mhurhangee/ep-ind-claims huggingface dataset:
System for locating the barycenter of at least one identified object orbiting in space adapted to allow the physical and mechanical characterization of said identified object, comprising: - at least one remote sensor suitable for being placed on board of a station adapted to detect the space coordinates of certain points (Pi) belonging to said identified object, with respect to at least one space reference system; - first means for acquiring data related to positions assumed in time by said certain points (Pi) for reconstructing the trajectory followed by said certain points (Pi); - second means for determining the instantaneous rotation axes of the at least one identified object whose certain points (Pi) are associated with said trajectory, characterized in that: said second means is further adapted to determine a segment perpendicular to each pair of said instantaneous rotation axes in a sequence and to locate the median point of said segment; and the system further comprises third means for computing a discrete function d(tk) of the length of said segments, for computing an envelope curve (c) of the local maxima of said discrete function d(tk) and for determining the minimum of said envelope curve (c) for locating the barycenter G(tk*) of said identified object. - at least one remote sensor suitable for being placed on board of a station adapted to detect the space coordinates of certain points (Pi) belonging to said identified object, with respect to at least one space reference system; - first means for acquiring data related to positions assumed in time by said certain points (Pi) for reconstructing the trajectory followed by said certain points (Pi); - second means for determining the instantaneous rotation axes of the at least one identified object whose certain points (Pi) are associated with said trajectory, said second means is further adapted to determine a segment perpendicular to each pair of said instantaneous rotation axes in a sequence and to locate the median point of said segment; and the system further comprises third means for computing a discrete function d(tk) of the length of said segments, for computing an envelope curve (c) of the local maxima of said discrete function d(tk) and for determining the minimum of said envelope curve (c) for locating the barycenter G(tk*) of said identified object.
Reusable packaging (2; 102) for transporting food product(s) (4; 104), comprising an envelope (6; 106) extending in a longitudinal direction and with an opening (8; 108), adapted to receive, via said opening, said one or more food products, said envelope (6; 106) being made of silicone material; and a first system (10; 110) on the envelope (6; 106) for closing the opening (8; 108); characterized in that the envelope (6; 106) extends in the longitudinal direction over a length greater than three times, preferably five times, the average width of said envelope, so as to be able to contain one or more bread baguettes; and the package comprises a second system (12; 112) on the envelope (6; 106) configured to cooperate with the first system (10; 110) for securing the envelope in a folded and/or rolled state.
Garment comprising at least one sleeve, intended to cover a part of the body of a wearer, said sleeve having at least one region, the inner surface of which is equipped with a network of picots, said sleeve being designed to be able to exert compressive stress from said picots onto the skin of the body part that is intended to be positioned facing said network, each picot having a trigonal base, said picots being distributed in the network so as to form alveoli between adjacent picots, said sleeve being designed such that the picots can exert pressure on the skin great enough to form a skin protrusion in at least one alveolus in order to ensure a micro-massage of said protrusion during relative movements taking place between said network and said body part, said garment being characterised in that the picots have a pyramidal geometry which extends from the base to a tip by having three walls spaced in pairs by an edge, the alveoli being each formed between the walls opposite the adjacent picots.
Filter having a filter pot and a threaded insert which can be inserted into the filter pot, an end edge of the threaded insert having at least one region with a toothing system, and a collar of the filter pot having at least one region which corresponds thereto with a mating toothing system, the collar and the mating toothing system being oriented axially in the direction of the filter pot interior, and the mating toothing system being manufactured from a drawn-up region of the collar.
Method for producing a sheet of a material containing alkaloids, the method comprising: o mixing a material containing alkaloids with water to form a slurry; o forming a sheet from the slurry; o compressing the sheet between a first roller and a second roller, said first roller and second roller forming a gap therebetween where the sheet is inserted, to form a compressed sheet having a desired thickness; characterised in that it is provided for o changing the diameter of the first roller in order to change the desired thickness of the compressed sheet. o mixing a material containing alkaloids with water to form a slurry; o forming a sheet from the slurry; o compressing the sheet between a first roller and a second roller, said first roller and second roller forming a gap therebetween where the sheet is inserted, to form a compressed sheet having a desired thickness; characterised in that it is provided for o changing the diameter of the first roller in order to change the desired thickness of the compressed sheet.
A method for using demodulation reference signals, DM-RSs, to obtain channel state information, CSI, for a precoder selection, the method comprising: receiving a DM-RS in at least one subframe; determining the CSI based on the DM-RS; demodulating user data received during the at least one subframe using the DM-RS, characterized in that the method further comprises: predicting equivalent channels of a subset of a codebook, given the CSI obtained from the DM-RS, and selecting a precoder, including a rank and a precoding matrix, that maximizes at least one of a signal-to-interference-plus-noise ratio, SINR, and a throughput in the subset of the codebook of the predicted equivalent channels; and estimating a variation of a transmitter imbalance between sounding reference signal, SRS, transmissions and DM-RS transmissions; and using at least one of the estimated variation of the transmitter imbalance and the CSI obtained from the DM-RS to perform the precoder selection. receiving a DM-RS in at least one subframe; determining the CSI based on the DM-RS; demodulating user data received during the at least one subframe using the DM-RS, characterized in that the method further comprises: predicting equivalent channels of a subset of a codebook, given the CSI obtained from the DM-RS, and selecting a precoder, including a rank and a precoding matrix, that maximizes at least one of a signal-to-interference-plus-noise ratio, SINR, and a throughput in the subset of the codebook of the predicted equivalent channels; and estimating a variation of a transmitter imbalance between sounding reference signal, SRS, transmissions and DM-RS transmissions; and using at least one of the estimated variation of the transmitter imbalance and the CSI obtained from the DM-RS to perform the precoder selection. predicting equivalent channels of a subset of a codebook, given the CSI obtained from the DM-RS, and selecting a precoder, including a rank and a precoding matrix, that maximizes at least one of a signal-to-interference-plus-noise ratio, SINR, and a throughput in the subset of the codebook of the predicted equivalent channels; and estimating a variation of a transmitter imbalance between sounding reference signal, SRS, transmissions and DM-RS transmissions; and using at least one of the estimated variation of the transmitter imbalance and the CSI obtained from the DM-RS to perform the precoder selection.
A fuel injector isolator (18,18') for mounting a fuel injector in a bore of a fuel consuming device, said fuel injector isolator (18,18') comprising: a support member (46,46') which is rigid and which is annular in shape being centered about an axis such that said support member (46,46') has a support member inner periphery which circumferentially surrounds said axis, said support member (46,46') extending along said axis from a support member first end surface to a support member second end surface, wherein a profile of said support member inner periphery includes a concave region; and an isolation member (48,48') which is resilient and compliant and which is annular in shape being centered about said axis such that said support member (46,46') has an isolation member outer periphery and an isolation member inner periphery which accommodates said fuel injector therein, said isolation member (48,48') being located within said support member inner periphery, said isolation member outer periphery having 1) an isolation member outer periphery upper retention surface which engages said support member first end surface, thereby fixing said isolation member (48,48') relative to said support member (46,46') in a first direction along said axis and 2) an isolation member outer periphery lower retention surface (90,90') which extends into said concave region and engages said concave region of said support member (46,46'), thereby fixing said isolation member (48,48') relative to said support member (46,46') in a second direction along said axis which is opposite to said first direction. a support member (46,46') which is rigid and which is annular in shape being centered about an axis such that said support member (46,46') has a support member inner periphery which circumferentially surrounds said axis, said support member (46,46') extending along said axis from a support member first end surface to a support member second end surface, wherein a profile of said support member inner periphery includes a concave region; and an isolation member (48,48') which is resilient and compliant and which is annular in shape being centered about said axis such that said support member (46,46') has an isolation member outer periphery and an isolation member inner periphery which accommodates said fuel injector therein, said isolation member (48,48') being located within said support member inner periphery, said isolation member outer periphery having 1) an isolation member outer periphery upper retention surface which engages said support member first end surface, thereby fixing said isolation member (48,48') relative to said support member (46,46') in a first direction along said axis and 2) an isolation member outer periphery lower retention surface (90,90') which extends into said concave region and engages said concave region of said support member (46,46'), thereby fixing said isolation member (48,48') relative to said support member (46,46') in a second direction along said axis which is opposite to said first direction.
Vacuum device for affixing an ophthalmological patient interface on a patient's eye, said vacuum device comprising: a vacuum generator and a vacuum interface for fluidic coupling of the vacuum generator on a vacuum cavity of the patient interface; an internal pressure sensor that is fluidically coupleable to the patient interface and/or a pressure-measuring interface for a signal-coupling of an external pressure sensor of the patient interface; a movement detector which is configured to detect movements of the patient's eye; and a control unit which is configured to detect a faulty fluidic coupling of the vacuum cavity on the basis of a pressure that is detected by the coupled pressure sensor (11, 11'), characterized in that the control unit is furthermore configured to produce a control signal (s) for interrupting an ophthalmological treatment that is carried out by an ophthalmological treatment device if, simultaneously to the detected faulty fluidic coupling of the vacuum cavity, an eye movement is detected by the movement detector. a vacuum generator and a vacuum interface for fluidic coupling of the vacuum generator on a vacuum cavity of the patient interface; an internal pressure sensor that is fluidically coupleable to the patient interface and/or a pressure-measuring interface for a signal-coupling of an external pressure sensor of the patient interface; a movement detector which is configured to detect movements of the patient's eye; and a control unit which is configured to detect a faulty fluidic coupling of the vacuum cavity on the basis of a pressure that is detected by the coupled pressure sensor (11, 11'), characterized in that the control unit is furthermore configured to produce a control signal (s) for interrupting an ophthalmological treatment that is carried out by an ophthalmological treatment device if, simultaneously to the detected faulty fluidic coupling of the vacuum cavity, an eye movement is detected by the movement detector.
A method for installation of a power control module in a tower for a wind turbine including - providing a power control module, - providing a tower section, characterized by the steps of a) providing a temporary support device, b) placing the power control module on the temporary support device, c) placing the tower section around the power control module, d) connecting the power control module to the tower section, and e) removing the connected power control module and tower section from the temporary support device, which steps are carried out in the mentioned sequence. - providing a power control module, - providing a tower section, characterized by the steps of a) providing a temporary support device, b) placing the power control module on the temporary support device, c) placing the tower section around the power control module, d) connecting the power control module to the tower section, and e) removing the connected power control module and tower section from the temporary support device, which steps are carried out in the mentioned sequence. a) providing a temporary support device, b) placing the power control module on the temporary support device, c) placing the tower section around the power control module, d) connecting the power control module to the tower section, and e) removing the connected power control module and tower section from the temporary support device,
A pipe comprising a polypropylene composition, wherein the polypropylene composition comprises from 70 to 95 wt.-%, based on the total weight of the polypropylene composition, of a copolymer of propylene with comonomer units derived from 1-butene or 1-hexene having • a total comonomer content of from 0.5 to 5.0 wt.-%; • a melt flow rate MFR 2 of from 0.10 to 2.0 g/10 min, determined according to ISO 1133 at a load of 2.16 kg and a temperature of 230°C; and • a ratio of weight average molecular weight to number average molecular weight Mw/Mn of from 2.5 to 6.0, determined by Gel Permeation Chromatography according to ISO 16014-4:2003 and ASTM D 6474-99; and from 5 to 30 wt.-%, based on the total weight of the polypropylene composition, of a copolymer of ethylene with comonomer units derived from 1-butene and/or 1-hexene having • a total comonomer content of from 1.0 to 25.0 wt.-%; • a density of from 910.0 to 940.0 kg/m 3, determined according to ISO 1183; and • a melt flow rate MFR 2 of from 0.05 to 3.0 g/10 min, determined according to ISO 1133 at a load of 2.16 kg and a temperature of 190°C; wherein the polypropylene composition has a melt flow rate MFR 2 of from 0.1 to 1.0 g/10 min, determined according to ISO 1133 at a load of 2.16 kg and a temperature of 230°C. from 70 to 95 wt.-%, based on the total weight of the polypropylene composition, of a copolymer of propylene with comonomer units derived from 1-butene or 1-hexene having • a total comonomer content of from 0.5 to 5.0 wt.-%; • a melt flow rate MFR 2 of from 0.10 to 2.0 g/10 min, determined according to ISO 1133 at a load of 2.16 kg and a temperature of 230°C; and • a ratio of weight average molecular weight to number average molecular weight Mw/Mn of from 2.5 to 6.0, determined by Gel Permeation Chromatography according to ISO 16014-4:2003 and ASTM D 6474-99; and • a total comonomer content of from 0.5 to 5.0 wt.-%; • a melt flow rate MFR 2 of from 0.10 to 2.0 g/10 min, determined according to ISO 1133 at a load of 2.16 kg and a temperature of 230°C; and • a ratio of weight average molecular weight to number average molecular weight Mw/Mn of from 2.5 to 6.0, determined by Gel Permeation Chromatography according to ISO 16014-4:2003 and ASTM D 6474-99; and from 5 to 30 wt.-%, based on the total weight of the polypropylene composition, of a copolymer of ethylene with comonomer units derived from 1-butene and/or 1-hexene having • a total comonomer content of from 1.0 to 25.0 wt.-%; • a density of from 910.0 to 940.0 kg/m 3, determined according to ISO 1183; and • a melt flow rate MFR 2 of from 0.05 to 3.0 g/10 min, determined according to ISO 1133 at a load of 2.16 kg and a temperature of 190°C; • a total comonomer content of from 1.0 to 25.0 wt.-%; • a density of from 910.0 to 940.0 kg/m 3, determined according to ISO 1183; and • a melt flow rate MFR 2 of from 0.05 to 3.0 g/10 min, determined according to ISO 1133 at a load of 2.16 kg and a temperature of 190°C;
An aircraft actuator hydraulic system that includes hydraulically operated actuators (14a,14b) for driving a control surface of an aircraft and that supplies pressure oil to the actuators (14a,14b), the system comprising: a first actuator that is provided as one of the actuators and that drives the control surface by being operated by supply of pressure oil from a first aircraft central hydraulic power source including a first aircraft central hydraulic pump; a second actuator that is provided as another one of the actuators and that drives the control surface by being operated by supply of pressure oil from a second aircraft central hydraulic power source including a second aircraft central hydraulic pump; and a backup hydraulic pump that is installed inside a wing of the aircraft and that can supply pressure oil to the first actuator when a loss or degradation in a function of at least one of the first aircraft central hydraulic power source and the second aircraft central hydraulic power source occurs, characterized by the fact that a maximum discharge pressure of the backup hydraulic pump is set to be greater than maximum discharge pressures of the first aircraft central hydraulic pump and the second aircraft central hydraulic pump. a first actuator that is provided as one of the actuators and that drives the control surface by being operated by supply of pressure oil from a first aircraft central hydraulic power source including a first aircraft central hydraulic pump; a second actuator that is provided as another one of the actuators and that drives the control surface by being operated by supply of pressure oil from a second aircraft central hydraulic power source including a second aircraft central hydraulic pump; and a backup hydraulic pump that is installed inside a wing of the aircraft and that can supply pressure oil to the first actuator when a loss or degradation in a function of at least one of the first aircraft central hydraulic power source and the second aircraft central hydraulic power source occurs, characterized by the fact that a maximum discharge pressure of the backup hydraulic pump is set to be greater than maximum discharge pressures of the first aircraft central hydraulic pump and the second aircraft central hydraulic pump.
A vacuum chuck comprising: a base including a placement section on which an object is placed, and a coating film that coats at least a part of the placement section, wherein the placement section has a bottom face, a plurality of projections protruding from the bottom face, and an annular protrusion that protrudes from the bottom face at the same height as the plurality of projections and surrounds the plurality of projections, characterized in that the coating film has a first region that coats top faces of the projections, and a second region that coats a top face of the annular protrusion and has a smaller thickness than that of the first region. a base including a placement section on which an object is placed, and a coating film that coats at least a part of the placement section, wherein the placement section has a bottom face, a plurality of projections protruding from the bottom face, and an annular protrusion that protrudes from the bottom face at the same height as the plurality of projections and surrounds the plurality of projections, characterized in that the coating film has a first region that coats top faces of the projections, and a second region that coats a top face of the annular protrusion and has a smaller thickness than that of the first region.
A heating element comprising an annular housing in which a PTC heating resistor and a contact element (14, 15) contacting the PTC heating resistor are disposed, wherein the housing comprises an annular metal part forming a radially inner wall, a radially outer wall and a first end wall, characterized in that both the radially inner wall and the radially outer wall are each adjoined by a portion (11a, 11b) which forms at least part of a second end wall of the housing opposite the first end wall and which has been folded down after insertion of the PTC heating resistor and the contact element (14, 15). an annular housing in which a PTC heating resistor and a contact element (14, 15) contacting the PTC heating resistor are disposed, wherein the housing comprises an annular metal part forming a radially inner wall, a radially outer wall and a first end wall, characterized in that both the radially inner wall and the radially outer wall are each adjoined by a portion (11a, 11b) which forms at least part of a second end wall of the housing opposite the first end wall and which has been folded down after insertion of the PTC heating resistor and the contact element (14, 15).
Photo adapter for attaching to the eyepiece of an optical magnification device having a diopter compensation apparatus, equipped with an apparatus for compensating the diopter compensation by a) an adapter objective lens with a fixed focal length f that modifies the back focal length of the eyepiece and that has been inserted into the photo adapter in an immovable manner and b) a displaceable sleeve with connector for a camera housing with image-recording sensor, for compensating the back focal length change, wherein c) a scale displaying the displacement length Δ in diopter units dpt is attached to an adapter housing. a) an adapter objective lens with a fixed focal length f that modifies the back focal length of the eyepiece and that has been inserted into the photo adapter in an immovable manner and b) a displaceable sleeve with connector for a camera housing with image-recording sensor, for compensating the back focal length change, wherein c) a scale displaying the displacement length Δ in diopter units dpt is attached to an adapter housing.