mhurhangee/ep-ind-claims huggingface dataset:
Method for producing a shoe, especially a sports shoe, comprising a shoe sole and an upper, wherein the production of the shoe sole comprises the steps: a) Providing a casting mould for forming at least a part of the shoe sole, wherein the casting mould having a bottom region, which lies vertically at the bottom, and having a side region, wherein the side region forming a side wall of the casting mould cavity and initially being open in the end region lying vertically at the top; b) Injecting a first liquid plastic material into a first surface section of the bottom region of the casting mould and at least injecting a second liquid plastic material into a second surface section of the bottom region of the casting mould, wherein the two plastic materials being different, wherein the injection of the liquid plastic material being accomplished by means of at least one nozzle, by means of which the plastic material is injected in a free jet into the respective surface section (8, 9); c) Closing the casting mould by means of a cover region lying vertically at the top, which cover region is placed onto the side region of the casting mould, and allowing the plastic materials to solidify; d) Opening of the casting mould and removing the produced moulded part, characterized in that the at least one nozzle is arranged at a location of the side region of the casting mould and all plastic materials are injected from there. a) Providing a casting mould for forming at least a part of the shoe sole, wherein the casting mould having a bottom region, which lies vertically at the bottom, and having a side region, wherein the side region forming a side wall of the casting mould cavity and initially being open in the end region lying vertically at the top; b) Injecting a first liquid plastic material into a first surface section of the bottom region of the casting mould and at least injecting a second liquid plastic material into a second surface section of the bottom region of the casting mould, wherein the two plastic materials being different, wherein the injection of the liquid plastic material being accomplished by means of at least one nozzle, by means of which the plastic material is injected in a free jet into the respective surface section (8, 9); c) Closing the casting mould by means of a cover region lying vertically at the top, which cover region is placed onto the side region of the casting mould, and allowing the plastic materials to solidify; d) Opening of the casting mould and removing the produced moulded part,
Manually operated machine tool, in particular dowel cutter, comprising a drive part having at least one machining tool for drilling and/or cutting a recess in a workpiece front side of a workpiece and a motorised drive for the at least one machining tool, and further comprising a stop device having a front stop surface for contact with the workpiece, and further comprising a guide arrangement for guiding the drive part and the stop device relative to one another, so that the at least one machining tool can be adjusted forwards and backwards relative to the front stop surface along a depth adjustment path for setting a penetration depth of the at least one machining tool into the workpiece, and further comprising a depth stop arrangement for limiting a length of the depth adjustment path, wherein the depth stop arrangement comprises a stop surface and at least one depth stop body, which is movably mounted and locatable on a depth stop bearing device for adjusting the penetration depth of the at least one machining tool into the workpiece, and wherein the depth stop surface is or can be located in a fixed way on the stop device and the depth stop bearing device is or can be located in a fixed way on the drive part or vice versa, characterised in that the depth stop arrangement comprises as a longitudinal stop for the at least one depth stop body on the adjustment path thereof at least one indexing body, which is movably mounted on the depth stop bearing device separately from the at least one depth stop body relative to the adjustment path of the at least one depth stop body.
A stable, pulverulent lycopene formulation, comprising lycopene having a degree of crystallinity of greater than 20% and at least one protective colloid.
A high frequency heating apparatus with a plurality of switches (SW1, SW2, SW3) and a plurality of tilting levers (16, 24) that are tilted in accordance with opening and closing operations of a door that exposes and closes an opening on a front side of the microwave oven, characterized in that, the plurality of switches (SW1, SW2, SW3) are switched with time differences by the motion of the plurality of tilting levers (16, 24), wherein contact portions of a first switch are switched by elastically displacing a conductive contact piece in a switch case by urging the conductive contact piece by a first cam formed at an inner end of a first tilting lever when said first tilting lever is tilted; contact portions of a second switch are switched by elastically displacing another conductive contact piece in said switch case by urging the other conductive contact piece by a second cam formed at the inner end of said first tilting lever at a timing different from the timing for switching the contact portions of said first switch; and a third switch is switched through a third cam formed at the inner end of a second tilting lever when said second tilting lever is tilted.
A pneumatic tire comprising: a tread extending in a tire circumferential direction, wherein the tread includes a plurality of ribs defined in a tire width direction by a plurality of circumferential main grooves formed so as to extend continuously in the tire circumferential direction and a plurality of blocks divided in at least two of the plurality of ribs by a plurality of sipes formed in the at least two of the ribs in a traversing manner so as to be spaced apart in the tire circumferential direction, between each of the blocks a first groove is formed so as to cut across the rib, the groove in communication with the corresponding sipe along its length only on one side of the corresponding groove in the tire circumferential direction, wherein obtuse angles are set in all intersection angles, in a plane parallel to the tire tread, between circumferential rib edges and the first grooves on one side in the tire circumferential direction in each of the blocks; and a center rib in the plurality of ribs is defined by a pair of the circumferential main grooves so as to sandwich a tire equator line therebetween; and characterised in that a plurality of short sipes are formed at left and right rib edges of the center rib so as to be spaced apart in the tire circumferential direction; a plurality of center rib grooves, each in communication with the corresponding short sipes are formed so as to be spaced apart in the tire circumferential direction and to cut across the center rib; and in each sipe, a depth of a rib edge side portion is set smaller than a depth of a rib center portion. a tread extending in a tire circumferential direction, wherein the tread includes a plurality of ribs defined in a tire width direction by a plurality of circumferential main grooves formed so as to extend continuously in the tire circumferential direction and a plurality of blocks divided in at least two of the plurality of ribs by a plurality of sipes formed in the at least two of the ribs in a traversing manner so as to be spaced apart in the tire circumferential direction, between each of the blocks a first groove is formed so as to cut across the rib, the groove in communication with the corresponding sipe along its length only on one side of the corresponding groove in the tire circumferential direction, wherein obtuse angles are set in all intersection angles, in a plane parallel to the tire tread, between circumferential rib edges and the first grooves on one side in the tire circumferential direction in each of the blocks; and a center rib in the plurality of ribs is defined by a pair of the circumferential main grooves so as to sandwich a tire equator line therebetween; and characterised in that a plurality of short sipes are formed at left and right rib edges of the center rib so as to be spaced apart in the tire circumferential direction; a plurality of center rib grooves, each in communication with the corresponding short sipes are formed so as to be spaced apart in the tire circumferential direction and to cut across the center rib; and
A process for making polyurethane/acrylic hybrid dispersions comprising the following continuous steps: i) adding at least one polyol into a reactor; ii) adding dimethylolpropionic acid (DMPA) simultaneously with/after step i), but before step iii), as water dispersibility enhancing agent at a temperature of from 115 °C to 140 °C to obtain a homogeneous solution; iii) adding at least one polyisocyanate at a temperature of from 75°C to 95 °C until the NCO content reaches a constant value to prepare the polyurethane prepolymer; iv) adding at least one acrylate monomer, at least one styrenic monomer, or the mixture thereof, as diluent to the polyurethane prepolymer, at a temperature of from 40 °C to 65°C; v) adding a neutralizing agent; vi) dispersing and extending the polyurethane prepolymer in the presence of the acrylate monomer, and/or the styrenic monomer of step iv); and vii) adding at least one ethylenically unsaturated nonionic monomer, and co-polymerizing it together with the acrylate monomer, and/or the styrenic monomer of step iv), to get the polyurethane/acrylic hybrid dispersion. i) adding at least one polyol into a reactor; ii) adding dimethylolpropionic acid (DMPA) simultaneously with/after step i), but before step iii), as water dispersibility enhancing agent at a temperature of from 115 °C to 140 °C to obtain a homogeneous solution; iii) adding at least one polyisocyanate at a temperature of from 75°C to 95 °C until the NCO content reaches a constant value to prepare the polyurethane prepolymer; iv) adding at least one acrylate monomer, at least one styrenic monomer, or the mixture thereof, as diluent to the polyurethane prepolymer, at a temperature of from 40 °C to 65°C; v) adding a neutralizing agent; vi) dispersing and extending the polyurethane prepolymer in the presence of the acrylate monomer, and/or the styrenic monomer of step iv); and vii) adding at least one ethylenically unsaturated nonionic monomer, and co-polymerizing it together with the acrylate monomer, and/or the styrenic monomer of step iv), to get the polyurethane/acrylic hybrid dispersion.
An interventional procedure simulation system, comprising a control unit and an interface unit, said control unit communicating with said interface unit to simulate handling of at least one instrument interfaced by said interface unit, wherein the instrument is a self-expanding tool inserted inside a simulated vessel and the control unit comprises a set of instructions comprising a number of initial values: a vessel initial inner diameter and stiffness value for said vessel, characterized in that said self-expanding tool is covered with a sheath and that the set of instructions comprises further number of initial values: a rest expansion diameter for the self-expanding instruments expansion diameter and a spring constant for the self-expanding instrument, which determine how the control unit sets boundaries for expansion of the instrument and simulated part of the vessel.
A laser light source device (1, 21, 41, 61), comprising: a plurality of optical devices for coaxially superimposing a plurality of laser lights of which frequencies are shifted from each other and emitting as one laser beam; and a wavelength conversion device for generating sum frequency once or more times for said laser beams emitted from said plurality of optical devices to cancel the mutual frequency shift, and performing wavelength conversion for said laser beams. a plurality of optical devices for coaxially superimposing a plurality of laser lights of which frequencies are shifted from each other and emitting as one laser beam; and a wavelength conversion device for generating sum frequency once or more times for said laser beams emitted from said plurality of optical devices to cancel the mutual frequency shift, and performing wavelength conversion for said laser beams.
Frontal airbag unit adapted for being mounted above the person to be protected, with an inflator and an airbag, said airbag comprising: - a first outer skin extending in a first direction from an inflatornear first end to a second end when in its deployed state, and defining a filling and support chamber being in fluid communication with the inflator, said filling and support chamber having a first maximum thickness (t maxf); and - a protection chamber being in fluid communication with the filling and support chamber via at least one overflow opening, wherein the first outer skin is comprised of a first layer and a second layer, said first layer and said second layer being connected to one another by means of a first peripheral connection, the length (l) of the first outer skin between the first end and the second end exceeds the maximum thickness (t maxf) of the filling and support chamber by at least the factor 2, and wherein the filling and support chamber is divided into at least two sub-chambers extending into the first direction by means of a dividing connection (22, 23) connecting the first layer and the second layer, characterized in that a second outer skin comprising an impact surface defines the protection chamber, and two dividing connections (22, 23) are present, such that the filling and support chamber is divided into two lateral sub-chambers (20b, 20c) and one central sub-chamber extending into the first direction. - a first outer skin extending in a first direction from an inflatornear first end to a second end when in its deployed state, and defining a filling and support chamber being in fluid communication with the inflator, said filling and support chamber having a first maximum thickness (t maxf); and - a protection chamber being in fluid communication with the filling and support chamber via at least one overflow opening,
A crash barrier section comprising a deflector body extending in particular in a longitudinal direction and having at least one chassis movable between a standby position and a travelling position, wherein the at least one chassis is retracted into a receptacle of the deflector body in the standby position and is extended from the receptacle in the travelling position in such a way that the crash barrier section can be moved on a support, in particular a road section, characterised in that the crash barrier section additionally comprises a lifting device, in particular comprising a pressure medium cylinder, preferably a hydraulic cylinder, preferably an oil or water hydraulic cylinder, with which the crash barrier section can be lifted from the support for extending and retracting the chassis and thus it can be avoided that the weight of the crash barrier section acts on the chassis during its extension and retraction.
An integrated terrain modeling system comprising: a site module, the site module including a database having a terrain model of a site; a first field unit, the first field unit including a sensor operable to generate geodetic data of the site formatted in a first format; a further field unit, the further field unit including a sensor operable to generate geodetic data of the site formatted in a further format; an integration system including at least one conversion module operable to manipulate the geodetic data generated by the first field unit and the further field unit to be in a common geodetic data format; and a distributed database management system that seamlessly integrates the geodetic data in the common geodetic data format at the site module to update the terrain model in real time or near-real time and distributes the terrain model to the field units. a site module, the site module including a database having a terrain model of a site; a first field unit, the first field unit including a sensor operable to generate geodetic data of the site formatted in a first format; a further field unit, the further field unit including a sensor operable to generate geodetic data of the site formatted in a further format; an integration system including at least one conversion module operable to manipulate the geodetic data generated by the first field unit and the further field unit to be in a common geodetic data format; and a distributed database management system that seamlessly integrates the geodetic data in the common geodetic data format at the site module to update the terrain model in real time or near-real time and distributes the terrain model to the field units.
A terminal apparatus comprising: a reception unit configured to receive Radio Resource Control, RRC, information for a serving cell; and a generation unit configured to, in a case that the RRC information does not include a first RRC parameter relating to Code Block Groups (CBGs) transmission for the serving cell, generate 1 Hybrid Automatic Repeat request ACKnowledgement, HARQ-ACK, bit for a transport block, in a case that the RRC information includes the first RRC parameter and also includes a second RRC parameter indicating a maximum number X of CBGs for a transport block for the serving cell, generate X HARQ-ACK bits for the transport block, wherein the transport block includes N CB code blocks, CBs, in a case that the number N CB of CB is less than the maximum number X of CBGs, the number of CBGs for the transport block is N CB, and the generation unit generates N CB HARQ-ACK bits for N CB CBGs and X - N CB negative-acknowledgement, NACK, as the X HARQ-ACK bits. a reception unit configured to receive Radio Resource Control, RRC, information for a serving cell; and a generation unit configured to, in a case that the RRC information does not include a first RRC parameter relating to Code Block Groups (CBGs) transmission for the serving cell, generate 1 Hybrid Automatic Repeat request ACKnowledgement, HARQ-ACK, bit for a transport block, in a case that the RRC information includes the first RRC parameter and also includes a second RRC parameter indicating a maximum number X of CBGs for a transport block for the serving cell, generate X HARQ-ACK bits for the transport block, wherein the transport block includes N CB code blocks, CBs, in a case that the number N CB of CB is less than the maximum number X of CBGs, the number of CBGs for the transport block is N CB, and the generation unit generates N CB HARQ-ACK bits for N CB CBGs and X - N CB negative-acknowledgement, NACK, as the X HARQ-ACK bits.
A grid assembly, in particular for air distribution systems, comprising a substantially box-shaped casing having a front opening and one or more joint mouths for connection to respective air conduits; a grid positioned in front of the front opening of the casing to close said opening; a mounting frame provided with fastening members to fix the frame to the casing; and a coupling device for coupling the grid to the frame; wherein the coupling device comprises at least a pair of elastic coupling springs which project from a first side of the frame and cooperate with a first portion of an inner edge of the grid, and one or more undercut teeth projecting from a second portion of the inner edge of the grid, opposite to the first portion, and engaging respective coupling seats formed on a second side, opposite to the first side, of the frame; and wherein the springs are defined by respective projections which project from an outer perimetric edge of the frame and protrude, in undeformed conditions, beyond said outer perimetric edge of the frame; and wherein the springs face respective recesses formed in the outer perimetric edge of the frame and shaped to receive the springs following an elastic deformation thereof.
A rotor blade for a wind turbine, comprising: a first blade segment and a second blade segment extending in opposite directions from a chord-wise joint, each of the first and second blade segments (30, 32) comprising one or more shell members (31, 33, 37, 39) and an internal support structure, the internal support structure of the first blade segment comprising a beam structure extending between a receiving end and a second end, the internal support structure of the second blade segment comprising a receiving section that receives the receiving end of the beam structure of the first blade segment; and, one or more connection locations where the first and second blade segments (30, 32) are secured together, wherein, when the beam structure is received within the receiving section, a gap comprising a varying thickness is defined and maintained between the beam structure and the receiving section in a span-wise direction of the rotor blade, wherein the varying thickness is at a minimum at the one or more connection locations, wherein the one or more connection locations comprise one or more first pin joints at the receiving end of the beam structure and one or more second pin joints positioned along the beam structure toward the second end, and characterized in that the varying thickness is at a maximum at a halfway point between the one or more first pin joints and the one or more second pin joints. a first blade segment and a second blade segment extending in opposite directions from a chord-wise joint, each of the first and second blade segments (30, 32) comprising one or more shell members (31, 33, 37, 39) and an internal support structure, the internal support structure of the first blade segment comprising a beam structure extending between a receiving end and a second end, the internal support structure of the second blade segment comprising a receiving section that receives the receiving end of the beam structure of the first blade segment; and, one or more connection locations where the first and second blade segments (30, 32) are secured together, wherein, when the beam structure is received within the receiving section, a gap comprising a varying thickness is defined and maintained between the beam structure and the receiving section in a span-wise direction of the rotor blade, wherein the varying thickness is at a minimum at the one or more connection locations, wherein the one or more connection locations comprise one or more first pin joints at the receiving end of the beam structure and one or more second pin joints positioned along the beam structure toward the second end, and characterized in that the varying thickness is at a maximum at a halfway point between the one or more first pin joints and the one or more second pin joints.