mhurhangee/ep-ind-claims huggingface dataset:
Optical adapter which can be coupled to an image acquisition device, which device comprises a first objective, in particular for microscopic observation; said adapter comprising a support made of substantially transparent material, which can be removably coupled to said device; said support having a proximal surface intended for facing towards said device and a distal surface located at a distance from said proximal surface and intended for facing towards an object to be observed; said support having: - a substrate, substantially optically transparent, - a second objective located in a seat obtained in said substrate and facing towards said first objective of said device, and - a reflector located laterally relative to said second objective and arranged for facing towards a light source integrated into said device and conveying the light emitted by said light source in an oblique direction, transversally towards said objective and axially past said distal surface; wherein said substrate has at least one curved surface adapted for shortening the focal distance of a photographic field collected by said first objective of said device, outside the solid angle of radiation intersected by said second objective. - a substrate, substantially optically transparent, - a second objective located in a seat obtained in said substrate and facing towards said first objective of said device, and - a reflector located laterally relative to said second objective and arranged for facing towards a light source integrated into said device and conveying the light emitted by said light source in an oblique direction, transversally towards said objective and axially past said distal surface; wherein said substrate has at least one curved surface adapted for shortening the focal distance of a photographic field collected by said first objective of said device, outside the solid angle of radiation intersected by said second objective.
A hair treatment agent, containing in a cosmetic carrier a) from 0.1 to 40 wt.% of at least one surfactant, selected from the group of anionic, amphoteric/zwitterionic and/or cationic surfactants, and b) an extract of the naturally fermented brown algae species Laminaria Saccharina (sugar kelp), which can be obtained by natural (alcoholic) fermentation with a fungus, wherein the quantities stated relate to the total weight of the hair treatment agent. a) from 0.1 to 40 wt.% of at least one surfactant, selected from the group of anionic, amphoteric/zwitterionic and/or cationic surfactants, and b) an extract of the naturally fermented brown algae species Laminaria Saccharina (sugar kelp), which can be obtained by natural (alcoholic) fermentation with a fungus,
An integrated test method for testing the operation of an electrical power converter controlling a three-phase electric motor configured to actuate a thrust reverser of an aircraft turbojet, the electrical power converter being powered by an electrical power supply network of the aircraft and being controlled by means of field-oriented control using a current setpoint defined from an in-phase current component and a quadratic current component, the method comprising the following steps: a) receiving an order to initiate the integrated test; b) controlling the electrical power converter using a current setpoint defined from a non-zero in-phase component (I d_cons) and a zero quadratic component (I q_cons); c) measuring the currents delivered on each of the three outlet phases of the electrical power converter; d) determining in-phase and quadratic components (I d, I q) of the three phase currents measured in the preceding step; e) comparing the in-phase and quadratic components (I d, I q) of the measured current with the in-phase and quadratic components (I d_cons, I q_cons) of the current setpoint; and f) sending a notification to the crew of the aircraft concerning the malfunctioning or the functioning of the thrust reverser as a function of the result of said comparison. a) receiving an order to initiate the integrated test; b) controlling the electrical power converter using a current setpoint defined from a non-zero in-phase component (I d_cons) and a zero quadratic component (I q_cons); c) measuring the currents delivered on each of the three outlet phases of the electrical power converter; d) determining in-phase and quadratic components (I d, I q) of the three phase currents measured in the preceding step; e) comparing the in-phase and quadratic components (I d, I q) of the measured current with the in-phase and quadratic components (I d_cons, I q_cons) of the current setpoint; and f) sending a notification to the crew of the aircraft concerning the malfunctioning or the functioning of the thrust reverser as a function of the result of said comparison.
A respiratory mask including a nasal interface, comprising: a mask frame; a cushion provided to the mask frame and adapted to form a seal with the patient's face; and a forehead support having a general "T"-shape with a base extending from the frame and an upper cross-portion provided to the base, wherein at least a portion of the base includes a flexible portion including a material and/or physical characteristic that allows the base to ilex from an original, unloaded position to an operative position; wherein at least the flexible portion is constructed of a resilient material that allows the forehead support to substantially return to the original position when not loaded; and characterized in that in contrast to sitting away from or to meeting the patient's forehead in the unloaded position, the forehead support is adapted to press against the patient's forehead in the unloaded position, to engage with the patient's forehead, and to be flexed from the original position to the operative position in a direction away from the patient's face with respect to the mask frame as a result of a reaction force from the patient's forehead, until a spring force of the forehead support equals a reaction force from the patient's forehead to provide maximum sealing on the patient's nose, when the respiratory mask is applied to the patient's face. a mask frame; a cushion provided to the mask frame and adapted to form a seal with the patient's face; and a forehead support having a general "T"-shape with a base extending from the frame and an upper cross-portion provided to the base, wherein at least a portion of the base includes a flexible portion including a material and/or physical characteristic that allows the base to ilex from an original, unloaded position to an operative position; wherein at least the flexible portion is constructed of a resilient material that allows the forehead support to substantially return to the original position when not loaded; and characterized in that in contrast to sitting away from or to meeting the patient's forehead in the unloaded position, the forehead support is adapted to press against the patient's forehead in the unloaded position, to engage with the patient's forehead, and to be flexed from the original position to the operative position in a direction away from the patient's face with respect to the mask frame as a result of a reaction force from the patient's forehead, until a spring force of the forehead support equals a reaction force from the patient's forehead to provide maximum sealing on the patient's nose, when the respiratory mask is applied to the patient's face.
A middle frame, comprising: a border antenna, configured to be connected with a circuit board through a feed point of the border antenna; a sound output hole in the border antenna that is configured to be connected with an audio assembly through a sound output channel; a first mounting site, for arranging the circuit board; a second mounting site, for arranging the audio assembly; and wherein the first mounting site is between the border antenna and the second mounting site; characterized in that the first mounting site and the sound output channel are stacked in a thickness direction of the middle frame, the first mounting site comprises a groove, an opening of the groove faces is configured away from the display screen, a wall of the groove is configured to face the display screen, the sound output hole are located in the top of the wall of the groove, and a part of the wall of the groove is multiplexed as the walls of the sound output hole. a border antenna, configured to be connected with a circuit board through a feed point of the border antenna; a sound output hole in the border antenna that is configured to be connected with an audio assembly through a sound output channel; a first mounting site, for arranging the circuit board; a second mounting site, for arranging the audio assembly; and wherein the first mounting site is between the border antenna and the second mounting site; characterized in that the first mounting site and the sound output channel are stacked in a thickness direction of the middle frame, the first mounting site comprises a groove, an opening of the groove faces is configured away from the display screen, a wall of the groove is configured to face the display screen, the sound output hole are located in the top of the wall of the groove, and a part of the wall of the groove is multiplexed as the walls of the sound output hole.
A non-woven fabric current collector comprising: a upper conductive non-woven fabric sheet and a lower conductive non-woven fabric sheet including a network of a conductive fibers, respectively; and a tension reinforcing layer that has a greater tensile strength than the conductive non-woven fabric sheets and includes a non-woven fabric structure, a woven fabric structure, a mesh structure, a structure including fibers extending in a certain direction, or a combination thereof, arranged between the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet, mediates adhesion between the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet, and has pores via which the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet communicate with each other, characterized in that the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet are combined with each other by using a bridge via the pores of the tension reinforcing layer, and/or that the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet are combined with each other by using fiberized linear binders which are dispersed in the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet and are partially melted and adhered to the tension reinforcing layer. a upper conductive non-woven fabric sheet and a lower conductive non-woven fabric sheet including a network of a conductive fibers, respectively; and a tension reinforcing layer that has a greater tensile strength than the conductive non-woven fabric sheets and includes a non-woven fabric structure, a woven fabric structure, a mesh structure, a structure including fibers extending in a certain direction, or a combination thereof, arranged between the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet, mediates adhesion between the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet, and has pores via which the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet communicate with each other, characterized in that the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet are combined with each other by using a bridge via the pores of the tension reinforcing layer, and/or that the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet are combined with each other by using fiberized linear binders which are dispersed in the upper conductive non-woven fabric sheet and the lower conductive non-woven fabric sheet and are partially melted and adhered to the tension reinforcing layer.
Heat exchanger for a motor vehicle, comprising o a primary collector with at least one inlet for a primary and a secondary cooling circuit of a fluid, o a secondary collector with a primary drain for the primary cooling circuit of the fluid, and o multiple exchanger pipes arranged at the collector, with the primary collector being divided into a primary area and a secondary area that are fluid tight, with the exchanger pipes connecting the primary and the secondary areas (A, B) fluidically to the secondary collector, with the inlet being located in the primary area, with the heat exchanger disposing of a secondary drain for the secondary cooling circuit of the fluid that is designed as a low-temperature circuit, with the secondary drain being located at the secondary area, characterised in that the primary collector is equipped with a throttle element that is used to form a tertiary area in the primary collector located between the primary and the secondary areas (A, B), whereby a fluid flow between the primary area and the tertiary area is being throttled in a defined manner, with the exchanger pipes fluidically connecting the tertiary area with the secondary collector, with the fluid flowing in the same direction in the exchanger pipes connected to the primary area and the tertiary area. o a primary collector with at least one inlet for a primary and a secondary cooling circuit of a fluid, o a secondary collector with a primary drain for the primary cooling circuit of the fluid, and o multiple exchanger pipes arranged at the collector,
A surgical stapler designed to deliver a plurality of fasteners one after another, comprising at least one grip body, at least one mechanism for ejecting said plurality of fasteners, and a tubular ejection barrel in which the surgical fasteners are stored one behind another, the surgical fasteners being delivered distally, at the distal end of said ejection barrel and characterized in that it is loaded with: - at least a first set of fasteners that is composed of surgical fasteners of a first type; - at least a second set of fasteners that is composed of surgical fasteners of a second type different from said first type; said first and second sets of fasteners (405, 406) being arranged according to a pre-established loading plan in such a way as to obtain a predefined order of delivery of the different fasteners. - at least a first set of fasteners that is composed of surgical fasteners of a first type; - at least a second set of fasteners that is composed of surgical fasteners of a second type different from said first type;
A titanium or titanium alloy material for a fuel cell separator, the titanium or titanium alloy material comprising: an oxide film formed on a titanium or titanium alloy substrate by stabilization treatment performed after passivation treatment; and one or more kinds of conductive materials selected from carbide, nitride, carbonitride, and boride of tantalum, titanium, vanadium, zirconium, and chromium, the conductive materials being dispersed in the oxide film and having a major axis diameter from 1 nm to 100 nm, wherein a contact resistance value with a carbon paper is 20 mΩ·cm 2 or less at a surface pressure of 10 kgf/cm 2 before and after an accelerated deterioration test in which the titanium or titanium alloy material is immersed in a sulfuric acid aqueous solution having an adjusted pH of 4 at 80 °C for four days. an oxide film formed on a titanium or titanium alloy substrate by stabilization treatment performed after passivation treatment; and one or more kinds of conductive materials selected from carbide, nitride, carbonitride, and boride of tantalum, titanium, vanadium, zirconium, and chromium, the conductive materials being dispersed in the oxide film and having a major axis diameter from 1 nm to 100 nm, wherein a contact resistance value with a carbon paper is 20 mΩ·cm 2 or less at a surface pressure of 10 kgf/cm 2 before and after an accelerated deterioration test in which the titanium or titanium alloy material is immersed in a sulfuric acid aqueous solution having an adjusted pH of 4 at 80 °C for four days.
The sublimation transfer paper for inkjet printing, comprising: an ink holding layer, a paper fiber bonding layer, a base paper layer and a back coating layer; wherein the ink holding layer is an uppermost layer of the transfer paper, and the back coating layer is a lowermost layer of the transfer paper, wherein disposed between the ink holding layer and the back coating layer are the paper fiber bonding layer and the base paper layer or a layer of mixture of a paper fiber binding agent and the base paper layer, characterized in that the ink holding layer is used of polyanionic cellulose and dry stuffing.
A data processing method comprising: receiving, by an access network device, first information sent by a core network device or a terminal device; and determining, by the access network device according to the first information, whether to perform security processing on to-be-processed data, characterized in that the receiving, by an access network device, first information sent by a core network device or a terminal device comprises: receiving, by the access network device, the first information sent by the core network device, wherein the first information is used for indicating one type of the following information: security processing is required to be performed on the to-be-processed data, security processing is not needed to be performed on the to-be-processed data, and security processing is preferred to be performed on the to-be-processed data, wherein the determining, by the access network device according to the first information, whether to perform security processing on to-be-processed data comprises: when the first information indicates that security processing is preferred to be performed on the to-be-processed data, determining, by the access network device according to subscription information of the terminal device and/or capability information of the terminal device, whether to perform security processing on the to-be-processed data. receiving, by an access network device, first information sent by a core network device or a terminal device; and determining, by the access network device according to the first information, whether to perform security processing on to-be-processed data, characterized in that the receiving, by an access network device, first information sent by a core network device or a terminal device comprises: receiving, by the access network device, the first information sent by the core network device, wherein the first information is used for indicating one type of the following information: security processing is required to be performed on the to-be-processed data, security processing is not needed to be performed on the to-be-processed data, and security processing is preferred to be performed on the to-be-processed data, wherein the determining, by the access network device according to the first information, whether to perform security processing on to-be-processed data comprises: when the first information indicates that security processing is preferred to be performed on the to-be-processed data, determining, by the access network device according to subscription information of the terminal device and/or capability information of the terminal device, whether to perform security processing on the to-be-processed data.
Launcher with at least one launch tube for rocket-propelled missiles, which are given their launching acceleration and an initial spin by means of a gas generator, which is located in the launch tube and is connected thereto, with a de Laval nozzle, serving for the exiting of the volumetric flow of gas from the gas generator at the remote end of the launch tube, and with a shock absorber, which is fixed to the frame, is assigned to the launch tube and connected thereto and serves for compensating for the recoil of the launch tube, characterized in that the shock absorber consists of a guide sleeve, which is fixed to the frame, and a guide sleeve, which is arranged coaxially with respect to the first guide sleeve and mounted displaceably in relation thereto, between which sleeves there is for adjustment of the force-distance characteristics of the shock absorber and the time delay of the return stroke thereof, a frictional annular-spring arrangement, which influences the return travel and return time of the shock absorber during the launching process of the missile, wherein a guiding surface allowing a relative movement between the two guide sleeves (18, 19) and taking the form of an annular slit-shaped clearance is provided in the one displaceably mounted sleeve and corresponds to a guiding surface assigned to a cap, and the sleeve that is fixed to the frame is kept fixed to the frame by means of a graduation in the cap, wherein downstream of the de Laval nozzle there is arranged at the end of the launch tube a further de Laval nozzle arrangement, which serves for the adjustable deflection of the gas flow leaving the de Laval nozzle, corresponds to the de Laval nozzle and comprises a base part, two bulkheads and two jet-deflecting surfaces that are mounted in an articulated manner between these bulkheads and at the same time form the termination of the jet exit opening of the launch tube in the transporting state of the launcher.
A rubber composition comprising: 100 parts by mass of a chloroprene-based rubber; 20 to 80 parts by mass of silica; 1 part by mass or more and less than 20 parts by mass of a hydrate; and 0.3 to 1.4 parts by mass of an organic peroxide, wherein: the rubber composition includes 0.5 to 15 parts by mass of a silane coupling agent having a double bond in a structure of the silane coupling agent with respect to 100 parts by mass of the silica. 100 parts by mass of a chloroprene-based rubber; 20 to 80 parts by mass of silica; 1 part by mass or more and less than 20 parts by mass of a hydrate; and 0.3 to 1.4 parts by mass of an organic peroxide, wherein: the rubber composition includes 0.5 to 15 parts by mass of a silane coupling agent having a double bond in a structure of the silane coupling agent with respect to 100 parts by mass of the silica.
A solder composition, consisting of 50% to 83% tin; 13% to 45% indium; 1 to 10% silver; 0.25% to 6% bismuth; and 0.25% to 0.75% copper, wherein the solder composition has a solidus temperature below 157°C. 50% to 83% tin; 13% to 45% indium; 1 to 10% silver; 0.25% to 6% bismuth; and 0.25% to 0.75% copper, wherein the solder composition has a solidus temperature below 157°C.
A crystalline form of the compound of the formula: characterised by (a) an X-ray powder diffraction (XRPD) pattern that comprises peaks at 11.2, 12.9, 15.5, 17.8, 19.1, 20.0, 20.6, 20.7, 21.2 and 22.8 degrees 2θ (± 0.1 degrees 2θ), wherein said XRPD is made using CuK α1 radiation; or (b) a Raman spectra that comprises peaks at 353, 688 and 825 cm -1; or (c) the Raman peaks in accordance with those of Figure 4. (a) an X-ray powder diffraction (XRPD) pattern that comprises peaks at 11.2, 12.9, 15.5, 17.8, 19.1, 20.0, 20.6, 20.7, 21.2 and 22.8 degrees 2θ (± 0.1 degrees 2θ), wherein said XRPD is made using CuK α1 radiation; or (b) a Raman spectra that comprises peaks at 353, 688 and 825 cm -1; or (c) the Raman peaks in accordance with those of Figure 4.