mhurhangee/patent-ind-claim-en huggingface dataset:
Wafer level package (10, 10', 10", 10"', 10"") with integrated antenna, comprising: a contacting layer ; a rewiring layer with the integrated antenna; a chip layer including at least one chip arranged between the contacting layer and the rewiring layer ; wherein the integrated antenna is laterally arranged in the rewiring layer such that a projection area of the integrated antenna is offset from or partly overlapping with a projection area of the at least one chip , wherein the chip is connected to the integrated antenna with the help of the rewiring layer (16, 16", 16u'); wherein the contacting layer includes a reflector opposite to the antenna for the antenna or a reflector (12v"") is arranged opposite to the antenna on a side facing away from the antenna in order to cooperate with the same; and wherein at least one shielding via is arranged beside the chip , wherein the at least one shielding via is configured to establish shielding between the integrated antenna and the at least one chip and wherein no electrical connection exists between the at least one shielding via and the chip as well as the reflector (14a, 12v""). a contacting layer ; a rewiring layer with the integrated antenna; a chip layer including at least one chip arranged between the contacting layer and the rewiring layer ; wherein the integrated antenna is laterally arranged in the rewiring layer such that a projection area of the integrated antenna is offset from or partly overlapping with a projection area of the at least one chip , wherein the chip is connected to the integrated antenna with the help of the rewiring layer (16, 16", 16u'); wherein the contacting layer includes a reflector opposite to the antenna for the antenna or a reflector (12v"") is arranged opposite to the antenna on a side facing away from the antenna in order to cooperate with the same; and wherein at least one shielding via is arranged beside the chip , wherein the at least one shielding via is configured to establish shielding between the integrated antenna and the at least one chip and wherein no electrical connection exists between the at least one shielding via and the chip as well as the reflector (14a, 12v"").
A plug configured to seal a femoral opening drilled in a femur of a knee joint to position an intramedullary cutting guide, wherein the plug comprises: a substantially cylindrical body configured for insertion into the femoral opening ; and threads extending around the substantially cylindrical body configured to engage an internal wall of the femoral opening and thereby create a seal to prevent blood loss from the femoral opening into the knee joint after removal of the intramedullary cutting guide from the femoral opening . a substantially cylindrical body configured for insertion into the femoral opening ; and threads extending around the substantially cylindrical body configured to engage an internal wall of the femoral opening and thereby create a seal to prevent blood loss from the femoral opening into the knee joint after removal of the intramedullary cutting guide from the femoral opening .
Electric bicycle having a bicycle frame , an electronic control unit , a drive unit , a battery unit , a display unit and a remote control unit for the display unit , wherein the remote control unit is arranged in the region of a handlebar grip at a distance from the display unit , characterised in that the electronic control unit is arranged in the seat tube of the bicycle frame in the lower region and is fastened to the frame-side drive carrier of the bicycle frame via an L-shaped fastening angle , which is fastened to the rectangular housing of the control unit by means of screws (40; 44), and the angle is fastened to the drive carrier by means of a screw .
An annular seal (150; 250; 350) for a gas turbine engine , comprising: a first annular ring (252; 352); a second annular ring (254; 354); an annular brush (256; 356) having a first brush end (258; 358) disposed between the first annular ring (252; 352) and the second annular ring (254; 354); and an axial ring seal (264; 364) having a first seal end (272; 372) configured for contact with the second annular ring (254; 354), wherein the annular brush (256; 356) has a second brush end (260; 360) configured for contact with a radially outer surface (262; 362) of a blade outer air seal (120; 220; 320), wherein the second annular ring (254; 354) includes a socket (276; 376) configured to receive the first seal end (272; 372) of the axial ring seal (264; 364), characterised in that the axial ring seal (264; 364) has a second seal end (274; 374) configured for contact with an axial face (268; 368) of a component (270; 369) disposed downstream of the annular brush (256; 256). a first annular ring (252; 352); a second annular ring (254; 354); an annular brush (256; 356) having a first brush end (258; 358) disposed between the first annular ring (252; 352) and the second annular ring (254; 354); and an axial ring seal (264; 364) having a first seal end (272; 372) configured for contact with the second annular ring (254; 354), wherein the annular brush (256; 356) has a second brush end (260; 360) configured for contact with a radially outer surface (262; 362) of a blade outer air seal (120; 220; 320), wherein the second annular ring (254; 354) includes a socket (276; 376) configured to receive the first seal end (272; 372) of the axial ring seal (264; 364), characterised in that the axial ring seal (264; 364) has a second seal end (274; 374) configured for contact with an axial face (268; 368) of a component (270; 369) disposed downstream of the annular brush (256; 256).
An aircraft engine assembly comprising: an engine core including at least one internal combustion engine in driving engagement with an engine shaft ; a first casing (21; 321'); a turbine module including a second casing located outside of the first casing, the second casing containing a turbine section , the turbine section having an inlet in fluid communication with an outlet of the engine core, the turbine section including at least one turbine rotor connected to a turbine shaft , the turbine shaft extending into the first casing; and a compressor module including a third casing located outside of the first and second casings, the third casing containing a compressor having an outlet in fluid communication with an inlet of the engine core, the compressor including at least one compressor rotor in driving engagement with at least one of the turbine shaft and the engine shaft; wherein each casing defines an enclosure independently of the other casings; wherein the first casing is part of a gearbox module (20; 220; 320; 320') and contains at least part of a gear train (68; 368, 368'), and the turbine shaft is in driving engagement with the engine shaft through the gear train; characterised in that the turbine shaft is rotationally supported by a plurality of bearings all contained within the first casing; and the turbine shaft is free of rotational support within the second casing. an engine core including at least one internal combustion engine in driving engagement with an engine shaft ; a first casing (21; 321'); a turbine module including a second casing located outside of the first casing, the second casing containing a turbine section , the turbine section having an inlet in fluid communication with an outlet of the engine core, the turbine section including at least one turbine rotor connected to a turbine shaft , the turbine shaft extending into the first casing; and a compressor module including a third casing located outside of the first and second casings, the third casing containing a compressor having an outlet in fluid communication with an inlet of the engine core, the compressor including at least one compressor rotor in driving engagement with at least one of the turbine shaft and the engine shaft; wherein each casing defines an enclosure independently of the other casings; wherein the first casing is part of a gearbox module (20; 220; 320; 320') and contains at least part of a gear train (68; 368, 368'), and the turbine shaft is in driving engagement with the engine shaft through the gear train; characterised in that the turbine shaft is rotationally supported by a plurality of bearings all contained within the first casing; and the turbine shaft is free of rotational support within the second casing.
An apparatus for slicing food products, in particular a high-performance slicer, having a working region which comprises a cutting region and a transport region having a product feed , wherein the product feed supplies products to be sliced to the cutting region on one track or on multiple tracks and a cutting blade moves, in particular in a rotating and/or revolving manner, in a cutting plane at the end of the cutting region , wherein a transfer device is provided by means of which the products are transferred to the product feed and which comprises a pivotable product support which, in a downwardly pivoted state, takes over the products to be sliced from a conveying device of the transport region and, in an upwardly pivoted state, forms a product support, on which the products are disposed during the feed to the cutting region , together with a front conveyor , in particular a conveyor belt or a passive sliding support, and having a contactlessly working scanning device for detecting at least some of the outer contour of the products to be sliced, characterized in that the scanning device comprises at least one compact sensor which is arranged in the working region for contour detection and which is arranged in a separate self-contained sensor housing and defines a scanning region for the products , which is disposed outside the sensor housing , within the working region ; and in that the compact sensor is arranged in or at the cutting region or in the region of the product feed . having a working region which comprises a cutting region and a transport region having a product feed , wherein the product feed supplies products to be sliced to the cutting region on one track or on multiple tracks and a cutting blade moves, in particular in a rotating and/or revolving manner, in a cutting plane at the end of the cutting region , wherein a transfer device is provided by means of which the products are transferred to the product feed and which comprises a pivotable product support which, in a downwardly pivoted state, takes over the products to be sliced from a conveying device of the transport region and, in an upwardly pivoted state, forms a product support, on which the products are disposed during the feed to the cutting region , together with a front conveyor , in particular a conveyor belt or a passive sliding support, and having a contactlessly working scanning device for detecting at least some of the outer contour of the products to be sliced, characterized in that the scanning device comprises at least one compact sensor which is arranged in the working region for contour detection and which is arranged in a separate self-contained sensor housing and defines a scanning region for the products , which is disposed outside the sensor housing , within the working region ; and in that the compact sensor is arranged in or at the cutting region or in the region of the product feed .
A textile sleeve for routing and protecting an elongate member against abrasion, comprising: a flexible wall having a plurality of yarns interlaced with one another, at least some of said plurality of yarns being improved multifilament yarns (24"'") including low-melt multifilaments and non-low-melt multifilaments , said low-melt multifilaments having a first melt temperature and said non-low-melt multifilaments having a second melt temperature, said second melt temperature being greater than said first melt temperature, said low-melt multifilaments being bonded with said non-low-melt multifilaments to prevent relative sliding movement between said low-melt multifilaments and said non-low-melt multifilaments, wherein said wall has opposite edges extending generally parallel to a central axis between opposite ends , with the opposite edges being brought into overlapping relation with one another and said sleeve further including circumferentially extending, heat-set monofilaments biasing said opposite edges into overlapping relation with one another, said heat-set filaments being integrally provided in said improved multifilament yarns (24"'"). a flexible wall having a plurality of yarns interlaced with one another, at least some of said plurality of yarns being improved multifilament yarns (24"'") including low-melt multifilaments and non-low-melt multifilaments , said low-melt multifilaments having a first melt temperature and said non-low-melt multifilaments having a second melt temperature, said second melt temperature being greater than said first melt temperature, said low-melt multifilaments being bonded with said non-low-melt multifilaments to prevent relative sliding movement between said low-melt multifilaments and said non-low-melt multifilaments, wherein said wall has opposite edges extending generally parallel to a central axis between opposite ends , with the opposite edges being brought into overlapping relation with one another and said sleeve further including circumferentially extending, heat-set monofilaments biasing said opposite edges into overlapping relation with one another, said heat-set filaments being integrally provided in said improved multifilament yarns (24"'").
A plasma processing apparatus comprising: an impedance matching circuit ; a balun including a first unbalanced terminal connected to the impedance matching circuit , a grounded second unbalanced terminal , a first balanced terminal , and a second balanced terminal ; a grounded vacuum container ; a first electrode electrically connected to the first balanced terminal ; a second electrode electrically connected to the second balanced terminal ; characterized by an adjustment reactance configured to affect a relationship between a first voltage applied to the first electrode and a second voltage applied to the second electrode ; a high-frequency power supply configured to supply a high frequency between the first unbalanced terminal and the second unbalanced terminal via the impedance matching circuit ; and a controller configured to control an impedance of the impedance matching circuit and a reactance of the adjustment reactance , wherein the first electrode is configured to hold a first target , the second electrode is configured to hold a second target , the first electrode faces a space on a side of a substrate as a processing target via the first target , and the second electrode faces the space via the second target , and wherein the adjustment reactance includes capacitance arranged on a path that connects the first electrode and ground, and capacitance arranged on a path that connects the second electrode and the ground. an impedance matching circuit ; a balun including a first unbalanced terminal connected to the impedance matching circuit , a grounded second unbalanced terminal , a first balanced terminal , and a second balanced terminal ; a grounded vacuum container ; a first electrode electrically connected to the first balanced terminal ; a second electrode electrically connected to the second balanced terminal ; characterized by an adjustment reactance configured to affect a relationship between a first voltage applied to the first electrode and a second voltage applied to the second electrode ; a high-frequency power supply configured to supply a high frequency between the first unbalanced terminal and the second unbalanced terminal via the impedance matching circuit ; and a controller configured to control an impedance of the impedance matching circuit and a reactance of the adjustment reactance , wherein the first electrode is configured to hold a first target , the second electrode is configured to hold a second target , the first electrode faces a space on a side of a substrate as a processing target via the first target , and the second electrode faces the space via the second target , and wherein the adjustment reactance includes capacitance arranged on a path that connects the first electrode and ground, and capacitance arranged on a path that connects the second electrode and the ground.
Device having a base station and at least one processing unit that can be detached from the base station and has a tool for processing a medium, wherein the processing unit has a vessel for receiving the medium, a closure unit for closing the vessel and a sensor device for measuring at least one parameter of the medium, wherein at least a portion of the sensor device is disposed in and/or on the vessel in a stationary manner such that a parameter can be measured during the simultaneous processing of the medium, and wherein the device has a wireless module for producing a wireless connection and at least for transmitting data between the base station and the processing unit , wherein the device has a plurality of functionally different processing units , each processing unit , by means of coding stored on a transponder unit , is assigned a specific identification signal so that the base station can identify the respective processing unit , wherein the base station has a program memory having a plurality of processing programs, and wherein the base station is configured in a manner such that, by means of the specific identification signal, a specific processing program can be selected from the program memory, characterized in that a maximum operating time of a or each processing unit can be captured and/or stored by means of the transponder unit , with the result that a maximum operating time can be defined for a or each processing unit , wherein the base station can detect when this maximum operating time is reached.
System for detecting the crossing of a goal line of a goal frame by a ball, said goal frame extending vertically above the goal line, a vertical plane, called the goal line plane (P), being defined from a rear edge of the goal line , which system is characterized in that it comprises: - at least one lidar (4; 4a, 4b; 4c, 4d) arranged so as to scan, by means of a laser beam (L) and in a rotational movement, a vertical plane, called the detection plane (P1; P2), parallel to said goal line plane (P) and positioned behind the goal frame, said detection plane being located away from the goal line plane by a distance (d; d1, d2) that is smaller than the diameter (D) of the ball, said lidar generating a measurement signal, and - a processing unit for processing said measurement signal so as to detect the presence of a ball inside a zone, called the detection zone (Dl), of the detection plane delimited by the orthogonal projection of the goal frame onto the detection plane and to determine the position of the ball with respect to the goal line. - at least one lidar (4; 4a, 4b; 4c, 4d) arranged so as to scan, by means of a laser beam (L) and in a rotational movement, a vertical plane, called the detection plane (P1; P2), parallel to said goal line plane (P) and positioned behind the goal frame, said detection plane being located away from the goal line plane by a distance (d; d1, d2) that is smaller than the diameter (D) of the ball, said lidar generating a measurement signal, and - a processing unit for processing said measurement signal so as to detect the presence of a ball inside a zone, called the detection zone (Dl), of the detection plane delimited by the orthogonal projection of the goal frame onto the detection plane and to determine the position of the ball with respect to the goal line.
A mechanical seal suitable for sealing an annular gap between a rotary shaft and a housing having a shaft hole into which the rotary shaft is suitable for being inserted, the mechanical seal comprising: a rotary ring unit suitable for being mounted on the rotary shaft ; and a fixed ring unit suitable for being mounted on the housing , wherein the rotary ring unit includes: a sleeve suitable for being fixed to the rotary shaft ; and a rotary ring of which a movement in an axial direction and a rotation with respect to the sleeve is restricted; the fixed ring unit includes: a fixed ring suitable for sliding on an end surface of the rotary ring ; and a pressing member which presses the fixed ring toward the rotary ring ; the sleeve is provided with a stopper which restricts a movement of the rotary ring toward the fixed ring ; and the stopper includes: an annular part facing a fixed-ring-side end surface of the rotary ring ; characterized in that the stopper includes an inclined part extending from a radially-inner-side end of the annular part in a direction away from the rotary ring and toward a radially inner side, and in that the inclined part and the sleeve are fixed to each other by a welded part (Y). a rotary ring unit suitable for being mounted on the rotary shaft ; and a fixed ring unit suitable for being mounted on the housing , wherein the rotary ring unit includes: a sleeve suitable for being fixed to the rotary shaft ; and a rotary ring of which a movement in an axial direction and a rotation with respect to the sleeve is restricted; a sleeve suitable for being fixed to the rotary shaft ; and a rotary ring of which a movement in an axial direction and a rotation with respect to the sleeve is restricted; the fixed ring unit includes: a fixed ring suitable for sliding on an end surface of the rotary ring ; and a pressing member which presses the fixed ring toward the rotary ring ; a fixed ring suitable for sliding on an end surface of the rotary ring ; and a pressing member which presses the fixed ring toward the rotary ring ; the sleeve is provided with a stopper which restricts a movement of the rotary ring toward the fixed ring ; and the stopper includes: an annular part facing a fixed-ring-side end surface of the rotary ring ; characterized in that the stopper includes an inclined part extending from a radially-inner-side end of the annular part in a direction away from the rotary ring and toward a radially inner side, and in that the inclined part and the sleeve are fixed to each other by a welded part (Y).
A system comprising a surge arrester and an airfield lighting system, wherein the airfield lighting system comprises a primary circuit having multiple of transformers with primary windings and secondary windings, the primary windings of the transformers being connected in series in the primary circuit and at least one of the secondary windings of the transformers being adapted to feed electric power to a secondary circuit having an illumination device of the airfield lighting system, wherein the surge arrester is configured to provide a low impedance current path to ground for excessive voltages; characterized in that the surge arrester comprises a hermetically sealed enclosure for protecting a circuitry of the surge arrester; connectors (J1,J2,J4,J5) configured to electrically connect the surge arrester to the secondary circuit, wherein the connectors (J1,J2,J4,J5) are configured to associated mating connectors on the secondary circuit of the airfield lightning system and one of the connectors (J3) is configured to connect to a ground (GND), and wherein the surge arrester is adapted to protect the transformer and the primary circuit for excessive voltages that are applied to the illumination device or to a circuitry of the illumination device; wherein the surge arrester is a stand-alone unit that is configured to be attachable and installable to an existing airfield lightning system; and wherein the enclosure of the surge arrester is configured such that when the connectors are connected to the mating connectors, an outer material of the enclosure of the surge arrester extends over the point of connection.