mhurhangee/patent-ind-claim-en huggingface dataset:
An aircraft comprising: a fuselage ; a support bearing coupled to the fuselage ; a rotor shaft attached to the fuselage by the support bearing , wherein the rotor shaft can rotate about a first axis extending through the rotor shaft , and the support bearing always allows the rotor shaft to rotate about said first axis and relative to the fuselage ; a rotor blade coupled to the rotor shaft , such that rotation of the rotor shaft causes the rotor blade to rotate about said first axis; a thrust support structure coupled to the rotor shaft ; and an engine coupled to the thrust support structure ; wherein: the engine is configured to cause the thrust support structure to rotate about said first axis; rotation of the thrust support structure causes the rotor shaft to rotate about said first axis, which in turn causes the rotor blade to rotate about said first axis; and the support bearing isolates the fuselage from torque generated by rotation of at least the rotor blade ; characterized in that the thrust support structure comprises at least one duct and a distal end comprising an opening; the at least one duct is to receive a thrust air flow generated by the engine and convey the airflow to the opening; the thrust air flow has a first temperature T1; the engine is further configured to produce a compressor bleed air flow having a second temperature T2, wherein T2 is less than T1 for mixing the compressor bleed air flow with the thrust air flow. a fuselage ; a support bearing coupled to the fuselage ; a rotor shaft attached to the fuselage by the support bearing , wherein the rotor shaft can rotate about a first axis extending through the rotor shaft , and the support bearing always allows the rotor shaft to rotate about said first axis and relative to the fuselage ; a rotor blade coupled to the rotor shaft , such that rotation of the rotor shaft causes the rotor blade to rotate about said first axis; a thrust support structure coupled to the rotor shaft ; and an engine coupled to the thrust support structure ; the engine is configured to cause the thrust support structure to rotate about said first axis; rotation of the thrust support structure causes the rotor shaft to rotate about said first axis, which in turn causes the rotor blade to rotate about said first axis; and the support bearing isolates the fuselage from torque generated by rotation of at least the rotor blade ; the thrust support structure comprises at least one duct and a distal end comprising an opening; the at least one duct is to receive a thrust air flow generated by the engine and convey the airflow to the opening; the thrust air flow has a first temperature T1; the engine is further configured to produce a compressor bleed air flow having a second temperature T2, wherein T2 is less than T1 for mixing the compressor bleed air flow with the thrust air flow.
A method of receiving a physical downlink control channel, PDCCH, by a terminal in a wireless communication system, the method comprising: receiving (S1405), from a base station , configuration information, via a radio resource control, RRC, signaling, wherein Quasi-co-location, QCL, information for a spatial parameter between (i) a channel state information reference signal, CSI-RS, and antenna port of PDCCH demodulation reference signal, DM-RS, or (ii) a synchronization signal, SS, block and the antenna port of PDCCH DM-RS are configured based on the configuration information; receiving (S1410), from the base station , information for a specific QCL information among the QCL information, via Medium Access Control-Control Element, MAC-CE, signaling; and receiving (S1415), from the base station , the PDCCH based on the specific QCL information, wherein based on that the information via MAC-CE signaling is not received, a predetermined QCL information is used as the specific QCL information (S1420). receiving (S1405), from a base station , configuration information, via a radio resource control, RRC, signaling, wherein Quasi-co-location, QCL, information for a spatial parameter between (i) a channel state information reference signal, CSI-RS, and antenna port of PDCCH demodulation reference signal, DM-RS, or (ii) a synchronization signal, SS, block and the antenna port of PDCCH DM-RS are configured based on the configuration information; receiving (S1410), from the base station , information for a specific QCL information among the QCL information, via Medium Access Control-Control Element, MAC-CE, signaling; and receiving (S1415), from the base station , the PDCCH based on the specific QCL information, wherein based on that the information via MAC-CE signaling is not received, a predetermined QCL information is used as the specific QCL information (S1420).
A cell separation system comprising: a cartridge having a polygonal shape in cross section and comprising an injection part , a separation chip separating a flow channel of a sample injected through the injection part and being located downstream of the injection part to separate cancer cells, and a discharge part ; and a base plate coupled to the cartridge through its upper surface and comprising a magnetic chip for cancer cell capture, wherein the separation chip of the cartridge is separably coupled to the magnetic chip of the base plate , liquid sensors , and valves , and characterized in that: the discharge part , the liquid sensors , and the valves are provided downstream of the separation chip and the liquid sensors and the valves are located on an upper surface of the base plate to come into contact with discharge channels formed on a lower surface of the cartridge and serve to previously detect the inflow of air bubbles during discharge and adjust the flow of substances, wherein the channels of the discharge part of the cartridge are in contact with the liquid sensors and the valves when the cartridge is coupled to the base plate , wherein the separation chip comprises a top plate having holes into which pipes are insertable, each hole comprising a first portion having a larger diameter and a second portion having a smaller diameter, wherein the separation chip comprises a second member coupled to the top plate through a tape applied to the upper surface thereof and a first member located under the second member and coupled to the lower surface of the second member through a tape applied to the lower surface of the second member ; portions of the second member are cut-off to form channels in the second member ; the holes are formed so as to penetrate through the upper and lower surfaces of the top plate and to be in communication with the channels ; and the pipes are inserted into the first portions of the holes at acute angles to the upper surface of the top plate . wherein the separation chip comprises a top plate having holes into which pipes are insertable, each hole comprising a first portion having a larger diameter and a second portion having a smaller diameter, wherein the separation chip comprises a second member coupled to the top plate through a tape applied to the upper surface thereof and a first member located under the second member and coupled to the lower surface of the second member through a tape applied to the lower surface of the second member ; portions of the second member are cut-off to form channels in the second member ; the holes are formed so as to penetrate through the upper and lower surfaces of the top plate and to be in communication with the channels ; and the pipes are inserted into the first portions of the holes at acute angles to the upper surface of the top plate .
A bearing arrangement for a drive shaft of a turbo-machine , the bearing arrangement including a radial gas bearing configured to rotatably support the drive shaft , the radial gas bearing including a gas bearing sleeve (32.1) which is made in molybdenum or in a molybdenum alloy and which has a radial bearing surface configured to surround the drive shaft , characterized in that the radial gas bearing is a one-piece radial gas bearing, and in that the radial gas bearing includes a cooling part configured to dissipate heat from the radial gas bearing .
A synthetic resin container that is formed in a bottle shape having a mouth and a trunk and that is provided in the trunk with at least one reduced pressure absorbing panel , wherein the trunk has a density of 1.3695 g/cm 3 or more, characterized by that a ratio of a crystal orientation in a transverse direction with respect to a total value of a crystal orientation in a machine direction and the crystal orientation in the transverse direction in the trunk is less than 44%.
Nanoemulsion composition comprising: a) an internal phase comprising 40 to 75% by wt. of total nanoemulsion composition of oils selected from the group consisting of triglyceride, petrolatum and mixtures thereof, wherein the melting point of the petrolatum is 30 to 60°C; and (ii) 1 to 10% by wt. nanoemulsion of a C 8 to C 18 fatty acid; and b) an external aqueous phase comprising 1.6 to 15% by wt. (as active) of total nanoemulsion composition of a surfactant or surfactants which are N-acyl derivatives of amino acid salt; wherein the surfactant of (b) comprises 50% or greater of all surfactants present in said external aqueous phase of the nanoemulsion; wherein the volume average diameter of droplets of (a) is 20 to 400 nanometers. a) an internal phase comprising 40 to 75% by wt. of total nanoemulsion composition of oils selected from the group consisting of triglyceride, petrolatum and mixtures thereof, wherein the melting point of the petrolatum is 30 to 60°C; and (ii) 1 to 10% by wt. nanoemulsion of a C 8 to C 18 fatty acid; and b) an external aqueous phase comprising 1.6 to 15% by wt. (as active) of total nanoemulsion composition of a surfactant or surfactants which are N-acyl derivatives of amino acid salt; wherein the surfactant of (b) comprises 50% or greater of all surfactants present in said external aqueous phase of the nanoemulsion; wherein the volume average diameter of droplets of (a) is 20 to 400 nanometers.
An apparatus for delivering an annulus ring to the vicinity of an annulus , the apparatus comprising: an elongated core having (a) a distal end, (b) a main channel that runs through the core in a proximal-to-distal direction, and (c) at least four lumens that run through the core in a proximal-to-distal direction, each of the lumens being dimensioned to accommodate a respective pull wire ; at least four support arms mounted to the core that extend distally beyond the distal end of the core ; and at least four anchor launchers , each of the anchor launchers having a distal end, wherein each of the anchor launchers is supported by a respective one of the support arms ; a plurality of support rings , wherein the support arms are affixed to the support rings and extend in a distal direction from the support rings ; and a plurality of support rods that are affixed to the support rings , wherein the support rods extend in a proximal direction from the support rings , wherein the core has a plurality of support channels that run through the core in a proximal-to-distal direction and are dimensioned to accommodate the support rods , wherein the support arms are mounted to the core by inserting the support rods into the support channels, and wherein the support arms are configured to hold the distal ends of the anchor launchers at positions that correspond to a shape of the annulus , with the distal ends of the anchor launcher s distributed about a perimeter of the shape of the annulus . an elongated core having (a) a distal end, (b) a main channel that runs through the core in a proximal-to-distal direction, and (c) at least four lumens that run through the core in a proximal-to-distal direction, each of the lumens being dimensioned to accommodate a respective pull wire ; at least four support arms mounted to the core that extend distally beyond the distal end of the core ; and at least four anchor launchers , each of the anchor launchers having a distal end, wherein each of the anchor launchers is supported by a respective one of the support arms ; a plurality of support rings , wherein the support arms are affixed to the support rings and extend in a distal direction from the support rings ; and a plurality of support rods that are affixed to the support rings , wherein the support rods extend in a proximal direction from the support rings , wherein the core has a plurality of support channels that run through the core in a proximal-to-distal direction and are dimensioned to accommodate the support rods , wherein the support arms are mounted to the core by inserting the support rods into the support channels, and wherein the support arms are configured to hold the distal ends of the anchor launchers at positions that correspond to a shape of the annulus , with the distal ends of the anchor launcher s distributed about a perimeter of the shape of the annulus .
A wireless communication structure, comprising: a loop structure comprising a first connection end , a second connection end and a coil body , at least a part of the coil body being connected between the first connection end and the second connection end ; an antenna connected to the coil body , characterized in that the antenna comprises a non-millimeter-wave antenna , the non-millimeter-wave antenna comprises a non-millimeter-wave radiating portion and a non-millimeter-wave feeding portion , and the non-millimeter-wave radiating portion is connected to the coil body ; wherein the coil body is provided with one or more first blocking portions , the one or more first blocking portions are configured to allow wireless signal currents transmitted and/or received by the loop structure to pass through and block non-millimeter-wave wireless signal currents transmitted and/or received by the non-millimeter-wave antenna , wherein the antenna further comprises one or more millimeter-wave antenna units , and the one or more millimeter-wave antenna units are connected to the coil body . a loop structure comprising a first connection end , a second connection end and a coil body , at least a part of the coil body being connected between the first connection end and the second connection end ; an antenna connected to the coil body , characterized in that the antenna comprises a non-millimeter-wave antenna , the non-millimeter-wave antenna comprises a non-millimeter-wave radiating portion and a non-millimeter-wave feeding portion , and the non-millimeter-wave radiating portion is connected to the coil body ; wherein the coil body is provided with one or more first blocking portions , the one or more first blocking portions are configured to allow wireless signal currents transmitted and/or received by the loop structure to pass through and block non-millimeter-wave wireless signal currents transmitted and/or received by the non-millimeter-wave antenna , wherein the antenna further comprises one or more millimeter-wave antenna units , and the one or more millimeter-wave antenna units are connected to the coil body .
A system to regulate the internal temperature of a power source port , comprising: a connector electrically interconnecting the power source port and a power sink port ; an output control routing a power supply output to the connector ; a port controller having a plurality of source capabilities lists stored thereon in a non-transitory digital medium, each list identifying a different set of power source port capabilities that, based on their power requirements, may be advertised over a power delivery communication channel to the power sink port ; one or more temperature sensors measuring the surface temperature of heat dissipating elements or the internal temperature of the power supply and communicating the measured temperature to a comparator ; and the comparator comparing the measured temperature to predefined limit temperatures, wherein when the measured temperature exceeds a predefined maximum limit temperature, the port controller advertises to the power sink port a source capabilities list with reduced electrical power to reduce internal temperatures and when the measured temperature is below a predefined minimum temperature, the port controller advertises to the power sink port a source capabilities list with increased electrical power thereby maximizing the electrical power available from the power source port . a connector electrically interconnecting the power source port and a power sink port ; an output control routing a power supply output to the connector ; a port controller having a plurality of source capabilities lists stored thereon in a non-transitory digital medium, each list identifying a different set of power source port capabilities that, based on their power requirements, may be advertised over a power delivery communication channel to the power sink port ; one or more temperature sensors measuring the surface temperature of heat dissipating elements or the internal temperature of the power supply and communicating the measured temperature to a comparator ; and the comparator comparing the measured temperature to predefined limit temperatures, wherein when the measured temperature exceeds a predefined maximum limit temperature, the port controller advertises to the power sink port a source capabilities list with reduced electrical power to reduce internal temperatures and when the measured temperature is below a predefined minimum temperature, the port controller advertises to the power sink port a source capabilities list with increased electrical power thereby maximizing the electrical power available from the power source port .
A composition for use as a shampoo for treatment or removal of blood-sucking insects, comprising: between 10-60% of water by weight based upon the weight of the total composition; between 5-50% of a diethanolamide mixture by weight based upon the weight of the total composition, wherein the diethanolamide mixture comprises an amide content that is at least 80% by weight based upon the weight of the diethanolamide mixture, an at least one esterified fatty acid content that is between 8-15% by weight based upon the weight of the diethanolamide mixture, and a free amine content that is 1.5% or less by weight based upon the weight of the diethanolamide mixture; between 5-50% of polyethylene glycol by weight based upon the weight of the total composition; between 5-50% of at least one surfactant by weight based upon the weight of the total composition; between 5-35% of at least one alcohol by weight based upon the weight of the total composition; between 0.1-5% of at least one preservative by weight based upon the weight of the total composition; and at least one buffering agent, wherein the diethanolamide mixture is a coconut diethanolamide mixture, and wherein the at least one esterified fatty acid of the diethanolamide mixture comprises at least one esterified fatty acid from a coconut oil, and wherein the at least one esterified fatty acid is selected from any one of a fatty acid methyl ester, fatty acid ethyl ester, a fatty acid propyl ester, a fatty acid isopropyl ester, and a blend of one or more of a fatty acid methyl ester, a fatty acid ethyl ester, a fatty acid propyl ester, and a fatty acid isopropyl ester. between 10-60% of water by weight based upon the weight of the total composition; between 5-50% of a diethanolamide mixture by weight based upon the weight of the total composition, wherein the diethanolamide mixture comprises an amide content that is at least 80% by weight based upon the weight of the diethanolamide mixture, an at least one esterified fatty acid content that is between 8-15% by weight based upon the weight of the diethanolamide mixture, and a free amine content that is 1.5% or less by weight based upon the weight of the diethanolamide mixture; between 5-50% of polyethylene glycol by weight based upon the weight of the total composition; between 5-50% of at least one surfactant by weight based upon the weight of the total composition; between 5-35% of at least one alcohol by weight based upon the weight of the total composition; between 0.1-5% of at least one preservative by weight based upon the weight of the total composition; and at least one buffering agent, wherein the diethanolamide mixture is a coconut diethanolamide mixture, and wherein the at least one esterified fatty acid of the diethanolamide mixture comprises at least one esterified fatty acid from a coconut oil, and wherein the at least one esterified fatty acid is selected from any one of a fatty acid methyl ester, fatty acid ethyl ester, a fatty acid propyl ester, a fatty acid isopropyl ester, and a blend of one or more of a fatty acid methyl ester, a fatty acid ethyl ester, a fatty acid propyl ester, and a fatty acid isopropyl ester.
Single-track vehicle - having a display device (ANZ) and - having a control device (STE) which is set up and is coupled to the display device (ANZ) in such a manner - that at least a first display layout and a second display layout can be implemented by means of the display device (ANZ), - wherein the first display layout and the second display layout have at least one main display field (HAF), - wherein, in the case of switching to the first display layout, the current speed and/or the current engine speed and/or the current gear stage and/or a current desired speed of the single-track vehicle is/are displayed in the region of the main display field (HAF), and - wherein, in the case of switching to the second display layout, a plurality of menu items of a selection menu and/or information relating to comfort functions of the single-track vehicle is/are presented in the region of the main display field (HAF), characterized in that the single-track vehicle also comprises: - a capture device (SE) which interacts with the control device (STE) in such a manner that, in response to an output signal from the capture device (SE), there is a changeover from the first display layout to the second display layout and vice versa, wherein the capture device comprises a speed sensor and/or an acceleration sensor. - having a display device (ANZ) and - having a control device (STE) which is set up and is coupled to the display device (ANZ) in such a manner - that at least a first display layout and a second display layout can be implemented by means of the display device (ANZ), - wherein the first display layout and the second display layout have at least one main display field (HAF), - wherein, in the case of switching to the first display layout, the current speed and/or the current engine speed and/or the current gear stage and/or a current desired speed of the single-track vehicle is/are displayed in the region of the main display field (HAF), and - wherein, in the case of switching to the second display layout, a plurality of menu items of a selection menu and/or information relating to comfort functions of the single-track vehicle is/are presented in the region of the main display field (HAF), characterized in that the single-track vehicle also comprises: - a capture device (SE) which interacts with the control device (STE) in such a manner that, in response to an output signal from the capture device (SE), there is a changeover from the first display layout to the second display layout and vice versa, wherein the capture device comprises a speed sensor and/or an acceleration sensor. - a capture device (SE) which interacts with the control device (STE) in such a manner that, in response to an output signal from the capture device (SE), there is a changeover from the first display layout to the second display layout and vice versa, wherein the capture device comprises a speed sensor and/or an acceleration sensor.