mhurhangee/patent-ind-claim-en huggingface dataset:
A method for manufacturing a porous ceramic wall flow filter, comprising the steps of: providing a honeycomb structure defining a plurality of cell channels bounded by porous channel walls that extend longitudinally from an upstream inlet end to a downstream outlet end; providing a plugging mixture, the plugging mixture comprising an inorganic powder batch composition; a binder; a liquid vehicle; and a rheology modifier selected from the group consisting of a polyethylene glycol dioleate, an oil, and fumed silica, the rheology modifier being present as a super addition in an amount in the range of from 0.1 weight percent to 15 weight percent relative to the inorganic powder batch composition; the plugging mixture exhibiting an inclined plane flow rate less than 60mm/8 min when measured at an angle of 60 degrees; selectively plugging an end of at least one predetermined channel with the plugging mixture which exhibits a capillary viscosity less than 8000 Pa·s when measured at a shear rate of 10/sec; firing the selectively plugged honeycomb body under conditions effective to form a sintered phase ceramic plug in the at least one selectively plugged channel by converting the plugging material into a primary sintered phase ceramic composition, wherein the firing comprises heating the plugging material at a maximum temperature of at least 400°C. providing a honeycomb structure defining a plurality of cell channels bounded by porous channel walls that extend longitudinally from an upstream inlet end to a downstream outlet end; providing a plugging mixture, the plugging mixture comprising an inorganic powder batch composition; a binder; a liquid vehicle; and a rheology modifier selected from the group consisting of a polyethylene glycol dioleate, an oil, and fumed silica, the rheology modifier being present as a super addition in an amount in the range of from 0.1 weight percent to 15 weight percent relative to the inorganic powder batch composition; the plugging mixture exhibiting an inclined plane flow rate less than 60mm/8 min when measured at an angle of 60 degrees; selectively plugging an end of at least one predetermined channel with the plugging mixture which exhibits a capillary viscosity less than 8000 Pa·s when measured at a shear rate of 10/sec; firing the selectively plugged honeycomb body under conditions effective to form a sintered phase ceramic plug in the at least one selectively plugged channel by converting the plugging material into a primary sintered phase ceramic composition, wherein the firing comprises heating the plugging material at a maximum temperature of at least 400°C.
A solid catalyst system comprising a first chromium compound, a second chromium compound, a reaction product of an alkyl aluminium compound and a nitrogen containing compound and a silicon oxide support, wherein the first chromium compound is chromium trioxide or a compound convertible to chromium trioxide, the second chromium compound is a silylchromate compound and the nitrogen containing compound is a cycloalkylamine compound having the general formula: R 3 -NH 2 , wherein R 3 is selected from C3-C8 cycloalkyl groups. the first chromium compound is chromium trioxide or a compound convertible to chromium trioxide, the second chromium compound is a silylchromate compound and the nitrogen containing compound is a cycloalkylamine compound having the general formula: R 3 -NH 2 , wherein R 3 is selected from C3-C8 cycloalkyl groups.
A lighting system for a leaning vehicle , comprising: a pivot frame configured to be fixed to a light emitting device and to a light reflective device (201"), a mount configured to be fixed to a light fitting of a leaning vehicle, a motor attached to the pivot frame and the mount , wherein the motor is configured to provide rotational movement of the pivot frame relative to the mount around a rotational axis of the motor, whereby the rotational axis is a pivot axis being concentric with an optical axis of the light emitting device , and a controller in electrical communication with the motor and being configured to receive sensor data of a leaning angle (v) of the leaning vehicle , and wherein the controller is configured to control the motor to rotate the pivot frame to a desired angle (v') relative to the mount based on the leaning angle, whereby the light emitting device and the light reflective device (201") are rotatable by the motor relative the mount , characterized in that the motor is concentrically arranged with respect to the pivot frame , and wherein the pivot frame and the mount are connected at opposite sides of the motor and the mount comprising a connecting element configured for removably attaching the lighting system to a corresponding light fitting of an existing headlight assembly of the leaning vehicle. a pivot frame configured to be fixed to a light emitting device and to a light reflective device (201"), a mount configured to be fixed to a light fitting of a leaning vehicle, a motor attached to the pivot frame and the mount , wherein the motor is configured to provide rotational movement of the pivot frame relative to the mount around a rotational axis of the motor, whereby the rotational axis is a pivot axis being concentric with an optical axis of the light emitting device , and a controller in electrical communication with the motor and being configured to receive sensor data of a leaning angle (v) of the leaning vehicle , and wherein the controller is configured to control the motor to rotate the pivot frame to a desired angle (v') relative to the mount based on the leaning angle, whereby the light emitting device and the light reflective device (201") are rotatable by the motor relative the mount , characterized in that the motor is concentrically arranged with respect to the pivot frame , and wherein the pivot frame and the mount are connected at opposite sides of the motor and the mount comprising a connecting element configured for removably attaching the lighting system to a corresponding light fitting of an existing headlight assembly of the leaning vehicle.
A paging method, comprising: determining , by a first access network device, a paging parameter of a terminal, wherein the determining a paging parameter of a terminal is triggered by downlink data to the terminal reaching the first access network device from a core network device, wherein the paging parameter is used for the first access network device to send a paging message to the terminal, and the downlink data is downlink service data or downlink signaling; sending , by the first access network device based on the paging parameter of the terminal, a paging message to the terminal through the first access network device or a second access network device; and sending , by the first access network device, the downlink data to the terminal; wherein the paging parameter comprises a paging priority of the terminal; and the determining, by the first access network device, a paging parameter of the terminal comprises: determining, by the first access network device, the paging priority of the terminal based on a mapping relationship between a type of the downlink data and the paging priority, characterised in that the type of the downlink data comprises the following information: an allocation and retention priority, ARP, type. determining , by a first access network device, a paging parameter of a terminal, wherein the determining a paging parameter of a terminal is triggered by downlink data to the terminal reaching the first access network device from a core network device, wherein the paging parameter is used for the first access network device to send a paging message to the terminal, and the downlink data is downlink service data or downlink signaling; sending , by the first access network device based on the paging parameter of the terminal, a paging message to the terminal through the first access network device or a second access network device; and sending , by the first access network device, the downlink data to the terminal; wherein the paging parameter comprises a paging priority of the terminal; and the determining, by the first access network device, a paging parameter of the terminal comprises: determining, by the first access network device, the paging priority of the terminal based on a mapping relationship between a type of the downlink data and the paging priority, characterised in that the type of the downlink data comprises the following information: an allocation and retention priority, ARP, type.
Method for reducing the angular momentum of a spacecraft, said spacecraft comprising: - a propulsion device able to generate a torque of modulatable amplitude along a Z axis, said Z axis corresponding substantially to an axis of maximum inertia or minimum inertia of the spacecraft, an X axis and a Y axis forming with Z a direct orthogonal frame attached to the spacecraft; - an angular momentum accumulating device , able to generate and control, via control of the angular velocities of flywheels belonging to the angular momentum accumulating device, an angular momentum and a torque along the X, Y and Z axes; - a set of sensors able to measure the angular velocities (ω x , ω y , ω z ) of the spacecraft along the X, Y and Z axes, and to deliver an estimation of the angular momentum (h) of the spacecraft; wherein said method comprises: - a first step of aligning the angular momentum of the spacecraft along the Z axis, consisting in slaving the angular momentum, along the X axis and the Y axis, respectively, of the angular momentum accumulating device , to the angular velocity of the spacecraft, along the Y axis and the X axis, respectively, creating gyroscopic torques that tend to reduce the angular velocities of the spacecraft along the X and Y axes; characterized in that the method further comprises: - a second step of reducing the angular momentum of the spacecraft by means of a Z-axis torque generated by the propulsion device . - a propulsion device able to generate a torque of modulatable amplitude along a Z axis, said Z axis corresponding substantially to an axis of maximum inertia or minimum inertia of the spacecraft, an X axis and a Y axis forming with Z a direct orthogonal frame attached to the spacecraft; - an angular momentum accumulating device , able to generate and control, via control of the angular velocities of flywheels belonging to the angular momentum accumulating device, an angular momentum and a torque along the X, Y and Z axes; - a set of sensors able to measure the angular velocities (ω x , ω y , ω z ) of the spacecraft along the X, Y and Z axes, and to deliver an estimation of the angular momentum (h) of the spacecraft; - a first step of aligning the angular momentum of the spacecraft along the Z axis, consisting in slaving the angular momentum, along the X axis and the Y axis, respectively, of the angular momentum accumulating device , to the angular velocity of the spacecraft, along the Y axis and the X axis, respectively, creating gyroscopic torques that tend to reduce the angular velocities of the spacecraft along the X and Y axes; - a second step of reducing the angular momentum of the spacecraft by means of a Z-axis torque generated by the propulsion device .
Light guide having an exit face and an elongate entrance face comprising a first elongate portion and a second elongate portion that are juxtaposed across the width of the entrance face, the light guide comprising, in line with said first portion , a first optical element and a second optical element , and, in line with said second portion , a third optical element and a fourth optical element , the first optical element adjoining the fourth optical element in the width of the elongate entrance face, the second optical element adjoining the third optical element in the width of the elongate entrance face, the first optical element being designed to reflect, in the direction at least of said second optical element , a first light flux (R1) received from the entrance face, and the second optical element being designed to transmit in the direction of the exit face a second light flux (R2) received from the entrance face and to reflect in the direction of the exit face the first light flux (R1) reflected by said first optical element , the third optical element being designed to reflect, in the direction at least of said fourth optical element , a third light flux (R3) received from the entrance face, and the fourth optical element being designed to transmit, in the direction of the exit face , a fourth light flux (R4) received from the entrance face and to reflect, in the direction of the exit face , the third light flux (R3) reflected by said third optical element .
A polymer material for a lithium secondary battery comprising a polythiophene-based polymer represented by the following Formula 1 and a conductive polymer: wherein n is 70 to 280, PEG is polyethylene glycol, and when the number of ethylene oxide units of PEG is m, m is 4 to 15; wherein the conductive polymer comprises poly-(3,4-ethylenedioxythiophene):poly(styrenesulfonate); and wherein the polythiophene-based polymer and the conductive polymer are contained in a weight ratio of 95:5 to 80:20. wherein n is 70 to 280, PEG is polyethylene glycol, and when the number of ethylene oxide units of PEG is m, m is 4 to 15; wherein the conductive polymer comprises poly-(3,4-ethylenedioxythiophene):poly(styrenesulfonate); and wherein the polythiophene-based polymer and the conductive polymer are contained in a weight ratio of 95:5 to 80:20.
Method of production of an annealed cold-rolled non grain-oriented Fe-Si steel sheet consisting of the successive following steps: - melting a steel composition that contains in weight percentage: C ≤ 0.006 2.0 ≤ Si ≤ 5.0 0.1 ≤ Al 3.0 0.1 ≤ Mn ≤ 3.0 N ≤ 0.006 0.04≤ Sn ≤ 0.2 S ≤ 0.005 P ≤ 0.2 Ti ≤ 0.01 the balance being Fe and inevitable impurities - casting said melt into a slab - reheating said slab at a temperature between 1050°C and 1250°C - hot rolling said slab with a hot rolling finishing temperature between 750°C and 950°C to obtain a hot rolled steel band, - coiling said hot rolled steel band at a temperature between 500°C and 750°C, - said hot rolled steel band being annealed at a temperature between 650°C and 950°C for a time between 10s and 48 hours - cold rolling the hot rolled steel band to obtain a cold rolled steel sheet - heating the cold rolled steel sheet up to a soaking temperature between 850°C and 1150°C - holding the cold rolled steel at the soaking temperature for a time between 20s and 100s - cooling the cold rolled steel down to room. - melting a steel composition that contains in weight percentage: C ≤ 0.006 2.0 ≤ Si ≤ 5.0 0.1 ≤ Al 3.0 0.1 ≤ Mn ≤ 3.0 N ≤ 0.006 0.04≤ Sn ≤ 0.2 S ≤ 0.005 P ≤ 0.2 Ti ≤ 0.01 the balance being Fe and inevitable impurities C ≤ 0.006 2.0 ≤ Si ≤ 5.0 0.1 ≤ Al 3.0 0.1 ≤ Mn ≤ 3.0 N ≤ 0.006 0.04≤ Sn ≤ 0.2 S ≤ 0.005 P ≤ 0.2 Ti ≤ 0.01 - casting said melt into a slab - reheating said slab at a temperature between 1050°C and 1250°C - hot rolling said slab with a hot rolling finishing temperature between 750°C and 950°C to obtain a hot rolled steel band, - coiling said hot rolled steel band at a temperature between 500°C and 750°C, - said hot rolled steel band being annealed at a temperature between 650°C and 950°C for a time between 10s and 48 hours - cold rolling the hot rolled steel band to obtain a cold rolled steel sheet - heating the cold rolled steel sheet up to a soaking temperature between 850°C and 1150°C - holding the cold rolled steel at the soaking temperature for a time between 20s and 100s - cooling the cold rolled steel down to room.
A discovery method performed by a first mission critical push to talk, MCPTT, user equipment, UE, wherein the method comprises: sending a discovery message, wherein the discovery message comprises an application layer identifier information of a discovery target, and the discovery target is one or more target users of a first user that uses the first MCPTT UE; and receiving a response message from a second MCPTT UE, wherein the response message comprises a layer 2 identifier of the second MCPTT UE and an application layer identifier of a second user who is currently using the second MCPTT UE, wherein the second user is one of the one or more target users, wherein when a target user of the discovery target and the first user are in a first communications group, the sending a discovery message comprises: acquiring a group layer 2 address of the first communications group; and sending the discovery message to the group layer 2 address. sending a discovery message, wherein the discovery message comprises an application layer identifier information of a discovery target, and the discovery target is one or more target users of a first user that uses the first MCPTT UE; and receiving a response message from a second MCPTT UE, wherein the response message comprises a layer 2 identifier of the second MCPTT UE and an application layer identifier of a second user who is currently using the second MCPTT UE, wherein the second user is one of the one or more target users, wherein when a target user of the discovery target and the first user are in a first communications group, the sending a discovery message comprises: acquiring a group layer 2 address of the first communications group; and sending the discovery message to the group layer 2 address. acquiring a group layer 2 address of the first communications group; and sending the discovery message to the group layer 2 address.
A front-end monitoring device, comprising: a Bluetooth low energy, BLE, module , configured to establish a BLE link between the front-end monitoring device and a back-end monitoring device; a universal asynchronous receiver/transmitter , UART, configured to receive, by using the BLE link, a first body temperature value sent by the back-end monitoring device, wherein the first body temperature value is obtained by the back-end monitoring device by measuring body temperature of a monitored person; a thermistor sensor , configured to measure body temperature of a monitoring person to obtain a second body temperature value; and a processing module , configured to determine, according to a variation of the first body temperature value relative to the second body temperature value, whether first prompt information needs to be generated. a Bluetooth low energy, BLE, module , configured to establish a BLE link between the front-end monitoring device and a back-end monitoring device; a universal asynchronous receiver/transmitter , UART, configured to receive, by using the BLE link, a first body temperature value sent by the back-end monitoring device, wherein the first body temperature value is obtained by the back-end monitoring device by measuring body temperature of a monitored person; a thermistor sensor , configured to measure body temperature of a monitoring person to obtain a second body temperature value; and a processing module , configured to determine, according to a variation of the first body temperature value relative to the second body temperature value, whether first prompt information needs to be generated.
Laser sensor, comprising a laser source configured to emit a laser beam , optics configured to project the laser beam as a one- or two-dimensional patterned laser beam onto an object to be examined, such that a distance of the patterned laser beam from the laser source varies along the patterned laser beam projected on the object , a detector configured to determine a self-mixing interference signal generated by laser light of the patterned laser beam reflected from the object back into the laser source , and circuitry configured to spectrally analyze the self-mixing interference signal and extract from the spectrum of the self-mixing interference signal multiple frequencies indicative of at least one of the following: multiple distances along the patterned laser beam from the laser source , multiple velocities along the patterned laser beam with respect to the laser source . a laser source configured to emit a laser beam , optics configured to project the laser beam as a one- or two-dimensional patterned laser beam onto an object to be examined, such that a distance of the patterned laser beam from the laser source varies along the patterned laser beam projected on the object , a detector configured to determine a self-mixing interference signal generated by laser light of the patterned laser beam reflected from the object back into the laser source , and circuitry configured to spectrally analyze the self-mixing interference signal and extract from the spectrum of the self-mixing interference signal multiple frequencies indicative of at least one of the following: multiple distances along the patterned laser beam from the laser source , multiple velocities along the patterned laser beam with respect to the laser source .
A metal roofing material comprising: a front substrate made of a metal sheet, the front substrate comprising a body portion formed in a box shape; a back substrate disposed on a back side of the front substrate so as to cover an opening of the body portion ; a core material filled between the body portion and the back substrate , the metal roofing material being adapted to be arranged side by side on a roof base together with other metal roofing materials, said metal roofing material being characterised in that at least one edge indicator in the form of protrusion is provided at an edge portion of a top plate of the body portion ; and in that ; the top plate further comprises a plurality of protruding eave direction indicators arranged along the eave direction of the top plate ; and in that each of the eave direction indicators is formed by a plurality of protrusions, wherein said protrusions are spaced in the eave direction and the number of said protrusions is an odd number.