mhurhangee/ep-ind-claims huggingface dataset:
A compound of formula (Ia') wherein: X 1 is C-R 11 or N, X 3 is C-R 13 or N, X 4 is C-R 14 or N, X 5 is C-R 15 or N, with the proviso that not more than one of X 1, X 3, X 4 and X 5 is N; X 6 is C-R 16 or N, X 7 is C-R 17 or N, X 8 is C-R 18 or N, X 9 is C-R 19 or N, with the proviso that not more than one of X 5, X 6, X 7, X 8 and X 9 is N; R 11, R 13, R 14, R 15, R 16, R 17, R 18 and R 19 are each individually selected from hydrogen, halogen, C 1-7 -alkyl, C 1-7 -haloalkyl and C 1-7 -alkoxy; R 1 is -(CH 2) m -NH 2; R 2 is -(CH 2) m -NH 2; R 3 is -(CH 2) m -heteroaryl optionally substituted with one or more halo, C 1-7 -alkyl, C 1-7 -haloalkyl or C 1-7 -alkoxy; m is 1, 2 or 3; n is 1, 2, 3, or 4; o is 1, 2, 3, or 4; or a pharmaceutically acceptable salt thereof. X 1 is C-R 11 or N, X 3 is C-R 13 or N, X 4 is C-R 14 or N, X 5 is C-R 15 or N, with the proviso that not more than one of X 1, X 3, X 4 and X 5 is N; X 6 is C-R 16 or N, X 7 is C-R 17 or N, X 8 is C-R 18 or N, X 9 is C-R 19 or N, with the proviso that not more than one of X 5, X 6, X 7, X 8 and X 9 is N; R 11, R 13, R 14, R 15, R 16, R 17, R 18 and R 19 are each individually selected from hydrogen, halogen, C 1-7 -alkyl, C 1-7 -haloalkyl and C 1-7 -alkoxy; R 1 is -(CH 2) m -NH 2; R 2 is -(CH 2) m -NH 2; R 3 is -(CH 2) m -heteroaryl optionally substituted with one or more halo, C 1-7 -alkyl, C 1-7 -haloalkyl or C 1-7 -alkoxy; m is 1, 2 or 3; n is 1, 2, 3, or 4; o is 1, 2, 3, or 4;
An air compressor that includes a main frame and a motor mounted to the main frame, said main frame comprising a cylinder fitted with a piston body, the motor being capable of driving the piston body to conduct reciprocating motion within the cylinder for producing compressed air, wherein: the cylinder has a first open wall, through which the piston body is fitted into the cylinder, and a second wall on the side opposite to the first open wall, the second wall being not fully closed, wherein the cylinder is provided with a first flange at its surrounding wall, adjacent to its second wall, the first flange has two opposite holding portions each defining a first recess; an air storage container has an open side and a closed side opposite to the open side and said air storage container defines therein an inner space terminating at the open side, wherein the air storage container comprises at least two outlets, one of which is connected with an elongated pressure indicator and another of which is connected with a hose having an air nozzle, characterized in that the air storage container comprises at its open side a second flange that has two opposite holding portions each defining a second recess; the air storage container is capable of being fitted over the cylinder and rotated about the cylinder to allow the second flange of the air storage container to slide in the first recesses of the cylinder and to allow the first flange of the cylinder to slide in the second recess of the air storage container, so that the air storage container is detachably mounted to the cylinder, thereby sealing the cylinder and defining an air chamber therebetween.
Conductive gripping element for retaining and conductively connecting electric wires (1, 1a) comprising a single body in the form of an overturned "U" with legs extending in the vertical direction (Z-Z) and head connecting in the transverse direction the top ends of the said legs, characterized in that the head of the "U" is cross-shaped with longitudinal arms and transverse arms and has a hole with a female thread, suitable for engagement with an actuating screw (2,2a), and a punched annular part whose thickness is partially comprised in the transverse direction (Y-Y) within the thickness of the legs of the "U" opposite a respective eyelet formed in the end of the leg adjacent to said head, and in that one of the two legs has a first lug folded in an L shape with side parallel to the vertical direction (Z-Z) and side folded parallel to the longitudinal direction (X-X).
Method for installing a support structure for a passenger transport system which is designed as an escalator or moving walkway, in a building, the support structure comprising a truss comprising interconnected load-bearing truss components including top chords, bottom chords, cross braces, diagonal braces and uprights, the method comprising: introducing a plurality of individual truss components having connecting openings formed therein at an installation position inside the building, assembling the truss at or near the installation position inside the building by interconnecting the truss components by means of load-bearing connector components, by in each case one connector component being arranged so as to pass through adjoining connecting openings of at least two adjacent truss components and then being deformed in terms of its outer geometry, the connector components being designed and, when the truss components are connected, being deformed such that they fill the connecting openings through which they pass completely and without play after the truss components are connected and they interlockingly interconnect the truss components in all spatial directions and position the truss components relative to one another when the truss components are connected, installing the assembled truss at prepared installation points of the building inside the building, characterized in that the truss components are interconnected in the following sequence during assembly of the truss: pre-installing H-frames by connecting in each case two uprights to at least one cross brace by means of the connector components; connecting the pre-installed H-frames to the top chords and the bottom chords in each case by means of the connector components; inserting and connecting the diagonal braces by means of the connector components. pre-installing H-frames by connecting in each case two uprights to at least one cross brace by means of the connector components; connecting the pre-installed H-frames to the top chords and the bottom chords in each case by means of the connector components; inserting and connecting the diagonal braces by means of the connector components.
Liquid tank for holding liquid in a motor vehicle, with: a liquid tank shell, which encloses an interior of the liquid tank for receiving liquid, wherein the liquid tank shell is formed from a plastic, wherein an antimicrobial agent is embedded within the plastic, wherein the plastic is penetrable by the antimicrobial agent; and wherein the plastic is adapted to deliver the embedded antimicrobial agent to a liquid in the interior of the liquid tank by diffusion, and wherein the plastic of the liquid tank shell has small pores through which the antimicrobial agent, which is embedded in the plastic, can penetrate in the course of a diffusion process, so that the plastic is penetrable by the antimicrobial agent. a liquid tank shell, which encloses an interior of the liquid tank for receiving liquid, wherein the liquid tank shell is formed from a plastic, wherein an antimicrobial agent is embedded within the plastic, wherein the plastic is penetrable by the antimicrobial agent; and wherein the plastic is adapted to deliver the embedded antimicrobial agent to a liquid in the interior of the liquid tank by diffusion, and wherein the plastic of the liquid tank shell has small pores through which the antimicrobial agent, which is embedded in the plastic, can penetrate in the course of a diffusion process, so that the plastic is penetrable by the antimicrobial agent.
A refrigerator oil composition comprising a base oil which is at least one member selected from mineral oils and synthetic oils, at least one imide compound selected from nonylphthalimide, laurylglutarimide, nonylsuccinic acid bisimide and 2,2'bis(3-(2-lauryl)succinimino)diethylamine in an amount of 0.01 to 5 % by mass based on the total amount of the refrigerator oil composition.
A saddle, particularly for cycles, motorcycles and quadricycles, which is constituted by: a rigid shell; a respective covering; means of connection of said shell to a frame; and at least one stratified insert that is integral with said covering, said at least one insert being arranged in the rear portion of said saddle at the points that support the right and left ischial bones of the user, said at least one insert comprising two layers, a first layer made of polyester or silicone material and a second layer made of polyvinyl chloride, said at least one insert (4a, 4b) being two in number and being arranged asymmetrically in the rear portion of said saddle. a rigid shell; a respective covering; means of connection of said shell to a frame; and at least one stratified insert that is integral with said covering, said at least one insert being arranged in the rear portion of said saddle at the points that support the right and left ischial bones of the user, said at least one insert comprising two layers, a first layer made of polyester or silicone material and a second layer made of polyvinyl chloride, said at least one insert (4a, 4b) being two in number and being arranged asymmetrically in the rear portion of said saddle.
A gas turbine engine comprising: a main fan delivering air into a bypass duct and into a core engine; a heat exchanger positioned within said bypass duct, and in the path of said air delivered by said main fan into said bypass duct, said heat exchanger receiving a fluid to be cooled from a component associated with the gas turbine engine; a heat exchanger fan positioned to draw air in said bypass duct across said heat exchanger and a control for said heat exchanger fan, said control being programmed to stop operation of the heat exchanger fan during certain conditions, and to drive the heat exchanger fan under other conditions; wherein said control commands a motor to drive the heat exchanger fan under high heat load conditions; wherein said high heat load conditions at least include takeoff of an associated aircraft; wherein said control commanding said motor to turn off said heat exchanger fan under low heat load conditions, and preferably wherein said low heat load conditions include a cruise condition of an associated aircraft; wherein said motor is positioned within a space of a fairing such that it is out of a path of air downstream of said heat exchanger fan. a main fan delivering air into a bypass duct and into a core engine; a heat exchanger positioned within said bypass duct, and in the path of said air delivered by said main fan into said bypass duct, said heat exchanger receiving a fluid to be cooled from a component associated with the gas turbine engine; a heat exchanger fan positioned to draw air in said bypass duct across said heat exchanger and a control for said heat exchanger fan, said control being programmed to stop operation of the heat exchanger fan during certain conditions, and to drive the heat exchanger fan under other conditions; wherein said control commands a motor to drive the heat exchanger fan under high heat load conditions; wherein said high heat load conditions at least include takeoff of an associated aircraft; wherein said control commanding said motor to turn off said heat exchanger fan under low heat load conditions, and preferably wherein said low heat load conditions include a cruise condition of an associated aircraft; wherein said motor is positioned within a space of a fairing such that it is out of a path of air downstream of said heat exchanger fan.
Circular loom for weaving a weaving core with at least one shuttle, which has a weft thread spool and is movable along a circular orbit path around the weaving core, with at least one stationarily arranged warp spool device, which has a warp thread spool which is arranged essentially in a lengthening of the radial extent of the circular orbit path, where at least one guide device, designed to guide at least one warp thread provided from a warp thread spool of a warp spool device is provided, which is movably arranged or designed outside a track plane enclosed by the outer circumference of the circular orbit path and has at least one positioning part, movably arranged or designed parallel to the weaving axis of the circular loom, with at least one thread guide element, where the warp thread spool of the warp spool device is arranged essentially in a straight and hence deflection-free extension of the running path of the warp thread through the thread guide element and where only the guided warp thread, crossing the track plane, passes through a recess in the circular orbit path.
A method of making a cleated plate member for an article of footwear comprising: forming a blade cleat assembly having an anchor member molded with a blade member, the blade member having a planar body, the body having a planar base portion, a planar head portion opposite the base portion, a pair of opposing flange portions (404, 405), and a through hole (306, 406) formed through the blade member, a first molding material of the anchor member surrounding the base portion of the blade member and the pair of opposing flange portions (404, 405), and extending through the through hole (306, 406) formed in the blade member through the blade member from one side of the blade member to the other side of the blade member; and molding the blade cleat assembly with an exposed surface of a plate body to form a cleated plate member, a portion of the blade member extending out from the exposed surface of the plate body. forming a blade cleat assembly having an anchor member molded with a blade member, the blade member having a planar body, the body having a planar base portion, a planar head portion opposite the base portion, a pair of opposing flange portions (404, 405), and a through hole (306, 406) formed through the blade member, a first molding material of the anchor member surrounding the base portion of the blade member and the pair of opposing flange portions (404, 405), and extending through the through hole (306, 406) formed in the blade member through the blade member from one side of the blade member to the other side of the blade member; and molding the blade cleat assembly with an exposed surface of a plate body to form a cleated plate member, a portion of the blade member extending out from the exposed surface of the plate body.
A method of forming a component of an article of footwear, the method comprising: placing an element configured to be maintained in a relative position by one or more fiber layers as a fiber-bound element, the element being a snap, a button, a zipper, a hook and loop structure, tubing, a ring, a grommet, an electrical sensor, an electrical transmission element, a fiber optic, a bladder, a tread element or a traction element and the element having an impervious portion adjacent and overlapping a first fiber layer in a first Z-directional placement, the first fiber layer comprising a first plurality of fibers, the element having a first part that is adjacent the first fiber layer and a second part; placing a second fiber layer comprising a second plurality of fibers adjacent and overlapping the second part of the element in a second Z-directional placement; entangling at least a portion of the first plurality of fibers and at least a portion of the second plurality of fibers such that at least part of the element is encased within an encasement volume defined by the entangled fibers to fiber-bind the element; and removing at least a portion of the entangled fibers to expose one or more portions of the element, wherein the entangling is performed with a fluid stream, and wherein the impervious portion of the element is a portion through which fibers do not extend as a result of the entanglement process.
A composite material blank comprising an elongate blank body extending between a first end face and a second end face; said blank body extending in a longitudinal direction, parallel to a longitudinal axis thereof, and having four peripheral side faces (341, 342, 343, 344); each said first and second end face (312a, 312b) having edges (361a-364a; 361b-364b) which define a trapezoid shape; wherein the peripheral side faces (341, 342, 343, 344) of said blank body connect the edges (361a-364a) of said first end face with the edges (361b-364b) of said second end face; Z r characterised in that said first trapezoid end face is inverted in relation to said second trapezoid end face. said blank body extending in a longitudinal direction, parallel to a longitudinal axis thereof, and having four peripheral side faces (341, 342, 343, 344); each said first and second end face (312a, 312b) having edges (361a-364a; 361b-364b) which define a trapezoid shape; wherein the peripheral side faces (341, 342, 343, 344) of said blank body connect the edges (361a-364a) of said first end face with the edges (361b-364b) of said second end face; Z r characterised in that said first trapezoid end face is inverted in relation to said second trapezoid end face.
A method performed by a user equipment for performing preamble transmissions on a random access channel to a network node, the method comprising: receiving a system frame number, SFN, from the network node; receiving a random access channel configuration from the network node; determining a number of times, R, a preamble transmission is to be repeated; determining a starting subframe for the preamble transmission(s) based at least on the received SFN, the received random access channel configuration, and the determined number of times, R, the preamble transmission is to be repeated; and transmitting, to the network node, the preamble repeatedly starting in the determined starting subframe. receiving a system frame number, SFN, from the network node; receiving a random access channel configuration from the network node; determining a number of times, R, a preamble transmission is to be repeated; determining a starting subframe for the preamble transmission(s) based at least on the received SFN, the received random access channel configuration, and the determined number of times, R, the preamble transmission is to be repeated; and transmitting, to the network node, the preamble repeatedly starting in the determined starting subframe.
Method for determining a characteristic value of a magnetic switch valve, which can be switched from a first switch state into a second switch state by movement of a rotor by means of a switching magnet to which current is applied, against a conservative restoring force, wherein the first switch state is either a closed switch state or an open switch state and the second switch state is correspondingly either the open switch state or the closed switch state and wherein the the characteristic value belongs to a group, comprising: • the time required for switching the switch valve from the second switch state into the first switch state, • the spring constant of the restoring force, • the coefficient of friction effective during the valve actuation and • the switching path, which the rotor covers when switching between the first and the second state, wherein during the switching of the switch valve from the second into the first state, the time course of the current flowing through the switching magnet and/or of the voltage at the switching magnet is measured, and the characteristic value is evaluated from this time course, characterized in that the time attenuation course is determined with which the potential energy stored in the magnetic circuit formed by the rotor and the switching magnet against the restoring force in the case of the position of the rotor fixed in the second and/or first state is dissipated in the ohmic resistor of the magnetic circuit, and in that the stored potential energy is evaluated as an integral over the attenuation course for the second state between a first point in time, at which the rotor begins to move by means of the restoring force when switching from the second into the first state, and a second point in time, at which the rotor first strikes the end position thereof during said switching. • the time required for switching the switch valve from the second switch state into the first switch state, • the spring constant of the restoring force, • the coefficient of friction effective during the valve actuation and • the switching path, which the rotor covers when switching between the first and the second state, wherein during the switching of the switch valve from the second into the first state, the time course of the current flowing through the switching magnet and/or of the voltage at the switching magnet is measured, and the characteristic value is evaluated from this time course, characterized in that the time attenuation course is determined with which the potential energy stored in the magnetic circuit formed by the rotor and the switching magnet against the restoring force in the case of the position of the rotor fixed in the second and/or first state is dissipated in the ohmic resistor of the magnetic circuit, and in that the stored potential energy is evaluated as an integral over the attenuation course for the second state between a first point in time, at which the rotor begins to move by means of the restoring force when switching from the second into the first state, and a second point in time, at which the rotor first strikes the end position thereof during said switching.
A lipid-modified double-stranded RNA comprising a sense strand having a nucleotide sequence complementary to a target sequence in a target gene, and an antisense strand having a nucleotide sequence complementary to the sense strand, the double-stranded RNA being capable of suppressing expression of the target gene, and the sense strand having a double-stranded lipid bound directly or via a linker to at least one of the first to sixth nucleotides from the 5' end, wherein the double-stranded lipid is phosphatidylethanolamine.
A method for configuring a transponder for a vehicle access device, comprising: deriving a signature from a physical unclonable function of the transponder by the transponder; verifying said signature by the transponder, generating an enable signal by the transponder in dependence on the result of verifying the signature, and proceeding to authenticate to a base station if the enable signal indicates a positive verification result; and transmitting the signature by the transponder to the base station and verifying said signature by the base station; and initiating by the base station a key training sequence between the base station and the transponder if the signature is valid and if the authentication between the base station and the transponder is successful. deriving a signature from a physical unclonable function of the transponder by the transponder; verifying said signature by the transponder, generating an enable signal by the transponder in dependence on the result of verifying the signature, and proceeding to authenticate to a base station if the enable signal indicates a positive verification result; and transmitting the signature by the transponder to the base station and verifying said signature by the base station; and initiating by the base station a key training sequence between the base station and the transponder if the signature is valid and if the authentication between the base station and the transponder is successful.