mhurhangee/ep-ind-claims huggingface dataset:
Motor vehicle air guiding device, in particular for a lorry, wherein at least one flat air guiding wing can be connected or is connected to the vehicle in a lower connection region of a rear of the vehicle, wherein the lower connection region is arranged 50 to 220 cm, preferably 60 to 210 cm, in particular 80 to 210 cm above the lower wheel surface of a rear wheel of the motor vehicle, wherein the air guiding wing can be connected or is connected to the rear of the motor vehicle in the lower connection region without adjustment elements or actuator elements, wherein the air guiding wing can be connected or is connected to an upper air guiding element of the motor vehicle with the proviso that the air guiding wing, together with the upper air guiding element, can be transitioned - preferably, can be pivoted - from a resting position to an operating position and vice versa, and wherein the air guiding wing is designed to be flexible, or formed from a flexible material, characterized in that the air guiding wing consists of a more flexible material than the air guiding element, and/or is connected to the upper air guiding element via a predetermined breaking point or predetermined breaking line.
A decelerating clutch of a washing machine, comprising: a bearing seat, an input shaft, an output shaft, and an output shaft sleeve, wherein, the input shaft and the output shaft are arranged coaxially, the output shaft sleeve is sleeved on the input shaft and the output shaft, the output shaft sleeve is installed on the bearing seat via a bearing, the output shaft sleeve is connected with the input shaft in a transmission manner via a planetary gear train, two ends and a middle part of the output shaft sleeve are respectively provided with at least one bearing, an inner ring of the at least one bearing is coordinated with the output shaft sleeve, and an outer ring of the at least one bearing is coordinated with the bearing seat, wherein the output shaft sleeve additionally comprises an inner barrel shaft, a brake wheel and an oil seal cover, wherein the inner barrel shaft and the oil seal cover are respectively arranged at two sides of the brake wheel, and are fixedly connected with the brake wheel, and the three move synchronously, characterized in that the at least one bearing comprises a first bearing installed on the inner barrel shaft, a second bearing installed on the brake wheel, and a third bearing installed on the oil seal cover, wherein an inner ring of the first bearing and the third bearing is respectively in interference fit with the inner barrel shaft and the oil seal cover, and an outer ring of the first bearing and the third bearing is respectively in interference fit or clearance fit with the bearing seat. the input shaft and the output shaft are arranged coaxially, the output shaft sleeve is sleeved on the input shaft and the output shaft, the output shaft sleeve is installed on the bearing seat via a bearing, the output shaft sleeve is connected with the input shaft in a transmission manner via a planetary gear train, two ends and a middle part of the output shaft sleeve are respectively provided with at least one bearing, an inner ring of the at least one bearing is coordinated with the output shaft sleeve, and an outer ring of the at least one bearing is coordinated with the bearing seat, wherein the output shaft sleeve additionally comprises an inner barrel shaft, a brake wheel and an oil seal cover, wherein the inner barrel shaft and the oil seal cover are respectively arranged at two sides of the brake wheel, and are fixedly connected with the brake wheel, and the three move synchronously, characterized in that the at least one bearing comprises a first bearing installed on the inner barrel shaft, a second bearing installed on the brake wheel, and a third bearing installed on the oil seal cover, wherein an inner ring of the first bearing and the third bearing is respectively in interference fit with the inner barrel shaft and the oil seal cover, and an outer ring of the first bearing and the third bearing is respectively in interference fit or clearance fit with the bearing seat.
Filling plant for treating bottles as required, comprising: at least one bottle treating device (1; 190); a first supply line, which supplies a first bottle type (2, 3, 4, 5); at least one further supply line, which supplies a first further bottle type (2, 3, 4, 5), wherein the first further bottle type (2, 3, 4, 5) differs in the shape and/or in the size from the first bottle type (2, 3, 4, 5); a sorter, which is configured to remove bottles selectively arbitrarily from each of the supply lines, and to line up the bottles arranged in a predetermined order on an infeed section, and to feed them to the bottle handline device (1; 190) in the predetermined order, wherein the predetermined order can be chosen freely, and wherein the sorter comprises several movers (18, 19, 20, 21, 27, 118), which are driven independently and individually, characterized in that the bottle treating device (1; 190) is formed as carousel device and that the filling plant has a removal system for removing the bottles from the bottle treating device (1; 190), wherein a number of cycles in the bottle treating device (1; 190) can be controlled individually for each bottle, and that each mover (18, 19, 20, 21, 27, 118) comprises a gripper for removing a bottle from the supply lines and/or for feeding the bottle into the bottle treating device (1; 190). at least one bottle treating device (1; 190); a first supply line, which supplies a first bottle type (2, 3, 4, 5); at least one further supply line, which supplies a first further bottle type (2, 3, 4, 5), wherein the first further bottle type (2, 3, 4, 5) differs in the shape and/or in the size from the first bottle type (2, 3, 4, 5); a sorter, which is configured to remove bottles selectively arbitrarily from each of the supply lines, and to line up the bottles arranged in a predetermined order on an infeed section, and to feed them to the bottle handline device (1; 190) in the predetermined order, wherein the predetermined order can be chosen freely, and wherein the sorter comprises several movers (18, 19, 20, 21, 27, 118), which are driven independently and individually, characterized in that the bottle treating device (1; 190) is formed as carousel device and that the filling plant has a removal system for removing the bottles from the bottle treating device (1; 190), wherein a number of cycles in the bottle treating device (1; 190) can be controlled individually for each bottle, and that each mover (18, 19, 20, 21, 27, 118) comprises a gripper for removing a bottle from the supply lines and/or for feeding the bottle into the bottle treating device (1; 190).
Method for additively manufacturing at least one three-dimensional object by means of successive layerwise selective irradiation and consolidation of layers of a powder build material which can be consolidated by means of at least one energy beam, comprising the steps of: - providing a plurality of process parameter sets (PPS1 - PPSn) respectively comprising a plurality of process parameters (PP1 - PPn) allowing for a selective consolidation of a layer of the powder build material, wherein respective ones of the plurality of process parameter sets (PPS1 - PPSn) result in specific properties of a microstructure of an area of the respective layer of the powder build material selectively irradiated and consolidated on basis of the respective process parameter set (PPS 1 - PPSn); and - using at least two different process parameter sets (PPS1 - PPSn) from among the plurality of process parameter sets (PPS1 - PPSn) for additively manufacturing at least one three-dimensional object by means of the successive layerwise selective irradiation and consolidation of respective layers of the powder build material which can be consolidated by means of at least one energy beam, wherein the at least two different process parameter sets (PPS1 - PPSn) are used, respectively, to irradiate respective ones of a plurality of adj acent irradiation path vectors (V1 - V4) across the powder build material and thereby provide an interlocking microstructure in which adjacently disposed grains are disposed in an interlocking arrangement. - providing a plurality of process parameter sets (PPS1 - PPSn) respectively comprising a plurality of process parameters (PP1 - PPn) allowing for a selective consolidation of a layer of the powder build material, wherein respective ones of the plurality of process parameter sets (PPS1 - PPSn) result in specific properties of a microstructure of an area of the respective layer of the powder build material selectively irradiated and consolidated on basis of the respective process parameter set (PPS 1 - PPSn); and - using at least two different process parameter sets (PPS1 - PPSn) from among the plurality of process parameter sets (PPS1 - PPSn) for additively manufacturing at least one three-dimensional object by means of the successive layerwise selective irradiation and consolidation of respective layers of the powder build material which can be consolidated by means of at least one energy beam, wherein the at least two different process parameter sets (PPS1 - PPSn) are used, respectively, to irradiate respective ones of a plurality of adj acent irradiation path vectors (V1 - V4) across the powder build material and thereby provide an interlocking microstructure in which adjacently disposed grains are disposed in an interlocking arrangement.
A method for a TOF-PET scanner, the TOF-PET scanner comprising a scintillation chamber and a detection system comprising detection modules that surround the scintillation chamber; the method comprising: - providing a radiation source in the scintillation chamber, wherein the radiation source is configured to emit, in the scintillation chamber, both positrons for annihilation with emission of annihilation quanta and de-excitation quanta having an energy different from an energy of the annihilation quanta; - registering the annihilation quanta and the de-excitation quanta deposited in the detection modules; - selecting the registered annihilation quanta and the registered de-excitation quanta based on times of registration and energies of the deposited quanta; - assigning the annihilation quanta and the de-excitation quanta to common events; characterized by further comprising, for each detection module being calibrated: - determining distributions (n=f( T Diff)) of lifetimes of positrons based on differences ( T Diff) of the times of registration of annihilation quanta ( T anni) and of the times of registration of the de-excitation quanta ( T deex) assigned to the common events and registered by the module being calibrated; - extracting, from the determined distributions (n=f( T Diff)) of lifetimes of positrons, a distribution ( n = f T X p − Ps) of lifetimes of positrons with annihilation by para-positronium; and - determining a time delay constant ( D delay X) based on the extracted distributions of lifetimes of positrons with annihilation by para-positronium ( n = f T X p − Ps). - providing a radiation source in the scintillation chamber, wherein the radiation source is configured to emit, in the scintillation chamber, both positrons for annihilation with emission of annihilation quanta and de-excitation quanta having an energy different from an energy of the annihilation quanta; - registering the annihilation quanta and the de-excitation quanta deposited in the detection modules; - selecting the registered annihilation quanta and the registered de-excitation quanta based on times of registration and energies of the deposited quanta; - assigning the annihilation quanta and the de-excitation quanta to common events; characterized by further comprising, for each detection module being calibrated: - determining distributions (n=f( T Diff)) of lifetimes of positrons based on differences ( T Diff) of the times of registration of annihilation quanta ( T anni) and of the times of registration of the de-excitation quanta ( T deex) assigned to the common events and registered by the module being calibrated; - extracting, from the determined distributions (n=f( T Diff)) of lifetimes of positrons, a distribution ( n = f T X p − Ps) of lifetimes of positrons with annihilation by para-positronium; and - determining a time delay constant ( D delay X) based on the extracted distributions of lifetimes of positrons with annihilation by para-positronium ( n = f T X p − Ps).
A method for preparing a thermoplastic resin film laminate by thermal compressing, wherein the laminate comprises: at least a thermoplastic resin film layer with a thickness of 1-250 μm; at least a thermoplastic resin product layer; and a bonding layer of glue in between said thermoplastic resin film layer and said thermoplastic resin product layer; wherein the thermoplastic resin product layer is of a thermoplastic resin film or thermoplastic resin fabric, wherein said thermoplastic resin fabric is a woven fabric and/or a nonwoven (a non spunbond nonwoven or a material containing spunbond nonwoven structure); in which laminate said fabric has a gram weight of 1-250g/m 2, and the bonding layer has a gram weight of more than 0.1g/m 2, wherein, when the thermoplastic resin product layer is a thermoplastic resin film, the thermoplastic resin film has a thickness of 1-250 μm, wherein the method comprises: providing a thermoplastic resin film layer with a thickness of 1-250 μm; coating the thermoplastic resin film layer with a bonding layer of glue; applying a thermoplastic resin product layer on the thermoplastic resin film layer coated with the bonding layer of glue, to thereby bond the thermoplastic resin product layer to the thermoplastic resin film layer; thermal after-treatment, wherein the thermal after-treatment in Step is conducted at a temperature of 10°C-100°C lower than the melting point of thermoplastic resin film layer and thermoplastic resin product layer and at a pressure of 0.01-1MPa, and the thermal after-treatment time ranges from 0.001s-3600s, wherein the thermal after-treatment is conducted with a thermal after-treatment device selected from a drying oven or a board press machine. at least a thermoplastic resin film layer with a thickness of 1-250 μm; at least a thermoplastic resin product layer; and a bonding layer of glue in between said thermoplastic resin film layer and said thermoplastic resin product layer; providing a thermoplastic resin film layer with a thickness of 1-250 μm; coating the thermoplastic resin film layer with a bonding layer of glue; applying a thermoplastic resin product layer on the thermoplastic resin film layer coated with the bonding layer of glue, to thereby bond the thermoplastic resin product layer to the thermoplastic resin film layer; thermal after-treatment,
Heat exchanger, in particular for controlling the temperature of batteries or electronics, having at least one header with a bottom and a top, with openings which are provided in the bottom for receiving tube ends of tubes which are in fluidic communication with the headers, wherein the headers being formed from a U-shaped element with two parallel limbs (11, 12) and a bottom region which connects the limbs, wherein the openings being provided in the bottom region and characterised in that a wall region which is introduced between the limbs (11, 12) is provided as top.
Operating apparatus for a household appliance, with an operating element receptacle and an operating element, which can be positioned on the operating element receptacle such that it can be removed and attached, wherein the operating element is held on the operating element receptacle by means of magnetic holding force in the state in which it is attached thereto, and for this purpose the operating element has a holding magnet, characterised in that the holding magnet is arranged such that it can be moved in a defined manner in the operating element, wherein for this purpose it is not installed therein in a permanent manner at a fixed location, meaning that it can be located at different positions and can be moved in this context, wherein the holding magnet can be positioned in the operating element in a use position and a stowing position that is different therefrom, wherein the use position is the position in which the holding magnet generates a greatest possible magnetic field towards the outside, in order to achieve a highest possible magnetic force in the state in which it is attached to the operating element receptacle, and the stowing position is the position in which the holding magnet is positioned lying inside the operating element itself such that its magnetic field towards the outside and therefore beyond the operating element is reduced, in particular compared to the use position, wherein the coverage of the magnetic field out of the operating element in the stowing position is reduced compared to the use position and/or the strength of the magnetic field is reduced in this respect, wherein the holding magnet in the use position rests against a lower side, which faces the operating element receptacle in the state in which the operating element is attached to the operating element receptacle, of a housing of the operating element and the holding magnet in the stowing position is arranged at a distance from a lower side, which faces the operating element receptacle in the state in which the operating element is attached to the operating element receptacle, of the housing of the operating element and is set back into the interior of the housing, and wherein the operating element has a positioning apparatus, which is coupled to the holding magnet, and with which the holding magnet can be modified in terms of its position in the operating element in such that way that the desired different positions of the holding magnet can be set in a very precise and reliable manner.
Endoscope, comprising an elongated shaft (12; 52), a headpiece (14; 54) at a proximal end (18; 58) of the shaft (12; 52), the headpiece (14; 54) having a housing (16; 56), at least one light source (22; 62, 64), which is arranged in the shaft (12; 52) in a distal area thereof and produces lost heat, and a passive cooling, which has at least one heat pipe (24; 66, 68, 74) which is arranged in the shaft (12; 52) and is thermally coupled to the at least one light source (22; 62, 64) in order to lead away the lost heat in proximal direction, wherein the at least one heat pipe (24; 66, 68, 74) extends into the headpiece (14; 54), and wherein a heat sink body (32; 78) is arranged in the headpiece (14; 54), to which heat sink body (32; 78) the at least one heat pipe (24; 66, 68, 74) is thermally coupled, and which absorbs the lost heat from the at least one heat pipe (24; 66, 68, 74) and emits the lost heat to the environment directly or via the housing (16; 56) of the headpiece (14; 54), characterized in that the at least one heat pipe (66, 68) comprises a first heat pipe (66, 68) which is coupled to the at least one light source (62, 64) and extends to an intermediate area in the shaft between the distal and proximal ends (60, 58) thereof, and at least one second heat pipe which is thermally coupled to the first heat pipe (66, 68), which second heat pipe extends from the intermediate area into the headpiece, and is thermally coupled to the heat sink body, and that the at least one second heat pipe can rotate relative to the shaft about a longitudinal axis of the at least one second heat pipe, and in that the at least one second heat pipe is connected on the one hand to a camera, which is arranged in the distal area of the shaft, and on the other hand to a rotating drive, in order to allow the camera to rotate relative to the shaft about its own optical axis.
An aircraft galley unit characterized in that it comprises: a fixed-position galley structure mounted laterally adjacent to an aircraft cabin door, and a movable galley structure mounted for reciprocal movements between a stowed position wherein the moveable galley structure is stacked with and covers the fixed-position galley structure and an operative position wherein the movable galley structure is stacked with and covers the aircraft cabin door and thereby allow access to the fixed-position galley structure; wherein the fixed-position galley structure includes a table that is pivotally foldable between a closed position wherein the table is substantially vertically oriented, and an opened position wherein the table is substantially horizontally oriented; wherein the table, while in its opened position, will positionally lock the movable galley structure 10 in its operative position to prevent that it translates back to its stowed position. a fixed-position galley structure mounted laterally adjacent to an aircraft cabin door, and a movable galley structure mounted for reciprocal movements between a stowed position wherein the moveable galley structure is stacked with and covers the fixed-position galley structure and an operative position wherein the movable galley structure is stacked with and covers the aircraft cabin door and thereby allow access to the fixed-position galley structure; wherein the fixed-position galley structure includes a table that is pivotally foldable between a closed position wherein the table is substantially vertically oriented, and an opened position wherein the table is substantially horizontally oriented; wherein the table, while in its opened position, will positionally lock the movable galley structure 10 in its operative position to prevent that it translates back to its stowed position.
A rope hoist, comprising: a rope drum around which a wire rope can be wound; a drum motor for rotating the rope drum; a reduction gear mechanism reducing the rotation of the drum motor and transmitting the rotation to the rope drum; and a control unit controlling driving of the drum motor, and the rope drum and the drum motor are attached in a parallel manner to one surface of an end frame member, the reduction gear mechanism is arranged on the other surface of the end frame member, and the end frame member has a motor cover covering an end surface on the reduction gear mechanism side of the drum motor; characterizing in that the motor cover is provided with a recess which is dug so as to project from a surface of the motor cover toward the inside of the drum motor, at a position isolated from the reduction gear mechanism; and a connecting member (22,25,27) connecting a lead wire extended from a stator winding of the drum motor and a cable extended from the control unit is housed in the recess. a rope drum around which a wire rope can be wound; a drum motor for rotating the rope drum; a reduction gear mechanism reducing the rotation of the drum motor and transmitting the rotation to the rope drum; and a control unit controlling driving of the drum motor, and the rope drum and the drum motor are attached in a parallel manner to one surface of an end frame member, the reduction gear mechanism is arranged on the other surface of the end frame member, and the end frame member has a motor cover covering an end surface on the reduction gear mechanism side of the drum motor; characterizing in that the motor cover is provided with a recess which is dug so as to project from a surface of the motor cover toward the inside of the drum motor, at a position isolated from the reduction gear mechanism; and a connecting member (22,25,27) connecting a lead wire extended from a stator winding of the drum motor and a cable extended from the control unit is housed in the recess.