mhurhangee/patent-ind-claim-en huggingface dataset:
A system configured to detect and neutralize a target aerial vehicle (104a; 104b), the system comprising: a counter-attack unmanned aerial vehicle (UAV) (102a-c; 302; 402; 502; 602; 702; 802; 902; 1002) comprising: a flight body ; a flight control system flight body that controls flight of the counter-attack UAV ; and an aerial vehicle countermeasure supported by the flight body , an aerial vehicle detection system comprising a plurality of detection sensors configured to detect a target aerial vehicle (104a; 104b) and to generate position data associated with the target aerial vehicle, the aerial vehicle detection system being configured to provide command data to the counter-attack UAV to intercept the target aerial vehicle by the counter-attack UAV; wherein, in response to interception of the target aerial vehicle, the counter-attack UAV disrupts operation of the detected target aerial vehicle with the aerial vehicle capture countermeasure , characterized in that the aerial vehicle detection system is configured to eliminate position data associated with one or more detection sensors of the plurality of detection sensors based on a credibility hierarchy associated with the plurality of detection sensors. a counter-attack unmanned aerial vehicle (UAV) (102a-c; 302; 402; 502; 602; 702; 802; 902; 1002) comprising: a flight body ; a flight control system flight body that controls flight of the counter-attack UAV ; and an aerial vehicle countermeasure supported by the flight body , a flight body ; a flight control system flight body that controls flight of the counter-attack UAV ; and an aerial vehicle countermeasure supported by the flight body , an aerial vehicle detection system comprising a plurality of detection sensors configured to detect a target aerial vehicle (104a; 104b) and to generate position data associated with the target aerial vehicle, the aerial vehicle detection system being configured to provide command data to the counter-attack UAV to intercept the target aerial vehicle by the counter-attack UAV; wherein, in response to interception of the target aerial vehicle, the counter-attack UAV disrupts operation of the detected target aerial vehicle with the aerial vehicle capture countermeasure , characterized in that the aerial vehicle detection system is configured to eliminate position data associated with one or more detection sensors of the plurality of detection sensors based on a credibility hierarchy associated with the plurality of detection sensors.
Process for the production of polyesters comprising: a) a dicarboxylic component comprising: a1) 40-60% mol of units deriving from at least one aromatic dicarboxylic acid, a2) 60-40% mol of units deriving from at least one aliphatic dicarboxylic acid, b) a diol component comprising units deriving from at least one aliphatic diol; said process comprising an esterification step and a following polycondensation step, characterized in that : said esterification step is performed in the presence of an esterification catalyst selected from Titanium compounds, and said polycondensation step is performed in the presence of a catalyst comprising a mixture of at least one Titanium-based compound and at least one Zirconium-based compound in which the weight ratio Ti/(Ti+Zr) is equal to or higher than 0.01 and equal to or lower than 0.70. a) a dicarboxylic component comprising: a1) 40-60% mol of units deriving from at least one aromatic dicarboxylic acid, a2) 60-40% mol of units deriving from at least one aliphatic dicarboxylic acid, a1) 40-60% mol of units deriving from at least one aromatic dicarboxylic acid, a2) 60-40% mol of units deriving from at least one aliphatic dicarboxylic acid, b) a diol component comprising units deriving from at least one aliphatic diol; said process comprising an esterification step and a following polycondensation step, characterized in that : said esterification step is performed in the presence of an esterification catalyst selected from Titanium compounds, and said polycondensation step is performed in the presence of a catalyst comprising a mixture of at least one Titanium-based compound and at least one Zirconium-based compound in which the weight ratio Ti/(Ti+Zr) is equal to or higher than 0.01 and equal to or lower than 0.70. said process comprising an esterification step and a following polycondensation step, characterized in that : said esterification step is performed in the presence of an esterification catalyst selected from Titanium compounds, and said polycondensation step is performed in the presence of a catalyst comprising a mixture of at least one Titanium-based compound and at least one Zirconium-based compound in which the weight ratio Ti/(Ti+Zr) is equal to or higher than 0.01 and equal to or lower than 0.70. said esterification step is performed in the presence of an esterification catalyst selected from Titanium compounds, and said polycondensation step is performed in the presence of a catalyst comprising a mixture of at least one Titanium-based compound and at least one Zirconium-based compound in which the weight ratio Ti/(Ti+Zr) is equal to or higher than 0.01 and equal to or lower than 0.70.
A method for manufacturing an e-fuse, comprising: providing a semiconductor substrate, the semiconductor substrate comprising a preset active region, wherein the preset active region is a region on the semiconductor substrate where no isolating region is to be formed; forming an isolating region on the semiconductor substrate, wherein the isolating region and the preset active region have a height difference and are connected by at least one side wall; forming a negative electrode and a positive electrode on the preset active region; and forming a fuse link on the side wall and partial regions of the isolating region close to the at least one side wall for connecting the negative electrode and the positive electrode; wherein the forming an isolating region on the semiconductor substrate comprises: forming a trench extending downward from an upper surface of the semiconductor substrate, wherein a bottom surface of the trench forms the isolating region, and a side wall of the trench is used to connect the isolating region with the preset active region. providing a semiconductor substrate, the semiconductor substrate comprising a preset active region, wherein the preset active region is a region on the semiconductor substrate where no isolating region is to be formed; forming an isolating region on the semiconductor substrate, wherein the isolating region and the preset active region have a height difference and are connected by at least one side wall; forming a negative electrode and a positive electrode on the preset active region; and forming a fuse link on the side wall and partial regions of the isolating region close to the at least one side wall for connecting the negative electrode and the positive electrode; wherein the forming an isolating region on the semiconductor substrate comprises: forming a trench extending downward from an upper surface of the semiconductor substrate, wherein a bottom surface of the trench forms the isolating region, and a side wall of the trench is used to connect the isolating region with the preset active region.
A motor brake unit for a winch , comprising: a) an electric motor comprising a rotor , which is connected to a motor shaft , and a stator which is connected to a housing , wherein the rotor can be rotated together with the motor shaft relative to the stator about a rotational axis (D); b) a brake which comprises at least one first brake body and at least one second brake body which is or can be connected, non-rotationally about the rotational axis (D), to the motor shaft , wherein the at least one first brake body and the at least one second brake body can be pressed against each other in order to achieve a braking effect based on a frictional engagement, c) wherein the housing comprises a cup-shaped section into which the brake is or can be inserted, such that the brake is at least partially surrounded by the cup-shaped section , characterised in that d) the cup-shaped section is at least partially surrounded by the rotor of the electric motor . a) an electric motor comprising a rotor , which is connected to a motor shaft , and a stator which is connected to a housing , wherein the rotor can be rotated together with the motor shaft relative to the stator about a rotational axis (D); b) a brake which comprises at least one first brake body and at least one second brake body which is or can be connected, non-rotationally about the rotational axis (D), to the motor shaft , wherein the at least one first brake body and the at least one second brake body can be pressed against each other in order to achieve a braking effect based on a frictional engagement, c) wherein the housing comprises a cup-shaped section into which the brake is or can be inserted, such that the brake is at least partially surrounded by the cup-shaped section , characterised in that d) the cup-shaped section is at least partially surrounded by the rotor of the electric motor .
A method implemented by a wireless transmit receive unit, WTRU, the method comprising: the WTRU transmitting capability information indicating a bandwidth capability of the WTRU; the WTRU receiving a radio resource control, RRC, connection reconfiguration message via a first frequency block, wherein the RRC connection reconfiguration message comprises a configuration for at least a second frequency block, the configuration for the second frequency block comprising frequency information for the second frequency block and bandwidth information for the second frequency block; the WTRU receiving a physical downlink control channel, PDCCH, transmission over the first frequency block, the PDCCH transmission comprising a downlink control information, DCI, message indicating that the WTRU activate the second frequency block; and the WTRU receiving a downlink transmission using the second frequency block based on the PDCCH transmission received via the first frequency block. the WTRU transmitting capability information indicating a bandwidth capability of the WTRU; the WTRU receiving a radio resource control, RRC, connection reconfiguration message via a first frequency block, wherein the RRC connection reconfiguration message comprises a configuration for at least a second frequency block, the configuration for the second frequency block comprising frequency information for the second frequency block and bandwidth information for the second frequency block; the WTRU receiving a physical downlink control channel, PDCCH, transmission over the first frequency block, the PDCCH transmission comprising a downlink control information, DCI, message indicating that the WTRU activate the second frequency block; and the WTRU receiving a downlink transmission using the second frequency block based on the PDCCH transmission received via the first frequency block.
A refrigerator comprising: a cabinet that defines a storage space; a mounting bracket disposed at a top surface of the cabinet ; a door configured to rotate relative to the cabinet to thereby open and close at least a portion of the storage space, the door comprising a hinge mounting portion and a guide device mounting portion that are disposed at a top surface of the door ; a hinge cover that is disposed at the top surface of the cabinet and covers the mounting bracket , the hinge cover defining a cover opening at a front surface thereof facing the door ; a hinge comprising a door bracket disposed at the hinge mounting portion , a hinge bracket disposed at the mounting bracket , and a plurality of links that connect the door bracket to the hinge bracket ; a guide device having a first side that is disposed at the guide device mounting portion and a second side that passes through the cover opening and is disposed inside the hinge cover ; an electric wire and a water pipe that are disposed along an inside of the guide device , wherein the guide device comprises an electric wire guide guiding the electric wire , and characterized in that the guide device further comprises a pipe guide guiding the water pipe ; and the refrigerator further comprises a guide bush that is disposed at the guide device mounting portion and defines a through-hole guiding the electric wire and the water pipe into the door , wherein the guide bush defines a rotation center of an end of the electric wire guide and an end of the pipe guide that are connected to each other at the guide device mounting portion . a cabinet that defines a storage space; a mounting bracket disposed at a top surface of the cabinet ; a door configured to rotate relative to the cabinet to thereby open and close at least a portion of the storage space, the door comprising a hinge mounting portion and a guide device mounting portion that are disposed at a top surface of the door ; a hinge cover that is disposed at the top surface of the cabinet and covers the mounting bracket , the hinge cover defining a cover opening at a front surface thereof facing the door ; a hinge comprising a door bracket disposed at the hinge mounting portion , a hinge bracket disposed at the mounting bracket , and a plurality of links that connect the door bracket to the hinge bracket ; a guide device having a first side that is disposed at the guide device mounting portion and a second side that passes through the cover opening and is disposed inside the hinge cover ; an electric wire and a water pipe that are disposed along an inside of the guide device , wherein the guide device comprises an electric wire guide guiding the electric wire , and characterized in that the guide device further comprises a pipe guide guiding the water pipe ; and the refrigerator further comprises a guide bush that is disposed at the guide device mounting portion and defines a through-hole guiding the electric wire and the water pipe into the door , wherein the guide bush defines a rotation center of an end of the electric wire guide and an end of the pipe guide that are connected to each other at the guide device mounting portion .
An aerofoil for a gas turbine engine, the aerofoil comprising: a pressure surface ; a suction surface ; a leading edge ; a trailing edge ; a stagnation zone located in the region of the leading edge; and an elongate channel in the surface of the aerofoil running along the leading edge at the stagnation zone; characterised in that the cross section of the elongate channel varies along its length, is largest at the ends of the elongate channel, and decreases towards the midpoint of the length of the elongate channel. a pressure surface ; a suction surface ; a leading edge ; a trailing edge ; a stagnation zone located in the region of the leading edge; and an elongate channel in the surface of the aerofoil running along the leading edge at the stagnation zone;
Rotating electrical machine comprising: electronic components that are intended to operate said machine, a heat sink for the electronic components and a rear bracket, said heat sink comprising a top face and a bottom face incorporating fins and being added onto the rear bracket, characterized in that the heat sink is disposed between the rear bracket of said machine and said electronic components, said bottom face incorporating said fins facing said rear bracket, and in that the heat sink further comprises a boss on its bottom face at the level of the fins , the boss comprising a first slope (813P1) for guiding an axial air flow (FA) towards the interior of the machine, and a second slope (813P2) for guiding a radial air flow (FR) towards the interior of the machine.
A vehicle-drive assisting apparatus comprising: a wheel position storing section storing a position (K) of a wheel when a vehicle effects traveling; a road surface information acquiring section acquiring road surface information indicating a road surface condition of a road surface on which the vehicle has traveled; and a display image generating section generating a display image displaying the position (K) of the wheel stored in the wheel position storing section and of the road surface information stored in the wheel position storing section and relating to the wheel position at the position (K) of the wheel on a displaying unit provided in the vehicle ; characterized in that the display image generating section superposes the road surface information with the wheel position (K) stored in the wheel position storing section . a wheel position storing section storing a position (K) of a wheel when a vehicle effects traveling; a road surface information acquiring section acquiring road surface information indicating a road surface condition of a road surface on which the vehicle has traveled; and a display image generating section generating a display image displaying the position (K) of the wheel stored in the wheel position storing section and of the road surface information stored in the wheel position storing section and relating to the wheel position at the position (K) of the wheel on a displaying unit provided in the vehicle ;
Belt-type traction means, which comprises a herringbone toothed belt , which has at least a tooth part and a support structure supporting the tooth part , which support structure comprises a plurality of reinforcement means in the longitudinal direction of the toothed belt , wherein in the transverse direction of the toothed belt the toothed belt comprises two edge parts side by side and a center part between the edge parts and connecting the edge parts , characterized in that the spring constant of which center part in the transverse direction of the toothed belt is smaller than the corresponding spring constant of the edge parts .
A method for monitoring a vane wheel of an aircraft engine, comprising: - acquiring (101 1 ) at least one time signal, each time signal relating to passage time instants of the blades of the vane wheel in front of a sensor ; and - determining (101 2 ) a current flight phase of the aircraft; - for each flight of the flight series of the aircraft, mapping (102 1 ) at least one part of each time signal with a predetermined flight phase of a set of predetermined flight phases comprising at least one predetermined flight phase; characterised in that it comprises the step of: - for each blade , for each flight of said flight series of the aircraft, and for each predetermined flight phase, measuring (102 2 ) a first position of interest (PI1; PI1a; PI1b; PI1c) equal to the average position of the apex of the blade, called a balance position, the average position of the apex of the blade being the temporally averaged position of this point of the blade. - acquiring (101 1 ) at least one time signal, each time signal relating to passage time instants of the blades of the vane wheel in front of a sensor ; and - determining (101 2 ) a current flight phase of the aircraft; - for each flight of the flight series of the aircraft, mapping (102 1 ) at least one part of each time signal with a predetermined flight phase of a set of predetermined flight phases comprising at least one predetermined flight phase; characterised in that it comprises the step of: - for each blade , for each flight of said flight series of the aircraft, and for each predetermined flight phase, measuring (102 2 ) a first position of interest (PI1; PI1a; PI1b; PI1c) equal to the average position of the apex of the blade, called a balance position, the average position of the apex of the blade being the temporally averaged position of this point of the blade. - for each blade , for each flight of said flight series of the aircraft, and for each predetermined flight phase, measuring (102 2 ) a first position of interest (PI1; PI1a; PI1b; PI1c) equal to the average position of the apex of the blade, called a balance position, the average position of the apex of the blade being the temporally averaged position of this point of the blade.
Aircraft , provided with a buoyancy system , said buoyancy system including a plurality of floats , each float comprising a casing that separates an internal space (INT) of the float from an external environment (EXT), such that at least one of said floats is a luminous float , characterised in that the luminous float comprises at least one internal light source arranged in said internal space (INT) of this luminous float , said casing of a luminous float being at least partially translucent.
An air conditioning apparatus that includes an indoor heat exchanger and is configured to allow the indoor heat exchanger to function as a radiator for refrigerant and perform a heating operation, comprising: a distributor including: a distributor body positioned in the neighborhood of a refrigerant outlet of the indoor heat exchanger functioning as a radiator; and a plurality of distribution pipes branching from the distributor body and each connected to one of a plurality of refrigerant paths (P) formed in the indoor heat exchanger ; and a temperature sensor configured to detect a saturation temperature of refrigerant flowing through the indoor heat exchanger , wherein the temperature sensor is mounted above a height-wise center of the indoor heat exchanger in use state or the distributor body , characterized in that on a particular path, among the plurality of refrigerant paths (P), to which the temperature sensor is mounted, the temperature sensor is mounted to a gas-side end side of the particular path, with respect to a flow of refrigerant flowing through the particular path. a distributor including: a distributor body positioned in the neighborhood of a refrigerant outlet of the indoor heat exchanger functioning as a radiator; and a plurality of distribution pipes branching from the distributor body and each connected to one of a plurality of refrigerant paths (P) formed in the indoor heat exchanger ; and a distributor body positioned in the neighborhood of a refrigerant outlet of the indoor heat exchanger functioning as a radiator; and a plurality of distribution pipes branching from the distributor body and each connected to one of a plurality of refrigerant paths (P) formed in the indoor heat exchanger ; and a temperature sensor configured to detect a saturation temperature of refrigerant flowing through the indoor heat exchanger , wherein the temperature sensor is mounted above a height-wise center of the indoor heat exchanger in use state or the distributor body , characterized in that on a particular path, among the plurality of refrigerant paths (P), to which the temperature sensor is mounted, the temperature sensor is mounted to a gas-side end side of the particular path, with respect to a flow of refrigerant flowing through the particular path.
An improved Cell-Permeable (iCP)-SOCS3 recombinant protein, which comprises a SOCS3 protein and an advanced macromolecule transduction domain (aMTD) being fused to one end or both ends of the SOCS3 protein and having improved cell and/or tissue permeability, wherein the aMTD has an amino acid sequence of SEQ ID NO: 122.