mhurhangee/patent-ind-claim-en huggingface dataset:
A catheter assembly comprising: a catheter sub-assembly comprising a gripping member and a catheter tube carried by said gripping member , said catheter sub-assembly having a central longitudinal axis , said catheter tube defining a flow path and being angularly adjustable relative to said axis , said gripping member having a distal end and an aperture in said distal end, wherein said gripping member includes a notch at or near said proximal end of said gripping member configured for receiving and retaining said catheter tube in an angularly adjusted position relative to said axis .
A compound of Formula I: or a pharmaceutically acceptable salt thereof, wherein: L-Ar is Ar is R 1 is H, -CN, halogen, C 1 -C 4 alkyl, -O-(C 3 -C 5 cycloalkyl), -O-(4- to 6-membered heterocycle) or -O-(C 1 -C 4 alkyl), wherein when R 1 is not H, -CN or halogen, R 1 is optionally substituted with one or more halogen; each R 2 is independently hydrogen, halogen or C 1 -C 4 alkyl; R 3 is H or F; R 21 is H, halogen, C 1 -C 4 alkyl, C 3 -C 5 cycloalkyl or 4- to 6-membered heterocycle; R 22 is H, halogen or C 1 -C 2 alkyl; R 24 is -O-(C 1 -C 4 alkyl)-O-(C 1 -C 4 alkyl), -O-(C 3 -C 5 cycloalkyl), or -O-(4- to 6-membered heterocycle), wherein R 24 is substituted with one or more hydroxyl or halogen; or R 24 is -O-(C 1 -C 4 alkyl) substituted with one or more hydroxyl; and R 25 is H, halogen, C 1 -C 4 alkyl or C 3 -C 5 cycloalkyl, wherein R 25 is optionally substituted with one or more halogen. or a pharmaceutically acceptable salt thereof, wherein: L-Ar is Ar is R 1 is H, -CN, halogen, C 1 -C 4 alkyl, -O-(C 3 -C 5 cycloalkyl), -O-(4- to 6-membered heterocycle) or -O-(C 1 -C 4 alkyl), wherein when R 1 is not H, -CN or halogen, R 1 is optionally substituted with one or more halogen; each R 2 is independently hydrogen, halogen or C 1 -C 4 alkyl; R 3 is H or F; R 21 is H, halogen, C 1 -C 4 alkyl, C 3 -C 5 cycloalkyl or 4- to 6-membered heterocycle; R 22 is H, halogen or C 1 -C 2 alkyl; R 24 is -O-(C 1 -C 4 alkyl)-O-(C 1 -C 4 alkyl), -O-(C 3 -C 5 cycloalkyl), or -O-(4- to 6-membered heterocycle), wherein R 24 is substituted with one or more hydroxyl or halogen; or R 24 is -O-(C 1 -C 4 alkyl) substituted with one or more hydroxyl; and R 25 is H, halogen, C 1 -C 4 alkyl or C 3 -C 5 cycloalkyl, wherein R 25 is optionally substituted with one or more halogen.
Gasoline fuel composition suitable for use in an internal combustion engine comprising: (a) Fischer-Tropsch derived naphtha at a level from 2 to 20 % v/v, wherein the Fischer-Tropsch derived naphtha is a liquid hydrocarbon distillate with a final boiling point of up to 220°C and an initial boiling point of at least 25°C and which comprises at least 95% w/w of hydrocarbons having 5 or more carbon atoms and wherein the Fischer-Tropsch derived naphtha consists of at least 90% w/w of paraffinic components and has a Research Octane Number (RON), as measured by ASTM D2699, of at most 40; (b) at least one aromatic octane booster present at a level of 0.75 to 8% v/v, wherein the aromatic octane booster is selected from aromatic amines, phenols, and mixtures thereof; and (c) a gasoline base fuel; wherein the gasoline fuel composition comprises 40% v/v or less of aromatics and comprises an increase in RON compared to the RON of the gasoline base fuel (c). (a) Fischer-Tropsch derived naphtha at a level from 2 to 20 % v/v, wherein the Fischer-Tropsch derived naphtha is a liquid hydrocarbon distillate with a final boiling point of up to 220°C and an initial boiling point of at least 25°C and which comprises at least 95% w/w of hydrocarbons having 5 or more carbon atoms and wherein the Fischer-Tropsch derived naphtha consists of at least 90% w/w of paraffinic components and has a Research Octane Number (RON), as measured by ASTM D2699, of at most 40; (b) at least one aromatic octane booster present at a level of 0.75 to 8% v/v, wherein the aromatic octane booster is selected from aromatic amines, phenols, and mixtures thereof; and (c) a gasoline base fuel;
A cutting mill for cutting up samples with a cutting rotor , comprising: a device housing ; a drive motor for driving the cutting rotor for rotation; a grinding chamber with the cutting rotor arranged therein for cutting and comminuting the samples in the grinding chamber , with the cutting rotor defining an axis of rotation (A) and the grinding chamber being delimited axially, on the motor side, by a grinding chamber rear wall ; wherein the device housing comprises a sealing lid on the side of the cutting rotor axially opposite the grinding chamber rear wall , which lid can be opened to open the grinding chamber , wherein the sealing lid comprises a support bearing element for the cutting rotor ; characterized by comprising a first labyrinth seal on the side of the sealing lid . a device housing ; a drive motor for driving the cutting rotor for rotation; a grinding chamber with the cutting rotor arranged therein for cutting and comminuting the samples in the grinding chamber , with the cutting rotor defining an axis of rotation (A) and the grinding chamber being delimited axially, on the motor side, by a grinding chamber rear wall ; wherein the device housing comprises a sealing lid on the side of the cutting rotor axially opposite the grinding chamber rear wall , which lid can be opened to open the grinding chamber , wherein the sealing lid comprises a support bearing element for the cutting rotor ;
A method of wireless communications, comprising: receiving , by a user plane of a base station from a control plane of the base station , a quality of service, QoS, update, wherein the QoS update includes information indicative of a mapping between a QoS flow and a corresponding radio resource for user data transmission, and one or more quality of service flow identities, QFIs, for one or more quality of service, QoS, flows that are non-access stratum, NAS, reflective, and wherein the QoS update is received in response to the QoS flow and the corresponding radio resource that are remapped by the control plane of the base station; storing , at the user plane, the information from the QoS update; receiving , by the user plane, a downlink data packet of the QoS flow from a core network, wherein the downlink data packet comprises a quality of service flow identity, QFI; performing a determination, by the user plane, that the QFI is same as one of the one or more QFIs that are NAS reflective; and transmitting, by the user plane, the downlink data packet of the QoS flow on the corresponding radio resource, wherein the downlink data packet is transmitted with the QFI in the downlink data packet in response to the determination. receiving , by a user plane of a base station from a control plane of the base station , a quality of service, QoS, update, wherein the QoS update includes information indicative of a mapping between a QoS flow and a corresponding radio resource for user data transmission, and one or more quality of service flow identities, QFIs, for one or more quality of service, QoS, flows that are non-access stratum, NAS, reflective, and wherein the QoS update is received in response to the QoS flow and the corresponding radio resource that are remapped by the control plane of the base station; storing , at the user plane, the information from the QoS update; receiving , by the user plane, a downlink data packet of the QoS flow from a core network, wherein the downlink data packet comprises a quality of service flow identity, QFI; performing a determination, by the user plane, that the QFI is same as one of the one or more QFIs that are NAS reflective; and transmitting, by the user plane, the downlink data packet of the QoS flow on the corresponding radio resource, wherein the downlink data packet is transmitted with the QFI in the downlink data packet in response to the determination.
A DNA aptamer that binds to a vWF protein, having at least one of improved binding ability, improved dissociation rate, and improved stability compared to the nucleotide sequence as shown in SEQ ID NO: 10, the aptamer comprising any of the nucleotide sequences (i) - (ii) below: (i) the nucleotide sequence as shown in any of SEQ ID NOs: 1, 11 to 16 and 18 to 21; (ii) a nucleotide sequence in which one to four nucleotides are added, deleted, and/or substituted in the nucleotide sequence (i) at position(s) other than that of 7-(2-thienyl)-3H-imidazo[4,5-b]pyridin-3-yl. (i) the nucleotide sequence as shown in any of SEQ ID NOs: 1, 11 to 16 and 18 to 21; (ii) a nucleotide sequence in which one to four nucleotides are added, deleted, and/or substituted in the nucleotide sequence (i) at position(s) other than that of 7-(2-thienyl)-3H-imidazo[4,5-b]pyridin-3-yl.
An implantable medical device for defibrillating the heart of patient, comprising: - an energy storage device for providing a voltage, - at least one electrode , wherein the implantable medical device is configured to deliver an electrical current pulse through said electrode for a defibrillation shock by means of the voltage, characterized by - a short-circuit protection which is configured to be triggered in the event of a short-circuit of the at least one electrode and to interrupt or prevent delivery of an electrical current pulse for a defibrillation shock by said electrode, wherein the energy storage device for providing the voltage comprises at least two capacitors (Cl, C2), wherein, in the event of a short-circuit, the implantable medical device is configured to cause the delivery of a further current pulse for a defibrillation shock with reduced voltage from a parallel circuit of the at least two capacitors (Cl, C2) by said electrode. - an energy storage device for providing a voltage, - at least one electrode , wherein the implantable medical device is configured to deliver an electrical current pulse through said electrode for a defibrillation shock by means of the voltage, characterized by - a short-circuit protection which is configured to be triggered in the event of a short-circuit of the at least one electrode and to interrupt or prevent delivery of an electrical current pulse for a defibrillation shock by said electrode, wherein the energy storage device for providing the voltage comprises at least two capacitors (Cl, C2),
A solid form of 2-(4-chlorophenyl)-N-((2-(2,6-dioxopiperidin-3-yl)-1-oxoisoindolin-5-yl)methyl)-2,2-difluoroacetamide or a tautomer thereof, which is Form A having an X-ray powder diffraction pattern comprising peaks at about 15.6, 16.6, 17.2 or 24.8 degrees 2θ.
A quantum cascade laser element having a semiconductor superlattice structure sandwiched between a pair of electrodes , wherein the semiconductor superlattice structure has an active region that emits electromagnetic waves of a frequency in a THz region under an external voltage applied through the pair of electrodes for operation, the active region has plural unit structures , each of which is repeatedly layered over one another, each of the unit structures has a double quantum well structure formed of a first well layer (10W1) and a second well layer (10W2) separated from each other by a barrier layer (10B2), the first well layer (10W1) and the second well layer (10W2) have compositions different from each other, and when the external voltage is not being applied, potential energy for electrons in the second well layer (10W2) is less than that in the first well layer (10W1), characterized in that a thickness of the second well layer (10W2) has been reduced such that under the external voltage, the second well layer (10W2) has one thickness direction confinement level at most, the thickness direction confinement level having: a maximum value of probability of existence in the second well layer (10W2); and an energy value lower than potentials of two barrier layers (10B1, 10B2) sandwiching the second well layer (10W2).
A vitreous body cutter comprising: a pipe comprising an opening at one terminal end thereof, a cutter , which slides along an inner surface of the pipe , a power output section , which is connected to the pipe and slides the cutter , and an outer case , through which the pipe passes, and which comprises the power output section inside; further comprising a joint on the outer case configured to connect the outer case and a cannula which is attached to an eyeball ; wherein said connection by the joint and a cannula allows integrated movement of the cannula and the pipe when the outer case is moved while they are connected, and wherein the pipe, the cutter, and the power output section are configured to be shifted along the axis of the pipe relative to the outer case, wherein the protrusion length of the pipe from the outer case can be changed by shifting the pipe, the cutter, and the power output section. a pipe comprising an opening at one terminal end thereof, a cutter , which slides along an inner surface of the pipe , a power output section , which is connected to the pipe and slides the cutter , and an outer case , through which the pipe passes, and which comprises the power output section inside; further comprising a joint on the outer case configured to connect the outer case and a cannula which is attached to an eyeball ; wherein said connection by the joint and a cannula allows integrated movement of the cannula and the pipe when the outer case is moved while they are connected, and wherein the pipe, the cutter, and the power output section are configured to be shifted along the axis of the pipe relative to the outer case, wherein the protrusion length of the pipe from the outer case can be changed by shifting the pipe, the cutter, and the power output section.
A command method for an aircraft , comprising: • determining (S220) a flight regime of the aircraft , the flight regime determined from a set of flight regimes comprising: a forward regime and a hover regime; • receiving (S210) a set of input commands from a user at one or more input mechanisms , the set of input commands comprising: a first angular position on a first axis of the one or more input mechanisms and a second angular position on a second axis of the one or more input mechanisms; • based on the flight regime of the aircraft , mapping (S230) the set of input commands into a set of desired aircraft responses, wherein: • the first angular position maps to a desired pitch response in the forward regime and a desired vertical translation response in the hover regime; and • the second angular position maps to a desired speed response in the forward regime and a desired longitudinal translation response in the hover regime; • based on the set of desired aircraft responses, determining (S236) a control output; and • executing (S240) the control output by actuating a set of effectors of the aircraft , wherein the set of effectors comprises a rotor. • determining (S220) a flight regime of the aircraft , the flight regime determined from a set of flight regimes comprising: a forward regime and a hover regime; • receiving (S210) a set of input commands from a user at one or more input mechanisms , the set of input commands comprising: a first angular position on a first axis of the one or more input mechanisms and a second angular position on a second axis of the one or more input mechanisms; • based on the flight regime of the aircraft , mapping (S230) the set of input commands into a set of desired aircraft responses, wherein: • the first angular position maps to a desired pitch response in the forward regime and a desired vertical translation response in the hover regime; and • the second angular position maps to a desired speed response in the forward regime and a desired longitudinal translation response in the hover regime; • the first angular position maps to a desired pitch response in the forward regime and a desired vertical translation response in the hover regime; and • the second angular position maps to a desired speed response in the forward regime and a desired longitudinal translation response in the hover regime; • based on the set of desired aircraft responses, determining (S236) a control output; and • executing (S240) the control output by actuating a set of effectors of the aircraft , wherein the set of effectors comprises a rotor.
A silencer duct adapted for the intake duct of a gas turbine system, the duct comprising: a frame forming a working fluid flow path; a silencer panel ; and a plurality of silencer panel mounts positioned within the frame and configured to slidingly receive the silencer panel ; each silencer panel mount including: a pair of grooves in opposing relation on the frame , each groove including a closed end at a downstream end of the frame to axially position the silencer panel ; and at least one lock positioned upstream and separate from at least one of the pair of grooves , the lock configured to prevent removal of the silencer panel from a respective groove ; wherein the silencer panel includes a plurality of silencer panel sections , wherein each silencer panel section includes: an acoustic absorbing material ; a first enclosure surrounding the acoustic absorbing material ; and a first coupler configured to couple the first enclosure to a second enclosure of an adjacent silencer panel section . a frame forming a working fluid flow path; a silencer panel ; and a plurality of silencer panel mounts positioned within the frame and configured to slidingly receive the silencer panel ; each silencer panel mount including: a pair of grooves in opposing relation on the frame , each groove including a closed end at a downstream end of the frame to axially position the silencer panel ; and at least one lock positioned upstream and separate from at least one of the pair of grooves , the lock configured to prevent removal of the silencer panel from a respective groove ; a pair of grooves in opposing relation on the frame , each groove including a closed end at a downstream end of the frame to axially position the silencer panel ; and at least one lock positioned upstream and separate from at least one of the pair of grooves , the lock configured to prevent removal of the silencer panel from a respective groove ; wherein the silencer panel includes a plurality of silencer panel sections , wherein each silencer panel section includes: an acoustic absorbing material ; a first enclosure surrounding the acoustic absorbing material ; and a first coupler configured to couple the first enclosure to a second enclosure of an adjacent silencer panel section . an acoustic absorbing material ; a first enclosure surrounding the acoustic absorbing material ; and a first coupler configured to couple the first enclosure to a second enclosure of an adjacent silencer panel section .
A method of forming a carbon aerogel, comprising 3-D printing an ink to make a printed part, wherein the ink comprises solvent, a resorcinol-formaldehyde resin, and an organic thickener; removing the solvent from the printed part; and carbonizing the printed part to make the aerogel, wherein the resorcinol-formaldehyde resin comprises an acid catalyst and has a formaldehyde: resorcinol molar ratio greater than 1:1, wherein the thickener is soluble in water, is made of only C, H, and O atoms, and contains only ether or alcohol functional groups. 3-D printing an ink to make a printed part, wherein the ink comprises solvent, a resorcinol-formaldehyde resin, and an organic thickener; removing the solvent from the printed part; and carbonizing the printed part to make the aerogel, wherein the resorcinol-formaldehyde resin comprises an acid catalyst and has a formaldehyde: resorcinol molar ratio greater than 1:1, wherein the thickener is soluble in water, is made of only C, H, and O atoms, and contains only ether or alcohol functional groups.
An automated vertical plant cultivation system comprising: a magazine structure for plant cultivation comprising: at least one fluid channel extending between a double wall along a long axis of the magazine structure; a light source substantially concealed from direct view; and at least two seed or plant reservoirs adjacent each other, each seed or plant reservoir comprising a bottom surface and two side walls extending from said double wall for retaining a seed or plant capsule and in fluid communication with said at least one fluid channel , and each seed or plant reservoir comprising outer surface of the side walls , characterised in that one outer surface of each of the at least two adjacent seed or plant reservoirs form a reflector with an opening at an apex of the reflector wherein the light source extends into the reflector through the opening at the apex and conceals the light source , the light source illuminating plants below the light source . at least one fluid channel extending between a double wall along a long axis of the magazine structure; a light source substantially concealed from direct view; and at least two seed or plant reservoirs adjacent each other, each seed or plant reservoir comprising a bottom surface and two side walls extending from said double wall for retaining a seed or plant capsule and in fluid communication with said at least one fluid channel , and each seed or plant reservoir comprising outer surface of the side walls , characterised in that one outer surface of each of the at least two adjacent seed or plant reservoirs form a reflector with an opening at an apex of the reflector wherein the light source extends into the reflector through the opening at the apex and conceals the light source , the light source illuminating plants below the light source .
A liquid spray device comprising: a liquid spray head including a spray surface provided with a plurality of nozzles (N) that spray liquid to a medium ; a conveyance mechanism that includes an opposing surface opposite to the spray surface and conveys the medium in a first direction (Y) between the spray surface and the opposing surface; a plurality of supports arrayed in a second direction (X) which intersects with the first direction, the supports protruding from the opposing surface to support the medium being conveyed; and characterized by a plurality of protrusions protruding from the spray surface, and arrayed in the second direction (X), wherein the protrusions each have at least a part overlapping with a position other than a middle area between the supports adjacent to each other. a liquid spray head including a spray surface provided with a plurality of nozzles (N) that spray liquid to a medium ; a conveyance mechanism that includes an opposing surface opposite to the spray surface and conveys the medium in a first direction (Y) between the spray surface and the opposing surface; a plurality of supports arrayed in a second direction (X) which intersects with the first direction, the supports protruding from the opposing surface to support the medium being conveyed; and characterized by a plurality of protrusions protruding from the spray surface, and arrayed in the second direction (X), wherein the protrusions each have at least a part overlapping with a position other than a middle area between the supports adjacent to each other.
Conductor connection terminal for connecting electrical conductors to a busbar , the conductor connection terminal having an insulating material housing with at least two conductor insertion openings and a conductor connection space adjoining the conductor insertion openings , a busbar and a clamping spring for a spring-loaded clamping connection, and wherein the clamping spring has a clamping limb and a contact limb which are connected to one another by a spring bow , wherein the contact limb of the clamping spring has a separating section , by means of which the conductor connection space can be divided into at least two spatially separate conductor connection chambers , characterized in that the busbar has a recess on each connection side through which the contact limb is guided and is mounted on a support , wherein the contact limb is mounted on at least one clamping spring on the busbar and, starting from the spring bow behind the support of the contact limb on the busbar , has an elastic, deflectable spring section with a run-up slope for guiding the conductor to be connected.