the display image on a display device. The display image includes a spherical shell with a track angle scale projected onto the spherical shell along a latitude line of the spherical shell and with a pitch angle scale projected onto the spherical shell along a longitude line of the spherical shell. Furthermore, the display image includes a graphical aircraft attitude indicator inside the spherical shell rotated with respect to the spherical shell such that the graphical aircraft attitude indicator indicates the roll angle, the pitch angle and the yaw angle of the aircraft with respect to the spherical shell.

Abstract: An aircraft is capable of passing from the aerial domain to the spatial domain and method for automatically adapting the configuration of same. An additional breathable gas supply is provided to be activated only during a flight phase during which aerobic propulsion is interrupted, and is capable of supplying the control system of the manned cabin environment instead of the system associated with the aerobic propulsion means.

Abstract: A process control arrangement (PKA), having a number of fieldbus systems (DP1, PA1, FH), especially different fieldbus systems (DP1, PA1, FH), and having a number of fieldbus interfaces (PAP1, PAP2, PAP3), wherein each of the fieldbus systems (DP1, PA1, FH) is connected to at least one of the fieldbus interfaces (PAP1, PAP2, PAP3), wherein the fieldbus interfaces (PAP1, PAP2, PAP3) serve for communication between the fieldbus systems (DP1, PA1, FH) and a communication plane (ET2) superordinated to the fieldbus systems, only a first of the fieldbus interfaces (PAP1) is directly connected to the superordinated communication plane (ET2), and wherein the fieldbus interfaces (PAP1, PAP2, PAP3) are connected in series with one another beginning with the first of the fieldbus interfaces (PAP1).

Abstract: A method for retrieving process, operation or maintenance relevant data of a process plant by way of a field monitor, wherein multiple wireless field device networks are present in the process plant. Data from the field devices from different field device networks are gathered by way of the field monitor. Plant information from the field devices belonging to different field device networks are displayed on a display of the field monitor to a user regardless of the respective field device network they belong to.

Abstract: An aircraft is capable of passing from the aerial domain to the spatial domain and method for automatically adapting the configuration of same. An additional breathable gas supply is provided to be activated only during a flight phase during which aerobic propulsion is interrupted, and is capable of supplying the control system of the manned cabin environment instead of the system associated with the aerobic propulsion means.

Abstract: A method for integrating at least one field device into a network of automation technology, wherein a plurality of field devices are arranged distributed in an automated plant, wherein accessing of the field devices occurs via a field access unit, which communicates with at least one automation/integration platform and at least one web server of a service provider, wherein the service provider provides for each field device a virtual image of the field device in a database, wherein the service provider transmits to the operator of the automated plant via cloud-computing web services, or Internet based services, automatically or on query, the virtual image of the field device with concrete field device- and application-specific properties at run time (the virtual image is preferably transmitted directly into the field device, and wherein the field device performs its function in the automated plant, as soon as it is integrated into the network.

Abstract: A spaceplane suitable for aeronautical flight comprising a body and a wing defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters disposed under the lower airfoil surface of same and maneuverable between a stowed position and an inclined extended position for aerodynamic braking during the transition from a phase of space flight to a phase of aeronautical flight of the aircraft.

Abstract: A method for displaying an attitude of an aircraft includes receiving a roll angle, a pitch angle and a yaw angle of the aircraft, generating a display image indicating the roll angle, the pitch angle and the yaw angle, and displaying the display image on a display device. The display image includes a spherical shell with a track angle scale projected onto the spherical shell along a latitude line of the spherical shell and with a pitch angle scale projected onto the spherical shell along a longitude line of the spherical shell. Furthermore, the display image includes a graphical aircraft attitude indicator inside the spherical shell rotated with respect to the spherical shell such that the graphical aircraft attitude indicator indicates the roll angle, the pitch angle and the yaw angle of the aircraft with respect to the spherical shell.

Abstract: According to the invention, said space aircraft comprises, at the front of each of the air inlets of the turbo engines, a mobile flap that can move, in both directions, between a first position for which said flap opens said air inlet and a second position for which said flap prevents air from entering said air inlet.

Abstract: A method for retrieving process, operation or maintenance relevant data of a process plant by way of a field monitor, wherein multiple wireless field device networks are present in the process plant. Data from the field devices from different field device networks are gathered by way of the field monitor. Plant information from the field devices belonging to different field device networks are displayed on a display of the field monitor to a user regardless of the respective field device network they belong to.

Abstract: An arcuate spring having a plurality of coils which are configured and dimensioned to provide an arcuate shape to the spring and being substantially free of internal stresses which would tend to urge the coils into linear alignment. The spring is designed to function under load conditions while maintaining its natural arcuate shape. The spring is can be heated by use of an induction heating process.

Abstract: A method for integrating at least one field device into a network of automation technology, wherein a plurality of field devices are arranged distributed in an automated plant, wherein accessing of the field devices occurs via a field access unit, which communicates with at least one automation/integration platform and at least one web server of a service provider, wherein the service provider provides for each field device a virtual image of the field device in a database, wherein the service provider transmits to the operator of the automated plant via cloud-computing web services, or Internet based services, automatically or on query, the virtual image of the field device with concrete field device- and application-specific properties at run time (the virtual image is preferably transmitted directly into the field device, and wherein the field device performs its function in the automated plant, as soon as it is integrated into the network.

Abstract: An improved stamped metal part and method for making the same.