mhurhangee/patent-ind-claim-en huggingface dataset:
A packaged device having a front surface , a back surface , opposite to the front surface, and a side surface extending between the front surface and the back surface, the packaged device comprising: a carrying base ; an accommodation cavity in the carrying base; a semiconductor die in the accommodation cavity , the semiconductor die having die pads ; a protective layer , covering the semiconductor die and the carrying base; first vias in the protective layer, at the die pads ; and connection terminals of conductive material, the connection terminals having first connection portions in the first vias , in electrical contact with the die pads , characterized by second connection portions , extending on the protective layer , along the side surface of the packaged device. a carrying base ; an accommodation cavity in the carrying base; a semiconductor die in the accommodation cavity , the semiconductor die having die pads ; a protective layer , covering the semiconductor die and the carrying base; first vias in the protective layer, at the die pads ; and connection terminals of conductive material, the connection terminals having first connection portions in the first vias , in electrical contact with the die pads , characterized by second connection portions , extending on the protective layer , along the side surface of the packaged device.
A method for producing a purified hydrogen gas stream, the method comprising: flowing a feed gas containing nitrogen gas (N 2 ) as the majority component, hydrogen gas (H 2 ), and carbon monoxide (CO) and having an initial H 2 to CO ratio into a processing unit to produce an enhanced gas containing carbon dioxide (CO 2 ) and having a second H 2 to CO ratio greater than the initial H 2 to CO ratio; flowing the enhanced gas into a purification unit comprising a N 2 removal unit to remove N 2 and a CO 2 removal unit to remove CO 2 , wherein the purification unit produces a purified hydrogen gas stream and a tail gas; and recycling at least a portion of the tail gas to a point upstream of the N 2 removal unit, wherein flowing the enhanced gas into the purification unit comprises flowing the enhanced gas into the N 2 removal unit to produce a permeate stream and a retentate stream, and flowing the permeate stream into the CO 2 removal unit to produce the purified hydrogen gas stream and the tail gas, wherein the N 2 removal unit comprises a membrane separation unit configured to receive the enhanced gas, and wherein the CO 2 removal unit comprises a pressure swing adsorption (PSA) unit. flowing a feed gas containing nitrogen gas (N 2 ) as the majority component, hydrogen gas (H 2 ), and carbon monoxide (CO) and having an initial H 2 to CO ratio into a processing unit to produce an enhanced gas containing carbon dioxide (CO 2 ) and having a second H 2 to CO ratio greater than the initial H 2 to CO ratio; flowing the enhanced gas into a purification unit comprising a N 2 removal unit to remove N 2 and a CO 2 removal unit to remove CO 2 , wherein the purification unit produces a purified hydrogen gas stream and a tail gas; and recycling at least a portion of the tail gas to a point upstream of the N 2 removal unit, wherein flowing the enhanced gas into the purification unit comprises flowing the enhanced gas into the N 2 removal unit to produce a permeate stream and a retentate stream, and flowing the permeate stream into the CO 2 removal unit to produce the purified hydrogen gas stream and the tail gas, wherein the N 2 removal unit comprises a membrane separation unit configured to receive the enhanced gas, and wherein the CO 2 removal unit comprises a pressure swing adsorption (PSA) unit. wherein flowing the enhanced gas into the purification unit comprises flowing the enhanced gas into the N 2 removal unit to produce a permeate stream and a retentate stream, and flowing the permeate stream into the CO 2 removal unit to produce the purified hydrogen gas stream and the tail gas, wherein the N 2 removal unit comprises a membrane separation unit configured to receive the enhanced gas, and wherein the CO 2 removal unit comprises a pressure swing adsorption (PSA) unit.
A curable silicone composition comprising: (A) an organopolysiloxane represented by the average unit formula: (R 1 3 SiO 1/2 ) x (R 2 2 SiO 2/2 ) y (R 3 SiO 3/2 ) z in the formula, R 1 are the same or different, and alkyl groups having from 1 to 12 carbons or an alkenyl groups having from 2 to 12 carbons; R 2 are the same or different, and alkyl groups having from 1 to 12 carbons or alkenyl groups having from 2 to 12 carbons; R 3 is an aryl group having from 6 to 20 carbons or an aralkyl group having from 7 to 20 carbons, provided that, in a molecule, at least 0.5 mol% of a total content of the groups represented by R 1 , R 2 , and R 3 are the alkenyl groups; and x, y and z are numbers satisfying: 0.05 ≤ x ≤ 0.4, 0.1 ≤ y ≤ 0.4, 0.3 ≤ z ≤ 0.8, and x + y + z = 1; (B) from 0.1 to 60 parts by mass, relative to 100 parts by mass of component (A), of a straight-chain organopolysiloxane having at least two alkenyl groups in a molecule; (C) an organopolysiloxane having at least two silicon atom-bonded hydrogen atoms in a molecule, in an amount such that a content of the silicon atom-bonded hydrogen atoms contained in this component is from 0.1 to 10 mol relative to 1 mol of the total content of the alkenyl groups contained in components (A) and (B); and (D) a hydrosilylation reaction catalyst, in an amount that accelerates curing of the composition. (A) an organopolysiloxane represented by the average unit formula: (R 1 3 SiO 1/2 ) x (R 2 2 SiO 2/2 ) y (R 3 SiO 3/2 ) z in the formula, R 1 are the same or different, and alkyl groups having from 1 to 12 carbons or an alkenyl groups having from 2 to 12 carbons; R 2 are the same or different, and alkyl groups having from 1 to 12 carbons or alkenyl groups having from 2 to 12 carbons; R 3 is an aryl group having from 6 to 20 carbons or an aralkyl group having from 7 to 20 carbons, provided that, in a molecule, at least 0.5 mol% of a total content of the groups represented by R 1 , R 2 , and R 3 are the alkenyl groups; and x, y and z are numbers satisfying: 0.05 ≤ x ≤ 0.4, 0.1 ≤ y ≤ 0.4, 0.3 ≤ z ≤ 0.8, and x + y + z = 1; (B) from 0.1 to 60 parts by mass, relative to 100 parts by mass of component (A), of a straight-chain organopolysiloxane having at least two alkenyl groups in a molecule; (C) an organopolysiloxane having at least two silicon atom-bonded hydrogen atoms in a molecule, in an amount such that a content of the silicon atom-bonded hydrogen atoms contained in this component is from 0.1 to 10 mol relative to 1 mol of the total content of the alkenyl groups contained in components (A) and (B); and (D) a hydrosilylation reaction catalyst, in an amount that accelerates curing of the composition.
A multichip module , comprising: a first transceiver die (501-1) having first transceivers ; a second transceiver die (501-2) having second transceivers ; a crossbar switch die having at least one crossbar switch ; a first protocol logic blocks die (502-1) having first protocol logic blocks ; a second protocol logic blocks die (502-2) having second protocol logic blocks ; and a silicon interposer to which the first transceiver die, the second transceiver die, the crossbar switch die, the first protocol logic blocks die, and the second protocol logic blocks die are coupled; wherein the first and second transceiver dice, the first and second protocol logic blocks dice, and the crossbar switch die are mounted on the interposer; and wherein the interposer interconnects the first transceivers and the first protocol logic blocks to one another, interconnects the second transceivers and the second protocol logic blocks to one another, interconnects the first protocol logic blocks and the at least one crossbar switch to one another, and further interconnects the second protocol logic blocks and the at least one crossbar switch to one another. a first transceiver die (501-1) having first transceivers ; a second transceiver die (501-2) having second transceivers ; a crossbar switch die having at least one crossbar switch ; a first protocol logic blocks die (502-1) having first protocol logic blocks ; a second protocol logic blocks die (502-2) having second protocol logic blocks ; and a silicon interposer to which the first transceiver die, the second transceiver die, the crossbar switch die, the first protocol logic blocks die, and the second protocol logic blocks die are coupled; wherein the first and second transceiver dice, the first and second protocol logic blocks dice, and the crossbar switch die are mounted on the interposer; and wherein the interposer interconnects the first transceivers and the first protocol logic blocks to one another, interconnects the second transceivers and the second protocol logic blocks to one another, interconnects the first protocol logic blocks and the at least one crossbar switch to one another, and further interconnects the second protocol logic blocks and the at least one crossbar switch to one another.
An airfoil for a turbine engine comprising: an outer wall delimiting an airfoil interior , the outer wall extending span-wise in a radial direction (R) of the turbine engine and being formed by a pressure side and a suction side joined at a leading edge and at a trailing edge , wherein a chordal axis is defined extending centrally between the pressure and suction sides ; a plurality of pins (22a-1) positioned in the airfoil interior toward the trailing edge , each extending from the pressure side to the suction side and further being elongated in a radial direction (R), the plurality of pins (22a-1) being arranged in multiple radial rows (A-L) spaced along the chordal axis , with the pins (22a-1) in each row being interspaced to define coolant passages (24a-1) therebetween; a row of radially spaced apart partition walls positioned aft of a last row (L) pins , wherein each partition wall extends from the pressure side to the suction side and is elongated in a generally axial direction, extending along the chordal axis to terminate at the trailing edge , whereby axially extending coolant exit slots are defined in the interspaces between adjacent partition walls (26a-b) that direct coolant exiting the last row (L) of pins to be discharged from the airfoil into a hot gas path; and wherein the partition walls occupy radial positions that are staggered with respect to coolant passages in the last row (L) of pins . an outer wall delimiting an airfoil interior , the outer wall extending span-wise in a radial direction (R) of the turbine engine and being formed by a pressure side and a suction side joined at a leading edge and at a trailing edge , wherein a chordal axis is defined extending centrally between the pressure and suction sides ; a plurality of pins (22a-1) positioned in the airfoil interior toward the trailing edge , each extending from the pressure side to the suction side and further being elongated in a radial direction (R), the plurality of pins (22a-1) being arranged in multiple radial rows (A-L) spaced along the chordal axis , with the pins (22a-1) in each row being interspaced to define coolant passages (24a-1) therebetween; a row of radially spaced apart partition walls positioned aft of a last row (L) pins , wherein each partition wall extends from the pressure side to the suction side and is elongated in a generally axial direction, extending along the chordal axis to terminate at the trailing edge , whereby axially extending coolant exit slots are defined in the interspaces between adjacent partition walls (26a-b) that direct coolant exiting the last row (L) of pins to be discharged from the airfoil into a hot gas path; and wherein the partition walls occupy radial positions that are staggered with respect to coolant passages in the last row (L) of pins .
A filter for a submersible pump, said filter comprising a filter housing configured to releasably engage a housing of the pump overlying a pump intake ; wherein the filter housing comprises a plurality of perforate filter housing walls disposed generally inline with the pump intake, and at least one imperforate sidewall extending between the plurality of perforate filter housing walls , wherein one of the plurality of perforate filter housing walls comprises a perforate filter intake grate and another one of the plurality of perforate filter housing walls comprises a filtrate outlet grate that is disposed inline with the perforate filter intake grate between the pump intake and the perforate filter intake grate ; wherein the plurality of perforate filter housing walls and at least one imperforate sidewall define a filter chamber disposed between the generally parallel filter intake grate and the filtrate outlet grate ; and wherein the filter chamber has filter media disposed therein. wherein the filter housing comprises a plurality of perforate filter housing walls disposed generally inline with the pump intake, and at least one imperforate sidewall extending between the plurality of perforate filter housing walls , wherein one of the plurality of perforate filter housing walls comprises a perforate filter intake grate and another one of the plurality of perforate filter housing walls comprises a filtrate outlet grate that is disposed inline with the perforate filter intake grate between the pump intake and the perforate filter intake grate ; wherein the plurality of perforate filter housing walls and at least one imperforate sidewall define a filter chamber disposed between the generally parallel filter intake grate and the filtrate outlet grate ; and wherein the filter chamber has filter media disposed therein.
Filter device with a removable end part (81; 82) and with an enclosure which accommodates a replaceable filter element that comprises two end caps , between which a filter material extends, wherein arranged between the end part (81; 82) and the one end cap is a positioning device which, in cooperation with at least one corresponding positioning element of this end cap , positions the filter element inside the enclosure , at least when viewed in its circumferential direction, characterised in that the positioning device forms an annular body which, on the bottom side, has an insert ring and, on the top side, bears a head ring which is at least partially in contact with contact parts of the removable end part ; in that the positioning device has a guide bar which engages in a guide channel , which is arranged as a positioning element in the one end cap , the guide channel being open towards the inside of the filter element ; in that the one end cap has on its inside a guide ring which protrudes on both sides beyond a contact ring to which the filter material is fixed with its one free face end; and in that the guide channel , fixed on the outer circumference to the guide ring , extends over the entire height thereof. characterised in that the positioning device forms an annular body which, on the bottom side, has an insert ring and, on the top side, bears a head ring which is at least partially in contact with contact parts of the removable end part ; in that the positioning device has a guide bar which engages in a guide channel , which is arranged as a positioning element in the one end cap , the guide channel being open towards the inside of the filter element ; in that the one end cap has on its inside a guide ring which protrudes on both sides beyond a contact ring to which the filter material is fixed with its one free face end; and in that the guide channel , fixed on the outer circumference to the guide ring , extends over the entire height thereof.
A communication method, characterized in that the method comprises: receiving, by a user equipment, UE, from a network, a higher layer signaling to indicate a dependency of a Zadoff-Chu, ZC, root on an orthogonal frequency division multiplexing, OFDM, symbol, wherein the higher layer signaling comprises a UE-specific sounding reference signal, SRS, sequence identifier, ID; generating, by the UE, a first sounding reference signal, SRS, sequence based on a first ZC root of the first SRS sequence, wherein the first ZC root depends on a first OFDM symbol and the UE-specific SRS sequence ID; and sending, by the UE, the first SRS sequence in the first OFDM symbol. receiving, by a user equipment, UE, from a network, a higher layer signaling to indicate a dependency of a Zadoff-Chu, ZC, root on an orthogonal frequency division multiplexing, OFDM, symbol, wherein the higher layer signaling comprises a UE-specific sounding reference signal, SRS, sequence identifier, ID; generating, by the UE, a first sounding reference signal, SRS, sequence based on a first ZC root of the first SRS sequence, wherein the first ZC root depends on a first OFDM symbol and the UE-specific SRS sequence ID; and sending, by the UE, the first SRS sequence in the first OFDM symbol.
A method for wireless communication, comprising: identifying , at a user equipment, UE, two or more transmission time intervals, TTIs, that are configured for either transport block, TB, feedback or code block group, CBG, feedback; identifying an amount of resources available for transmitting feedback information; selecting TB feedback or CBG feedback for each of the two or more TTIs based at least in part on the amount of resources available for transmitting feedback information; and transmitting the feedback information to a base station according to the selecting. identifying , at a user equipment, UE, two or more transmission time intervals, TTIs, that are configured for either transport block, TB, feedback or code block group, CBG, feedback; identifying an amount of resources available for transmitting feedback information; selecting TB feedback or CBG feedback for each of the two or more TTIs based at least in part on the amount of resources available for transmitting feedback information; and transmitting the feedback information to a base station according to the selecting.
A method comprising: applying a gain to a reference signal; estimating a wireless channel, over which a received signal passed, using the reference signal with the applied gain; adjusting equalization values obtained from the estimating to remove effects of the applied gain; and equalizing at least a data portion of the received signal using the adjusted equalization values and storing the result in a computer readable memory, wherein the received signal comprises a first portion comprising the reference signal and the at least data portion, and wherein at least prior to the equalizing the gain is not applied to any of the at least data portion. applying a gain to a reference signal; estimating a wireless channel, over which a received signal passed, using the reference signal with the applied gain; adjusting equalization values obtained from the estimating to remove effects of the applied gain; and equalizing at least a data portion of the received signal using the adjusted equalization values and storing the result in a computer readable memory, wherein the received signal comprises a first portion comprising the reference signal and the at least data portion, and wherein at least prior to the equalizing the gain is not applied to any of the at least data portion.
An air conditioning control system comprising: air conditioning devices which are configured to condition air of a single space and are not configured to directly communicate with one another; a relay unit configured to mutually communicate with each of the air conditioning devices via a first communication line ; and a mobile terminal or a non-portable device configured to connect to a public communication network and configured to communicate with the relay unit via a second communication line , the air conditioning devices configured to be controlled in a linked manner such that the mobile terminal or the non-portable device sends a control signal, which indicates a temperature level or a set temperature in accordance with a temperature level or a set temperature of one of the air conditioning devices , to another one of the air conditioning devices , via the relay unit . air conditioning devices which are configured to condition air of a single space and are not configured to directly communicate with one another; a relay unit configured to mutually communicate with each of the air conditioning devices via a first communication line ; and a mobile terminal or a non-portable device configured to connect to a public communication network and configured to communicate with the relay unit via a second communication line , the air conditioning devices configured to be controlled in a linked manner such that the mobile terminal or the non-portable device sends a control signal, which indicates a temperature level or a set temperature in accordance with a temperature level or a set temperature of one of the air conditioning devices , to another one of the air conditioning devices , via the relay unit .
A braking system for an aircraft operable to apply one or more aircraft wheel brakes according to at least one of a plurality of wheel brake control functions, the braking system comprising: an aircraft speed indicator ; a brake condition indicator comprising a brake temperature characteristic indicator ; and characterised by a controller configured to: control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; select a second wheel brake control function from the plurality of wheel brake control functions based on a brake temperature characteristic of the one or more aircraft wheel breaks, wherein a thermal oxidation limiting function is selected as the second wheel brake control function if the brake temperature characteristic of at least one aircraft wheel brake meets a thermal oxidation limiting criterion; and control the wheel braking operation of the aircraft according to at least the second wheel brake control function if the aircraft speed does not exceed the speed threshold. an aircraft speed indicator ; a brake condition indicator comprising a brake temperature characteristic indicator ; and characterised by a controller configured to: control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; select a second wheel brake control function from the plurality of wheel brake control functions based on a brake temperature characteristic of the one or more aircraft wheel breaks, wherein a thermal oxidation limiting function is selected as the second wheel brake control function if the brake temperature characteristic of at least one aircraft wheel brake meets a thermal oxidation limiting criterion; and control the wheel braking operation of the aircraft according to at least the second wheel brake control function if the aircraft speed does not exceed the speed threshold. control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; select a second wheel brake control function from the plurality of wheel brake control functions based on a brake temperature characteristic of the one or more aircraft wheel breaks, wherein a thermal oxidation limiting function is selected as the second wheel brake control function if the brake temperature characteristic of at least one aircraft wheel brake meets a thermal oxidation limiting criterion; and control the wheel braking operation of the aircraft according to at least the second wheel brake control function if the aircraft speed does not exceed the speed threshold.