mhurhangee/patent-ind-claim-en huggingface dataset:
Device for cleaning an ink or ink-jet print head equipped with an upstream pressure absorber , wherein the pressure absorber is provided with a closed damper chamber that is at least partially limited by a damper film , comprising a refill valve arranged in the damper chamber for refilling the damper chamber with ink in response to a curvature of the damper film into the damper chamber , and a controllable device arranged outside the damper chamber for exerting an external pressure on an area of the damper film limiting the damper chamber in order to open the refill valve arranged in the damper chamber and thereby create a continuously open channel through the pressure absorber for cleaning the ink or ink-jet print head, wherein the device for opening the refill valve comprises a control chamber which is hermetically sealed from the surroundings, a) with a connector for a control line which is arranged on the housing of the control chamber in order to allow a control fluid to flow into the control chamber or out of the control chamber and to influence the filling pressure inside the control chamber , and b) with an opening facing to the damper film so that the damper chamber and the control chamber are separated from each other only by the damper film , c) wherein the damper film is designed as a flexurally elastic film and is subjected to the pressure difference between the pressures in the damper chamber and in the control chamber and bulges into the chamber where the lower pressure prevails, characterized in that d) the opening in the control chamber has a circular periphery, so that the damper film can bulge uniformly over its entire surface without local overloading of individual surface areas. a) with a connector for a control line which is arranged on the housing of the control chamber in order to allow a control fluid to flow into the control chamber or out of the control chamber and to influence the filling pressure inside the control chamber , and b) with an opening facing to the damper film so that the damper chamber and the control chamber are separated from each other only by the damper film , c) wherein the damper film is designed as a flexurally elastic film and is subjected to the pressure difference between the pressures in the damper chamber and in the control chamber and bulges into the chamber where the lower pressure prevails, characterized in that d) the opening in the control chamber has a circular periphery, so that the damper film can bulge uniformly over its entire surface without local overloading of individual surface areas.
Transportation system in an environment comprising several people conveyors as well as a navigation system installed on mobile devices held by the passengers of the transportation system, which transportation system comprises at least one wireless transmission device located in connection with at least one of the passenger conveyors, wherein the navigation system comprises a calibration routine for generating a reference position of the mobile device in the environment, and the calibration routine can be initiated, if the distance of the mobile device to the wireless transmission device goes below a threshold value, in which calibration routine the wireless transmission device transfers position and/or identification data to the mobile device, whereupon the navigation system on the mobile device adopts the reference position of the related passenger conveyor, characterized in that the wireless transmission device is located at an elevator entrance or in an elevator car and transmits the floor of the elevator car as part of the position data, and that the wireless transmission device is integrated in a structure of an elevator car or in a door jamb of a landing- or car door of an elevator.
A vehicle information system for a vehicle having a detection unit , by means of which operational data of the vehicle can be detected; a control unit , by means of which graphic data of a display of information describing the detected operational data can be generated as a function of the detected operational data of the vehicle ; wherein the display comprises a background region and a first and a second display object displayed in perspective, wherein an intermediate space is formed between the first and the second display object ; and a vehicle information screen , by which the display can be displayed; wherein the vehicle information system has a first operating mode and a second operating mode; wherein if the first operating mode is activated, the first and second display object are displayed at a first viewing angle and, if the second operating mode is activated, the first and second display object are displayed at a second viewing angle, wherein the surface of the intermediate space between the first and the second display object is changed at a transition between the first and the second operating mode, wherein the graphic data are generated such that the first and second display object of the display can be displayed at a first viewing angle in a top view and at a second viewing angle in a side view, characterized in that in the side view the information from the top view is displayed alphanumerically.
A bed comprising: a foundation having a foundation connector positioned at a bottom of the foundation ; and a frame having a frame connector positioned at a top of the frame and positioned in a location configured to mate with the foundation connector positioned at the bottom of the foundation when the foundation is positioned on top of the frame , wherein the frame comprises first and second longitudinal support structures extending along a portion of the longitudinal length of the frame at first and second sides of the frame , first and second cross-members extending laterally from the first longitudinal support structure to the second longitudinal support structure , and a plurality of fastening mechanisms connecting each end of the first and second cross-members to the first and second longitudinal support structures , wherein the fastening mechanism has a bracket , a flange , and a lock , wherein the bracket includes a ridge for connecting the foundation to the frame , and wherein the foundation connector defines a valley that extends along a longitudinal length of the foundation connector and defines at least one slot along the valley , characterised in that both the valley and the slot are configured to receive the ridge of the bracket of the frame connector. a foundation having a foundation connector positioned at a bottom of the foundation ; and a frame having a frame connector positioned at a top of the frame and positioned in a location configured to mate with the foundation connector positioned at the bottom of the foundation when the foundation is positioned on top of the frame , wherein the frame comprises first and second longitudinal support structures extending along a portion of the longitudinal length of the frame at first and second sides of the frame , first and second cross-members extending laterally from the first longitudinal support structure to the second longitudinal support structure , and a plurality of fastening mechanisms connecting each end of the first and second cross-members to the first and second longitudinal support structures , wherein the fastening mechanism has a bracket , a flange , and a lock , wherein the bracket includes a ridge for connecting the foundation to the frame , and wherein the foundation connector defines a valley that extends along a longitudinal length of the foundation connector and defines at least one slot along the valley , characterised in that both the valley and the slot are configured to receive the ridge of the bracket of the frame connector.
A method of operating a gimbal on-board a vehicle , said method comprising: receiving a gimbal mode signal indicative of whether the gimbal is to be in an active mode or a simulation mode; receiving gimbal control data from a remote control system ; and generating, at the gimbal control system , gimbal response data based on the gimbal control data from the remote control system , wherein the gimbal response data is communicated to one or more actuators configured to adjust an arrangement of the gimbal when the gimbal is in the active mode and is - 2-not communicated to one or more actuators when the gimbal is in the simulation mode. receiving a gimbal mode signal indicative of whether the gimbal is to be in an active mode or a simulation mode; receiving gimbal control data from a remote control system ; and generating, at the gimbal control system , gimbal response data based on the gimbal control data from the remote control system , wherein the gimbal response data is communicated to one or more actuators configured to adjust an arrangement of the gimbal when the gimbal is in the active mode and is - 2-not communicated to one or more actuators when the gimbal is in the simulation mode.
A transverse propulsion device of a ship , comprising: - a maneuvering tunnel defined in a hull of the ship , and adapted to contain at least one maneuvering propeller ; - said maneuvering tunnel being delimited by tunnel walls , which extend between a first tunnel entrance and an opposite second tunnel entrance ; - said transverse propulsion device further comprising at least two closing doors shaped so as to close the at least one tunnel entrance , as a whole, when in the closing position; characterized in that - said transverse propulsion device comprises at least one coupling , which extends from the tunnel walls at the at least one tunnel entrance ; - said transverse propulsion device comprises at least one support structure ; said at least one support structure comprising at least one counter-coupling ; - said at least one counter-coupling and said at least one coupling , when geometrically coupled, are locked together by means of captive screws ; - said support structure being connected in a separable manner with said at least one counter-coupling thereof to said at least one coupling ; - said at least one support structure comprises hinges ; and wherein - said at least two closing doors are rotatably supported only on said hinges of the support structure , so that, when said at least one counter-coupling of the support structure is separated from said at least one coupling , the closing doors separate from the maneuvering tunnel , together with the support structure , thus allowing access to the maneuvering tunnel also when the maneuvering tunnel is immersed. - a maneuvering tunnel defined in a hull of the ship , and adapted to contain at least one maneuvering propeller ; - said maneuvering tunnel being delimited by tunnel walls , which extend between a first tunnel entrance and an opposite second tunnel entrance ; - said transverse propulsion device further comprising at least two closing doors shaped so as to close the at least one tunnel entrance , as a whole, when in the closing position; characterized in that - said transverse propulsion device comprises at least one coupling , which extends from the tunnel walls at the at least one tunnel entrance ; - said transverse propulsion device comprises at least one support structure ; said at least one support structure comprising at least one counter-coupling ; - said at least one counter-coupling and said at least one coupling , when geometrically coupled, are locked together by means of captive screws ; - said support structure being connected in a separable manner with said at least one counter-coupling thereof to said at least one coupling ; - said at least one support structure comprises hinges ; and wherein - said at least two closing doors are rotatably supported only on said hinges of the support structure , so that, when said at least one counter-coupling of the support structure is separated from said at least one coupling , the closing doors separate from the maneuvering tunnel , together with the support structure , thus allowing access to the maneuvering tunnel also when the maneuvering tunnel is immersed.
A process for the recovery of precious metal (PM) from PM oil comprising combustion of PM oil within a furnace, wherein the PM oil is burned in atomized form, wherein the PM oil combustion takes place in an enclosed furnace chamber with an exhaust or abatement system, wherein the furnace chamber is equipped with a PM collector for the PM oil combustion residues contained in the combustion off-gas, wherein the PM collector is an air- or water-cooled container at the walls of which the PM oil combustion residues are deposited, wherein after completion of the combustion process, the PM oil combustion residues are collected from the inner walls of the furnace chamber and its exhaust or abatement system and from the PM collector walls, wherein collecting is performed by scratching the PM oil combustion residues off from said walls' surfaces, and wherein the precious metal being platinum, palladium, ruthenium or rhodium. combustion of PM oil within a furnace, wherein the PM oil is burned in atomized form, wherein the PM oil combustion takes place in an enclosed furnace chamber with an exhaust or abatement system, wherein the furnace chamber is equipped with a PM collector for the PM oil combustion residues contained in the combustion off-gas, wherein the PM collector is an air- or water-cooled container at the walls of which the PM oil combustion residues are deposited, wherein after completion of the combustion process, the PM oil combustion residues are collected from the inner walls of the furnace chamber and its exhaust or abatement system and from the PM collector walls, wherein collecting is performed by scratching the PM oil combustion residues off from said walls' surfaces, and wherein the precious metal being platinum, palladium, ruthenium or rhodium.
An uncrewed aerial vehicle control method implemented by a first uncrewed aerial vehicle or a component that is configured in an uncrewed aerial vehicle, the method comprising: receiving, information about a flight path from a second uncrewed aerial vehicle, wherein the second uncrewed aerial vehicle is at least one uncrewed aerial vehicle different from the first uncrewed aerial vehicle; determining, based on information about a flight path of the first uncrewed aerial vehicle and the information about the flight path received from the second uncrewed aerial vehicle, that there is a collision risk; and updating the flight path of the first uncrewed aerial vehicle, characterized in that after the determining, based on information about a flight path of the first uncrewed aerial vehicle and the information about the flight path received from the second uncrewed aerial vehicle, that there is a collision risk, the method further comprises: reporting collision risk information; and in that the updating, the flight path of the first uncrewed aerial vehicle comprises: receiving flight path update information, and updating a current flight path of the first uncrewed aerial vehicle based on the flight path update information. receiving, information about a flight path from a second uncrewed aerial vehicle, wherein the second uncrewed aerial vehicle is at least one uncrewed aerial vehicle different from the first uncrewed aerial vehicle; determining, based on information about a flight path of the first uncrewed aerial vehicle and the information about the flight path received from the second uncrewed aerial vehicle, that there is a collision risk; and updating the flight path of the first uncrewed aerial vehicle, characterized in that after the determining, based on information about a flight path of the first uncrewed aerial vehicle and the information about the flight path received from the second uncrewed aerial vehicle, that there is a collision risk, the method further comprises: reporting collision risk information; and
An information providing apparatus comprising: a display unit configured to display an information providing image to be provided as a virtual image outside a moving body; and a display controller configured to control the display unit so as to change a display position of the information providing image, wherein the information providing image includes two information providing images (721-1, 704) to be provided as a first information providing image and a second information providing image, and wherein the display controller is configured to control the display unit such that the changing rate of the display position of the information providing image increases as a moving velocity of the moving body increases; characterized in that the display controller is further configured to control the display unit such that a changing rate of the display position of the first information providing image (721-1) differs from a changing rate of a display position of the second information providing image , and a lower changing rate from among the changing rate of the display position of the first information providing image and the changing rate of the display position of the second information providing image increases as the moving velocity of the moving body increases. a display unit configured to display an information providing image to be provided as a virtual image outside a moving body; and a display controller configured to control the display unit so as to change a display position of the information providing image, wherein the information providing image includes two information providing images (721-1, 704) to be provided as a first information providing image and a second information providing image, and wherein the display controller is configured to control the display unit such that the changing rate of the display position of the information providing image increases as a moving velocity of the moving body increases; characterized in that the display controller is further configured to control the display unit such that a changing rate of the display position of the first information providing image (721-1) differs from a changing rate of a display position of the second information providing image , and a lower changing rate from among the changing rate of the display position of the first information providing image and the changing rate of the display position of the second information providing image increases as the moving velocity of the moving body increases.
A process of producing a near-net shape component , the process comprising: forming, by additive manufacturing, a consolidation shell comprising a first and a second material, the consolidation shell defining an interior space having a geometry corresponding to a component ; providing a metallic powder to the interior space; removing gas from the interior space; consolidating the metallic powder in the consolidation shell under sufficient heat and pressure to form the near-net shape component , wherein the near-net shape component is a compressor blade; and removing said second material by a physical or chemical means to form channels in the component . forming, by additive manufacturing, a consolidation shell comprising a first and a second material, the consolidation shell defining an interior space having a geometry corresponding to a component ; providing a metallic powder to the interior space; removing gas from the interior space; consolidating the metallic powder in the consolidation shell under sufficient heat and pressure to form the near-net shape component , wherein the near-net shape component is a compressor blade; and removing said second material by a physical or chemical means to form channels in the component .
A method of manufacturing a planar transformer , the method comprising: forming a first electrically conductive trace (W a P2) of at least one primary winding of the planar transformer on a first circuit layer (L2P2), the first electrically conductive trace having a first termination portion (T in L2) and a second termination portion (T out L2) defining a first gap (GP a L2, GP b L2) therebetween; forming a second electrically conductive trace (W a P1) of at least one primary winding of the planar transformer on a second circuit layer (L3P1), the second electrically conductive trace having a first termination portion (T in L3) and a second termination portion (T out L3) defining a second gap (GP a L3, GP b L3) therebetween; forming a third electrically conductive trace as a grounded portion (GDL4; GDL1) on a third circuit layer (L4S1; L1S1), wherein the third circuit layer includes an electrically conductive trace (W3S1, W4S1; W1S1, W2S1) forming a winding of at least one secondary winding of the planar transformer; stacking the first, second and third circuit layers together in a first direction so that the second gap (GP b L3) is offset from the first gap (GP b L2) in a second direction perpendicular to the first direction and so that the grounded portion is positioned adjacent to the first gap and aligned therewith in the first direction or is positioned adjacent to the second gap and aligned therewith in the first direction. forming a first electrically conductive trace (W a P2) of at least one primary winding of the planar transformer on a first circuit layer (L2P2), the first electrically conductive trace having a first termination portion (T in L2) and a second termination portion (T out L2) defining a first gap (GP a L2, GP b L2) therebetween; forming a second electrically conductive trace (W a P1) of at least one primary winding of the planar transformer on a second circuit layer (L3P1), the second electrically conductive trace having a first termination portion (T in L3) and a second termination portion (T out L3) defining a second gap (GP a L3, GP b L3) therebetween; forming a third electrically conductive trace as a grounded portion (GDL4; GDL1) on a third circuit layer (L4S1; L1S1), wherein the third circuit layer includes an electrically conductive trace (W3S1, W4S1; W1S1, W2S1) forming a winding of at least one secondary winding of the planar transformer; stacking the first, second and third circuit layers together in a first direction so that the second gap (GP b L3) is offset from the first gap (GP b L2) in a second direction perpendicular to the first direction and so that the grounded portion is positioned adjacent to the first gap and aligned therewith in the first direction or is positioned adjacent to the second gap and aligned therewith in the first direction.