mhurhangee/ep-ind-claims huggingface dataset:
An applicator for applying a cosmetic to eyelashes, comprising a shaft section or at least a coupling section and an applicator section, the applicator section being configured as an internally hollow cage for accommodating the cosmetic, which is substantially or completely closed in the circumferential direction, characterized in that the cage, in the direction perpendicular to its longitudinal axis, has a triangular cross section and comprises on at least one of its circumferential tips an alternating sequence of ribs and passages that communicate with the interior of the cage and into which the eyelashes insert themselves during application, wherein the extent of the ribs, measured in the direction of the longitudinal axis of the applicator, decreases from the respective rib base point towards the respective rib apex point, and wherein the passage between two ribs adjacent in the direction parallel to the longitudinal axis is greater than the extent of an individual rib in the direction parallel to the longitudinal axis.
A lamp comprising, a one piece envelope mounted on a base, an internal structure arranged within the envelope, the internal structure comprising a stem extending from the base, a solid state light source arranged on the stem, and a screen (112, 212) obscuring at least a portion of light emitted from the solid state light source such that light emitted from the solid state light source is diffused by the screen (112, 212), wherein the stem is arranged to support the screen (112, 212), characterized in that the screen (112, 212) is arranged to adopt a collapsed state such that the screen (112, 212) is passable through a base opening of the envelope and an un-collapsed state such that the screen (112, 212) is impassable through the base opening of the envelope.
Liquid (meth) acrylic syrup comprising: a) a (meth)acrylic polymer, b) a (meth)acrylic monomer, c) at least one initiating system for starting the polymerization of the (meth) acrylic monomer, characterized that said initiating system comprises at least one accelerator, at least one organic aldehyde and a peroxy compound and organic peracid characterized in that the peroxy compound is a liquid at least at a temperature range between 0°C and 50°C. a) a (meth)acrylic polymer, b) a (meth)acrylic monomer, c) at least one initiating system for starting the polymerization of the (meth) acrylic monomer,
A machine for dry decoration of ceramic slabs or tiles, comprising: a support element, provided with a plurality of cavities with a pre-established shape; at least one dispensing device, configured to deposit a pre-fixed amount of powder material inside one or more pre-established cavities; an unloading device, configured to move the cavities from a loading position, in which they can receive the powder material from the dispensing device, to an unloading position, in which they can unload the powder material; characterised in that: the dispensing device comprises a number of dispensing elements, placed consecutively, one next to the other, transversely and above the upper portion of the support element, which can be controlled digitally so as to open and close, and each of which is configured to dispense the powder material into one or more cavities. a support element, provided with a plurality of cavities with a pre-established shape; at least one dispensing device, configured to deposit a pre-fixed amount of powder material inside one or more pre-established cavities; an unloading device, configured to move the cavities from a loading position, in which they can receive the powder material from the dispensing device, to an unloading position, in which they can unload the powder material; characterised in that: the dispensing device comprises a number of dispensing elements, placed consecutively, one next to the other, transversely and above the upper portion of the support element, which can be controlled digitally so as to open and close, and each of which is configured to dispense the powder material into one or more cavities.
A semiconductor device comprising: a semiconductor substrate; a first coil formed on the semiconductor substrate via a first insulation film; a second insulation film formed on the semiconductor substrate so as to cover the first insulation film and the first coil; a first pad formed on the second insulation film and disposed at a position not overlapped with the first coil in a planar view; a laminated insulation film formed on the second insulation film, the laminated insulation film having a first opening from which the first pad is exposed; a second coil formed on the laminated insulation film and disposed above the first coil; and a first wiring formed on the laminated insulation film including an upper portion of the first pad exposed from the first opening, the first wiring being electrically connected to the first pad, wherein the laminated insulation film is composed of a silicon oxide film, a silicon nitride film on the silicon oxide film, and a resin film on the silicon nitride film, the first coil and the second coil are not connected by a conductor but magnetically coupled to each other, and a part of the first pad is covered by the laminated insulation film. a semiconductor substrate; a first coil formed on the semiconductor substrate via a first insulation film; a second insulation film formed on the semiconductor substrate so as to cover the first insulation film and the first coil; a first pad formed on the second insulation film and disposed at a position not overlapped with the first coil in a planar view; a laminated insulation film formed on the second insulation film, the laminated insulation film having a first opening from which the first pad is exposed; a second coil formed on the laminated insulation film and disposed above the first coil; and a first wiring formed on the laminated insulation film including an upper portion of the first pad exposed from the first opening, the first wiring being electrically connected to the first pad, wherein the laminated insulation film is composed of a silicon oxide film, a silicon nitride film on the silicon oxide film, and a resin film on the silicon nitride film, the first coil and the second coil are not connected by a conductor but magnetically coupled to each other, and a part of the first pad is covered by the laminated insulation film.
Use of resorufin and/or toluidine blue as organic redox dyes, one or more polyols, especially glycerol, and water, incorporated as auxiliary agents into gelatin and/or hydroxyethyl starch and/or methylcellulose, as an oxygen indicator.
A method for testing for FVIII inhibitors in a patient sample, the method comprising the following steps: a. providing a previously obtained patient plasma sample, b. providing buffered normal pool plasma samples, c. providing a control plasma sample which is FVIII and VWF deficient, d. heat treatment of the samples of step a) to c), e. adding recombinant FVIII (rFVlll) to the control plasma sample, f. combining the patient plasma sample and the control plasma sample with rFVIII to obtain a test mixture, g. combining the normal pool plasma sample with the control plasma with rFVIII to obtain a control mixture, h. incubating the test mixture and the control mixture for less than 30 minutes, and i. analyzing the mixtures for residual rFVIII activity in the absence of VWF. a. providing a previously obtained patient plasma sample, b. providing buffered normal pool plasma samples, c. providing a control plasma sample which is FVIII and VWF deficient, d. heat treatment of the samples of step a) to c), e. adding recombinant FVIII (rFVlll) to the control plasma sample, f. combining the patient plasma sample and the control plasma sample with rFVIII to obtain a test mixture, g. combining the normal pool plasma sample with the control plasma with rFVIII to obtain a control mixture, h. incubating the test mixture and the control mixture for less than 30 minutes, and i. analyzing the mixtures for residual rFVIII activity in the absence of VWF.
An aircraft comprising: an airframe including first and second wings (104a, 104b), each of the first and second wings (104a, 104b) having first and second oppositely disposed wing tips (105e-105h), wherein the first and second wings (104a, 104b) are arranged in a tandem wing configuration or a canard configuration; first and second booms (106a, 106b) respectively extending longitudinally between the first and second wings (104a, 104b), the first and second booms (106a, 106b) each having forward and aft ends; first and second tail assemblies (112a, 112b) respectively coupled to aft ends of the first and second booms (106a, 106b); first and second forward propulsion assemblies (116a, 116b) respectively coupled to the forward ends of the first and second booms (106a, 106b), wherein the first and second forward propulsion assemblies (116a, 116b) are tiltable between a vertical takeoff and landing ("VTOL") flight mode orientation and a forward flight mode orientation; first and second aft propulsion assemblies (116c, 116d) respectively coupled to upper ends of the tail assemblies (112a, 112b), wherein the first and second aft propulsion assemblies (116c, 116d) are tiltable between a VTOL flight mode orientation and a forward flight mode orientation; and a payload module removably coupled to the airframe. an airframe including first and second wings (104a, 104b), each of the first and second wings (104a, 104b) having first and second oppositely disposed wing tips (105e-105h), wherein the first and second wings (104a, 104b) are arranged in a tandem wing configuration or a canard configuration; first and second booms (106a, 106b) respectively extending longitudinally between the first and second wings (104a, 104b), the first and second booms (106a, 106b) each having forward and aft ends; first and second tail assemblies (112a, 112b) respectively coupled to aft ends of the first and second booms (106a, 106b); first and second forward propulsion assemblies (116a, 116b) respectively coupled to the forward ends of the first and second booms (106a, 106b), wherein the first and second forward propulsion assemblies (116a, 116b) are tiltable between a vertical takeoff and landing ("VTOL") flight mode orientation and a forward flight mode orientation; first and second aft propulsion assemblies (116c, 116d) respectively coupled to upper ends of the tail assemblies (112a, 112b), wherein the first and second aft propulsion assemblies (116c, 116d) are tiltable between a VTOL flight mode orientation and a forward flight mode orientation; and a payload module removably coupled to the airframe.
A method of making a sensor assembly, comprising: fusing a metallic particulate using an additive manufacturing technique to define a mounting portion arranged to support a sensing device; fusing the metallic particulate to define a thermal shunt portion extending from the mounting portion; and fusing the metallic particulate to define a housing portion extending from the thermal shunt portion, wherein the housing portion is arranged on a side of the thermal shunt portion opposite the mounting portion to limit temperature of a sensor connector fixed to the housing portion of the sensor assembly; wherein: the thermal shunt portion comprises an airfoil structure extending between the housing portion and the mounting portion of the sensor assembly, wherein the airfoil structure comprises a plurality of airfoils each having a leading edge, wherein the leading edge extends between the mounting portion and the housing portion of the sensor assembly; or wherein the thermal shunt portion comprises a lattice structure extending between the housing portion and the mounting portion of the sensor assembly, the lattice structure including a plurality of stringers having gaps therebetween. fusing a metallic particulate using an additive manufacturing technique to define a mounting portion arranged to support a sensing device; fusing the metallic particulate to define a thermal shunt portion extending from the mounting portion; and fusing the metallic particulate to define a housing portion extending from the thermal shunt portion, wherein the housing portion is arranged on a side of the thermal shunt portion opposite the mounting portion to limit temperature of a sensor connector fixed to the housing portion of the sensor assembly; wherein: the thermal shunt portion comprises an airfoil structure extending between the housing portion and the mounting portion of the sensor assembly, wherein the airfoil structure comprises a plurality of airfoils each having a leading edge, wherein the leading edge extends between the mounting portion and the housing portion of the sensor assembly; or wherein the thermal shunt portion comprises a lattice structure extending between the housing portion and the mounting portion of the sensor assembly, the lattice structure including a plurality of stringers having gaps therebetween. the thermal shunt portion comprises an airfoil structure extending between the housing portion and the mounting portion of the sensor assembly, wherein the airfoil structure comprises a plurality of airfoils each having a leading edge, wherein the leading edge extends between the mounting portion and the housing portion of the sensor assembly; or wherein the thermal shunt portion comprises a lattice structure extending between the housing portion and the mounting portion of the sensor assembly, the lattice structure including a plurality of stringers having gaps therebetween.
A driver state estimation device configured to estimate a state of a driver who is in a movable body, the driver state estimation device comprising: a first measurement section configured to measure a first index value correlated with an amount of an attention source allocated to top-down attention of the driver in a first area where the top-down attention of the driver is predominant in the driver's surrounding environment; a second measurement section configured to measure a second index value correlated with an amount of an attention source allocated to bottom-up attention of the driver in a second area where the bottom-up attention of the driver is predominant in the driver's surrounding environment; and an estimation section that estimates the driver state including an attention function degraded state of the driver on the basis of the first index value in the first area and the second index value in the second area, wherein a size of the first area is capable of being changed according to a moving speed of the movable body. a first measurement section configured to measure a first index value correlated with an amount of an attention source allocated to top-down attention of the driver in a first area where the top-down attention of the driver is predominant in the driver's surrounding environment; a second measurement section configured to measure a second index value correlated with an amount of an attention source allocated to bottom-up attention of the driver in a second area where the bottom-up attention of the driver is predominant in the driver's surrounding environment; and an estimation section that estimates the driver state including an attention function degraded state of the driver on the basis of the first index value in the first area and the second index value in the second area, wherein a size of the first area is capable of being changed according to a moving speed of the movable body.
An electrochemical secondary battery having an inbuilt charging circuit, comprising: a battery housing (101, 206), a battery cell (102, 204), a positive electrode cap, a negative electrode cap (103, 203, 303), a circuit board module, and an insulating washer (106, 207), wherein a recessed crimp shoulder structure (107, 205) is provided at an end of the battery housing (101, 206) in proximity to the negative electrode cap (103, 203, 303), the battery cell (102, 204) is arranged within the battery housing (101, 206) and arranged between the positive electrode cap and the crimp shoulder structure (107, 205), and the battery housing (101, 206) is a steel case of a cylinder and used to output a positive electrode and fix the circuit board module; the positive electrode cap is connected to the battery housing (101, 206) to constitute the positive electrode of the secondary battery; the negative electrode cap (103, 203, 303) is arranged on the circuit board module to provide electromagnetic shielding, electrostatic shielding, and heat dissipation for the circuit; the circuit board module is arranged between the crimp shoulder (107, 205) and the negative electrode cap (103, 203, 303), and the circuit board module is configured with the diameter thereof being sized between an inner diameter of a recess constituted by the crimp shoulder (107, 205) and an inner diameter of the battery housing (101, 206), thus being engaged at either end of the crimp shoulder (107, 205) and separated from the battery cell (102, 204); electrode connecting wires (108a, 108b, 208a, 208b), are arranged on the battery cell (102, 204) to lead out the positive and negative electrodes of the battery respectively; and at least one through hole is provided on the circuit board module, an electrically-conductive material is coated onto an inner surface of the through hole for enhancing the welding strength and increasing the electrical contact area and leading out the electrode connecting wires (108a, 108b, 208a, 208b) so as to be connected to the circuit board module; the circuit board module is configured to provide charging protection and charging indication for the battery as well as discharge protection, short-circuit protection, over discharge protection, and output voltage control for the battery; and the insulating washer (106, 207) is arranged in a gap between both the battery housing (101, 206) and the circuit board module and the negative electrode cap, thus pressingly fixing the circuit board module between the crimp shoulder (107, 205) and the battery housing (101, 206), and separating the battery housing (101, 206) from the negative electrode cap, the insulating washer (106, 207) has a shaped section, one segment of the shape being used to pressingly fix the circuit board module between the crimp shoulder (107, 205) and the battery housing (101, 206), and other segment of the shape being used to separate the battery housing (101, 206) from the negative electrode cap (103, 203, 303).
An accessory of footwear comprising a cap for adhering to an upper surface of a shoe, wherein said cap comprises a first set of fingers, a second set of fingers, and a midline, characterised in that said first set of fingers projects towards said midline, said second set of fingers projects towards said midline, said first and second sets of fingers extend towards each other, said first and second sets of fingers are inter-digitated, and said fingers each have an adhesive side covered by a release layer configured to be peeled off to expose adhesive, thereby permitting said fingers to adhere to said upper surface of said shoe.
A hot-rolled steel sheet comprising, as a chemical composition, by mass%, C: 0.04% to 0.18%, Si: 0.10% to 1.70%, Mn: 0.50% to 3.00%, Al: 0.010% to 1.00%, B: 0% to 0.005%, Cr: 0% to 1.0%, Mo: 0% to 1.0%, Cu: 0% to 2.0%, Ni: 0% to 2.0%, Mg: 0% to 0.05%, REM: 0% to 0.05%, Ca: 0% to 0.05%, Zr: 0% to 0.05%, P: limited to equal to or less than 0.050%, S: limited to equal to or less than 0.010%, and N: limited to equal to or less than 0.0060%, with the remainder including Fe and impurities; wherein a structure includes, by area ratio, a ferrite and a bainite in a range of 75% to 95% in total, and a martensite in a range of 5% to 20%, and wherein in the structure, in a case where a boundary having an orientation difference of equal to or greater than 15° is defined as a grain boundary, and an area which is surrounded by the grain boundary and has an equivalent circle diameter of equal to or greater than 0.3 μm is defined as a grain, the ratio of the grains having an intragranular orientation difference in a range of 5° to 14° is, by area ratio, in a range of 10% to 60%, the ratio of the grains having the intragranular orientation difference in the range of 5° to 14° is measured by the method described in the description, and the area ratio of the ferrite and the bainite in total and the ratio of the martensite are measured by the method described in the description. wherein a structure includes, by area ratio, a ferrite and a bainite in a range of 75% to 95% in total, and a martensite in a range of 5% to 20%, and wherein in the structure, in a case where a boundary having an orientation difference of equal to or greater than 15° is defined as a grain boundary, and an area which is surrounded by the grain boundary and has an equivalent circle diameter of equal to or greater than 0.3 μm is defined as a grain, the ratio of the grains having an intragranular orientation difference in a range of 5° to 14° is, by area ratio, in a range of 10% to 60%, the ratio of the grains having the intragranular orientation difference in the range of 5° to 14° is measured by the method described in the description, and the area ratio of the ferrite and the bainite in total and the ratio of the martensite are measured by the method described in the description.
Valve, in particular for a hydraulic hybrid system, comprising - an electromagnet for moving an armature, - a control valve piston which is in a mechanical operative connection with the movable armature, with the result that a movement of the armature necessitates a movement of the control valve piston, and the control valve piston can be moved between a first control position and a second control position, - the movable armature, - a pole tube with a bore for mounting the movable armature, - a control space, in which the pressure of a fluid, in particular a liquid, can be changed on account of a different control position of the control valve piston, - a main valve piston which can be moved hydraulically between a closed position and an open position on account of a different pressure of the fluid in the control space, with the result that the valve is closed in the closed position of the main valve piston and the valve is open in the open position of the main valve piston, the pole tube having a first section with the bore and a second section outside the bore, characterized in that the first section is constructed from a mechanically hard and a magnetically hard material, and the second section is constructed from a magnetically soft material, in order to obtain a low residual magnetism at the armature after the electromagnet is switched off, and to obtain a great mechanical durability of the first section of the pole tube, the mechanically hard material of the first section having a hardness in accordance with Rockwell of more than 30 HRC, and the magnetically soft material of the second section having a coercive field strength of less than 1000 A/m, and the magnetically hard material of the first section having a coercive field strength of greater than 1000 A/m, and the material of the first section being tempering steel, and the material of the second section being machining steel. - an electromagnet for moving an armature, - a control valve piston which is in a mechanical operative connection with the movable armature, with the result that a movement of the armature necessitates a movement of the control valve piston, and the control valve piston can be moved between a first control position and a second control position, - the movable armature, - a pole tube with a bore for mounting the movable armature, - a control space, in which the pressure of a fluid, in particular a liquid, can be changed on account of a different control position of the control valve piston, - a main valve piston which can be moved hydraulically between a closed position and an open position on account of a different pressure of the fluid in the control space, with the result that the valve is closed in the closed position of the main valve piston and the valve is open in the open position of the main valve piston,