Abstract: Systems and methods include creation of a first instance of a tenant object in a database instance, association of the first instance of the tenant object with a first plurality of database artifacts including first data associated with the first instance of the tenant object, creation of a second instance of the tenant object in the database instance, association of the second instance of the tenant object with a second plurality of database artifacts including second data associated with the second instance of the tenant object, and reception and response to queries on the first data associated with the first instance of the tenant object and to queries on the second data associated with the second instance of the tenant object.

Abstract: The present invention relates to a process for making a compound of formula (I) as described herein Formula (I) comprising reducing a compound of formula (II) as described herein with hydrogen in the presence of a palladium catalyst and a solvent wherein the solvent is a polar, aprotic solvent or a C3-C10 alcohol Formula (II). The present invention further relates to a hydrochloride salt and a monohydrochloride salt of the compound of formula (I) as described herein and to a process for making the same Formula (I).

Abstract: The present invention relates to a process for making a compound of formula (I) as described herein Formula (I) comprising reducing a compound of formula (II) as described herein with hydrogen in the presence of a palladium catalyst and a solvent wherein the solvent is a polar, aprotic solvent or a C3-C10 alcohol Formula (II). The present invention further relates to a hydrochloride salt and a monohydrochloride salt of the compound of formula (I) as described herein and to a process for making the same Formula (I).

Abstract: The present invention relates to a process for making a compound of formula (I) as described herein Formula (I) comprising reducing a compound of formula (II) as described herein with hydrogen in the presence of a palladium catalyst and a solvent wherein the solvent is a polar, aprotic solvent or a C3-C10 alcohol Formula (II). The present invention further relates to a hydrochloride salt and a monohydrochloride salt of the compound of formula (I) as described herein and to a process for making the same Formula (I).

Abstract: Replicating a tenant database includes receiving at a source system a first request from a target system for replicating a first tenant database of the source system, which includes one or more first servers. Characteristics of the one or more first servers are sent to the target system to generate at the target system a second tenant database including one or more second servers. Each second server corresponds to one first server and has the same characteristics as the corresponding first server. Information from each first server is replicated, in an asynchronous mode, to the corresponding second server through a communication channel that is established between each first server and the second server. Upon receiving a second request for stopping the replication, a synchronous mode of processing statements from client applications of the first tenant database is entered. Related apparatus, systems, techniques and articles are described.

Abstract: Replicating a tenant database includes receiving at a source system a first request from a target system for replicating a first tenant database of the source system, which includes one or more first servers. Characteristics of the one or more first servers are sent to the target system to generate at the target system a second tenant database including one or more second servers. Each second server corresponds to one first server and has the same characteristics as the corresponding first server. Information from each first server is replicated, in an asynchronous mode, to the corresponding second server through a communication channel that is established between each first server and the second server. Upon receiving a second request for stopping the replication, a synchronous mode of processing statements from client applications of the first tenant database is entered. Related apparatus, systems, techniques and articles are described.

Abstract: The invention relates to a flight guidance system for the flight support of a aircraft (1), said system comprising a plurality of fixed ground stations (4a to 4e) respectively comprising a transmitting and/or receiving unit (5a to 5e), and at least one transmitting and/or receiving unit (6) that is arranged on the aircraft (1), the transmitting units being act up to send position signals (7) and the receiving units being set up to receive said position signals (7).

Abstract: A measured value transmitting device for serially transmitting data in accordance with the SSI method, includes a slave providing the data bits of a measured value detected by a sensor for serial bit-by-bit transmission to a master. The master requests a measured value from the slave with a clock burst having multiple clock cycles matching the number of data bits to be transmitted. In a first device, the clock cycles have a specified duty cycle corresponding to the ratio of the pulse duration to the period duration of one clock cycle, and the master contains a comparator. The master reads the clock bursts outputted on the clock line and checks the duty cycle in the comparator to determine whether an upper and/or lower threshold has been exceeded. In a second device a corresponding check of the duty cycle is carried out in the slave.

Abstract: A control device is provided for an aircraft, the aircraft having at least one undercarriage with one or more undercarriage wheels. A control mechanism interacts with the aircraft undercarriage and is configured to turn the undercarriage wheels relative to the longitudinal axis of the aircraft. The control device has an alignment unit which is connected to the control mechanism and which is configured to control the turning of the undercarriage wheels by means of the control mechanism during at least one part of the landing or take-off phase of the aircraft in such a way that the running direction of the undercarriage wheels is aligned in the direction of a fixed point which may be a corrected fixed point situated below a fixed point by a compensation angle.

Abstract: The invention relates to a device (10) for stabilizing the guidance of a vehicle (1), the vehicle (1) having at least one or two which is arranged in such a way that it can be turned relative to the longitudinal axis of the vehicle (1), and steering means that interact with the at least one wheel (2) and are designed to guide the vehicle (1) by turning the at least one wheel (2). The device (10) has a detecting unit (12), which is designed to detect an at least partial transition from static friction to dynamic friction between the at least one wheel (2) and a ground covering (3), and furthermore has a control unit (11), which, when the detecting unit (12) detects the transition from static friction to dynamic friction, is designed to turn the at least one wheel (2) by means of the steering means in such a way that the dynamic friction between the wheel (2) and the ground covering (3) changes back to static friction.

Abstract: The invention relates to measured value transmitting devices for serially transmitting data in accordance with the SSI method, Synchronous Serial Interface. At least one slave is provided which provides the data bits of a measured value detected by at least one sensor for the purpose of a serial bit-by-bit transmission to a master. The master requests a measured value from the slave by means of a clock burst that has multiple clock cycles, the number of which matches the number of the data bits to be transmitted. A first measured value transmitting device according to the invention is characterized in that the clock cycles of the clock burst have a specified duty cycle which corresponds to the ratio of the pulse duration to the period duration of one clock cycle, and the master contains a comparator. The master reads the clock bursts outputted on the at least one clock line and checks the duty cycle in the comparator to determine whether an upper threshold and/or a lower threshold has been exceeded.

Abstract: The invention relates to a ground-based positioning system for determining a location of a mobile object (1), comprising a plurality of fixed ground stations (2a-2c) respectively comprising a transmitting and/or receiving unit (3a-3c), and at least one transmitting and/or receiving unit (5) that is arranged on the object, the transmitting mils being set up so transmit position signals and the receiving units being set up to receive the position signals transmitted by the transmitting units.

Abstract: The invention relates to a flight guidance system for the flight support of a aircraft (1), said system comprising a plurality of fixed ground stations (4a to 4e) respectively comprising a transmitting and/or receiving unit (5a to 5e), and at least one transmitting and/or receiving unit (6) that is arranged on the aircraft (1), the transmitting units being act up to send position signals (7) and the receiving units being set up to receive said position signals (7).

Abstract: The invention relates to a cutting insert for chip-forming machining, of which at least the top surface, on one side, forms the face (1) and the peripheral, planar side surface, which are located at right angles to one another, form the flanks (2), wherein, downstream of a planar face portion (3) which is adjacent to the flanks and is arranged at a rake angle of 0°, the face terminates, via downwardly sloping planar wall portions (4), in a lower-level, planar chip-forming base (5) and, in the direction of the centre, it slopes up, via upwardly sloping planar wall portions (6), to a central, planar face plateau (7).

Abstract: The invention relates to a control device for aircraft comprising at least one aircraft undercarriage 4a, 4b, 4c arranged on an aircraft 1, which aircraft undercarriage has one or more undercarriage wheels 3, and comprising a control mechanism 5 which interacts with the aircraft undercarriage 4a, 4b, 4c and which is set up to turn the undercarriage wheels 3 relative to the longitudinal axis A of the aircraft 1. The control device has an alignment unit 6 which is connected to the control mechanism 5 and which is set up to control the turning of the undercarriage wheels 3 by means of the control mechanism 5 during at least one part of the landing or take-off phase I, II, III of the aircraft 1, in such a way that the running direction of the undercarriage wheels 3 is aligned in the direction of a fixed point 9, which may be a corrected fixed point situated below a fixed point 9 by a compensation angle.

Abstract: The invention relates to a device (10) for stabilizing the guidance of a vehicle (1), the vehicle (1) having at least one or two which is arranged in such a way that it can be turned relative to the longitudinal axis of the vehicle (1), and steering means that interact with the at least one wheel (2) and are designed to guide the vehicle (1) by turning the at least one wheel (2). The device (10) has a detecting unit (12), which is designed to detect an at least partial transition from static friction to dynamic friction between the at least one wheel (2) and a ground covering (3), and furthermore has a control unit (11), which, when the detecting unit (12) detects the transition from static friction to dynamic friction, is designed to turn the at least one wheel (2) by means of the steering means in such a way that the dynamic friction between the wheel (2) and the ground covering (3) changes back to static friction.

Abstract: A cooking device disposable on a horizontal surface. The cooking device includes a support mechanism that is movable by a drive, in a direction substantially vertical to the surface, between an operating position and an inactive position. The cooking device also has a heating unit disposed on the support mechanism and a food tray disposed on the support mechanism. The food tray and heating unit are held on the support mechanism such that the food tray and heating unit are movable relative to one another. In an inactive position of the support mechanism, the food tray has a height position that is lower than a height position of the surface.

Abstract: A control device for aircraft for reducing the turbulence and gust influences on the flying characteristics is designed to generate an additional incidence angle drive signal for control surfaces on surfaces which generate an air force, in particular wing and/or tailplane as a function of an instantaneous bank angle (?) and sideslip angle (?).

Abstract: A control device for aircraft for reducing the turbulence and gust influences on the flying characteristics is designed to generate an additional incidence angle drive signal for control surfaces on surfaces which generate an air force, in particular wing and/or tailplane as a function of an instantaneous bank angle (?) and sideslip angle (?).

Abstract: The invention relates to a cutting insert for chip-forming machining, of which at least the top surface, on one side, forms the face (1) and the peripheral, planar side surface, which are located at right angles to one another, form the flanks (2), wherein, downstream of a planar face portion (3) which is adjacent to the flanks and is arranged at a rake angle of 0°, the face terminates, via downwardly sloping planar wall portions (4), in a lower-level, planar chip-forming base (5) and, in the direction of the centre, it slopes up, via upwardly sloping planar wall portions (6), to a central, planar face plateau (7).