mhurhangee/patent-ind-claim-en huggingface dataset:
A method for pairing a stylus with a touch enabled computing device, comprising: detecting presence of the stylus in proximity of the touch enabled computing device ; negotiating electrostatic communication capabilities between the stylus and a digitizer system integrated in the touch enabled computing device , wherein negotiation is capability identification; configuring at least one of the stylus and the digitizer system to match a defined communication capability of the other of the at least one of the stylus and digitizer system ; storing the defined communication configuration in association with an identification code, wherein the configuration is stored locally in the stylus or in the touch enabled computing device or remotely in a network memory or a cloud memory; tracking input from the stylus via an electrostatic communication channel between the stylus and the digitizer system based on the defined communication configuration; and characterized by once the electrostatic communication channel is broken, reinstating pairing based on the stylus transmitting and the touch enabled computing device confirming the identification code previously defined, alternatively, reinstating pairing based on the touch enabled computing device transmitting and the stylus confirming the identification code previously defined, wherein reinstating pairing is only initiated after a pre-defined time period that electrostatic communication is broken. detecting presence of the stylus in proximity of the touch enabled computing device ; negotiating electrostatic communication capabilities between the stylus and a digitizer system integrated in the touch enabled computing device , wherein negotiation is capability identification; configuring at least one of the stylus and the digitizer system to match a defined communication capability of the other of the at least one of the stylus and digitizer system ; storing the defined communication configuration in association with an identification code, wherein the configuration is stored locally in the stylus or in the touch enabled computing device or remotely in a network memory or a cloud memory; tracking input from the stylus via an electrostatic communication channel between the stylus and the digitizer system based on the defined communication configuration; and characterized by once the electrostatic communication channel is broken, reinstating pairing based on the stylus transmitting and the touch enabled computing device confirming the identification code previously defined, alternatively, reinstating pairing based on the touch enabled computing device transmitting and the stylus confirming the identification code previously defined, wherein reinstating pairing is only initiated after a pre-defined time period that electrostatic communication is broken.
Method for heat treating a steel component comprising the steps of: a) carbonitriding the steel component at a temperature of 930-970°C for 5-10 hours, b) cooling the steel component , c) re-heating the steel component to a temperature of 780-820°C and d) quenching the steel component , characterized in that the method comprises the step of f) holding the steel component at an initial temperature (T 1 ) above the initial martensite formation temperature (Ms), and lowering the initial temperature (T 1 ) to a temperature (T 2 ) that is below the initial martensite formation temperature (Ms) but above the actual martensite formation temperature during the bainite transformation and in that step f) comprises subsequently raising the temperature from (T 2 ) to a temperature (T 3 ) that is above the initial martensite formation temperature (Ms) during the bainite transformation, wherein 50-90% of the austenite is transformed to bainite before increasing the temperature to (T 3 ) to speed up the transformation of the remaining austenite to bainite, and wherein the steel component comprises steel with a carbon content of 0.6 to 1.20 weight %. a) carbonitriding the steel component at a temperature of 930-970°C for 5-10 hours, b) cooling the steel component , c) re-heating the steel component to a temperature of 780-820°C and d) quenching the steel component ,
A double rotating flipper locking mechanism for maintaining tension on a halyard, the double rotating flipper locking mechanism comprising: a housing having an internal space and configured to receive a slug that moves along a path through the housing , the slug being configured to be operably connected to the halyard, the housing including a first housing side and a second housing side coupled to one another; and first and second flippers rotatably disposed in the housing , the first and second flippers configured to rotate between at least a cocked position in which the slug is inserted into the housing , a locked position in which a surface of the first and second flippers receive the slug and impede the slug from exiting the housing along the path, wherein the halyard is tensioned in the locked position, and a neutral position in which the first and second flippers allow movement of the slug , characterized by a magnet assembly configured to effect rotation of the first and second flippers , the magnet assembly including at least: first and second housing magnets disposed within the first housing side , third and fourth housing magnets disposed within the second housing side , first and second flipper magnets disposed within the first flipper , and third and fourth flipper magnets disposed within the second flipper . a housing having an internal space and configured to receive a slug that moves along a path through the housing , the slug being configured to be operably connected to the halyard, the housing including a first housing side and a second housing side coupled to one another; and first and second flippers rotatably disposed in the housing , the first and second flippers configured to rotate between at least a cocked position in which the slug is inserted into the housing , a locked position in which a surface of the first and second flippers receive the slug and impede the slug from exiting the housing along the path, wherein the halyard is tensioned in the locked position, and a neutral position in which the first and second flippers allow movement of the slug , characterized by a magnet assembly configured to effect rotation of the first and second flippers , the magnet assembly including at least: first and second housing magnets disposed within the first housing side , third and fourth housing magnets disposed within the second housing side , first and second flipper magnets disposed within the first flipper , and third and fourth flipper magnets disposed within the second flipper .
Assembly comprising a portable human-machine interface device and a controller of at least one surgical or dental instrument , the human-machine interface device being removably connected to the controller which is installed in a power and control unit or in a table top equipment , the interface device including the hardware and software means allowing a user to enter an instruction or data into the interface device to control, via the controller , the operation of the surgical or dental instrument , the interface device comprising all the programmes necessary for using the surgical or dental instrument connected to the power and control unit or to the table top equipment in addition to the communication protocol between the interface device and the controller , the interface device and the controller form a master/slave assembly in which the interface device is the master and the controller is the slave.
A fan blade platform , comprising: an outer wall ; a first sidewall (110; 152) extending from the outer wall to a circular member ; a second sidewall (112; 154) extending from the outer wall to the circular member ; a stiffening member extending from the circular member to the outer wall , the stiffening member formed integrally with the first sidewall (110; 152), the second sidewall (112; 154), and the outer wall ; a mounting structure (134; 170) connected to, extending between and formed integrally with the first sidewall (110; 152) and the second sidewall (112; 154), wherein the circular member defines a cylindrical opening in the mounting structure (134;170) and the first sidewall (110; 152), the second sidewall (112; 154), the circular member , and the stiffening member are formed integrally; characterised in that the stiffening member comprises arms defining an opening such that the mounting structure (134; 170) is configured to mount around a tab of a hub and receive a pin extending through the mounting structure (134; 170) in the circular member . an outer wall ; a first sidewall (110; 152) extending from the outer wall to a circular member ; a second sidewall (112; 154) extending from the outer wall to the circular member ; a stiffening member extending from the circular member to the outer wall , the stiffening member formed integrally with the first sidewall (110; 152), the second sidewall (112; 154), and the outer wall ; a mounting structure (134; 170) connected to, extending between and formed integrally with the first sidewall (110; 152) and the second sidewall (112; 154), wherein the circular member defines a cylindrical opening in the mounting structure (134;170) and the first sidewall (110; 152), the second sidewall (112; 154), the circular member , and the stiffening member are formed integrally; characterised in that the stiffening member comprises arms defining an opening such that the mounting structure (134; 170) is configured to mount around a tab of a hub and receive a pin extending through the mounting structure (134; 170) in the circular member .
A heat-resistant composition comprising: a binder resin comprising at least two of: a silicone-modified polyester resin, a siloxane compound, or a silanol compound; a pigment and a catalyst, wherein the pigment consists of a mixture of one of iron cobalt chromite black spinel, copper chromite black spinel or iron chromite manganese, and the carbon black in a weight ratio of 1:1 to 9:1, or wherein the pigment includes a mixture of the iron cobalt chromite black spinel and the iron chromite manganese in a weight ratio of 1:1 to 9:1. a binder resin comprising at least two of: a silicone-modified polyester resin, a siloxane compound, or a silanol compound; a pigment and a catalyst, wherein the pigment consists of a mixture of one of iron cobalt chromite black spinel, copper chromite black spinel or iron chromite manganese, and the carbon black in a weight ratio of 1:1 to 9:1, or wherein the pigment includes a mixture of the iron cobalt chromite black spinel and the iron chromite manganese in a weight ratio of 1:1 to 9:1.
An exhaust gas purification catalyst which is configured to be arranged in an exhaust pipe of an internal combustion engine and configured to purify an exhaust gas exhausted from the internal combustion engine, comprising: a base material ; and a catalyst layer formed on the base material , the catalyst layer having an alkaline-earth metal carrying region including, a porous carrier constituted of an inorganic compound and comprising secondary porous carrier particles, Pt carried on the porous carrier, and a sulfuric acid salt of at least one alkaline-earth metal carried on the porous carrier, wherein a value of R Ae/Pt is 0.5 or more, where R Ae/Pt represents a Pearson's correlation coefficient, the Pearson's correlation coefficient being determined by performing an area analysis of a cross section of the alkaline-earth metal carrying region of the catalyst layer by FE-EPMA under a condition of pixel size 0.34 μm × 0.34 μm; and number of measured pixels 256 × 256; and measuring an intensity (α: cps) of a characteristic X ray of an element (Ae) of the alkaline-earth metal and an intensity (β: cps) of a characteristic X ray of Pt for each pixel, to measure the Pearson's correlation coefficient using α and β in each pixel, the alkaline-earth metal sulfuric acid salt is carried on the outer surface and in the inside of the secondary porous carrier particles in a highly dispersed state, and the exhaust gas purification catalyst further comprises a catalyst layer including Rh as a catalyst metal on the downstream side in the direction in which the exhaust gas in the catalyst layer flows. a base material ; and a catalyst layer formed on the base material , the catalyst layer having an alkaline-earth metal carrying region including, a porous carrier constituted of an inorganic compound and comprising secondary porous carrier particles, Pt carried on the porous carrier, and a sulfuric acid salt of at least one alkaline-earth metal carried on the porous carrier, wherein a value of R Ae/Pt is 0.5 or more, where R Ae/Pt represents a Pearson's correlation coefficient, the Pearson's correlation coefficient being determined by performing an area analysis of a cross section of the alkaline-earth metal carrying region of the catalyst layer by FE-EPMA under a condition of pixel size 0.34 μm × 0.34 μm; and number of measured pixels 256 × 256; and measuring an intensity (α: cps) of a characteristic X ray of an element (Ae) of the alkaline-earth metal and an intensity (β: cps) of a characteristic X ray of Pt for each pixel, to measure the Pearson's correlation coefficient using α and β in each pixel, the alkaline-earth metal sulfuric acid salt is carried on the outer surface and in the inside of the secondary porous carrier particles in a highly dispersed state, and the exhaust gas purification catalyst further comprises a catalyst layer including Rh as a catalyst metal on the downstream side in the direction in which the exhaust gas in the catalyst layer flows.
A drone, comprising a main circuit board on which are mounted electronic components as well as an inertial unit, IMU, comprising gyrometric sensors for measuring instantaneous rotations of the drone in an absolute reference frame, and/or accelerometric sensors for measuring accelerations of the drone in said reference frame, the IMU including an internal temperature sensor issuing a chip temperature signal (θ° puce ), characterized in that it comprises: - a heating component mounted on the circuit board near the IMU ; - a thermal guide incorporated to the circuit board , said thermal guide extending between the heating component and the IMU so as to allow a transfer to the IMU of the heat produced by the heating component; and - a thermal regulation circuit (44-62), receiving as an input the chip temperature signal (θ° puce ) and a predetermined set-point temperature signal (θ° ref ), and outputting a heating component piloting signal (TH_PWM), so as to control the heat supply to the IMU according to the difference between chip temperature and set-point temperature. - a heating component mounted on the circuit board near the IMU ; - a thermal guide incorporated to the circuit board , said thermal guide extending between the heating component and the IMU so as to allow a transfer to the IMU of the heat produced by the heating component; and - a thermal regulation circuit (44-62), receiving as an input the chip temperature signal (θ° puce ) and a predetermined set-point temperature signal (θ° ref ), and outputting a heating component piloting signal (TH_PWM), so as to control the heat supply to the IMU according to the difference between chip temperature and set-point temperature.
A bottle assembly in combination with a dispenser having a housing to which the bottle assembly is removably coupled to dispense fluid from a bottle , the bottle assembly comprising: the bottle having an outlet opening , a bottle cap member secured to the bottle about the outlet opening , a vent port through the bottle cap member having an inner end open into the bottle and an outer end open to the atmosphere, characterized in that a frangible plug member is received in the vent port , the frangible plug member preventing flow through the vent port when the frangible plug member is intact and not broken, a vent tab on an exterior of the bottle cap member , the vent tab coupled to the frangible plug member , the vent tab extending from the frangible plug member accessible on the exterior of the bottle cap member for engagement to apply forces to the vent tab that become translated to the frangible plug member breaking the frangible plug member , the frangible plug member when broken permitting flow through the vent port , the bottle assembly movable relative the housing to couple the bottle assembly to the housing in a dispensing position for dispensing of the fluid from the bottle assembly , during movement of the bottle assembly relative the housing toward the dispensing position engagement between an engagement surface provided on the vent tab and a cam surface on the housing applies forces to the vent tab that moves the vent tab to break the frangible plug member . the bottle having an outlet opening , a bottle cap member secured to the bottle about the outlet opening , a vent port through the bottle cap member having an inner end open into the bottle and an outer end open to the atmosphere, characterized in that a frangible plug member is received in the vent port , the frangible plug member preventing flow through the vent port when the frangible plug member is intact and not broken, a vent tab on an exterior of the bottle cap member , the vent tab coupled to the frangible plug member , the vent tab extending from the frangible plug member accessible on the exterior of the bottle cap member for engagement to apply forces to the vent tab that become translated to the frangible plug member breaking the frangible plug member , the frangible plug member when broken permitting flow through the vent port , the bottle assembly movable relative the housing to couple the bottle assembly to the housing in a dispensing position for dispensing of the fluid from the bottle assembly , during movement of the bottle assembly relative the housing toward the dispensing position engagement between an engagement surface provided on the vent tab and a cam surface on the housing applies forces to the vent tab that moves the vent tab to break the frangible plug member .
A method of performing an optimal safe landing area determination for an aircraft , the method comprising: accessing a probabilistic safe landing area map comprising a plurality of probabilistic indicators of safe landing areas for the aircraft; generating, by a processing subsystem comprising one or more processing resources , a list of candidate safe landing areas based on the probabilistic safe landing area map and one or more constraints; providing at least two of the candidate safe landing areas to a path planner ; ranking the list of candidate safe landing areas based on results from the path planner indicating an estimated cost to reach each of the candidate safe landing areas; and based on the ranking, outputting an indicator of an optimal safe landing area as a desired landing location for the aircraft , characterized in that the candidate safe landing areas are provided to the path planner as a single multi-goal query, such that a single path-tree is generated once for all of the candidate safe landing areas. accessing a probabilistic safe landing area map comprising a plurality of probabilistic indicators of safe landing areas for the aircraft; generating, by a processing subsystem comprising one or more processing resources , a list of candidate safe landing areas based on the probabilistic safe landing area map and one or more constraints; providing at least two of the candidate safe landing areas to a path planner ; ranking the list of candidate safe landing areas based on results from the path planner indicating an estimated cost to reach each of the candidate safe landing areas; and based on the ranking, outputting an indicator of an optimal safe landing area as a desired landing location for the aircraft , characterized in that the candidate safe landing areas are provided to the path planner as a single multi-goal query, such that a single path-tree is generated once for all of the candidate safe landing areas.
Deployable structure comprising: • a support , • a tape spring fixed to the support , able to switch from a wound configuration about an axis Z, to a deployed configuration, the tape spring having two ends , characterized in that it further comprises an arm rotatably mounted with respect to the support about the Z-axis, able to form a first contact with the tape spring so as to control the deployment of the tape spring , in that the tape spring is fixed between its two ends to a fixing point on the support , in that the arm is able to form a second contact with the tape spring so as to control the deployment of the tape spring , in that a first end is able to deploy with respect to the fixing point along a first axis perpendicular to the Z axis in a first direction, and in that a second end is able to unfold along a second axis perpendicular to the Z axis in a second direction different from the first direction, and in that both ends are able to deploy simultaneously. • a support , • a tape spring fixed to the support , able to switch from a wound configuration about an axis Z, to a deployed configuration, the tape spring having two ends , characterized in that it further comprises an arm rotatably mounted with respect to the support about the Z-axis, able to form a first contact with the tape spring so as to control the deployment of the tape spring , in that the tape spring is fixed between its two ends to a fixing point on the support , in that the arm is able to form a second contact with the tape spring so as to control the deployment of the tape spring , in that a first end is able to deploy with respect to the fixing point along a first axis perpendicular to the Z axis in a first direction, and in that a second end is able to unfold along a second axis perpendicular to the Z axis in a second direction different from the first direction, and in that both ends are able to deploy simultaneously.
Apparatus for determining the position of an object in three-dimensional space by means of an antenna structure , wherein the antenna structure has an L-, U- or T-shaped structure and can be mounted in the region of the front radiator of a vehicle with radiator grille, wherein the antenna structure is a radar sensor and a housing and an antenna arrangement of the radar sensor are formed in such a way that they can be integrated into the structure of the radiator grille, wherein the antenna structure is provided behind the air-impermeable region of the radiator grille and a combined frequency and phase modulation of the transmission signals and simultaneous operation of all transmitters is enabled.
A method of providing multi-link operation channel access in a multi-link network, the method comprising: initiating a first backoff countdown and a second backoff countdown associated with a first link and a second link of the multi-link network, respectively ; in response to the first backoff countdown reaching zero , determining whether the second backoff countdown is less than or equal to an aggregation threshold ; and in response to determining that the second backoff countdown is less than or equal to the aggregation threshold, transmitting a first frame and a second frame on the first and second links . initiating a first backoff countdown and a second backoff countdown associated with a first link and a second link of the multi-link network, respectively ; in response to the first backoff countdown reaching zero , determining whether the second backoff countdown is less than or equal to an aggregation threshold ; and in response to determining that the second backoff countdown is less than or equal to the aggregation threshold, determining whether the second backoff countdown is less than or equal to an aggregation threshold ; and in response to determining that the second backoff countdown is less than or equal to the aggregation threshold,