Abstract: In a self-propelling road construction machine, particularly a road roller (1), comprising a travel drive, a steering device, a control device (30) for the travel drive and the steering device, and a driver's seat (5) rotatable by at least 180° and including an integrated operating element (8) for the vehicle speed, with the operating element (8) generating the control signals for the travel drive in dependence on the direction of the control movement of the operating element (8) or the direction of force application on the operating element (8), it is provided that, in response to a first switching command, the control device (30) will automatically perform a reversing process comprising deceleration, seat rotation, change of direction of travel, and acceleration to the set vehicle speed in opposite direction to the original direction of travel.

Abstract: A method is provided for diagnosing the operability of fuel vapor intermediate stores (4), in particular of activated carbon filters, in tank-venting systems with at least one tank (3) and at least one fuel vapor intermediate store (4). In this case an actual change degree of filling of the fuel vapor intermediate store (4) is determined as a consequence of absorption or desorption processes of gaseous hydrocarbons in the fuel vapor intermediate store (4). The actual change in degree of filling is compared with a desired change in degree of filling and, from the comparison, a conclusion about the operability of the fuel vapor intermediate store (4) is drawn.

Abstract: A lock cylinder having: a cylinder core having a key channel for inserting a key which is provided with profiling; at least one feeler element which is disposed in the cylinder core, is acted on by a spring and is held in a blocking position by the spring when the key is not inserted in the key channel; and a blocking element which, when the feeler element is in the blocking position, is held in a blocking position which blocks rotation of the cylinder core. The feeler element can be shifted against the return force of the spring into a release position by the profiling on the matching key inserted into the key channel, in which position the locking element can be deflected into a position releasing the cylinder core.

Abstract: The invention relates to a lock cylinder comprising: a cylinder core (2) having a key channel (7) for inserting a key (5) which is provided with profiling (18); at least one feeler element (9) which is disposed in the cylinder core (2), is acted on by a spring (8) and is held in a blocking position by the spring (8) when the key (5) is not inserted in the key channel (7); and a blocking element (13) which, when the feeler element (9) is in the blocking position, is held in a blocking position which blocks rotation of the cylinder core (2), it being possible for the feeler element (9) to be shifted against the return force of the spring (8) into a release position by the profiling (18) on the matching key (5) inserted into the key channel (7), in which position the locking element (13) can be deflected into a position releasing the cylinder core (2).

Abstract: The invention refers to a docking device for the docking of a maintenance device to a nozzle of a satellite, including a distance sensor for determining the distance between the maintenance device and the nozzle of the satellite. Further, a locking device is provided for connecting the docking device with the nozzle of the satellite.

Abstract: The present invention relates to a device and a method of generatively manufacturing a three-dimensional object in a device, comprising the following steps: layerwise applying a powdery material (11) onto a support (5) or a previously applied layer after having lowered the support (5) by the amount of one layer thickness; selectively solidifying the powdery material (11) by energetic radiation (8, 8?) at locations corresponding to the object (3); repeating the steps a) and b), until the object (3) is completed. The device defines a two-dimensional maximum working field (6) with a maximum length (L) and a maximum width (B), in which the powdery material (11) can be applied and solidified. According to the invention, a reduced working field (13) is additionally realized, in which the powdery material (11) is applied and radiated by less than the maximum length (L) and/or by less than the maximum width (B) of the maximum working field (6).

Abstract: In a space shuttle with a device for docking to a satellite, especially a communication or navigation satellite, at least two spreading elements in the form of lever spreaders are pivotally disposed at a retaining part of the docking device, which is concentric to a linkage. The lever spreaders have their proximal ends—relative to the space shuttle—provided with inward projections projecting inward towards the linkage, which inward projections engage in a recess formed in the linkage when the lever spreaders, spread apart to a defined opening angle by the cone of the linkage. When the linkage is retracted further, a pressure spring is compressed. At the same time, the lever spreader caught in the recess are retracted so far that the ends of the lever spreaders, spread apart in a defined manner, positively abut the inner wall of the nozzle neck.

Abstract: A device provided on a space shuttle for docking to satellites, has a linkage with a cone at its distal end and a spreader mechanism, actuatable from the shuttle, with lever spreaders having their proximal ends provided with inward projections towards the linkage. At least two lever spreaders are pivotally arranged at a retaining part concentric to the linkage; the curvature at the distal end of each lever spreader is adapted to the curvature of the nozzle neck of the jet nozzle of a satellite engine. A rotatable sleeve concentric to the linkage is provided below the retaining part. A distal annular portion of the sleeve is formed with respective alternating engaging positions of different heights, and wherein, from the proximal end portion of the sleeve, two pins project that are guided by associated obliquely oriented slide faces in a stationary housing, the pins being provided for setting the adjustment travel of the linkage.

Abstract: The present invention relates to a device for generatively manufacturing a three-dimensional object (3), comprising: a frame (1) defining a building field (6) at an upper portion (2) thereof; a plate (12) which connects the frame (1) with a housing (100) of the device; a support (5) which is arranged in the frame (1) and vertically movable by a lift mechanics (4) at least below the building field (6); a radiation device (7) which generates an energetic beam (8, 8?) which is focused by a deflection means (9) to arbitrary points in the building field (6), so as to selectively sinter or melt a powdery material (11) which is present in the building field (6); a coater (10) for applying a layer of powdery material (11) onto the support (5) or a previously applied layer of the powdery material (11). A thermal insulation (13) is arranged between the frame (1) and the plate.

Abstract: A device for generatively manufacturing a three-dimensional object (3) is disclosed, comprising: a frame (1), the upper portion (2) thereof surrounds a building field (6); a support (5) which is arranged in the frame (1) and vertically movable at least below the building field (6) by a lift mechanics (4); a radiation device (7) which generates an energetic beam (8, 8?) which is focused to arbitrary points in the building field (6) by a deflection means (9), so as to selectively sinter or melt a powdery material (11) which is present in the building field (6); a coater (10) for applying a layer of a powdery material (11) onto the support (5) or a previously applied layer of the powdery material (11); a housing (100), in which at least the frame (1) and the support (5) are arranged and which surrounds a building space; and a heating device (13; 14; 15; 16) which continuously supplies heat at least to the building field environment or the building space there above.

Abstract: Method and apparatus for detecting tank leaks, in which a gas pressure acts on a fluid which is situated in a tank, and in which the gas pressure in the tank or tank system is changed, wherein a tank leak is detected by evaluation of a temporal profile of a sum pressure of the fluid which is situated in the tank.

Abstract: A method is provided for diagnosing the operability of fuel vapor intermediate stores (4), in particular of activated carbon filters, in tank-venting systems with at least one tank (3) and at least one fuel vapor intermediate store (4). In this case an actual change degree of filling of the fuel vapor intermediate store (4) is determined as a consequence of absorption or desorption processes of gaseous hydrocarbons in the fuel vapor intermediate store (4). The actual change in degree of filling is compared with a desired change in degree of filling and, from the comparison, a conclusion about the operability of the fuel vapor intermediate store (4) is drawn.

Abstract: The invention refers to a docking device for the docking of a maintenance device to a nozzle (12) of a satellite, comprising a distance sensor (14) for determining the distance between the maintenance device and the nozzle (12) of the satellite. Further, a locking device is provided for connecting the docking device (10) with the nozzle (12) of the satellite.

Abstract: In a space shuttle with a device for docking to a satellite, especially a communication or navigation satellite, at least two spreading elements in the form of lever spreaders (4) are pivotally disposed at a retaining part (3) of the docking device, which is concentric to a linkage (2). The lever spreaders (4) have their proximal ends—relative to the space shuttle—provided with noses (41) projecting inward towards the linkage (2), which noses engage in a recess (22) formed in the linkage (2) when the lever spreaders (4), spread apart to a defined opening angle by the cone (21) of the linkage (2), are retracted. When the linkage (2) is retracted further, a pressure spring (5) is compressed.

Abstract: A method for generating a flexible display field on a monitor includes providing a display field with a main window, into which a plurality of information windows are incorporatable and which has a basic grid with a regular raster, allocating individual grid fields to a respective information window for displaying in an assigned grid field, setting a grid stage of a basic field via a central first user control device for the main window, switching the main window between a regular grid occupancy in which a size of each incorporated information window corresponds to a size of one grid field of the basic field, and an irregular grid occupancy in which a size of at least one information window corresponds to a size of an integral multiple of one grid field of the basic grid, and initiating a switchover of a user by a selection and a change in size of an information window and also a video management system and a software program are provided.

Abstract: In a method and a device for operating an injection device (5) for an internal combustion engine, the injection device (5) includes injection valves (40), via which fuel is injected directly into combustion chambers (100) of the internal combustion engine. Mechanisms are provided for detecting misfirings (310), and for determining a fuel pressure (320). A mechanical fault of an injection valve (40) is detected when a misfire occurs in a cylinder (110) and the fuel pressure simultaneously drops below a threshold value (SW). An electrical fault in an injection device (5) is detected when misfirings of cylinders (110) assigned to an output stage bank of the injection device (5) are observed, and the fuel pressure has dropped below a threshold value (SW). The responses to the faults that are implemented differ depending on the faults that were detected.

Abstract: The invention relates to the field of ceramics and relates to composite molded articles, such are used, for example, for chip-removal tools. The object of the invention is to disclose composite molded articles that are free in the design of their surface and interface and can be produced in series production. The object is attained through ceramic and/or powder metallurgical composite molded articles comprising a green tape and an injection molded article. The object is further attained through a method in which a green tape is inserted into or placed onto a mold, and subsequently at least one ceramic and/or powder metallurgical injection molding mass is placed on and/or applied to and/or inserted into the mold by means of injection molding, and subsequently the one-part or multi-part mold is removed and/or the one-part or multi-part composite molded part parts are removed from the mold, wherein these process steps can be repeated once or several times.

Abstract: The invention relates to the field of material sciences and relates to a metal-ceramic composite with good adhesive strength, such as can be used, for example, for forming tools or cutting tools. The object of the present invention lies in the disclosure of a metal-ceramic composite with good adhesive strength which has a strong and durable bond between ceramic and metal. The object is attained with a metal-ceramic composite with good adhesive strength, comprising a metal component and a ceramic component and which are connected to one another by adhesive force or by adhesive force and in a non-positive manner, wherein silicon, beryllium, titanium, chromium, nickel, manganese, hafnium, vanadium, zirconium, aluminum and/or the organic compounds thereof is present in the area of the connection surfaces and wherein the components have been processed as a greenbody to form a composite and jointly sintered.

Abstract: In a procedure for the functional diagnosis of an activateable fuel tank ventilation valve of the fuel tank system of an internal combustion engine, especially of a motor vehicle, whereby in specifiable time intervals when the fuel tank ventilation valve is activated to open, regeneration gas is added to the air drawn into the combustion chamber, whereby fuel is delivered to the combustion chamber, whereby the fuel, the air, respectively the fuel, the air and the regeneration gas are combusted in the combustion chamber and whereby by comparison of at least one operating parameter, which characterizes the combustion of fuel and intake air with the corresponding operating parameter, which characterizes the combustion of fuel, intake air and regeneration gas, inference can be made about the functional capability of the fuel tank ventilation valve, the HC-concentration of the regeneration gas is specifically affected by changing the regeneration gas stream.

Abstract: A device provided on a space shuttle for docking to satellites, in particular communication or navigation satellites, which device comprises a linkage with a cone at its distal end—relative to the space shuttle—and a spreader mechanism, actuatable from the space shuttle, with spreader elements in the form of lever spreaders having their proximal ends—relative to the space shuttle—provided with noses protruding inward towards the linkage. At least two lever spreaders of the device are pivotally arranged at a retaining part concentric to the linkage; the curvature at the distal end of each lever spreader is adapted to the curvature of the nozzle neck of the jet nozzle of a satellite engine. A rotatable sleeve is provided below the retaining part, which sleeve is concentric to the linkage.