mhurhangee/patent-ind-claim-en huggingface dataset:
A message management method performed by a terminal , comprising: receiving a first input that is performed on a target message on a group communication interface by an operator , the target message being a message that has been sent or a message to be sent; displaying a message management control in response to the first input, wherein the message management control comprises information about processing progress of the target message ; and updating the information about the processing progress of the target message in the case of receiving, from at least one message recipient, a feedback message regarding processing of the target message ; characterised in that the method further comprises: when a first display interface of the terminal where the message management control is displayed is exited and a second display interface of the terminal that is different from the first display interface is displayed, displaying the message management control on the second display interface, such that the processing progress of the target message is available on any display interface of the terminal. receiving a first input that is performed on a target message on a group communication interface by an operator , the target message being a message that has been sent or a message to be sent; displaying a message management control in response to the first input, wherein the message management control comprises information about processing progress of the target message ; and updating the information about the processing progress of the target message in the case of receiving, from at least one message recipient, a feedback message regarding processing of the target message ; characterised in that the method further comprises: when a first display interface of the terminal where the message management control is displayed is exited and a second display interface of the terminal that is different from the first display interface is displayed, displaying the message management control on the second display interface, such that the processing progress of the target message is available on any display interface of the terminal.
An in vitro method for determining the risk of developing a radio-induced sarcoma in a patient treated with radiotherapy, said method comprising a step of detecting, in a biological sample obtained from said patient, a nucleotide change in the sequence of at least 11 genes selected from the group consisting of KLRF1, Clorf234, PKD2L2, ZNF845, GRB2, TMEM117, KIRREL2, GCNT7, USP3, C1R, TOE1, QSER1, SCAMP1, SEPT7, SLC4A3, TBC1D10A, ZFP41, ZNF2, ICAM2, PRG4, MZT1, SYCE1, MAP1B, PRSS35, RPL11, JMJD4, SHISA4, FZD5, ISCU, LGI1, OSCAR, KDM4B, MIR3199-1, MIR3199-2, LIPI, ATP11C, ESF1, BCAS3, FAM63A, SNAP47, MUTYH, TTC28-AS1, and SPRNP1.
A gas turbomachine comprising: a casing assembly surrounding a portion of the gas turbomachine , wherein the casing assembly includes an outer casing portion and an inner casing portion and wherein the inner casing portion includes a plurality of shroud support elements located at distinct axial positions; and a counter-flow cooling system arranged within the casing assembly , the counter-flow cooling system being configured and disposed to guide cooling fluid through the casing assembly in a first axial direction and return cooling fluid through the casing assembly in a second axial direction that is opposite the first axial direction, wherein the counter-flow cooling system includes a first duct member extending axially through the casing assembly , a second duct member spaced from and extending substantially parallel to the first duct member , and at least one cross-flow duct linking the first and second duct members . characterized in that the counter-flow cooling system is arranged within the inner casing portion and extends through at least two of the plurality of shroud support elements , and wherein the counter-flow cooling system has an outlet portion which leads through the inner casing portion and fluidly connects to one or more vanes of the gas turbomachine . a casing assembly surrounding a portion of the gas turbomachine , wherein the casing assembly includes an outer casing portion and an inner casing portion and wherein the inner casing portion includes a plurality of shroud support elements located at distinct axial positions; and a counter-flow cooling system arranged within the casing assembly , the counter-flow cooling system being configured and disposed to guide cooling fluid through the casing assembly in a first axial direction and return cooling fluid through the casing assembly in a second axial direction that is opposite the first axial direction, wherein the counter-flow cooling system includes a first duct member extending axially through the casing assembly , a second duct member spaced from and extending substantially parallel to the first duct member , and at least one cross-flow duct linking the first and second duct members . characterized in that the counter-flow cooling system is arranged within the inner casing portion and extends through at least two of the plurality of shroud support elements , and wherein the counter-flow cooling system has an outlet portion which leads through the inner casing portion and fluidly connects to one or more vanes of the gas turbomachine .
Oven for heating and frying food, particularly a rapid cook oven, which includes • heating means , • an oven space , which is delimited by walls and an openable oven door leading to the oven space , and • a structure delimiting a cooker space , wherein the heating means include a cooker situated in the said cooker space , and the said structure includes thermal insulation between the oven space and the cooker space , • the heating means further including the following heating means for heating food in the oven space : - microwave radiation devices , - a frying plate , and - heating circulating-air devices comprising a flow channel and a fan installed in the flow channel for creating a circulating-air flow in the said flow channel ; characterized in that the flow channel is for removing circulating air from the oven space and leading it back into the oven space after cleaning; in that said cooker comprises a cooking tank ; and in that the microwave radiation devices include at least two magnetrons arranged to create at least two different temperature zones in the oven space . • heating means , • an oven space , which is delimited by walls and an openable oven door leading to the oven space , and • a structure delimiting a cooker space , wherein the heating means include a cooker situated in the said cooker space , and the said structure includes thermal insulation between the oven space and the cooker space , • the heating means further including the following heating means for heating food in the oven space : - microwave radiation devices , - a frying plate , and - heating circulating-air devices comprising a flow channel and a fan installed in the flow channel for creating a circulating-air flow in the said flow channel ; - microwave radiation devices , - a frying plate , and - heating circulating-air devices comprising a flow channel and a fan installed in the flow channel for creating a circulating-air flow in the said flow channel ;
A driving tool comprising: a striking cylinder including a piston configured to be actuated by a combustion pressure of a mixed gas of compressed oxidant and fuel; a combustion chamber in which the mixed gas of compressed oxidant and fuel is to be combusted; a valve member configured to open and close communication between the striking cylinder and the combustion chamber ; and a striking cylinder exhaust valve configured to open and close communication between the striking cylinder and an outside, characterized by a combustion chamber exhaust valve configured to open and close communication between the combustion chamber and the outside. a striking cylinder including a piston configured to be actuated by a combustion pressure of a mixed gas of compressed oxidant and fuel; a combustion chamber in which the mixed gas of compressed oxidant and fuel is to be combusted; a valve member configured to open and close communication between the striking cylinder and the combustion chamber ; and a striking cylinder exhaust valve configured to open and close communication between the striking cylinder and an outside, characterized by a combustion chamber exhaust valve configured to open and close communication between the combustion chamber and the outside.
A material for blocking crosstalk, wherein the material comprises a first layer of film , a substrate , and a second layer of film , the first layer of film and the second layer of film are respectively plated on two sides of the substrate, characterized in that the first layer of film is a composite transparent conductive oxide material with alternately arranged grids and grid lines optically embossed on a first surface of the first layer of film, the first surface opposite a second surface of the first layer of film wherein the second surface is in contact with the substrate, and the first layer of film is non-hollowed-out.
A method for receiving, by a user equipment, UE, a downlink channel, in a 3rd generation partnership project, 3GPP, based communication system, the method comprising: receiving, by the UE, a physical downlink control channel, PDCCH, carrying downlink control information, DCI, in a transmission time interval, TTI, on a resource block, RB, set configured for PDCCH reception; and receiving, by the UE, a physical downlink shared channel, PDSCH, in the TTI according to the DCI, wherein the TTI is equal to or shorter than 0.5 ms in a time domain, wherein each RB of the RB set is defined as 12 consecutive subcarriers in a frequency domain, wherein the PDCCH consists of one or more consecutive control channel elements, CCEs, wherein each of the one or more CCEs consists of multiple resource element groups, REGs that are selected in an ascending order of orthogonal frequency division multiplexing, OFDM, symbol index in an RB and then selected in a next RB within OFDM symbols used for the PDCCH reception on the RB set, and wherein each of the multiple REGs are composed of 12 consecutive resource elements, REs, along the frequency domain, within an OFDM symbol regardless of a RE in which a reference signal, RS, is received. receiving, by the UE, a physical downlink control channel, PDCCH, carrying downlink control information, DCI, in a transmission time interval, TTI, on a resource block, RB, set configured for PDCCH reception; and receiving, by the UE, a physical downlink shared channel, PDSCH, in the TTI according to the DCI, wherein the TTI is equal to or shorter than 0.5 ms in a time domain, wherein each RB of the RB set is defined as 12 consecutive subcarriers in a frequency domain, wherein the PDCCH consists of one or more consecutive control channel elements, CCEs, wherein each of the one or more CCEs consists of multiple resource element groups, REGs that are selected in an ascending order of orthogonal frequency division multiplexing, OFDM, symbol index in an RB and then selected in a next RB within OFDM symbols used for the PDCCH reception on the RB set, and wherein each of the multiple REGs are composed of 12 consecutive resource elements, REs, along the frequency domain, within an OFDM symbol regardless of a RE in which a reference signal, RS, is received.
An apparatus of a Narrowband Internet-of-Things, NB-IoT, user equipment, UE operating in a dense small cells deployment wireless environment, the apparatus comprising: processing circuitry , wherein to configure the NB-IoT UE for open loop transmit power control, the processing circuitry is configured to: decode a narrowband system information block, NB-SIB, to obtain a narrowband physical random access channel, NPRACH, resource set and power control information associated with the NPRACH resource set; encode a random access channel, RACH, preamble for transmission to a base station during a RACH procedure and using the NPRACH resource set, the transmission having transmission power based on the power control information; decode a narrowband uplink resource assignment received during the RACH procedure; and encode a connection setup completion message for transmission to the base station using the narrowband uplink resource assignment; and memory coupled to the processing circuitry , the memory configured to store the NB-SIB. processing circuitry , wherein to configure the NB-IoT UE for open loop transmit power control, the processing circuitry is configured to: decode a narrowband system information block, NB-SIB, to obtain a narrowband physical random access channel, NPRACH, resource set and power control information associated with the NPRACH resource set; encode a random access channel, RACH, preamble for transmission to a base station during a RACH procedure and using the NPRACH resource set, the transmission having transmission power based on the power control information; decode a narrowband uplink resource assignment received during the RACH procedure; and encode a connection setup completion message for transmission to the base station using the narrowband uplink resource assignment; and decode a narrowband system information block, NB-SIB, to obtain a narrowband physical random access channel, NPRACH, resource set and power control information associated with the NPRACH resource set; encode a random access channel, RACH, preamble for transmission to a base station during a RACH procedure and using the NPRACH resource set, the transmission having transmission power based on the power control information; decode a narrowband uplink resource assignment received during the RACH procedure; and encode a connection setup completion message for transmission to the base station using the narrowband uplink resource assignment; and memory coupled to the processing circuitry , the memory configured to store the NB-SIB.
An air diffusion duct for an aeration system, in particular for a railway vehicle, the duct including a plurality of elements assembled to one another and fastened on a ceiling structure of said railway vehicle, said elements together forming at least one air distribution conduit , each element having a hollow volume delimited by an upper wall and a lower wall extending in a longitudinal direction (X) of the vehicle and two side walls substantially perpendicular to the upper and lower walls, characterized in that each element comprises an upper profile in the shape of an inverted U, forming the side and upper walls of said element , intended to be fastened on the ceiling structure and in that the lower wall is formed by a central ceiling wall having first removable fastening means to the ceiling structure and wherein the upper profile has two side panels and an upper panel , the side panels being fastened by snapping perpendicular to the upper panel by first fastening means comprising pultruded snapping profiles , these first fastening means preferably comprising watertight and airtight means.
An attachment structure for securing a robot arm to a support structure, the attachment structure comprising: a mount for mounting to the support structure; and a carrier for connecting to the base of the robot arm, the carrier comprising: a carrier rotational alignment feature for engaging a complementary robot arm base rotational alignment feature, , a carrier axial alignment feature for engaging a complementary robot arm base axial alignment feature, , and a locking mechanism moveable, once the robot arm base and the carrier are engaged, between an unlocked position which does not constrain the location of the robot arm base along an axis of the carrier, and a locked position which does constrain the location of the robot arm base along the said axis of the carrier relative to the carrier, wherein the locking mechanism is independent of the carrier rotational alignment feature and the carrier axial alignment feature such that the locking mechanism is not actuated during engagement of the carrier and the robot arm base; wherein the locking mechanism is compressible between a compressed state in the unlocked position such that no force is applied to the robot arm base by the locking mechanism, and an uncompressed state in the locked position such that force compressing the robot arm base and carrier together is applied to the robot arm base by the locking mechanism. a mount for mounting to the support structure; and a carrier for connecting to the base of the robot arm, the carrier comprising: a carrier rotational alignment feature for engaging a complementary robot arm base rotational alignment feature, , a carrier axial alignment feature for engaging a complementary robot arm base axial alignment feature, , and a locking mechanism moveable, once the robot arm base and the a carrier rotational alignment feature for engaging a complementary robot arm base rotational alignment feature, , a carrier axial alignment feature for engaging a complementary robot arm base axial alignment feature, , and a locking mechanism moveable, once the robot arm base and the carrier are engaged, between an unlocked position which does not constrain the location of the robot arm base along an axis of the carrier, and a locked position which does constrain the location of the robot arm base along the said axis of the carrier relative to the carrier, wherein the locking mechanism is independent of the carrier rotational alignment feature and the carrier axial alignment feature such that the locking mechanism is not actuated during engagement of the carrier and the robot arm base;
A floating wind turbine assembly , configured to self-stabilize in water without a fixed anchor, the floating wind turbine assembly comprising: a wind turbine , joined to a turbine shaft ; a beam anchor , joined to the turbine shaft ; a hollow moving mass , arranged around a beam shaft joined to the beam anchor , such that the hollow moving mass can be moved up or down the beam shaft ; and further comprising: a pump , having a pump first end connected to the water with a first pump hose and a pump second end arranged within the hollow moving mass with a second pump hose ; a first plurality of sensors , arranged proximate the turbine shaft ; a second plurality of sensors , arranged on the turbine shaft ; a controller , communicatively coupled to the first plurality of sensors , the second plurality of sensors , the hollow moving mass , and the pump ; wherein the controller is programmed with instructions to perform the following instructions in a loop until a natural frequency equals an excitation frequency: receive a movement data from the plurality of sensors; determine the excitation frequency from the movement data; receive a natural frequency data from the second plurality of sensors; determine the natural frequency of the wind turbine from the natural frequency data adjust the hollow moving mass wherein when the natural frequency equals the excitation frequency inertial forces in a sea state of the water and the wind turbine equalize in order to stabilize the wind turbine. a wind turbine , joined to a turbine shaft ; a beam anchor , joined to the turbine shaft ; a hollow moving mass , arranged around a beam shaft joined to the beam anchor , such that the hollow moving mass can be moved up or down the beam shaft ; and further comprising: a pump , having a pump first end connected to the water with a first pump hose and a pump second end arranged within the hollow moving mass with a second pump hose ; a first plurality of sensors , arranged proximate the turbine shaft ; a second plurality of sensors , arranged on the turbine shaft ; a controller , communicatively coupled to the first plurality of sensors , the second plurality of sensors , the hollow moving mass , and the pump ; wherein the controller is programmed with instructions to perform the following instructions in a loop until a natural frequency equals an excitation frequency: receive a movement data from the plurality of sensors; determine the excitation frequency from the movement data; receive a natural frequency data from the second plurality of sensors; determine the natural frequency of the wind turbine from the natural frequency data adjust the hollow moving mass receive a movement data from the plurality of sensors; determine the excitation frequency from the movement data; receive a natural frequency data from the second plurality of sensors; determine the natural frequency of the wind turbine from the natural frequency data adjust the hollow moving mass wherein when the natural frequency equals the excitation frequency inertial forces in a sea state of the water and the wind turbine equalize in order to stabilize the wind turbine.
A nicotinamide composition for use in the treatment of hand-foot skin reaction induced by sorafenib, characterized in that , the composition consists of nicotinamide and sorafenib, wherein nicotinamide has a chemical name of 3-pyridinecarboxamide, a molecular formula of C 6 H 6 N 2 O, and a molecular weight of 122.13, and sorafenib has a chemical name of 4-{4-[({4-chloro-3-(trifluoromethyl)phenyl]amino}carbonyl)amino]phenoxy}-N-methylpyridine-2-carboxamide, a molecular formula of C 21 H 16 ClF 3 N 4 O 3 , and a molecular weight of 464.83. wherein nicotinamide has a chemical name of 3-pyridinecarboxamide, a molecular formula of C 6 H 6 N 2 O, and a molecular weight of 122.13, and sorafenib has a chemical name of 4-{4-[({4-chloro-3-(trifluoromethyl)phenyl]amino}carbonyl)amino]phenoxy}-N-methylpyridine-2-carboxamide, a molecular formula of C 21 H 16 ClF 3 N 4 O 3 , and a molecular weight of 464.83.
Reinforcement element for motor vehicle body means the reinforcement element comprising means of protection against the rear impact of the vehicle, characterized as it includes at least two tubes to be positioned globally in the direction of the vehicle length and to be attached to the body , and a rigid surface of contact comprising impactors , the rigid surface of contact being arranged opposite the two tubes to allow the vehicle to move in the event of a rear impact, the reinforcement element comprising in addition to the means of energy absorption protruding to the rigid surface of contact and to position to the rear of the vehicle, so that impactors can only be used for such activation if the means of energy absorption were requested and overcome by such a shock from the rear.
A subsea flying lead for transmitting an electric current to a component of a subsea structure, the subsea flying lead comprising: a fluid line comprising a tubing , characterised in that , in use, an electric current is transmitted along the tubing ; a flying plate , wherein the fluid line terminates in a fluid coupler on the flying plate ; and an electrical connector (!2a,12b) in the flying plate , and wherein an electrical conductor runs from the tubing of fluid line to the electrical connector ; wherein the flying plate is arranged to be connected to a fixed plate on a subsea structure containing at least one fluid line comprising a tubing terminating in a fluid coupler in the fixed plate such that, in use, the flying plate fluid coupler is coupled to the fixed plate fluid coupler ; and electric current transmitted along the tubing of the fluid line is, in use, transmitted via the electrical conductor to a component of the subsea structure . a fluid line comprising a tubing , characterised in that , in use, an electric current is transmitted along the tubing ; a flying plate , wherein the fluid line terminates in a fluid coupler on the flying plate ; and an electrical connector (!2a,12b) in the flying plate , and wherein an electrical conductor runs from the tubing of fluid line to the electrical connector ; wherein the flying plate is arranged to be connected to a fixed plate on a subsea structure containing at least one fluid line comprising a tubing terminating in a fluid coupler in the fixed plate such that, in use, the flying plate fluid coupler is coupled to the fixed plate fluid coupler ; and electric current transmitted along the tubing of the fluid line is, in use, transmitted via the electrical conductor to a component of the subsea structure .