mhurhangee/patent-ind-claim-en huggingface dataset:
A reactor for producing a sulfur-infused carbonaceous material as a cathode material for use in a Li-S battery, comprising: a reactor body configured to withstand a pressure from 101.3 kPa (1 atm) to 15200 kPa (150 atm); and an inner sulfur-resistant layer at the inner surface of the reactor body, wherein the inner layer is inert to sulfur vapor at a temperature from 450 °C to 1000 °C wherein either: (i) the reactor body and the inner layer are made of the same material, wherein the material is selected from the group consisting of titanium, molybdenum, tungsten and a combination thereof; or (ii) the reactor body and the inner layer are made of different materials, wherein the reactor body is made of a material selected from the groups consisting of titanium, molybdenum, tungsten, and a combination thereof and wherein the inner layer is made of a material selected from the group consisting of titanium, molybdenum, tungsten, alumina, silicon carbide, SiO 2 , and a combination thereof. a reactor body configured to withstand a pressure from 101.3 kPa (1 atm) to 15200 kPa (150 atm); and an inner sulfur-resistant layer at the inner surface of the reactor body, wherein the inner layer is inert to sulfur vapor at a temperature from 450 °C to 1000 °C wherein either: (i) the reactor body and the inner layer are made of the same material, wherein the material is selected from the group consisting of titanium, molybdenum, tungsten and a combination thereof; or (ii) the reactor body and the inner layer are made of different materials, wherein the reactor body is made of a material selected from the groups consisting of titanium, molybdenum, tungsten, and a combination thereof and wherein the inner layer is made of a material selected from the group consisting of titanium, molybdenum, tungsten, alumina, silicon carbide, SiO 2 , and a combination thereof. (i) the reactor body and the inner layer are made of the same material, wherein the material is selected from the group consisting of titanium, molybdenum, tungsten and a combination thereof; or (ii) the reactor body and the inner layer are made of different materials, wherein the reactor body is made of a material selected from the groups consisting of titanium, molybdenum, tungsten, and a combination thereof and wherein the inner layer is made of a material selected from the group consisting of titanium, molybdenum, tungsten, alumina, silicon carbide, SiO 2 , and a combination thereof.
A ducting system (20;60;80) comprising: a first upstream location in a duct to be connected to a first source of air ; a downstream location in said duct to be connected to a second source of air ; said upstream location having a first valve , and said downstream location having a second valve ; an end location of said duct to be connected to a sink of air ; characterized in that the ducting system further comprises: a control configured for controlling said first and second valve to achieve a desired pressure and temperature of air at said end location; and a first temperature sensor located at a position intermediate said upstream location and said downstream location, and a second temperature sensor located at a position intermediate said downstream location and said end location, and said control being programmed to determine the health of said first and second valves based upon a comparison of a difference between temperatures sensed by said first and second sensors and a predicted temperature difference, said predicted temperature difference being based upon an intended position of said first valve and said second valve . a first upstream location in a duct to be connected to a first source of air ; a downstream location in said duct to be connected to a second source of air ; said upstream location having a first valve , and said downstream location having a second valve ; an end location of said duct to be connected to a sink of air ; characterized in that the ducting system further comprises: a control configured for controlling said first and second valve to achieve a desired pressure and temperature of air at said end location; and a first temperature sensor located at a position intermediate said upstream location and said downstream location, and a second temperature sensor located at a position intermediate said downstream location and said end location, and said control being programmed to determine the health of said first and second valves based upon a comparison of a difference between temperatures sensed by said first and second sensors and a predicted temperature difference, said predicted temperature difference being based upon an intended position of said first valve and said second valve . a control configured for controlling said first and second valve to achieve a desired pressure and temperature of air at said end location; and a first temperature sensor located at a position intermediate said upstream location and said downstream location, and a second temperature sensor located at a position intermediate said downstream location and said end location, and said control being programmed to determine the health of said first and second valves based upon a comparison of a difference between temperatures sensed by said first and second sensors and a predicted temperature difference, said predicted temperature difference being based upon an intended position of said first valve and said second valve .
A method for manufacturing a sound absorbing panel for an interior of an aircraft, comprising: determining a desired set of sound absorption properties by measuring sound to be absorbed in a particular location of an aircraft, wherein the desired set of sound absorption properties are determined based on the measurement(s) and include a sound absorption coefficient of a material as a function of sound frequency and three-dimensional position; determining a desired sound absorbing geometry based on the sound absorption properties; constructing a three-dimensional computer-aided design model of the sound absorbing geometry shaped to fit the particular location; and additively manufacturing a three-dimensional sound absorbing panel based on the three-dimensional computer-aided design model, characterised in that: the sound absorbing geometry includes an array of pyramids. determining a desired set of sound absorption properties by measuring sound to be absorbed in a particular location of an aircraft, wherein the desired set of sound absorption properties are determined based on the measurement(s) and include a sound absorption coefficient of a material as a function of sound frequency and three-dimensional position; determining a desired sound absorbing geometry based on the sound absorption properties; constructing a three-dimensional computer-aided design model of the sound absorbing geometry shaped to fit the particular location; and additively manufacturing a three-dimensional sound absorbing panel based on the three-dimensional computer-aided design model, determining a desired sound absorbing geometry based on the sound absorption properties; constructing a three-dimensional computer-aided design model of the sound absorbing geometry shaped to fit the particular location; and additively manufacturing a three-dimensional sound absorbing panel based on the three-dimensional computer-aided design model, characterised in that: the sound absorbing geometry includes an array of pyramids.
Annular gap scrubber with a longitudinal axis, - having a flow channel defined at least by a confusor, a diffusor and an annular gap body, wherein the annular gap body with at least the diffusor, and optionally also with the confusor, forms an annular gap of the flow channel, and - having nozzles for injecting scrubbing liquid into the flow channel, wherein at least several, particularly preferably all of these nozzles open into the annular gap and the nozzles opening into the annular gap for injecting scrubbing liquid are arranged in at least two, preferably in four, successive planes viewed from the confusor toward the diffusor along the longitudinal axis of the annular gap scrubber, characterised in that the nozzles of planes lying in succession in the direction of the longitudinal axis of the flow channel are arranged offset with respect to one another on the perimeter of the annular gap. - having a flow channel defined at least by a confusor, a diffusor and an annular gap body, wherein the annular gap body with at least the diffusor, and optionally also with the confusor, forms an annular gap of the flow channel, and - having nozzles for injecting scrubbing liquid into the flow channel,
A high strength steel plate for a sour-resistant line pipe, comprising: a chemical composition containing, by mass%, C: 0.02 % to 0.08 %, Si: 0.01 % to 0.50 %, Mn: 0.50 % to 1.80 %, P: 0.001 % to 0.015 %, S: 0.0002 % to 0.0015 %, Al: 0.01 % to 0.08 %, and Ca: 0.0005 % to 0.005 %, optionally, by mass%, at least one selected from the group consisting of Cu: 0.50 % or less, Ni: 0.50 % or less, Cr: 0.50 % or less, Mo: 0.50 % or less, Nb: 0.005 % to 0.1 %, V: 0.005 % to 0.1 %, and Ti: 0.005 % to 0.1 %, where a CP value determined by the following Expression is 1.00 or less, with the balance being Fe and inevitable impurities: CP = 4.46 % C + 2.37 % Mn / 6 + 1.74 % Cu + 1.7 % Ni / 15 + 1.18 % Cr + 1.95 % Mo + 1.74 % V / 5 + 22.36 % P where [%X] indicates the content by mass% of the element X in steel; a steel microstructure at 0.5 mm below a surface of the steel plate consisting of a bainite microstructure having a dislocation density of 0.5 × 10 14 to 7.0 × 10 14 m -2 and the balance being at least one of ferrite, martensite, pearlite, martensite austenite constituent and retained austenite having a volume fraction of less than 5 %; a difference ΔHV between an average value of Vickers hardness at 0.5 mm below the surface of the steel plate and an average value of Vickers hardness at a mid-thickness part being 25 HV or less; and a tensile strength being 520 MPa or more, whereas the HV, the average value and the dislocation density are determined as indicated in the description. a chemical composition containing, by mass%, C: 0.02 % to 0.08 %, Si: 0.01 % to 0.50 %, Mn: 0.50 % to 1.80 %, P: 0.001 % to 0.015 %, S: 0.0002 % to 0.0015 %, Al: 0.01 % to 0.08 %, and Ca: 0.0005 % to 0.005 %, optionally, by mass%, at least one selected from the group consisting of Cu: 0.50 % or less, Ni: 0.50 % or less, Cr: 0.50 % or less, Mo: 0.50 % or less, Nb: 0.005 % to 0.1 %, V: 0.005 % to 0.1 %, and Ti: 0.005 % to 0.1 %, where a CP value determined by the following Expression is 1.00 or less, with the balance being Fe and inevitable impurities: CP = 4.46 % C + 2.37 % Mn / 6 + 1.74 % Cu + 1.7 % Ni / 15 + 1.18 % Cr + 1.95 % Mo + 1.74 % V / 5 + 22.36 % P where [%X] indicates the content by mass% of the element X in steel; a steel microstructure at 0.5 mm below a surface of the steel plate consisting of a bainite microstructure having a dislocation density of 0.5 × 10 14 to 7.0 × 10 14 m -2 and the balance being at least one of ferrite, martensite, pearlite, martensite austenite constituent and retained austenite having a volume fraction of less than 5 %; a difference ΔHV between an average value of Vickers hardness at 0.5 mm below the surface of the steel plate and an average value of Vickers hardness at a mid-thickness part being 25 HV or less; and a tensile strength being 520 MPa or more, whereas the HV, the average value and the dislocation density are determined as indicated in the description.
A depth camera assembly (DCA) comprising: an illumination source comprising a plurality of emitters on a single substrate including a first emitter and a second emitter, the illumination source configured to project light into a local area using one or more of the plurality of emitters , the illumination source further comprising: a first diffractive optical element corresponding to the first emitter, the first emitter configured to generate a first structured light pattern in the local area using the first diffractive optical element , and a second diffractive optical element corresponding to the second emitter, the second emitter configured to generate a second structured light pattern in the local area using a second diffractive optical element , the first structured light pattern being a different pattern from the second structured light pattern; an imaging device configured to capture one or more images of the local area illuminated with the light from the illumination source ; and a controller configured to determine depth information for objects in the local area using the one or more images and/or configured to provide the one or more images to a virtual reality (VR) console , wherein the VR console is configured to determine depth information based in part on the one or more images and generate a virtual object based in part on the depth information. a first diffractive optical element corresponding to the first emitter, the first emitter configured to generate a first structured light pattern in the local area using the first diffractive optical element , and a second diffractive optical element corresponding to the second emitter, the second emitter configured to generate a second structured light pattern in the local area using a second diffractive optical element , the first structured light pattern being a different pattern from the second structured light pattern; an imaging device configured to capture one or more images of the local area illuminated with the light from the illumination source ; and a controller configured to determine depth information for objects in the local area using the one or more images and/or configured to provide the one or more images to a virtual reality (VR) console , wherein the VR console is configured to determine depth information based in part on the one or more images and generate a virtual object based in part on the depth information.
A method for removing redundant content of communication, CC, flows, which are generated by Lawful Interception in the IMS domain from one or more intercepted target communication sessions of intercepted users, targets, wherein each CC flow comprises a flow of data packets, each data packet comprising a flow identity of the CC flow, wherein the flow identity comprises an address of a sending intercept access point, IAP, at least one identifier of the target, TID, and a communication session Correlation Identifier, CI , the method comprising: - Receiving (S110) a CC flow of data packets from an IAP; - Retrieving (S120) the CC flow identity from the received CC flow, the method comprising - Identifying (S130) any other CC flow being delivered to a Law Enforcement Agency, LEA, wherein said other CC flow has identical TID and CI, respectively, as the received CC flow; - Forwarding (S140) to the LEA only one of the CC flows of data packets having identical TID and CI, respectively, by dropping the received CC flow if having other sending IAP address than said other CC flow being delivered. - Receiving (S110) a CC flow of data packets from an IAP; - Retrieving (S120) the CC flow identity from the received CC flow, the method comprising - Identifying (S130) any other CC flow being delivered to a Law Enforcement Agency, LEA, wherein said other CC flow has identical TID and CI, respectively, as the received CC flow; - Forwarding (S140) to the LEA only one of the CC flows of data packets having identical TID and CI, respectively, by dropping the received CC flow if having other sending IAP address than said other CC flow being delivered.
An article comprising a glass substrate comprising two main faces defining two main surfaces separated by edges, said substrate bearing: - a functional coating deposited on at least one portion of a main surface and - a temporary protective layer deposited on at least one portion of the functional coating having a thickness of at least 1 micrometer, characterized in that the temporary protective layer comprises an organic polymer matrix and infrared-absorbing materials. - a functional coating deposited on at least one portion of a main surface and - a temporary protective layer deposited on at least one portion of the functional coating having a thickness of at least 1 micrometer,
A method for constructing a sequencing plan for a plurality of tasks (Tp, Tc) to be executed on a real-time system implemented off-line by a developing tool from a formalised definition of the tasks according to which each task (Tp, Tc) is decomposed into a sequence of frames, wherein each frame is associated with an elementary process (Tp(m)) having an execution need (Bp(m)), and defines a start date (Dp(m)) from which the process can start and an end date (Dp(m+1)), or deadline, at which the process must complete; associating respective order constraints (C) to process pairs (Tp(m), Tc(n)); projecting the dates on a time scale (S) associated with an execution unit of the real-time system, thus forming a sequence of time slots; sequentially parsing the time slots of the sequence; identifying eligible processes within a current time slot, a process being eligible if it meets the following two criteria: it is executable in the current slot, and if it has an order constraint, the process referenced by the order constraint is also executable in the current time slot, or the deadline of the referenced process is in a previous time slot; sorting the eligible processes in a list by order of increasing deadlines; modifying the list to reorder the processes according to their order constraints; distributing the execution needs of the eligible processes in the current time slot in the order of the list to build the sequencing plan; and producing the sequencing plan in a format suitable for configuring the real-time system. associating respective order constraints (C) to process pairs (Tp(m), Tc(n)); projecting the dates on a time scale (S) associated with an execution unit of the real-time system, thus forming a sequence of time slots; sequentially parsing the time slots of the sequence; identifying eligible processes within a current time slot, a process being eligible if it meets the following two criteria: it is executable in the current slot, and if it has an order constraint, the process referenced by the order constraint is also executable in the current time slot, or the deadline of the referenced process is in a previous time slot; it is executable in the current slot, and if it has an order constraint, the process referenced by the order constraint is also executable in the current time slot, or the deadline of the referenced process is in a previous time slot; sorting the eligible processes in a list by order of increasing deadlines; modifying the list to reorder the processes according to their order constraints; distributing the execution needs of the eligible processes in the current time slot in the order of the list to build the sequencing plan; and producing the sequencing plan in a format suitable for configuring the real-time system.
A method of controlling a wind turbine comprising the step of boosting the output power of the wind turbine above the nominal power (Pw) of the wind turbine, according to a boost operational function representing a boost level for the wind turbine , the boost operational function being a crescent linear function of a wind speed or a turbulence intensity at least between a first threshold (Tv1, Tv1', Tv1") value and a second threshold value (Tv2, Tv2') of the wind speed or turbulence intensity, the boost operational function is defined at constant pitch between the first threshold (Tv1, Tv1', Tv1") value and the second threshold value (Tv2, Tv2').
A method for improving tensile strength of an aggregate of carbon nanotube (CNT) fibers, comprising the steps of: 1) dispersing the aggregate of CNT fibers in chlorosulfonic acid (CSA) 2) treating the aggregate of CNT fibers dispersed in the CSA with a solvent for removing the CSA, thereby removing the CSA; and 3) treating by heating the aggregate of CNT fibers from which the CSA has been removed, wherein the tension/tex is applied to at least one of the steps 1) to 3) in the range of 2 to 50 cN/tex, and the usage ratio of the aggregate of CNT fibers to the weight of the CSA in the step 1) is from 0.01 to 1.0 wt%. 1) dispersing the aggregate of CNT fibers in chlorosulfonic acid (CSA) 2) treating the aggregate of CNT fibers dispersed in the CSA with a solvent for removing the CSA, thereby removing the CSA; and 3) treating by heating the aggregate of CNT fibers from which the CSA has been removed,
An encoding method, comprising: obtaining (S201), by a transmit end, a post-polar-encoding data length S A corresponding to to-be-encoded data; segmenting (S202), by the transmit end, the to-be-encoded data into one or more C code blocks based on the post-polar-encoding data length S A and a preset threshold Z, wherein C is a segment quantity, and C is a positive integer; and performing (S203), by the transmit end, polar encoding on each of the one or more C code blocks, and transmitting (S204) encoded data to a receive end; wherein: if S A is not greater than Z, C is equal to 1; or if S A is greater than Z, C is equal to or greater than 2; wherein C is determined by using the formula ┌ S A / Z ┐, and the one or more C code blocks comprise one or more C+ first kind of code blocks and one or more C - second kind of code blocks, C = C + + C - , a pre-encoding length of the first kind of code block is K+, a pre-encoding length of the second kind of code block is K - , K - = K + - P, P > 1, and P is an odd number; wherein K + is determined by using the following formula K + =┌( S TB + C × l CB ) / C ┐ , C - is determined by using the following formula C - =└( C×K + - S TB -C×l CB ) / P ┘, S TB is a length of the to-be-encoded data, l CB is a length of check information in a code block, ┌·┐ is a rounding-up operation and └·┘ is a rounding-down operation. obtaining (S201), by a transmit end, a post-polar-encoding data length S A corresponding to to-be-encoded data; segmenting (S202), by the transmit end, the to-be-encoded data into one or more C code blocks based on the post-polar-encoding data length S A and a preset threshold Z, wherein C is a segment quantity, and C is a positive integer; and performing (S203), by the transmit end, polar encoding on each of the one or more C code blocks, and transmitting (S204) encoded data to a receive end; wherein: if S A is not greater than Z, C is equal to 1; or if S A is greater than Z, C is equal to or greater than 2; if S A is not greater than Z, C is equal to 1; or if S A is greater than Z, C is equal to or greater than 2; wherein C is determined by using the formula ┌ S A / Z ┐, and the one or more C code blocks comprise one or more C+ first kind of code blocks and one or more C - second kind of code blocks, C = C + + C - , a pre-encoding length of the first kind of code block is K+, a pre-encoding length of the second kind of code block is K - , K - = K + - P, P > 1, and P is an odd number; wherein K + is determined by using the following formula K + =┌( S TB + C × l CB ) / C ┐ , C - is determined by using the following formula C - =└( C×K + - S TB -C×l CB ) / P ┘, S TB is a length of the to-be-encoded data, l CB is a length of check information in a code block, ┌·┐ is a rounding-up operation and └·┘ is a rounding-down operation.