mhurhangee/patent-ind-claim-en huggingface dataset:
Process for producing hydrophobic silica granules, wherein i) a mixture containing hydrophilic silica is coated with hydrophobicizing agents at a temperature of not more than 55°C, ii) the mixture from step i is deaerated after a storage time of not more than 24 hours and iii) the mixture from step ii is densified to a target bulk density, iv) with granulation taking place during the densification in step iii. i) a mixture containing hydrophilic silica is coated with hydrophobicizing agents at a temperature of not more than 55°C, ii) the mixture from step i is deaerated after a storage time of not more than 24 hours and iii) the mixture from step ii is densified to a target bulk density, iv) with granulation taking place during the densification in step iii.
An adsorbent material comprising a silicate composition, wherein the silicate composition comprises 5% to 95% by weight of a crystalline phase; wherein the silicate composition comprises an interconnected porous scaffold having a total mercury (Hg) pore volume of 0.005 cc/g to 0.25 cc/g for pores having a diameter of 20-10,000 Å, a total mercury (Hg) pore volume of 0.10 cc/g to 0.25 cc/g for pores having a diameter of 200-10,000 Å, and a total nitrogen (N) pore volume of 0.02 cc/g to 0.10 cc/g for pores having a diameter of 20-600 Å; wherein the silicate composition comprises: 20% to 60% by weight of the crystalline phase comprising Y-zeolite; 5% to 95% by weight of a non-zeolitic matrix phase based on the total weight of the silicate composition; and wherein the silicate composition has a surface composition comprising 5% to 20% sodium calculated as atomic percent and a surface area of 200 m 2 /g to 500 m 2 /g; and wherein the composition further comprises additional adsorbent comprising titanosilicate. wherein the silicate composition comprises an interconnected porous scaffold having a total mercury (Hg) pore volume of 0.005 cc/g to 0.25 cc/g for pores having a diameter of 20-10,000 Å, a total mercury (Hg) pore volume of 0.10 cc/g to 0.25 cc/g for pores having a diameter of 200-10,000 Å, and a total nitrogen (N) pore volume of 0.02 cc/g to 0.10 cc/g for pores having a diameter of 20-600 Å; wherein the silicate composition comprises: 20% to 60% by weight of the crystalline phase comprising Y-zeolite; 5% to 95% by weight of a non-zeolitic matrix phase based on the total weight of the silicate composition; and wherein the silicate composition has a surface composition comprising 5% to 20% sodium calculated as atomic percent and a surface area of 200 m 2 /g to 500 m 2 /g; and wherein the composition further comprises additional adsorbent comprising titanosilicate. 20% to 60% by weight of the crystalline phase comprising Y-zeolite; 5% to 95% by weight of a non-zeolitic matrix phase based on the total weight of the silicate composition; and wherein the silicate composition has a surface composition comprising 5% to 20% sodium calculated as atomic percent and a surface area of 200 m 2 /g to 500 m 2 /g; and wherein the composition further comprises additional adsorbent comprising titanosilicate.
A transport refrigeration system comprising: a vehicle having a refrigerated cargo space ; a compressed gas tank configured to store gas; an engine configured to power the vehicle through combustion of the gas; a pressure reducing mechanism fluidly connecting the compressed gas tank and the engine , the pressure reducing mechanism configured to reduce the pressure of the gas from the compressed gas tank ; an evaporator thermally coupled to the pressure reducing mechanism and the refrigerated cargo space ; wherein the evaporator is configured to cool the refrigerated cargo space ; and wherein a temperature of the gas and a temperature of the evaporator are reduced as a result of the reduction in pressure of the gas by the pressure reducing mechanism; characterized in that the pressure reducing mechanism is composed of an ejector system , the ejector system comprising an ejector fluidly connected to the compressed gas tank and a flash tank fluidly connected to the evaporator and the engine . a vehicle having a refrigerated cargo space ; a compressed gas tank configured to store gas; an engine configured to power the vehicle through combustion of the gas; a pressure reducing mechanism fluidly connecting the compressed gas tank and the engine , the pressure reducing mechanism configured to reduce the pressure of the gas from the compressed gas tank ; an evaporator thermally coupled to the pressure reducing mechanism and the refrigerated cargo space ; wherein the evaporator is configured to cool the refrigerated cargo space ; and wherein a temperature of the gas and a temperature of the evaporator are reduced as a result of the reduction in pressure of the gas by the pressure reducing mechanism; characterized in that the pressure reducing mechanism is composed of an ejector system , the ejector system comprising an ejector fluidly connected to the compressed gas tank and a flash tank fluidly connected to the evaporator and the engine .
Aqueous ink for textile printing comprising a disperse dye, a first dispersant selected from the group consisting of an alkali salt of aromatic sulfonic acid, an alkali salt of aromatic sulfonic acid-formalin condensate, an alkali salt of β-naphthalenesulfonic acid, and an alkali salt of β - naphthalenesulfonic acid-formalin condensate and a second dispersant, the second dispersant is a copolymer of an acrylate and an alkylene oxide.
A computer-implemented method comprising: detecting , by a processor of a computing device , a triggering event in an application executing on the computing device , wherein the application is a web browsing application and wherein the triggering event comprises a command present in a web site; parsing the website to obtain key control information; determining , by the processor , a configuration of a user interface of the computing device associated with the application in response to the detected triggering event, the user interface including a keyboard or a touch input zone of a trackpad , of a touch pad or of a touchscreen operating as a virtual keyboard; and configuring electronic ink of an electronic ink layer associated with at least one key of the keyboard or at least one virtual key of the virtual keyboard in response to the detected triggering event and the determined configuration according to the key control information, the configuring comprising configuring an appearance of the at least one key or the at least one virtual key to correspond to an element of the website. detecting , by a processor of a computing device , a triggering event in an application executing on the computing device , wherein the application is a web browsing application and wherein the triggering event comprises a command present in a web site; parsing the website to obtain key control information; determining , by the processor , a configuration of a user interface of the computing device associated with the application in response to the detected triggering event, the user interface including a keyboard or a touch input zone of a trackpad , of a touch pad or of a touchscreen operating as a virtual keyboard; and configuring electronic ink of an electronic ink layer associated with at least one key of the keyboard or at least one virtual key of the virtual keyboard in response to the detected triggering event and the determined configuration according to the key control information, the configuring comprising configuring an appearance of the at least one key or the at least one virtual key to correspond to an element of the website.
A polycarbonate resin composition comprising at least a polycarbonate resin (a) having at least structural units (a) derived from formula : and a polycarbonate resin (b) having structural units different from the polycarbonate resin (a), which satisfies the following requirements: (i) the pencil hardness of the polycarbonate resin (a) as specified by ISO 15184 is higher than the pencil hardness of the polycarbonate resin (b) as specified by ISO 15184; (ii) the weight ratio of the polycarbonate resin (a) to the polycarbonate resin (b) is from 1:99 to 45:55; (iii) the pencil hardness of the polycarbonate resin composition as specified by ISO 15184 is higher by at least two ranks than the pencil hardness of the polycarbonate resin (b) as specified by ISO 15184; and (iv) the Charpy impact strength of the polycarbonate resin composition is higher than the Charpy impact strength of the polycarbonate resin (a) and is at least 8 kJ/m 2 as determined in accordance with JIS K7111 with a notch of 0.25 mmR, wherein the polycarbonate resin (b) is a polycarbonate resin having at least 50 wt% structural units (b) derived from a compound represented by the following formula : and wherein the polycarbonate resin (a) and the polycarbonate resin (b) have a viscosity average molecular weight within a range of from 1,000 to 100,000 as measured by a method of dissolving the polycarbonate resin in methylene chloride (concentration: 6.0 g/L), the specific viscosity (ηsp) at 20°C is measured by using an Ubbelohde viscosity tube, and the viscosity average molecular weight (Mv) is calculated in accordance with the following formula: η ⁢ sp / C = η 1 + 0.28 η sp η = 1.23 × 10 − 4 Mv 0.83 . (i) the pencil hardness of the polycarbonate resin (a) as specified by ISO 15184 is higher than the pencil hardness of the polycarbonate resin (b) as specified by ISO 15184; (ii) the weight ratio of the polycarbonate resin (a) to the polycarbonate resin (b) is from 1:99 to 45:55; (iii) the pencil hardness of the polycarbonate resin composition as specified by ISO 15184 is higher by at least two ranks than the pencil hardness of the polycarbonate resin (b) as specified by ISO 15184; and (iv) the Charpy impact strength of the polycarbonate resin composition is higher than the Charpy impact strength of the polycarbonate resin (a) and is at least 8 kJ/m 2 as determined in accordance with JIS K7111 with a notch of 0.25 mmR, wherein the polycarbonate resin (b) is a polycarbonate resin having at least 50 wt% structural units (b) derived from a compound represented by the following formula : and wherein the polycarbonate resin (a) and the polycarbonate resin (b) have a viscosity average molecular weight within a range of from 1,000 to 100,000 as measured by a method of dissolving the polycarbonate resin in methylene chloride (concentration: 6.0 g/L), the specific viscosity (ηsp) at 20°C is measured by using an Ubbelohde viscosity tube, and the viscosity average molecular weight (Mv) is calculated in accordance with the following formula: η ⁢ sp / C = η 1 + 0.28 η sp η = 1.23 × 10 − 4 Mv 0.83 .
Multi-engine aircraft having a hybrid propulsion system , comprising • at least a first and a second hybrid-electric propulsion unit , each comprising an internal combustion engine , a motor-generator unit for transmitting propulsive power to a propulsor , • wherein the propulsor is connectable to the internal combustion engine and/or the motor-generator unit for the transmission of drive power, • the first and second motor-generator units are connected to a transmission device for distributing electrical power, • a fuel cell for supplying the first and/or second motor-generator unit with electrical energy, • a controller which is connected to the internal combustion engines and/or the transmission device and/or motor-generator units and/or the fuel cell to control the thermally and electrically generated drive power, • separate fuel tanks for supplying the internal combustion engines with fuel and the fuel cell with cryogenic hydrogen, • an airfoil accommodating the drive units and a fuel tank , a fuselage , • wherein the drive unit is formed by a turboprop engine having one respective gas turbine that can be coupled to a speed-reducing gearbox to drive a propeller , and • the motor-generator unit can be coupled to the gearbox under the control of the controller depending on the operating mode, characterized in that at least the predominant volume of the fuel tanks for supplying the internal combustion engines is integrated in the airfoil and at least the predominant volume of the fuel tanks for supplying the fuel cell is integrated in a tail region of the fuselage . • at least a first and a second hybrid-electric propulsion unit , each comprising an internal combustion engine , a motor-generator unit for transmitting propulsive power to a propulsor , • wherein the propulsor is connectable to the internal combustion engine and/or the motor-generator unit for the transmission of drive power, • the first and second motor-generator units are connected to a transmission device for distributing electrical power, • a fuel cell for supplying the first and/or second motor-generator unit with electrical energy, • a controller which is connected to the internal combustion engines and/or the transmission device and/or motor-generator units and/or the fuel cell to control the thermally and electrically generated drive power, • separate fuel tanks for supplying the internal combustion engines with fuel and the fuel cell with cryogenic hydrogen, • an airfoil accommodating the drive units and a fuel tank , a fuselage , • wherein the drive unit is formed by a turboprop engine having one respective gas turbine that can be coupled to a speed-reducing gearbox to drive a propeller , and • the motor-generator unit can be coupled to the gearbox under the control of the controller depending on the operating mode,
A method for determining a failure of a flow divider within a gas turbine engine fuel system , including a controller , fuel manifold and fuel pressure sensor , the method being performed by the controller and comprising the steps of: delivering a fuel command to cause a fuel pump to deliver fuel to the fuel manifold , a flow divider valve coupled to the fuel manifold and configured to limit fuel delivery to a combustor ; measuring an actual fuel pressure value with the fuel pressure sensor ; ascertaining an actual fill time of the fuel manifold based on at least one of the step of delivering the fuel command and the step of measuring the actual fuel pressure; calculating an expected fill time, wherein the expected fill time is indicative of the time required to fill a known fuel manifold volume; determining whether the expected fill time is greater than or equal to the actual fill time; when the expected fill time is less than the actual fill time, sending a first signal with the controller to annunciate a first condition indicative of a potential failure of the flow divider valve ; when the expected fill time is greater than or equal to the actual fill time, determining whether the actual fuel pressure value is less than or equal to an expected fuel pressure value based at least in part on at least one environmental signal; and when the actual fuel pressure value is less than the expected fuel pressure value, sending a second signal with the controller to annunciate a second condition, wherein the second condition is indicative of a potential failure of the flow divider valve . delivering a fuel command to cause a fuel pump to deliver fuel to the fuel manifold , a flow divider valve coupled to the fuel manifold and configured to limit fuel delivery to a combustor ; measuring an actual fuel pressure value with the fuel pressure sensor ; ascertaining an actual fill time of the fuel manifold based on at least one of the step of delivering the fuel command and the step of measuring the actual fuel pressure; calculating an expected fill time, wherein the expected fill time is indicative of the time required to fill a known fuel manifold volume; determining whether the expected fill time is greater than or equal to the actual fill time; when the expected fill time is less than the actual fill time, sending a first signal with the controller to annunciate a first condition indicative of a potential failure of the flow divider valve ; when the expected fill time is greater than or equal to the actual fill time, determining whether the actual fuel pressure value is less than or equal to an expected fuel pressure value based at least in part on at least one environmental signal; and when the actual fuel pressure value is less than the expected fuel pressure value, sending a second signal with the controller to annunciate a second condition, wherein the second condition is indicative of a potential failure of the flow divider valve .
A wire control device having high structural strength, which can be disposed on a handlebar of a bicycle, the wire control device comprising: a main body comprising a bearing fixing seat , the bearing fixing seat having an annular inner wall ; a bearing disposed in the bearing fixing seat and comprising an inner race and an outer race , the outer race of the bearing being in contact with the annular inner wall of the bearing fixing seat ; a handle assembly rotatably disposed on the main body , the handle assembly comprising a shift lever and a pivot screw , the shift lever having a protrusion, the protrusion having a threaded hole (H1) and an annular abutted surface , the inner race of the bearing being sleeved onto and in contact with the annular abutted surface of the protrusion, the pivot screw comprising a head portion and a threaded rod , the head portion being located on a side of the bearing opposite to the shift lever , the threaded rod being screwed into the threaded hole (H1) of the shift lever . a main body comprising a bearing fixing seat , the bearing fixing seat having an annular inner wall ; a bearing disposed in the bearing fixing seat and comprising an inner race and an outer race , the outer race of the bearing being in contact with the annular inner wall of the bearing fixing seat ; a handle assembly rotatably disposed on the main body , the handle assembly comprising a shift lever and a pivot screw , the shift lever having a protrusion, the protrusion having a threaded hole (H1) and an annular abutted surface , the inner race of the bearing being sleeved onto and in contact with the annular abutted surface of the protrusion, the pivot screw comprising a head portion and a threaded rod , the head portion being located on a side of the bearing opposite to the shift lever , the threaded rod being screwed into the threaded hole (H1) of the shift lever .
Method for providing a digital sensor signal (DS) from an ultrasonic sensor for signal transmission to a signal receiver , in which a - preferably digital - output signal (OS) from the ultrasonic sensor is processed to form the digital sensor signal for signal transmission, characterized in that the processing comprises the following steps: - determining a signal change (SC) of successive values of the output signal (OS), - scaling this signal change (SC) by means of a variable scaling factor (SF) which is specified by a scaling scheme known to the ultrasonic sensor and the signal receiver , and - outputting the scaled signal change (SC) as the digital sensor signal (DS). - output signal (OS) from the ultrasonic sensor is processed to form the digital sensor signal for signal transmission, - determining a signal change (SC) of successive values of the output signal (OS), - scaling this signal change (SC) by means of a variable scaling factor (SF) which is specified by a scaling scheme known to the ultrasonic sensor and the signal receiver , and - outputting the scaled signal change (SC) as the digital sensor signal (DS).
A refrigerator comprising: a body which is suitable for placing the foodstuffs therein; a door which provides access into the body ; a water dispenser having a receptacle , which is provided on the door and wherein water is stored; a channel which is provided on the lower side of the receptacle and which allows the water to exit the receptacle ; a spigot which provides the flow of water from the channel ; a trigger lever which triggers the movement of the spigot ; a locking mechanism having a shaft ; a lock body extending from the shaft ; a locking tab attached to at least one end of the shaft ; a lid having at least one side wall extending towards behind the trigger lever ; a first housing which is provided on the side wall so as to remain behind the trigger lever wherein the shaft is fitted, wherein the locking tab moves the lock body between the shaft and the trigger lever between a lock position, where the lock body almost bears against the trigger lever and a free position, where the lock body does not bear against the trigger lever ; a guide path which is provided on the side wall and which facilitates the movement of the locking tab between the locked position and the free position, characterized by the locking tab having a protrusion arranged on the guide path and a recess fitted over the protrusion to enable the locking tab to be fixed when the trigger lever is in the free or locked position. a channel which is provided on the lower side of the receptacle and which allows the water to exit the receptacle ; a spigot which provides the flow of water from the channel ; a trigger lever which triggers the movement of the spigot ; a locking mechanism having a shaft ; a lock body extending from the shaft ; a locking tab attached to at least one end of the shaft ; a lid having at least one side wall extending towards behind the trigger lever ; a first housing which is provided on the side wall so as to remain behind the trigger lever wherein the shaft is fitted, wherein the locking tab moves the lock body between the shaft and the trigger lever between a lock position, where the lock body almost bears against the trigger lever and a free position, where the lock body does not bear against the trigger lever ; a guide path which is provided on the side wall and which facilitates the movement of the locking tab between the locked position and the free position, characterized by the locking tab having a protrusion arranged on the guide path and a recess fitted over the protrusion to enable the locking tab to be fixed when the trigger lever is in the free or locked position.
A compound of formula (I): or a pharmaceutically acceptable salt or a stereoisomer thereof; wherein, ring Het is heterocyclyl; each Y 1 , Y 2 and Y 3 are independently CR a or N, wherein 0-2 of Y 1 , Y 2 and Y 3 are N; each Z 1 , Z 2 , Z 3 , Z 4 and Z 5 are independently CR a or N, wherein 0-3 of Z 1 , Z 2 , Z 3 , Z 4 and Z 5 are N; L is *-NR b -C(O)-(CR b R c ) n - or *-C(O)-NR b -(CR b R c ) n -; wherein the group marked with * is connected to the ring containing Y 1 , Y 2 and Y 3 ; each R 1 , R 2 , R 6 and R 7 are independently hydrogen, halo or alkyl; R 3 at each occurrence is independently hydroxy, halo, alkyl, alkoxy, haloalkyl or cycloalkyl; alternatively, two R 3 on the same carbon atom together form an oxo (=O) group; R 4 is hydrogen, alkyl or alkoxy; R 5 is alkyl, -(CH 2 ) n NR b R c or hydroxyalkyl; R a is hydrogen, alkyl, alkoxy, halo, cycloalkyl or aryl; R b and R c are each independently hydrogen or alkyl; alternatively, R b and R c on the same atom together form a ring; m is 0 to 3; and n is 1. ring Het is heterocyclyl; each Y 1 , Y 2 and Y 3 are independently CR a or N, wherein 0-2 of Y 1 , Y 2 and Y 3 are N; each Z 1 , Z 2 , Z 3 , Z 4 and Z 5 are independently CR a or N, wherein 0-3 of Z 1 , Z 2 , Z 3 , Z 4 and Z 5 are N; L is *-NR b -C(O)-(CR b R c ) n - or *-C(O)-NR b -(CR b R c ) n -; wherein the group marked with * is connected to the ring containing Y 1 , Y 2 and Y 3 ; each R 1 , R 2 , R 6 and R 7 are independently hydrogen, halo or alkyl; R 3 at each occurrence is independently hydroxy, halo, alkyl, alkoxy, haloalkyl or cycloalkyl; alternatively, two R 3 on the same carbon atom together form an oxo (=O) group; R 4 is hydrogen, alkyl or alkoxy; R 5 is alkyl, -(CH 2 ) n NR b R c or hydroxyalkyl; R a is hydrogen, alkyl, alkoxy, halo, cycloalkyl or aryl; R b and R c are each independently hydrogen or alkyl; alternatively, R b and R c on the same atom together form a ring; m is 0 to 3; and n is 1.