mhurhangee/ep-ind-claims huggingface dataset:
A toner comprising: toner base particles; and an external additive, the toner base particles each comprising a binder resin and a releasing agent, wherein the external additive comprises non-spherical coalesced particles in each of which primary particles are coalesced together, wherein the average of degrees of coalescence of the coalesced particles, being the particle diameter of coalesced particles divided by the average particle diameter of primary particles, as measured according to the description is 1.5 to 4,; and wherein the coalesced particles satisfy the following formula: Nx 1, 000 × 100 < 30 % where Nx is a number of the primary particles present alone relative to 1,000 of the coalesced particles, as observed under a scanning electron microscope after stirring 0.5 g of the coalesced particles and 49.5 g of a carrier placed in a 50 mL bottle for 10 minutes by means of a mixing and stirring device at 67 Hz, wherein the carrier is a coated ferrite powder obtainable by applying an acrylic resin-silicone resin coating layer forming solution containing alumina particles to surfaces of a baked ferrite powder, and drying the coated solution. toner base particles; and an external additive, the toner base particles each comprising a binder resin and a releasing agent, wherein the external additive comprises non-spherical coalesced particles in each of which primary particles are coalesced together, wherein the average of degrees of coalescence of the coalesced particles, being the particle diameter of coalesced particles divided by the average particle diameter of primary particles, as measured according to the description is 1.5 to 4,; and wherein the coalesced particles satisfy the following formula: Nx 1, 000 × 100 < 30 % where Nx is a number of the primary particles present alone relative to 1,000 of the coalesced particles, as observed under a scanning electron microscope after stirring 0.5 g of the coalesced particles and 49.5 g of a carrier placed in a 50 mL bottle for 10 minutes by means of a mixing and stirring device at 67 Hz, wherein the carrier is a coated ferrite powder obtainable by applying an acrylic resin-silicone resin coating layer forming solution containing alumina particles to surfaces of a baked ferrite powder, and drying the coated solution.
System for assisting with parking a motor vehicle, allowing the vehicle to be parked from a traffic lane into a free parking space and said parking space to be exited from into the traffic lane, said motor vehicle comprising a system for detecting obstacles, a system for detecting parking spaces, power assisted steering that is controllable to set steering angle, an engine or motor and a braking system that are controllable to set torque, an automatic gearbox or a shift-by-wire system, at least one odometric sensor, an accelerometer, and a means for activating an automatic driving function, the system for assisting with parking comprising: a module for regulating speed comprising a module for computing a setpoint value (V_cons) of the speed of the vehicle depending on the maximum speed (V_max) of the vehicle not to be exceeded and the distance (d_rest) remaining to be travelled; and a module for regulating any discontinuity in the distance (d_rest) remaining to be travelled, comprising: a module for verifying that the system is in a state of movement; and a module for detecting a discontinuity, this module being configured to detect a jump in the distance (d_rest) remaining to be travelled that has an impact on the speed setpoint (V_cons); characterized in that the system for assisting with parking comprises: a module for replacing the nominal deceleration profile with a degraded-mode deceleration profile if a discontinuity is detected; and a module for exiting from said degraded mode. a module for regulating speed comprising a module for computing a setpoint value (V_cons) of the speed of the vehicle depending on the maximum speed (V_max) of the vehicle not to be exceeded and the distance (d_rest) remaining to be travelled; and a module for regulating any discontinuity in the distance (d_rest) remaining to be travelled, comprising: a module for verifying that the system is in a state of movement; and a module for detecting a discontinuity, this module being configured to detect a jump in the distance (d_rest) remaining to be travelled that has an impact on the speed setpoint (V_cons); characterized in that the system for assisting with parking comprises: a module for replacing the nominal deceleration profile with a degraded-mode deceleration profile if a discontinuity is detected; and a module for exiting from said degraded mode. a module for verifying that the system is in a state of movement; and a module for detecting a discontinuity, this module being configured to detect a jump in the distance (d_rest) remaining to be travelled that has an impact on the speed setpoint (V_cons); characterized in that the system for assisting with parking comprises: a module for replacing the nominal deceleration profile with a degraded-mode deceleration profile if a discontinuity is detected; and a module for exiting from said degraded mode. a module for replacing the nominal deceleration profile with a degraded-mode deceleration profile if a discontinuity is detected; and a module for exiting from said degraded mode.
A rotor blade for a rotor of a wind power installation, the rotor blade comprising a hub-side end for fastening the rotor blade to a movable part of a blade bearing, wherein a bearing cover is arranged on an outer circumferential surface of the hub-side end of the rotor blade, wherein a portion of the bearing cover that is close to the bearing is further away from the outer circumferential surface of the hub-side end of the rotor blade than a portion of the bearing cover that is remote from the bearing by a multiple, characterized in that provision is made of a sealing element which at least partially seals off and/or covers a gap between the outer circumferential surface of the hub-side end of the rotor blade and that portion of the bearing cover which is remote from the bearing wherein a bearing cover is arranged on an outer circumferential surface of the hub-side end of the rotor blade, wherein a portion of the bearing cover that is close to the bearing is further away from the outer circumferential surface of the hub-side end of the rotor blade than a portion of the bearing cover that is remote from the bearing by a multiple, characterized in that provision is made of a sealing element which at least partially seals off and/or covers a gap between the outer circumferential surface of the hub-side end of the rotor blade and that portion of the bearing cover which is remote from the bearing
A hot melt adhesive composition comprising: a) an ethylene/α-olefin multi-block copolymer having a weight average molecular weight (Mw) less than 20,000, wherein the ethylene/α-olefin multi-block copolymer includes hard segments and soft segments, wherein the hard segments are blocks of polymerized units in which ethylene is present in an amount greater than 90 weight percent based on the weight of the polymer, and wherein the soft segments are blocks of polymerized units in which the comonomer content (content of monomers other than ethylene) is greater than 5 weight percent, based on the weight of the polymer; b) a tackifier having a softening temperature from 90°C to 150°C; and c) a wax. a) an ethylene/α-olefin multi-block copolymer having a weight average molecular weight (Mw) less than 20,000, wherein the ethylene/α-olefin multi-block copolymer includes hard segments and soft segments, wherein the hard segments are blocks of polymerized units in which ethylene is present in an amount greater than 90 weight percent based on the weight of the polymer, and wherein the soft segments are blocks of polymerized units in which the comonomer content (content of monomers other than ethylene) is greater than 5 weight percent, based on the weight of the polymer; b) a tackifier having a softening temperature from 90°C to 150°C; and c) a wax.
A spectrum sharing method, wherein the method comprises: acquiring load information of a first system and load information of a second system; acquiring a cycle period of a shared frequency of the first system and the second system; obtaining time slice allocation information according to the load information of the first system, the load information of the second system, and the cycle period, wherein the time slice allocation information comprises a first time slice and a second time slice; and sending the time slice allocation information to user equipment, so that the user equipment performs data transmission at the first time slice by using the first system and by using the shared frequency and performs data transmission at the second time slice by using the second system and by using the shared frequency. acquiring load information of a first system and load information of a second system; acquiring a cycle period of a shared frequency of the first system and the second system; obtaining time slice allocation information according to the load information of the first system, the load information of the second system, and the cycle period, wherein the time slice allocation information comprises a first time slice and a second time slice; and sending the time slice allocation information to user equipment, so that the user equipment performs data transmission at the first time slice by using the first system and by using the shared frequency and performs data transmission at the second time slice by using the second system and by using the shared frequency.
Assembly for an aircraft turbine engine, the assembly comprising a fan, a speed reducer driving the fan and located downstream thereof, an intermediate casing including an inner annular structure internally delimiting a cavity at least partially housing the reducer, the latter comprising an epicyclic gear train equipped with a planetary carrier, one ring of which is fixed to the inner annular structure of the intermediate casing, by means of a main retaining device, characterised in that the assembly includes a secondary retaining device of the ring of the planetary carrier relative to the inner annular structure of the intermediate casing, the secondary retaining device comprising: - first projections projecting radially inwardly from the inner annular structure of the intermediate casing, the first projections being spaced apart circumferentially from one another about a longitudinal axis of the turbine engine, each first projection having a recess open radially inwardly, open axially downstream, and open circumferentially in a first circumferential direction, and delimited by three faces, respectively an axial retaining face, a radial retaining face, as well as a circumferential retaining face; - second projections projecting radially outwardly from the ring of the planetary carrier, the second projections being spaced apart circumferentially from one another about the longitudinal axis of the turbine engine, and cooperating in pairs with the first projections in such a way that each second projection is partly housed in the recess of its associated first projection, downstream thereof. - first projections projecting radially inwardly from the inner annular structure of the intermediate casing, the first projections being spaced apart circumferentially from one another about a longitudinal axis of the turbine engine, each first projection having a recess open radially inwardly, open axially downstream, and open circumferentially in a first circumferential direction, and delimited by three faces, respectively an axial retaining face, a radial retaining face, as well as a circumferential retaining face; - second projections projecting radially outwardly from the ring of the planetary carrier, the second projections being spaced apart circumferentially from one another about the longitudinal axis of the turbine engine, and cooperating in pairs with the first projections in such a way that each second projection is partly housed in the recess of its associated first projection, downstream thereof.
A battery part configured to provide an external connection for a battery, the battery part comprising: a base portion; a lug portion extending from the base portion, wherein the base portion is configured to be a least partially embedded in battery container material; a through-hole extending longitudinally through the base portion and the lug portion, wherein the through-hole includes: a first hole portion extending from the base portion toward the lug portion and defining a first inner surface; a second hole portion extending from the first hole portion through a remainder of the lug portion and defining a second inner surface, wherein the first inner surface is radially offset from the second inner surface; and a shoulder portion at an interface between the first and second hole portions (621, 623); and a projection extending from the shoulder portion, wherein the projection is spaced apart from and deflected toward the first inner surface, wherein the projection and the first inner surface define a recess therebetween, and wherein an end portion of the projection is spaced apart from the first inner surface by a distance less than the radial offset of the first and second inner surfaces (637, 635). a base portion; a lug portion extending from the base portion, wherein the base portion is configured to be a least partially embedded in battery container material; a through-hole extending longitudinally through the base portion and the lug portion, a first hole portion extending from the base portion toward the lug portion and defining a first inner surface; a second hole portion extending from the first hole portion through a remainder of the lug portion and defining a second inner surface, wherein the first inner surface is radially offset from the second inner surface; and a shoulder portion at an interface between the first and second hole portions (621, 623); and a projection extending from the shoulder portion, wherein the projection is spaced apart from and deflected toward the first inner surface, wherein the projection and the first inner surface define a recess therebetween, and wherein an end portion of the projection is spaced apart from the first inner surface by a distance less than the radial offset of the first and second inner surfaces (637, 635).
A workstation assembly having a desk and a seating and/or leaning facility, wherein a treadmill is arranged in the foot area of the workstation assembly, wherein the treadmill is revolvingly supported on a frame, wherein the feet of a user can roll off in walking on the treadmill, and wherein the treadmill is passively driven by the walking movement of the user, characterized in that a return stop device is provided on the treadmill, wherein the return stop device precludes the driving of the treadmill opposite to the running direction directed towards the desk.
A strut system for coupling a ram-air turbine, RAT, to an aircraft, comprising: a strut that includes a strut body, the strut having a strut first end that is configured to connect to the aircraft and rotate about a first axis, the strut having a strut second end that is spaced apart from the strut first end by the strut body and is configured to connect to a RAT turbine generator unit, and a damper rod that includes a rod body; characterised in that the strut has a strut conduit extending from the strut first end toward the strut second end; and further characterised in that the damper rod is disposed within the strut conduit, the damper rod having a rod first end that is fixed within the strut conduit at the strut first end, and a rod second end that is spaced apart from the rod first end by the rod body and is located intermediate the strut first end and the strut second end, wherein the rod second end is configured to move along a second axis that is parallel to the first axis. a strut that includes a strut body, the strut having a strut first end that is configured to connect to the aircraft and rotate about a first axis, the strut having a strut second end that is spaced apart from the strut first end by the strut body and is configured to connect to a RAT turbine generator unit, and a damper rod that includes a rod body; characterised in that the strut has a strut conduit extending from the strut first end toward the strut second end; and further characterised in that the damper rod is disposed within the strut conduit, the damper rod having a rod first end that is fixed within the strut conduit at the strut first end, and a rod second end that is spaced apart from the rod first end by the rod body and is located intermediate the strut first end and the strut second end, wherein the rod second end is configured to move along a second axis that is parallel to the first axis.
A controller for a vehicle, the vehicle comprising: an internal combustion engine; a motor generator; a drive sprocket fixed to a crankshaft of the internal combustion engine; an idler sprocket (22, 23) to which a driving force is transmitted from the drive sprocket; a chain running around the drive sprocket and the idler sprocket (22, 23); a swing guide supported in a swingable manner; a chain tensioner that pushes the swing guide against the chain; and an oil pump that discharges oil when the crankshaft rotates, wherein the controller is configured to control a traveling mode of the vehicle in a Battery Electric Vehicle mode that stops the internal combustion engine and drives the motor generator when the vehicle travels or a non-BEV mode that drives the internal combustion engine when the vehicle travels, wherein the chain tensioner has an oil damper functionality that uses oil supplied from the oil pump, and when shifting the traveling mode of the vehicle from the BEV mode to the non-BEV mode, the controller is configured to execute a high-pressure process for controlling the oil pump to supply oil to the chain tensioner with a supply pressure that is higher when a duration of the BEV mode is greater than or equal to a specified time than when the BEV mode duration is less than the specified time. an internal combustion engine; a motor generator; a drive sprocket fixed to a crankshaft of the internal combustion engine; an idler sprocket (22, 23) to which a driving force is transmitted from the drive sprocket; a chain running around the drive sprocket and the idler sprocket (22, 23); a swing guide supported in a swingable manner; a chain tensioner that pushes the swing guide against the chain; and an oil pump that discharges oil when the crankshaft rotates, wherein the controller is configured to control a traveling mode of the vehicle in a Battery Electric Vehicle mode that stops the internal combustion engine and drives the motor generator when the vehicle travels or a non-BEV mode that drives the internal combustion engine when the vehicle travels, wherein the chain tensioner has an oil damper functionality that uses oil supplied from the oil pump, and when shifting the traveling mode of the vehicle from the BEV mode to the non-BEV mode, the controller is configured to execute a high-pressure process for controlling the oil pump to supply oil to the chain tensioner with a supply pressure that is higher when a duration of the BEV mode is greater than or equal to a specified time than when the BEV mode duration is less than the specified time.
A medical or dental treatment device, which can be connected to a plurality of different tools, wherein the medical or dental treatment device comprises: a tool retainer for connecting the treatment device to a tool, at least one measuring coil (5, 5A) which is connected to an electrical energy supply device via an electrical line and which can be supplied with a periodic, in particular sinusoidal electrical energy supply from the electrical energy supply device, and an evaluation device electrically connected to the at least one measuring coil (5, 5A) for detecting whether a tool is connected to the treatment device or which of a plurality of tools is connected to the treatment device, wherein due to an inductive coupling between the tool accommodated in the tool retainer and the at least one measuring coil (5, 5A) supplied with the periodic electrical energy, a periodic, in particular sinusoidal measurement signal can be generated which is specific to each tool and which can be assigned to the respective tool by the evaluation device, characterized in that the evaluation device determines the phase shift of the electrical voltage and of the electric current of the periodic, in particular sinusoidal measurement signal for detecting whether a tool is connected to the treatment device or which of a plurality of tools is connected to the treatment device.
A composition comprising hydrogen peroxide and from 0.1 to 0.8 wt% of a polyurethane for use in a treatment operation in cleaning a fabric material, wherein the polyurethane is a sodium hydrogen sulphite adduct of an ethylene oxide/propylene oxide copolymer reacted with hexamethylene diisocyanate.
. A method for image segmentation using an encoding-decoding network including (i) K encoding filters -th to (1-K)-th; (ii) K decoding filters (2-K)-th to -th, each of which corresponds to each of the -th to the (1-K)-th filters; and (iii) a 1-st to a K-th loss layers respectively interacting with the K filters included in the decoding layer, wherein K is an integer greater than or equal to 3, characterized in that the encoding-decoding network further comprises: H intermediate dilation convolution filters -th to (4-H)-th, each positioned between one of the encoding filters -th to the (1-K)-th and its corresponding decoding filter, wherein H is an integer greater than 0 and no larger than K.
Method for piloting a craft by propulsion means that can be oriented relative to the rear end (1 R) of said craft, according to which method, in accordance with a servo loop: - the attitude (θ M) of said craft is measured, and - the orientation (β) of said propulsion means is adjusted as a function of said attitude measurement (θM), in such a way as to stabilise said craft on its flight path, the attitude (θM) of said craft is measured in the vicinity of said rear end (1 R) and when adjusting the orientation (β) of said propulsion means, angular (δθM, δθT) and linear (δyM, δyT) deformations at the rear end (1 R) of said craft and at the location of the attitude measurement (θM) are taken into account. - the attitude (θ M) of said craft is measured, and - the orientation (β) of said propulsion means is adjusted as a function of said attitude measurement (θM), in such a way as to stabilise said craft on its flight path,