mhurhangee/ep-ind-claims huggingface dataset:
A laser surgical system, comprising: a pulsed laser, configured to produce a laser beam of laser pulses; an optics module configured to receive the laser beam; to direct the laser beam into a lens of an eye, and to focus the laser beam in the lens of the eye to cause photodisruption; an applanation plate, operable to be in contact with the target tissue to produce an interface and to transmit laser pulses to the target and reflected or scattered light or sound from the target through the interface; an Optical Coherence Tomography imaging device, configured to create an OCT image of the lens of the eye; a non-OCT imaging device, configured to generate a non-OCT image; and a system control module, characterized in that the system control module is configured to control the optics module to adjust and focus the laser beam based on positioning information of the eye obtained from images captured before applanation and images captured during a surgical procedure. a pulsed laser, configured to produce a laser beam of laser pulses; an optics module configured to receive the laser beam; to direct the laser beam into a lens of an eye, and to focus the laser beam in the lens of the eye to cause photodisruption; to receive the laser beam; to direct the laser beam into a lens of an eye, and to focus the laser beam in the lens of the eye to cause photodisruption; an applanation plate, operable to be in contact with the target tissue to produce an interface and to transmit laser pulses to the target and reflected or scattered light or sound from the target through the interface; an Optical Coherence Tomography imaging device, configured to create an OCT image of the lens of the eye; a non-OCT imaging device, configured to generate a non-OCT image; and a system control module, characterized in that the system control module is configured to control the optics module to adjust and focus the laser beam based on positioning information of the eye obtained from images captured before applanation and images captured during a surgical procedure.
A device for dispensing individual doses of powder from respective pockets of a carrier, the device including: an indexing mechanism for indexing the carrier between respective pockets; a first counter ring having an indication of unit counts on a first display surface, the first counter ring being rotatable about a counter axis; a second counter ring having an indication of tens counts on a second display surface, the second counter ring being rotatable about the counter axis; and an intermittent-motion mechanism for driving the second counter ring from the first counter ring and rotating the second counter ring between consecutive tens counts when the first counter ring rotates between two predetermined consecutive unit counts, the first counter ring being driven with the indexing mechanism, the first and second counter rings being positioned one within the other, with the first and second display surfaces adjacent each other, characterised in that the first and second display surfaces are generally planar and perpendicular to the counter axis. an indexing mechanism for indexing the carrier between respective pockets; a first counter ring having an indication of unit counts on a first display surface, the first counter ring being rotatable about a counter axis; a second counter ring having an indication of tens counts on a second display surface, the second counter ring being rotatable about the counter axis; and an intermittent-motion mechanism for driving the second counter ring from the first counter ring and rotating the second counter ring between consecutive tens counts when the first counter ring rotates between two predetermined consecutive unit counts, the first counter ring being driven with the indexing mechanism, the first and second counter rings being positioned one within the other, with the first and second display surfaces adjacent each other, characterised in that the first and second display surfaces are generally planar and perpendicular to the counter axis.
NFC component, comprising a first interface (TX1, TX2) which can be used in reader mode and is intended to be connected to an antenna via an impedance matching external circuit (C1-C3), and a second interface (RX1, RX2) which can be used in card mode and in reader mode and is intended to be connected to the antenna and to the first interface (TX1, TX2) via the impedance matching external circuit (C1-C3), characterized in that it further includes an internal module comprising at least first detection means configured to deliver a first detection signal which represents the phase antenna matching quality when the impedance matching external circuit (C1-C3) and the antenna are indeed connected between the first interface (TX1, TX2) and the second interface (RX1, RX2), the internal module being furthermore configured to deliver a check signal (SCTRL) from at least the first detection signal.
A computer system for accelerating three-dimensional graphics processing, comprising: a memory configured to store an octree for representing a three-dimensional shape, nodes of the octree including empty nodes and non-empty nodes, the empty nodes excluding the three-dimensional shape and being leaf nodes of the octree, and the non-empty nodes including at least a part of the three-dimensional shape; and a graphics processing unit coupled to the memory and configured to perform acts including: obtaining input comprising the octree representing the three-dimensional shape from the memory; and characterized in: for nodes in the octree with a depth, d, associated with a convolutional layer of a convolutional neural network, performing a convolutional operation of the convolutional layer to obtain an output of the convolutional layer, the output comprising a feature map of the three-dimensional shape obtained by the convolutional operation on the nodes with d-depth in the input. a memory configured to store an octree for representing a three-dimensional shape, nodes of the octree including empty nodes and non-empty nodes, the empty nodes excluding the three-dimensional shape and being leaf nodes of the octree, and the non-empty nodes including at least a part of the three-dimensional shape; and a graphics processing unit coupled to the memory and configured to perform acts including: obtaining input comprising the octree representing the three-dimensional shape from the memory; and characterized in: for nodes in the octree with a depth, d, associated with a convolutional layer of a convolutional neural network, performing a convolutional operation of the convolutional layer to obtain an output of the convolutional layer, the output comprising a feature map of the three-dimensional shape obtained by the convolutional operation on the nodes with d-depth in the input.
Composition for use in inhibiting growth of a cancer tumor in a host and/or preventing cancer cells from metastasis in a host, wherein the composition is implanted into and around the tumor and/or the cancer cells such that the amount of host serum is reduced upon the implantation and the host serum reduction terminates myoblast proliferation and induces TNF-alpha release and myoblast fusion, wherein the composition comprises a quantum of genetically normal non-host myoblasts and host serum and is adapted to induce myoblast proliferation before being implanted and to induce myoblast fusion upon implantation in that a host serum level in the composition is above a content of 15 % by weight in the composition, and wherein the composition is implanted in at least one dosage containing 75 million to 250 million myoblasts per millilitre of the composition, and wherein the cancer belongs to the group consisting of melanoma cancer, prostate cancer, one or more breast cancers, gastrointestinal cancer, lung cancer, Ehrlich ascites cancer and liver cancer.
An end mill with coolant holes, wherein a tip portion of an end mill body rotated around an axis serves as a cutting blade part, wherein a plurality of chip discharge grooves twisted to a backward side in a rotational direction of the end mill toward a rear end side in a direction of the axis are formed at predetermined intervals in a circumferential direction at an outer periphery of the cutting blade part, wherein peripheral blades are respectively formed at outer-peripheral-side ridge portions of wall faces of the chip discharge grooves that face the rotational direction of the end mill, and gashes are formed at tip portions of the chip discharge grooves, wherein bottom blades extending from tips of the peripheral blades to an inner peripheral side of the end mill body are respectively formed at intersecting ridgeline portions between wall faces of the gashes that face the rotational direction of the end mill and tip flank faces of the end mill body, wherein at least one bottom blade among the bottom blades serves as a long bottom blade extending to the inner peripheral side of the end mill body longer than the other two bottom blades adjacent to a forward side in the rotational direction of the end mill and the backward side in the rotational direction of the end mill, wherein coolant holes which are respectively formed between the chip discharge grooves adjacent to each other adjoin in the circumferential direction within the end mill body,, wherein a coolant hole among the coolant holes, which passes through a portion between a chip discharge groove connected to a gash along which the long bottom blade is formed and a chip discharge groove adjacent to a backward side of the chip discharge groove in the rotational direction of the end mill, is made open to a tip flank face connected to a backward side of the long bottom blade in the rotational direction of the end mill, characterised in that a coolant hole, which passes through a portion between the chip discharge groove connected to the gash along which the long bottom blade is formed, and a chip discharge groove adjacent to a forward side of the chip discharge groove in the rotational direction of the end mill, is made open to the gash along which the long bottom blade is formed.
A food concentrate in the form of a gel comprising a) 40 to 75 wt% of water by weight of the total food concentrate; b) Preferably at least 20 wt% NaCl by weight of the total water content of the food concentrate calculated as (weight of NaCl/(weight of NaCl+weight of total water content))*100%; c) 5.0 to 6.0 mmol/g water of the combined amount of sodium- and potassium-ions, preferably the ratio (w/w) of sodium to potassium- ions is at least 1; d) a binary gelling system said binary gelling system comprising i 4 to 13 wt% of type A gelatine by weight of the total water content of the food concentrate - calculated as (weight of gelatine /(weight of gelatine+weight of total water content))*100%; ii 9 to 35 wt% of sugar by weight of the total water content of the food concentrate said sugar selected from the group of sucrose, glucose, fructose and mixtures thereof - calculated as (weight of sugar /(weight of sugar+weight of total water content))*100%, iii Whereby the combined amount of gelatine and sugar is at least 20wt%, by weight of the total water content of the food concentrate and e) Preferably less than 0.1 wt% gelatinized starch by weight of the total food concentrate. a) 40 to 75 wt% of water by weight of the total food concentrate; b) Preferably at least 20 wt% NaCl by weight of the total water content of the food concentrate calculated as (weight of NaCl/(weight of NaCl+weight of total water content))*100%; c) 5.0 to 6.0 mmol/g water of the combined amount of sodium- and potassium-ions, preferably the ratio (w/w) of sodium to potassium- ions is at least 1; d) a binary gelling system said binary gelling system comprising i 4 to 13 wt% of type A gelatine by weight of the total water content of the food concentrate - calculated as (weight of gelatine /(weight of gelatine+weight of total water content))*100%; ii 9 to 35 wt% of sugar by weight of the total water content of the food concentrate said sugar selected from the group of sucrose, glucose, fructose and mixtures thereof - calculated as (weight of sugar /(weight of sugar+weight of total water content))*100%, iii Whereby the combined amount of gelatine and sugar is at least 20wt%, by weight of the total water content of the food concentrate and i 4 to 13 wt% of type A gelatine by weight of the total water content of the food concentrate - calculated as (weight of gelatine /(weight of gelatine+weight of total water content))*100%; ii 9 to 35 wt% of sugar by weight of the total water content of the food concentrate said sugar selected from the group of sucrose, glucose, fructose and mixtures thereof - calculated as (weight of sugar /(weight of sugar+weight of total water content))*100%, iii Whereby the combined amount of gelatine and sugar is at least 20wt%, by weight of the total water content of the food concentrate and e) Preferably less than 0.1 wt% gelatinized starch by weight of the total food concentrate.
A process for forming a silicon carbonitride barrier dielectric film between a dielectric film and a metal interconnect of an integrated circuit substrate, comprising the steps of; contacting an integrated circuit substrate with a barrier dielectric film precursor comprising: R x R' y (NR"R"') z Si wherein R, R', R" and R"' are each individually selected from hydrogen, linear or branched saturated or unsaturated alkyl, or aromatic, but R, R' cannot both be hydrogen; and wherein x+y+z=4; z = 1 to 3; and where z = 1 or 2 then each of x and y are at least 1; forming the silicon carbonitride barrier dielectric film with C/Si ratio >0.8 and a N/Si ratio >0.2 on the integrated circuit substrate.
A separator for separating one or more components selected from particulate material, hydrophobic material, non-polar material, microorganisms, or viruses from a mixture of water and the one or more components or from a mixture of a polar liquid and the one or more components, the separator comprising a porous retainer, characterised in that the separator comprises a continuous layer of a metal hydroxide hydrate gel and the porous retainer is for retaining the layer of metal hydroxide hydrate gel, the separator being structured such that liquid must pass through the layer of metal hydroxide hydrate gel before it can exit the separator to ensure that all filtrate has passed through the metal hydroxide hydrate gel layer, the porous retainer being located downstream of the layer of metal hydroxide hydrate gel, the continuous layer of the metal hydroxide hydrate gel retaining the one or more components on the continuous layer whilst the water or the polar liquid passes through the continuous layer, the continuous layer of the metal hydroxide hydrate gel having a thickness of from 1 micron to 1 metre, wherein the metal hydroxide hydrate gel is selected from one or more of aluminium hydroxide hydrate, magnesium hydroxide hydrate, zinc hydroxide hydrate, manganese hydroxide hydrate, cobalt hydroxide hydrate and nickel hydroxide hydrate.
System for fastening a covering roller blind, especially a self-winding sun roller blind of a tailgate of motor vehicles, wherein the roller blind has an end rod which is attached to that end of the roller blind strip which is to be pulled out, and wherein at least one fastening device for the releasable fastening of the end rod in the pulled-out roller blind position is located in the vehicle interior, wherein the fastening device has at least one permanent magnet, and wherein part of the end rod, which corresponds with the fastening device, is ferromagnetic and/or is provided with at least one permanent magnet which, in the fastened position of the end rod, is oriented by means of an opposite pole with respect to the magnet of the fastening device, and wherein the magnet is attached in the fastening device in such a manner that the pole connecting line of said magnet runs equidistantly per se from the surface to be covered, characterized in that the fastening devices are provided with at least two magnets, wherein the magnets are attached in such a manner that the pole connecting lines intersect at a point.
A process for the treatment of a gasoline containing sulphur-containing compounds, olefins and diolefins, the process comprising the following steps: a) fractionating the gasoline in a manner such as to recover at least one intermediate gasoline cut, MCN, comprising hydrocarbons and wherein the temperature difference (ΔT) between the 5% and 95% by weight distillation points is less than or equal to 60°C; b) desulphurizing the intermediate gasoline cut MCN alone and in the presence of a hydrodesulphurization catalyst and hydrogen, at a temperature in the range 160°C to 450°C, at a pressure in the range 0.5 to 8 MPa, with a liquid space velocity in the range 0.5 to 20 h -1 and with a ratio between the flow rate of hydrogen, expressed in normal m 3 per hour, and the flow rate of feed to be treated, expressed in m 3 per hour under standard conditions, in the range 50 Nm 3 /m 3 to 1000 Nm 3 /m 3 in a manner such as to produce a partially desulphurized intermediate gasoline cut MCN; and c) fractionating, in a splitter, the partially desulphurized intermediate gasoline cut MCN which has not undergone catalytic treatment subsequent to step b), in a manner such as to recover an intermediate gasoline with low sulphur and mercaptans contents from the column head and a cut of hydrocarbons containing sulphur-containing compounds including mercaptans from the column bottom. a) fractionating the gasoline in a manner such as to recover at least one intermediate gasoline cut, MCN, comprising hydrocarbons and wherein the temperature difference (ΔT) between the 5% and 95% by weight distillation points is less than or equal to 60°C; b) desulphurizing the intermediate gasoline cut MCN alone and in the presence of a hydrodesulphurization catalyst and hydrogen, at a temperature in the range 160°C to 450°C, at a pressure in the range 0.5 to 8 MPa, with a liquid space velocity in the range 0.5 to 20 h -1 and with a ratio between the flow rate of hydrogen, expressed in normal m 3 per hour, and the flow rate of feed to be treated, expressed in m 3 per hour under standard conditions, in the range 50 Nm 3 /m 3 to 1000 Nm 3 /m 3 in a manner such as to produce a partially desulphurized intermediate gasoline cut MCN; and c) fractionating, in a splitter, the partially desulphurized intermediate gasoline cut MCN which has not undergone catalytic treatment subsequent to step b), in a manner such as to recover an intermediate gasoline with low sulphur and mercaptans contents from the column head and a cut of hydrocarbons containing sulphur-containing compounds including mercaptans from the column bottom.
Drive coupler for automatically interlockingly connecting a drive train, in particular between self-driving agricultural harvesting machines or carrier vehicles and mounted implements, the drive coupler comprising means for compensating for angular and length deviations and at least one constant velocity joint, characterised in that the drive coupler comprises a compression spring which encases an entire propeller shaft consisting of two constant velocity joints and a connecting shaft and is designed, on account of its mounted position in which it is prestressed between external flanges of the constant velocity joints, to prevent the at least one constant velocity joint from bending and to orient the drive coupler in a linearly extended position so as to be altogether unsupported, the compression spring being centred and prestressed between supporting rings and the supporting rings each being connected to the external joint bodies of the constant velocity joints and the compression spring therefore axially orienting the two joints and keeping said joints extended.
A wind powered craft comprising a generally vertical mast which is rotatable about its vertical axis; a sail carried by said mast with its bottom edge attached in proximity to the bottom of the mast and extending to an attachment point in proximity to the top of the mast; a first member having an open end and partially extending around said mast, the mast being rotatable within said member; a bearing mounted stationary second member at the top of the mast and carried by the mast while allowing the mast to rotate; at least one support stay, being a wire or rope, running from said first member to said bearing mounted second member to support said first member; said sail being adapted to be reefed by turning completely around said mast by passing freely through the open end of said first member upon rotation of the mast. a sail carried by said mast with its bottom edge attached in proximity to the bottom of the mast and extending to an attachment point in proximity to the top of the mast; a first member having an open end and partially extending around said mast, the mast being rotatable within said member; a bearing mounted stationary second member at the top of the mast and carried by the mast while allowing the mast to rotate; at least one support stay, being a wire or rope, running from said first member to said bearing mounted second member to support said first member; said sail being adapted to be reefed by turning completely around said mast by passing freely through the open end of said first member upon rotation of the mast.
A self-securing latch arrangement configured to latch an aircraft door (3, 803) to an aircraft fuselage comprising: - a movable elongated latch bar (9, 809) being configured to be moved axially (9, 809) and configured to be movable from an open position to a latch position; - an anchorage-shaped latch fitting (11, 811) comprising a latch fitting end (13, 13', 13", 13′′′) configured for rigid engagement with an abutment surface (19, 819) of the movable elongated latch bar (9, 809) when a pressure differential between the aircraft fuselage interior and the atmosphere (atm) generates a force that pushes the aircraft door (3, 803), and thereby the anchorage-shaped latch fitting (11, 811) or movable elongated latch bar (9, 809), in a direction outward; characterized in that - the movable elongated latch bar (9, 809) comprises a latch fitting end facing side; and - the latch fitting end facing side comprises an indentation (18, 818) forming said abutment surface (19, 819). - a movable elongated latch bar (9, 809) being configured to be moved axially (9, 809) and configured to be movable from an open position to a latch position; - an anchorage-shaped latch fitting (11, 811) comprising a latch fitting end (13, 13', 13", 13′′′) configured for rigid engagement with an abutment surface (19, 819) of the movable elongated latch bar (9, 809) when a pressure differential between the aircraft fuselage interior and the atmosphere (atm) generates a force that pushes the aircraft door (3, 803), and thereby the anchorage-shaped latch fitting (11, 811) or movable elongated latch bar (9, 809), in a direction outward; - the movable elongated latch bar (9, 809) comprises a latch fitting end facing side; and - the latch fitting end facing side comprises an indentation (18, 818) forming said abutment surface (19, 819).