mhurhangee/ep-ind-claims huggingface dataset:
An in-mould labelling process for the manufacture of a labelled article comprising the steps of: - feeding a labelstock web into a mould; - forming an article in the mould such that the formed article contacts and effectively adheres to a label of the labelstock web; - detaching the adhered label from the labelstock web; and - removing the formed and labelled article from the mould, wherein the labelstock web comprises a label, a skeletal web and at least one area of weakness for facilitating detachment of the label from the skeletal web, and wherein the label is effectively adhered to the article whilst still being attached to the labelstock web and the step of detaching the adhered label from the labelstock web is effected by removing the formed and labelled article from the mould. - feeding a labelstock web into a mould; - forming an article in the mould such that the formed article contacts and effectively adheres to a label of the labelstock web; - detaching the adhered label from the labelstock web; and - removing the formed and labelled article from the mould,
A tip fairing for a horizontal airfoil of an aircraft, comprising stiffening elements and a skin covering the stiffening elements, the stiffening elements comprising a central web and two flanges located at the tips of the web, contact between the skin and the stiffening elements being made through the flanges of the stiffening elements, wherein - the tip fairing is manufactured from a composite material; - the tip fairing is manufactured as a single part, and - the planes defining the webs of any pair of stiffening elements taken in twos form an angle less than 30°, characterized in that the tip fairing further comprises two attachment areas each intended for receiving an attachment spar for attaching the fairing to the torsion box of a horizontal airfoil, at least one stiffening element being located between the two attachment areas and at least one stiffening element being located between the trailing edge of the fairing and the attachment area that is closest to said trailing edge, and the tip fairing further has a plurality of holes in the attachment areas suitable for fixing an attachment spar. - the tip fairing is manufactured from a composite material; - the tip fairing is manufactured as a single part, and - the planes defining the webs of any pair of stiffening elements taken in twos form an angle less than 30°, characterized in that
A pharmaceutical composition comprising: (a) naltrexone, or (b) a metabolite thereof selected from the group consisting of 6-β-naltrexol, 2-hydroxy-3-methoxy-6β-naltrexol and 2-hydroxy-3-methoxy-naltrexone, or (c) an analogue selected from the group consisting of methylnaltrexone, naloxone, nalmefene and nalorphine, for use in the treatment of cancer within a subject, wherein the subject is to be administered a chemotherapeutic agent before, during or following the treatment and wherein a therapeutically effective amount of the naltrexone or metabolite thereof or analogue of either is to be administered to the subject in a first treatment phase, and wherein after the first treatment phase the subject is to be administered a therapeutically effective amount of a cannabinoid in a second treatment phase. (a) naltrexone, or (b) a metabolite thereof selected from the group consisting of 6-β-naltrexol, 2-hydroxy-3-methoxy-6β-naltrexol and 2-hydroxy-3-methoxy-naltrexone, or (c) an analogue selected from the group consisting of methylnaltrexone, naloxone, nalmefene and nalorphine,
A liquid discharge apparatus comprising: a plurality of heads configured to discharge a liquid; a plurality of caps configured to contact and move away from the plurality of heads, respectively; a plurality of individual drain passages communicating with the plurality of caps, respectively; at least one common drain passage communicating with at least two of the plurality of individual drain passages; a plurality of suction devices provided in the plurality of individual drain passages, respectively; and a controller, wherein each of the plurality of individual drain passages is configured to allow and shut off communication between the cap and the at least one common drain passage, and characterized in that the controller is configured to: cause each of the plurality of individual drain passages to allow the communication between the cap and the at least one common drain passage when performing capping and decapping of the head; cap the sucking target with the cap after shutting off each individual drain passage communicating with the cap corresponding to the head that is not a sucking target, and control the corresponding suction device to perform suction of the head after the head has been capped with the cap. a plurality of heads configured to discharge a liquid; a plurality of caps configured to contact and move away from the plurality of heads, respectively; a plurality of individual drain passages communicating with the plurality of caps, respectively; at least one common drain passage communicating with at least two of the plurality of individual drain passages; a plurality of suction devices provided in the plurality of individual drain passages, respectively; and a controller, wherein each of the plurality of individual drain passages is configured to allow and shut off communication between the cap and the at least one common drain passage, and characterized in that the controller is configured to: cause each of the plurality of individual drain passages to allow the communication between the cap and the at least one common drain passage when performing capping and decapping of the head; cap the sucking target with the cap after shutting off each individual drain passage communicating with the cap corresponding to the head that is not a sucking target, and control the corresponding suction device to perform suction of the head after the head has been capped with the cap. cause each of the plurality of individual drain passages to allow the communication between the cap and the at least one common drain passage when performing capping and decapping of the head; cap the sucking target with the cap after shutting off each individual drain passage communicating with the cap corresponding to the head that is not a sucking target, and control the corresponding suction device to perform suction of the head after the head has been capped with the cap.
A thermoelectric material, expressed by Chemical Formula 1 below: <Chemical Formula 1> Cu x Se 1-y Q y where Q is at least one element selected from the group consisting of S and Te, 2.025≤x≤2.6 and 0<y<1.
One or more non-transitory computer-readable media storing instructions executed by one or more processors to perform a sequence comprising: detecting shot boundaries to segment video, wherein each segment includes a plurality of frames; for each frame of a set, V, of frames in a segment, determining a set of features of the frame using an object detection technique to compute a feature vector for each frame of the set of frames; for each frame of the set of frames, determining a coverage score as: c i = max w ij; j ∈ V, where c is a coverage vector for the set of frames V, w ij is a measure of similarity between a pair of frames i and j in V,; joining the coverage vector, c, with coverage scores of a set of frames previously selected from the plurality of frames as summary frames for the video so that the coverage vector, c, encompasses candidate frames, where the candidate frames are the frames of the set of frames and the set of frames previously selected; for each frame of the candidate frames, compute a diversity score as: D i j = d ij where D is a diversity matrix, d ij is a distance metric between frames i and j based on the feature vectors, where each of frames i and j are in the candidate frames; and selecting summary frames from the set of frames, V, and the set of previously selected frames, the selecting based on an optimization vector x, that satisfies: max x c T x + 1 2 x T D x where x T is the transpose of x, x i ∈ {0,1}∀ i, with ∑ i = 1 n + k x i = k, where there are n frames in the set of frames and k frames in the set of previously selected frames. detecting shot boundaries to segment video, wherein each segment includes a plurality of frames; for each frame of a set, V, of frames in a segment, determining a set of features of the frame using an object detection technique to compute a feature vector for each frame of the set of frames; for each frame of the set of frames, determining a coverage score as: c i = max w ij; j ∈ V, where c is a coverage vector for the set of frames V, w ij is a measure of similarity between a pair of frames i and j in V,; joining the coverage vector, c, with coverage scores of a set of frames previously selected from the plurality of frames as summary frames for the video so that the coverage vector, c, encompasses candidate frames, where the candidate frames are the frames of the set of frames and the set of frames previously selected; for each frame of the candidate frames, compute a diversity score as: D i j = d ij where D is a diversity matrix, d ij is a distance metric between frames i and j based on the feature vectors, where each of frames i and j are in the candidate frames; and selecting summary frames from the set of frames, V, and the set of previously selected frames, the selecting based on an optimization vector x, that satisfies: max x c T x + 1 2 x T D x where x T is the transpose of x, x i ∈ {0,1}∀ i, with ∑ i = 1 n + k x i = k, where there are n frames in the set of frames and k frames in the set of previously selected frames.
A flowmeter for a beverage preparation machine, comprising: - a moulded housing (2,4) delimiting a measuring chamber; - a rotatable measuring body having a rotatable shaft extending across the measuring chamber; and - point bearings (11,37) for mounting and positioning opposite extremities (32', 32") of the rotatable shaft in the housing, each point bearing being formed of a protruding part and a cooperating facing recessed counter-part, associated, respectively, with the housing and an extremity of the rotatable shaft, or vice versa, characterised in that said protruding part and said recessed counter-part are integrally formed with their associated moulded housing and rotatable shaft. - a moulded housing (2,4) delimiting a measuring chamber; - a rotatable measuring body having a rotatable shaft extending across the measuring chamber; and - point bearings (11,37) for mounting and positioning opposite extremities (32', 32") of the rotatable shaft in the housing,
A compound of Formula I: or a pharmaceutically acceptable salt thereof, wherein: R 1 is selected from the group consisting of H and (C 1 -C 6)alkyl; each of R 2, R 4, and R 5 are independently selected from the group consisting of: H, halo, substituted or unsubstituted (C 1 -C 6)alkyl, (C 1 -C 6)haloalkyl, OR A, CN, NO 2, C R A, NR A R B, -S 2 R A, -S 2 NR A R B, -S NR A R B, -NR A S 2 R B, - C(NR A)R B, -C NR A R B, a substituted or unsubstituted aryl, a substituted or unsubstituted heteroaryl, a substituted or unsubstituted cycloalkyl, and a substituted or unsubstituted heterocycloalkyl; R 3 is NO 2; each of R 6, R 7, R 8, R 9, and R 10 are independently selected from the group consisting of: H, substituted or unsubstituted (C 1 -C 6)alkyl, (C 1 -C 6)haloalkyl, OR A,NO 2, C R A, NR A R B, -S 2 NR A R B, -S NR A R B, -C(NR A)R B, -C NR A R B,-NR A S 2 R B, -NR A C R B, -S 2 R A, a substituted or unsubstituted aryl, a substituted or unsubstituted heteroaryl, a substituted or unsubstituted cycloalkyl, and a substituted or unsubstituted heterocycloalkyl; or R 6 and R 7, R 7 and R 8, R 8 and R 9, or R 9 and R 10 can come together to form a substituted or unsubstituted fused cycloalkyl ring, a substituted or unsubstituted fused heterocycloalkyl ring, or a substituted or unsubstituted fused heteroaryl ring; each R A and R B is independently selected from the group consisting of H and (C 1 -C 6)alkyl; and m is an integer from 1 to 2. R 1 is selected from the group consisting of H and (C 1 -C 6)alkyl; each of R 2, R 4, and R 5 are independently selected from the group consisting of: H, halo, substituted or unsubstituted (C 1 -C 6)alkyl, (C 1 -C 6)haloalkyl, OR A, CN, NO 2, C R A, NR A R B, -S 2 R A, -S 2 NR A R B, -S NR A R B, -NR A S 2 R B, - C(NR A)R B, -C NR A R B, a substituted or unsubstituted aryl, a substituted or unsubstituted heteroaryl, a substituted or unsubstituted cycloalkyl, and a substituted or unsubstituted heterocycloalkyl; R 3 is NO 2; each of R 6, R 7, R 8, R 9, and R 10 are independently selected from the group consisting of: H, substituted or unsubstituted (C 1 -C 6)alkyl, (C 1 -C 6)haloalkyl, OR A,NO 2, C R A, NR A R B, -S 2 NR A R B, -S NR A R B, -C(NR A)R B, -C NR A R B,-NR A S 2 R B, -NR A C R B, -S 2 R A, a substituted or unsubstituted aryl, a substituted or unsubstituted heteroaryl, a substituted or unsubstituted cycloalkyl, and a substituted or unsubstituted heterocycloalkyl; or R 6 and R 7, R 7 and R 8, R 8 and R 9, or R 9 and R 10 can come together to form a substituted or unsubstituted fused cycloalkyl ring, a substituted or unsubstituted fused heterocycloalkyl ring, or a substituted or unsubstituted fused heteroaryl ring; each R A and R B is independently selected from the group consisting of H and (C 1 -C 6)alkyl; and m is an integer from 1 to 2.
A device used for plasma-enhanced coating of a container, e.g. a plastic bottle, and/or a container blank, e.g. a container preform, and comprising at least one high-frequency source, at least one gas feed for feeding process gas, and at least one plasma nozzle as plasma source, wherein the plasma source comprises an inner electrode and said inner electrode is surrounded by a nozzle tube, the at least one plasma source is adapted to be introduced in a container to be coated and configured such that it is able to generate a plasma under ambient pressure, e.g. in a pressure range of 800 to 1,200 hPA, and the plasma can be discharged from a nozzle tube end, and wherein the temperature of the generated plasma lies within the range of the ambient temperature, e.g. between 10 and 50 °C, characterized in that the nozzle tube of the plasma source comprises a longitudinal nozzle tube element and a lateral nozzle tube element, said lateral nozzle tube element projecting laterally from the longitudinal nozzle tube element, and plasma being dischargeable through the lateral nozzle tube end.
A hair removal and fluid application device, having a hair removal means, a fluid dispensing means, a fluid reservoir and a support body, said device having a front surface comprising said hair removal device and a back surface comprising said fluid dispensing means, wherein said support body provides a predetermined location of said hair removal means and said fluid dispensing means with respective to one another and wherein said device has an at rest position and characterized in that in use said device has a hair removal means in use deflected position and a fluid dispensing means in use deflected position.
Apparatus for filling big bags and in particular FIBC big bags with at least one bulk material, comprising a frame structure, a filling spout for filling the big bag, a weighing unit and at least one compacting device, wherein the frame structure is provided with a holding device with multiple holding hooks to receive holding loops of a big bag to be filled and to retain the big bag during the filling process, wherein a supporting device is provided which defines a supporting surface, with which a bottom end of the big bag can be supported from beneath, wherein the supporting device has a compensating device assigned to it with an active unit that is shiftable relative to the supporting surface for the active unit to act upon the bottom end of the big bag, characterized in that the compacting device further comprises a head plate device that is provided for acting upon the big bag from above, and wherein at least one sensor is disposed at the head plate device for capturing a measure of a pressing force.
A method for managing an unmanned aerial vehicle, UAV, comprising: receiving flight plan information describing a flight path of the UAV; generating one or more cell lists based on the flight plan information; and transmitting the one or more cell lists to a source cell in a wireless network in which the UAV is currently operating, wherein the one or more cell lists are used in a handover procedure between the source cell that the UAV is currently connected to and a target cell that the UAV will connect to after completing the handover procedure, characterised in that the one or more cell lists include a neighbor cell black list that indicates a first set of cells in the wireless network that the UAV is to ignore while recording radio measurement information. receiving flight plan information describing a flight path of the UAV; generating one or more cell lists based on the flight plan information; and transmitting the one or more cell lists to a source cell in a wireless network in which the UAV is currently operating, wherein the one or more cell lists are used in a handover procedure between the source cell that the UAV is currently connected to and a target cell that the UAV will connect to after completing the handover procedure, characterised in that the one or more cell lists include a neighbor cell black list that indicates a first set of cells in the wireless network that the UAV is to ignore while recording radio measurement information.
Dispensing device for spraying a sprayable fluid which is formed as a hand-held appliance, having a housing in which an air pump and an electric drive motor driving the air pump is provided, having a spray head which is in communication with the housing for dispensing the fluid, having a receiving space arranged in the housing for a storage container in which the fluid to be dispensed is stored, having a fluid line leading from the storage container to the spray head and a hose line leading from the air pump to the spray head, characterised in that the spray head has a first nozzle which is in communication with the fluid line and, separately, has a second nozzle which is supplied with the air flow from the hose line, and in that the nozzle opening of the first nozzle projects at least slightly into the air flow emerging from the second nozzle in order to atomise the fluid supplied through the first nozzle.
Disc brake of a motor vehicle, in particular of a commercial vehicle, having a brake calliper which encompasses a brake disc in sections in a circumferential region and having an adapter which can be fixed in a static manner to the vehicle, in which adapter is guided at least one brake pad which is provided with a backing plate and with a friction lining fastened thereto, wherein the adapter has adapter lugs (2, 3) which support the backing plate of the brake pad at the entry side and exit side in a main direction of rotation of the brake disc, wherein the entry-side adapter lug of the adapter and the support surface, which is situated adjacent thereto, of the backing plate engage with one another, wherein the brake pad is supported on the exit-side adapter lug at a highest support point in the Y direction relative to the brake disc axis of rotation, which support point lies below a force action line (F Rxges) which represents the total friction force acting on the brake pad, wherein the Y direction describes a direction starting from the axis of rotation of the brake disc (Z axis) and extending radially through the centre of gravity of the brake pad, characterised in that the brake pad is held in the adapter in such a way that, during installation and removal, a combined pivoting and radial movement is required, wherein the exit-side adapter lug of the adapter and the support surface, which is adjacent thereto, of the backing plate are shaped such that the brake pad is pivotable about a pivot axis, which is parallel to the axis of rotation of the brake disc, counter to the main direction of rotation of the brake disc.
A pharmaceutical composition comprising: a pharmaceutically effective amount of at least one peptide; and a pharmaceutically acceptable amount of a combination of: (a) at least one metal in the form of any of, or a combination of, a salt thereof and a complex thereof; and (b) at least one reducing agent, wherein, said at least one metal is selected from any of, or a combination of: vanadium oxide, sodium vanadate, vanadium sulfate, vanadyl sulfate, vanadium biguanide, bis(maltolato)oxavandium, vanadium acetate, vanadyl picolinate, vanadyl citrate, chromium picolinate, chromium polynicotinate, chromium nicotinate, chromium chloride, chromium acetate, manganese gluconate, manganese sulfate, potassium permanganate and manganese chloride. a pharmaceutically effective amount of at least one peptide; and a pharmaceutically acceptable amount of a combination of: (a) at least one metal in the form of any of, or a combination of, a salt thereof and a complex thereof; and (b) at least one reducing agent, (a) at least one metal in the form of any of, or a combination of, a salt thereof and a complex thereof; and (b) at least one reducing agent, wherein, said at least one metal is selected from any of, or a combination of: vanadium oxide, sodium vanadate, vanadium sulfate, vanadyl sulfate, vanadium biguanide, bis(maltolato)oxavandium, vanadium acetate, vanadyl picolinate, vanadyl citrate, chromium picolinate, chromium polynicotinate, chromium nicotinate, chromium chloride, chromium acetate, manganese gluconate, manganese sulfate, potassium permanganate and manganese chloride.
A computer-implemented method for controlling a flight vehicle, comprising: receiving, by an autopilot of the flight vehicle, a guidance command generated by a guidance system of the flight vehicle; receiving, by the autopilot of the flight vehicle, a movement measurement measured by a movement measurement device of the flight vehicle; generating, by the autopilot of the flight vehicle, a plurality of state estimates utilizing the movement measurement when equipment to perform actual state measurements is unavailable, wherein the plurality of state estimates comprises an estimate of error, an estimate of an angle of attack, and an estimate of pitch rate; utilizing, by the autopilot of the flight vehicle, the guidance command and the plurality of state estimates to output a control surface command; determining, by a control logic module of the flight vehicle, an effector command from the control surface command; and outputting, by the control logic module of the flight vehicle, the effector command to at least one control effector to control the flight vehicle according to the effector command. receiving, by an autopilot of the flight vehicle, a guidance command generated by a guidance system of the flight vehicle; receiving, by the autopilot of the flight vehicle, a movement measurement measured by a movement measurement device of the flight vehicle; generating, by the autopilot of the flight vehicle, a plurality of state estimates utilizing the movement measurement when equipment to perform actual state measurements is unavailable, wherein the plurality of state estimates comprises an estimate of error, an estimate of an angle of attack, and an estimate of pitch rate; utilizing, by the autopilot of the flight vehicle, the guidance command and the plurality of state estimates to output a control surface command; determining, by a control logic module of the flight vehicle, an effector command from the control surface command; and outputting, by the control logic module of the flight vehicle, the effector command to at least one control effector to control the flight vehicle according to the effector command.