mhurhangee/ep-ind-claims huggingface dataset:
Transport device for transporting transport materials in a transport direction, with at least one transport element (3, 3', 3", 40, 40') which is driven in a circulating manner and forms a closed loop, which, for the formation in each case of a closed loop, is guided at a front end (1.1) over a deflection device (4.1), configured as a deflection roller and arranged as rotatable on a machine frame (1.10) of the transport device, upstream in relation to the transport direction, and a deflection device (4.2), arranged at a rear end (1.2) in relation to the transport direction and configured as a deflection roller at the rear and rotatable on the machine frame (1.10) of the transport device, and forms a transport section for the transport material between the front and rear deflection device (4.1, 4.2) by means of the at least one transport element (3, 3', 3", 40, 40'), wherein, for driving the at least one transport element (3, 3', 3", 40, 40'), at least two drive devices (5, 5.1, 5.2) are provided, which are in operational connection with the at least one transport element (3, 3', 3", 40, 40') at a distance from one another at different locations along the transport section, wherein the at least one transport element (3', 3", 40, 40') comprises several rotationally movable transport element sections (41, 41') arranged such as to be movable in relation to one another, in such a way that, by means of a relative displacement movement of the individual transport element sections (41, 41') in relation to one another, the total length of the respective transport element (3', 3", 40, 40') can be changed, and wherein the transport section comprises at least two transport section parts (TSA, TSA1, TSA2), which in each case extend between two drive devices following one another in the transport direction, such that, by means of a specific controlled actuation of adjacent transport section parts with a differential speed, by means of the respective drive devices, an accumulation and/or gap formation of the respective transport materials located on this transport section part can be adjusted, and wherein, for the specific controlled actuation of the individual transport section parts (TSA, TSA1, TSA2) in relation to one another, the drive devices assigned in each case to the transport section parts (TSA, TSA1, TSA2) are connected to a control unit, and wherein a first two transport section parts extends from a first drive device (5.1) in the transport direction as far as a second drive device (5.2), characterised in that a second transport section parts extends from the second drive device (5.2) as far as the rear end (1.2) of the transport section, seen in the transport direction.
A compound of formula I: wherein n is selected from 0, 1, 2 and 3; R 1 is selected from: R 2 is selected from chloro, methyl, hydrogen, fluoro and methoxy; R 3a is selected from cyano-methyl, 2-hydroxy-ethyl, 1-hydroxypropan-2-yl, 3-hydroxy-2-(hydroxy-methyl)propanoyl, 2-methoxy-ethyl, 2-fluoropropanoyl, (3-methyloxetan-3-yl)-methyl, methyl-sulfonyl, amino-carbonyl-methyl, cyclopropyl-sulfonyl, isopropyl-sulfonyl, dimethylcarbamoyl, 3-hydroxy-2-(hydroxy-methyl)propyl, 2-hydroxypropyl, 2-hydroxyacetyl, 2-acetoxyacetyl, 2-methoxyacetyl, (2,2,2-trifluoroethyl)carbamoyl, 2-aminoacetyl, oxetan-3-ylmethyl, -2-hydroxypropanoyl, 2-hydroxypropanoyl, acetyl, 2-amino-2-oxoethyl, carbamoyl, (oxetan-2-yl)-methanoyl, 2-(sulfooxy)acetyl, 2-fluoroethanoyl, 3-hydroxypropanoyl, and N,N-dimethylsulfonamidyl; each R 4 is independently selected from hydrogen, halo, methyl and hydroxy-methyl; and optionally two R 4 groups together with the carbon atoms to which they are attached form -(CH 2) 2-3 -; R 5 is selected from hydrogen and methyl; R 6 is selected from hydrogen, methoxy and halo; R 7 is selected from hydrogen, fluoro, CF 3, CH 2 OH, cyclopropyl and methyl; and R 8 is cyano; or a pharmaceutically acceptable salt thereof. n is selected from 0, 1, 2 and 3; R 1 is selected from: R 2 is selected from chloro, methyl, hydrogen, fluoro and methoxy; R 3a is selected from cyano-methyl, 2-hydroxy-ethyl, 1-hydroxypropan-2-yl, 3-hydroxy-2-(hydroxy-methyl)propanoyl, 2-methoxy-ethyl, 2-fluoropropanoyl, (3-methyloxetan-3-yl)-methyl, methyl-sulfonyl, amino-carbonyl-methyl, cyclopropyl-sulfonyl, isopropyl-sulfonyl, dimethylcarbamoyl, 3-hydroxy-2-(hydroxy-methyl)propyl, 2-hydroxypropyl, 2-hydroxyacetyl, 2-acetoxyacetyl, 2-methoxyacetyl, (2,2,2-trifluoroethyl)carbamoyl, 2-aminoacetyl, oxetan-3-ylmethyl, -2-hydroxypropanoyl, 2-hydroxypropanoyl, acetyl, 2-amino-2-oxoethyl, carbamoyl, (oxetan-2-yl)-methanoyl, 2-(sulfooxy)acetyl, 2-fluoroethanoyl, 3-hydroxypropanoyl, and N,N-dimethylsulfonamidyl; each R 4 is independently selected from hydrogen, halo, methyl and hydroxy-methyl; and optionally two R 4 groups together with the carbon atoms to which they are attached form -(CH 2) 2-3 -; R 5 is selected from hydrogen and methyl; R 6 is selected from hydrogen, methoxy and halo; R 7 is selected from hydrogen, fluoro, CF 3, CH 2 OH, cyclopropyl and methyl; and R 8 is cyano;
Method of joining panels, in particular for pieces of furniture or holding trolleys, comprising at least one portion of lightweight material (102, 109) and at least one metallic half-shell (103, 110), characterized by: making of a first panel provided with a plurality of pins arranged perpendicularly to said first panel and having at least one threaded portion; making a second panel provided with a plurality of cavities obtained, in use, in positions corresponding to said plurality of pins; filling said plurality of cavities with a suitable glue; joining said first panel to said second panel at orthogonal planes by inserting said pins into said cavities; permanently fastening said first panel to said second panel through the solidification and gripping of said glue on the threaded portion of said plurality of pins and on the portions surrounding said cavity. making of a first panel provided with a plurality of pins arranged perpendicularly to said first panel and having at least one threaded portion; making a second panel provided with a plurality of cavities obtained, in use, in positions corresponding to said plurality of pins; filling said plurality of cavities with a suitable glue; joining said first panel to said second panel at orthogonal planes by inserting said pins into said cavities; permanently fastening said first panel to said second panel through the solidification and gripping of said glue on the threaded portion of said plurality of pins and on the portions surrounding said cavity.
A medical system, comprising: a medical device having a treatment element; and a control unit in communication with the medical device, the control unit being configured to: deliver a low-voltage, pre-treatment pulse routine through the treatment element to an area of target tissue, the low-voltage, pre-treatment pulse routine being configured to have a stimulation effect within an area of non-target tissue when the non-target tissue is within a predetermined distance from the area of target tissue and to not have a stimulation effect within the area of non-target tissue when the area of non-target tissue is outside of the predetermined distance from the area of target tissue; and deliver an ablation energy routine through the treatment element to the area of target tissue when the low-voltage pulse routine does not have a stimulation effect on the area of non-target tissue, wherein the low-voltage, pre-treatment pulse routine includes the delivery of energy having a voltage between 0.1 V and 100 V. a medical device having a treatment element; and a control unit in communication with the medical device, the control unit being configured to: deliver a low-voltage, pre-treatment pulse routine through the treatment element to an area of target tissue, the low-voltage, pre-treatment pulse routine being configured to have a stimulation effect within an area of non-target tissue when the non-target tissue is within a predetermined distance from the area of target tissue and to not have a stimulation effect within the area of non-target tissue when the area of non-target tissue is outside of the predetermined distance from the area of target tissue; and deliver an ablation energy routine through the treatment element to the area of target tissue when the low-voltage pulse routine does not have a stimulation effect on the area of non-target tissue, wherein the low-voltage, pre-treatment pulse routine includes the delivery of energy having a voltage between 0.1 V and 100 V. deliver a low-voltage, pre-treatment pulse routine through the treatment element to an area of target tissue, the low-voltage, pre-treatment pulse routine being configured to have a stimulation effect within an area of non-target tissue when the non-target tissue is within a predetermined distance from the area of target tissue and to not have a stimulation effect within the area of non-target tissue when the area of non-target tissue is outside of the predetermined distance from the area of target tissue; and deliver an ablation energy routine through the treatment element to the area of target tissue when the low-voltage pulse routine does not have a stimulation effect on the area of non-target tissue, wherein the low-voltage, pre-treatment pulse routine includes the delivery of energy having a voltage between 0.1 V and 100 V.
Aircraft seat device with a seat bottom unit which forms a basic structure of a seat bottom, the seat bottom unit comprising a front carrier accommodation and a rear carrier accommodation for a coupling to a mounting unit and comprising a receiving region for receiving a lifejacket module, the receiving region spanning a volume in which to arrange the lifejacket module that is to be transported or stowed, the seat bottom unit comprising at least one upper wall element forming at least one support surface for a comfort element and delimiting the receiving region towards an upper side of the seat bottom unit, at least one lower wall element delimiting the receiving region downwards and at least one side wall element (40, 42, 44) delimiting the receiving region sidewise in a horizontal plane, the receiving region being implemented substantially obliquely in a sitting direction, the receiving region extending from a rear, lower region towards a front end upwards, away from a mounting plane, the seat bottom unit comprising a removal opening for a removal of the lifejacket module from the receiving region, which is arranged at least partly between the upper wall element and the front carrier accommodation of the seat bottom unit.
Magnetic Resonance Imaging, MRI, method for improving an MRI signal generated by a magnetization of interest when imaging an object placed in an examination volume of an MRI system, the method comprising: - performing, by the MRI system, an MRI pulse sequence comprising three consecutive radio frequency, RF, elements, namely, a first element that is an inversion-recovery pulse sequence characterized by a time of inversion, a second element that is an image-encoding pulse sequence starting at said time of inversion with an excitation RF pulse followed by at least one image-encoding gradient and at least one data sampling, said second element being followed by a third element; - acquiring, by the MRI system, an MRI signal generated by said object and sampled by image readout blocks applied to said object by the MRI system during each repetition time; - reconstructing, from said MRI signal, an image of said object; the method being characterized in that the third element is a modified driven-equilibrium, mDE, pulse sequence configured for achieving a conversion of a transverse magnetization component of the magnetization of interest into positive longitudinal magnetization, aligned with positive z-axis and B0 field direction. - performing, by the MRI system, an MRI pulse sequence comprising three consecutive radio frequency, RF, elements, namely, a first element that is an inversion-recovery pulse sequence characterized by a time of inversion, a second element that is an image-encoding pulse sequence starting at said time of inversion with an excitation RF pulse followed by at least one image-encoding gradient and at least one data sampling, said second element being followed by a third element; - acquiring, by the MRI system, an MRI signal generated by said object and sampled by image readout blocks applied to said object by the MRI system during each repetition time; - reconstructing, from said MRI signal, an image of said object;
A process for manufacture of a fluoroelastomer composition containing fluoroplastic fibrils, said process comprising: A) applying shear to a fluoroelastomer gum in a mixer; and B) adding a liquid dispersion of fibrillatable fluoroplastic particles to said fluoroelastomer gum while applying shear in said mixer, thereby forming a fluoroelastomer composition containing fluoroplastic fibrils dispersed therein. A) applying shear to a fluoroelastomer gum in a mixer; and B) adding a liquid dispersion of fibrillatable fluoroplastic particles to said fluoroelastomer gum while applying shear in said mixer, thereby forming a fluoroelastomer composition containing fluoroplastic fibrils dispersed therein.
Method of producing a stacking projection inwardly protruding from a wall of a cup with the following steps: i) inserting a mandrel within the cup, which mandrel comprises a receiving recess at least open to the outer circumference of the mandrel, ii) supporting in particular a bottom part of the cup by a supporting tool; iii) assigning a collet to a region of the cup wall where the stacking projection is to be formed; iv) pressing at least a part of the collet radially inwardly in direction to the receiving recess such that a portion of the cup wall is pressed into the receiving recess to form said stacking projection; v) simultaneously to step iv) reducing the height of the cup by displacing the mandrel and/or the supporting tool with respect to the other in axial direction, and vi) releasing pressure applied to the collet and removing the cup with the mandrel from the collet and the supporting tool. i) inserting a mandrel within the cup, which mandrel comprises a receiving recess at least open to the outer circumference of the mandrel, ii) supporting in particular a bottom part of the cup by a supporting tool; iii) assigning a collet to a region of the cup wall where the stacking projection is to be formed; iv) pressing at least a part of the collet radially inwardly in direction to the receiving recess such that a portion of the cup wall is pressed into the receiving recess to form said stacking projection; v) simultaneously to step iv) reducing the height of the cup by displacing the mandrel and/or the supporting tool with respect to the other in axial direction, and vi) releasing pressure applied to the collet and removing the cup with the mandrel from the collet and the supporting tool.
An absorbent pad having a chassis comprising a liquid-permeable topsheet and a liquid-impermeable backsheet, wherein the absorbent pad is geometrically symmetrical along its longitudinal and transversal centre lines and wherein the absorbent pad is provided with attaching arrangements by which the pad can be releasably attached to a separate belt adapted to be placed around the waist of the user, characterized in that the absorbent pad further comprises an absorbent core interposed between the topsheet and the backsheet, which absorbent core is also geometrically symmetrical along the longitudinal and transversal centre lines of the pad and the absorbent core is divided into a first longitudinal half and a second longitudinal half along its longitudinal length, wherein the absorbent core has a thickness which is substantially the same on the same distance from the transversal centre line measured perpendicular to the transversal centre line, before the core is wetted, wherein the first longitudinal half has a higher absorption capacity than the second longitudinal half, wherein the absorbent core comprises a superabsorbing polymeric material, and wherein the first longitudinal half contains a different amount of superabsorbing polymeric material than the second longitudinal half, which causes the two longitudinal halves to exhibit different absorption capacity.
A one-component toughened epoxy adhesive comprising in admixture A) at least one non-rubber-modified epoxy resin, B) at least one toughening agent, C) at least one epoxy curing catalyst and D) a curing agent mixture that includes dicyandiamide and one or more dihydrazide compounds, the dicyanadiamide and one or more dihydrazide compounds being present at a weight ratio of 1:99 to 99:1.
Vehicle restraining system for delimiting roadways, which comprises guide barriers which are removably placed against one another, each guide barrier comprising a housing-like base member which can be erected on the ground by means of support feet (24, 32), characterised in that the support feet (24, 32) are arranged underneath runners extending transversely below the base member, a support foot (24, 32) being provided at each end section (22, 23) of a runner, and each support foot (24, 32) comprising a metallic main body and an elastomer body connected to said main body at the end nearest the ground, the elastomer body having a Shore hardness of at least 50 and the support foot (24, 32) being detachably fixable to the base member by means of a connecting element, the connecting element cooperating with an abutment on the main body and the support feet being mounted on slots in the runners.
Mounting and latching mechanism of an electrical or electronic device for fastening on a standard rail, including an immoveable claw and a claw which is moveable against a spring force, wherein the moveable claw can be translationally moved relative to the immoveable claw, wherein the immoveable claw and the moveable claw are embodied in one piece with a connecting spring structure and wherein the moveable claw is rigidly connected to an actuation element, characterised in that the actuation element is guided in the direction of the immoveable claw and in this way protrudes therebeyond.
An aircraft component, for an emergency flotation system, that includes a hose hinge assembly and a compartment door for an aircraft compartment; the hose hinge assembly comprising: a first swivel fitting including a pair of elbow components rotatably coupled to each other; a second swivel fitting including a pair of elbow components rotatably coupled to each other; a third swivel fitting including a pair of elbow components rotatably coupled to each other; a feed line; a fill line connected to the compartment door; a first rigid line; and a second rigid line; wherein a first end of the first swivel fitting is connected to the feed line, a second end of the first swivel fitting is connected to the first end of the first rigid line and the second swivel fitting is connected to the second end of the first rigid line, and wherein the second rigid line is connected at its first end to the second swivel fitting and is connected at its second end to a first end of the third swivel fitting, and a second end of the third swivel fitting is connected to the fill line such that the feed line, the first swivel fitting, the first rigid line, the second swivel fitting, the second rigid line, the third swivel fitting, and the fill line are connected in series and provide a fluid path from the feed line to the fill line and the fluid path remains intact when the first rigid line and/or the second rigid line are moved relative to each other. a first swivel fitting including a pair of elbow components rotatably coupled to each other; a second swivel fitting including a pair of elbow components rotatably coupled to each other; a third swivel fitting including a pair of elbow components rotatably coupled to each other; a feed line; a fill line connected to the compartment door; a first rigid line; and a second rigid line;
Component of a metallurgical plant with a sensor element for measuring a temperature gradient in a measuring direction, wherein the sensor element comprises a base body at or in which at least two optical waveguides (4, 5) for temperature measurement are arranged at a defined spacing (a), characterised in that the base body has an elongate rod shape with a centre axis, wherein the base body has for the most part two diametrically opposite grooves or bores (7, 8) and the optical waveguides (4, 5) are respectively arranged in the grooves or bores (7, 8), which extend in the direction of the centre axis, wherein the sensor element is arranged in a bore in the component of the metallurgical plant.
A nacelle construction of a wind turbine, comprising: a nacelle supported by the tower, the nacelle rotatably supporting a rotor of the wind turbine and housing at least one drivetrain component that generates heat when operated, the nacelle having a structure defined at least in part by a pair of lateral outer surfaces and an upper surface that each lie substantially parallel to the direction of wind flow when the wind turbine is in an operative position; at least one heat exchanger positioned externally to the nacelle structure and adapted to transfer heat from the at least one drivetrain component; a heat exchanger support structure that extends laterally away from at least one of the lateral sides of the nacelle structure to position the at least one heat exchanger within wind flow passing the nacelle structure, said heat exchanger support structure is movable toward one of the pair of lateral surfaces and characterized in that said support structure includes support arms that are connected to the nacelle structure with a pivotal connection such that access to and service of said heat exchanger may be accomplished by rotating said support structure about said pivotal connection to bring said heat exchanger towards said lateral surface of said nacelle. a nacelle supported by the tower, the nacelle rotatably supporting a rotor of the wind turbine and housing at least one drivetrain component that generates heat when operated, the nacelle having a structure defined at least in part by a pair of lateral outer surfaces and an upper surface that each lie substantially parallel to the direction of wind flow when the wind turbine is in an operative position; at least one heat exchanger positioned externally to the nacelle structure and adapted to transfer heat from the at least one drivetrain component; a heat exchanger support structure that extends laterally away from at least one of the lateral sides of the nacelle structure to position the at least one heat exchanger within wind flow passing the nacelle structure, said heat exchanger support structure is movable toward one of the pair of lateral surfaces and characterized in that said support structure includes support arms that are connected to the nacelle structure with a pivotal connection such that access to and service of said heat exchanger may be accomplished by rotating said support structure about said pivotal connection to bring said heat exchanger towards said lateral surface of said nacelle.