mhurhangee/ep-ind-claims huggingface dataset:
A shoe insole comprising: an insole body; a calcaneal anterior-part support protrusion that is provided in a region corresponding to a calcaneal anterior part of a foot having a calcaneus whose calcaneal front-side upper end acts as a point of effort, whose calcaneal rear part acts as a fulcrum and on which a moment around the fulcrum is exerted, the calcaneal anterior part being directly below the point of effort, and that abuts the calcaneal anterior part in order to maintain an inner longitudinal arch, an outer longitudinal arch, and a transverse arch of the foot; and a toe ball support part that is formed on a back surface of the insole body whereby a gap is generated between a close part of the toe ball support part and an inner sole of a shoe and that supports a thenar and hypothenars of the foot, with the calcaneal anterior-part support protrusion maintaining the inner longitudinal arch, the outer longitudinal arch, and the transverse arch, wherein an anterior edge of the toe ball support part extends on a line connecting from a first proximal phalanx to a fifth proximal phalanx of the foot, and a portion of the anterior edge between the first proximal phalanx and a second proximal phalanx is recessed backward, an insole front part thinner than and softer than the toe ball support part is provided in front of the toe ball support part. an insole body; a calcaneal anterior-part support protrusion that is provided in a region corresponding to a calcaneal anterior part of a foot having a calcaneus whose calcaneal front-side upper end acts as a point of effort, whose calcaneal rear part acts as a fulcrum and on which a moment around the fulcrum is exerted, the calcaneal anterior part being directly below the point of effort, and that abuts the calcaneal anterior part in order to maintain an inner longitudinal arch, an outer longitudinal arch, and a transverse arch of the foot; and that is provided in a region corresponding to a calcaneal anterior part of a foot having a calcaneus whose calcaneal front-side upper end acts as a point of effort, whose calcaneal rear part acts as a fulcrum and on which a moment around the fulcrum is exerted, the calcaneal anterior part being directly below the point of effort, and that abuts the calcaneal anterior part in order to maintain an inner longitudinal arch, an outer longitudinal arch, and a transverse arch of the foot; and a toe ball support part that is formed on a back surface of the insole body whereby a gap is generated between a close part of the toe ball support part and an inner sole of a shoe and that supports a thenar and hypothenars of the foot, with the calcaneal anterior-part support protrusion maintaining the inner longitudinal arch, the outer longitudinal arch, and the transverse arch, wherein an anterior edge of the toe ball support part extends on a line connecting from a first proximal phalanx to a fifth proximal phalanx of the foot, and a portion of the anterior edge between the first proximal phalanx and a second proximal phalanx is recessed backward, an insole front part thinner than and softer than the toe ball support part is provided in front of the toe ball support part.
An actuating device for a system comprising an emergency ram air turbine, said device comprising a jack extending along a longitudinal axis and comprising: - a cylinder configured to be connected to an aircraft structure or to the emergency ram air turbine, - a piston extending inside of the cylinder and defining two chambers (31, 32) therein, the piston being provided with a rod extending partially outside of the cylinder, said portion extending outside of the cylinder being configured to be connected to the emergency ram air turbine or to the aircraft structure, the piston being configured to move with respect to the cylinder between a retracted position and a deployed position, in which the length of the portion of the rod extending outside of the cylinder is greater than in the retracted position, said actuating device being characterized in that one of the chambers of the cylinder is equipped with at least one gas generator configured to, the piston being in the retracted position, release gases into said chamber, so that the piston moves in the cylinder from the retracted position to the deployed position under the influence of a pressure difference between the two chambers (31, 32) of the cylinder. - a cylinder configured to be connected to an aircraft structure or to the emergency ram air turbine, - a piston extending inside of the cylinder and defining two chambers (31, 32) therein, the piston being provided with a rod extending partially outside of the cylinder, said portion extending outside of the cylinder being configured to be connected to the emergency ram air turbine or to the aircraft structure, the piston being configured to move with respect to the cylinder between a retracted position and a deployed position, in which the length of the portion of the rod extending outside of the cylinder is greater than in the retracted position,
A method for manufacturing a composite material comprising: a placement step of placing a netlike sheet (4;5;70), through which a resin composition can permeate, on a reinforcing fiber substrate disposed on a forming die; a covering step of covering the reinforcing fiber substrate and the netlike sheet (4;5;70) disposed on the forming die with a bag film to form a sealed forming space between the bag film and the forming die; an injection/impregnation step of injecting the resin composition into the forming space to impregnate the reinforcing fiber substrate with the resin composition; and a resin curing step of curing the resin composition impregnated in the reinforcing fiber substrate, wherein in the netlike sheet (4;5;70), a plurality of warp yarns and a plurality of weft yarns are disposed in a lattice pattern, and in the placement step, after the netlike sheet (4;5;70) is placed on the reinforcing fiber substrate such that the warp yarns and the weft yarns form acute angles with respect to corners of the reinforcing fiber substrate, the netlike sheet (4;5;70) protruding from the reinforcing fiber substrate is bent. a placement step of placing a netlike sheet (4;5;70), through which a resin composition can permeate, on a reinforcing fiber substrate disposed on a forming die; a covering step of covering the reinforcing fiber substrate and the netlike sheet (4;5;70) disposed on the forming die with a bag film to form a sealed forming space between the bag film and the forming die; an injection/impregnation step of injecting the resin composition into the forming space to impregnate the reinforcing fiber substrate with the resin composition; and a resin curing step of curing the resin composition impregnated in the reinforcing fiber substrate, wherein in the netlike sheet (4;5;70), a plurality of warp yarns and a plurality of weft yarns are disposed in a lattice pattern, and in the placement step, after the netlike sheet (4;5;70) is placed on the reinforcing fiber substrate such that the warp yarns and the weft yarns form acute angles with respect to corners of the reinforcing fiber substrate, the netlike sheet (4;5;70) protruding from the reinforcing fiber substrate is bent.
A method of predicting resistance to anti-PD-1 therapy in a subject suffering from colorectal cancer, said method comprising the steps of: a) determining, from a biological sample from the subject, in particular a feces or a colonic biopsy sample from the subject, the presence of a pks island, b) predicting from the result of step a) that the subject is likely to be resistant to anti-PD-1 therapy. a) determining, from a biological sample from the subject, in particular a feces or a colonic biopsy sample from the subject, the presence of a pks island, b) predicting from the result of step a) that the subject is likely to be resistant to anti-PD-1 therapy.
A variable valve actuating mechanism comprising; a camshaft having two concentric cam lobes that may be rotated relative to one another a summation lever engaging with both cam lobes, a valve actuating rocker pivotally connected by a pivot shaft to the summation lever and engaging with a hydraulic lash adjuster at a first end and with a valve at a second end, and a shim surface movable with the pivot axis connecting the summation lever to the valve actuating rocker for limiting the expansion of the hydraulic lash adjuster to control clearance in the rocker system, wherein, in order to reduce friction, the shim surface abuts with a stationary stop surface that forms part of a camshaft support bearing, characterised in that the stationary stop surface is an outer bearing race of a rolling element bearing, a bearing bush or a split bearing shell and the shim surface is on a separate component mounted on the pivot shaft connecting the summation levers to the valve actuating rocker.
A coating material comprising: a curable functional group-containing fluorinated polymer; and a polyisocyanate compound which is an adduct obtained by the addition polymerization of bis(isocyanatomethyl)cyclohexane with a trihydric or higher hydric aliphatic polyhydric alcohol, an isocyanurate structure provided by a trimerization reaction of bis(isocyanatomethyl)cyclohexane, an isocyanurate structure provided by a pentamerization reaction of bis(isocyanatomethyl)cyclohexane, an isocyanurate structure provided by a heptamerization reaction of bis (isocyanatomethyl) cyclohexane, or a biuret obtained by the trimerization of bis(isocyanatomethyl)cyclohexane. a curable functional group-containing fluorinated polymer; and a polyisocyanate compound which is an adduct obtained by the addition polymerization of bis(isocyanatomethyl)cyclohexane with a trihydric or higher hydric aliphatic polyhydric alcohol, an isocyanurate structure provided by a trimerization reaction of bis(isocyanatomethyl)cyclohexane, an isocyanurate structure provided by a pentamerization reaction of bis(isocyanatomethyl)cyclohexane, an isocyanurate structure provided by a heptamerization reaction of bis (isocyanatomethyl) cyclohexane, or a biuret obtained by the trimerization of bis(isocyanatomethyl)cyclohexane. bis(isocyanatomethyl)cyclohexane with a trihydric or higher hydric aliphatic polyhydric alcohol, an isocyanurate structure provided by a trimerization reaction of bis(isocyanatomethyl)cyclohexane, an isocyanurate structure provided by a pentamerization reaction of bis(isocyanatomethyl)cyclohexane, an isocyanurate structure provided by a heptamerization reaction of bis (isocyanatomethyl) cyclohexane, or a biuret obtained by the trimerization of bis(isocyanatomethyl)cyclohexane.
An open channel flow monitoring apparatus for measuring a fluid level, the apparatus comprising: a first sensor configured to obtain data indicative of a fluid level below a first threshold level; and a second sensor configured to obtain data indicative of fluid level above a second threshold level, which is lower than the first threshold level; wherein both the first sensor and the second sensor are configured to obtain data indicative of the fluid level when the fluid level is between the first threshold level and the second threshold, wherein the first sensor and the second sensor are configured to output data indicative of the sewage level on a single data line, wherein the output data transitions seamlessly from data obtained from the first sensor to data obtained from the second sensor. a first sensor configured to obtain data indicative of a fluid level below a first threshold level; and a second sensor configured to obtain data indicative of fluid level above a second threshold level, which is lower than the first threshold level; wherein both the first sensor and the second sensor are configured to obtain data indicative of the fluid level when the fluid level is between the first threshold level and the second threshold, wherein the first sensor and the second sensor are configured to output data indicative of the sewage level on a single data line, wherein the output data transitions seamlessly from data obtained from the first sensor to data obtained from the second sensor.
A kerf structure for a snow tire, comprising a straight lamella with a constant thickness being deformed to have spaced apart half-circular protrusions alternatingly protruding in opposite directions out of the plane of the lamella, and with the axes of these half-circular protrusions within the plane of the lamella and oriented in a radial direction, and wherein the kerf structure is provided on these half circular protrusions with at least one spiral-shaped profile portion which comprises portions being flush with the half-circular protrusions and which separate the raised spiral-shaped profile portions.
A ventilation device for supplying and/or dissipating a volume flow, which for integration between a wall and a fixed frame of a window or a door docks with the fixed frame in a wall connection joint and which extends from an outer side into an interior space of the window or the door, having a basic housing being divided into at least three functional channel sections (10, 11, 12) different in shape, wherein a first channel section, formed as a flat channel, rests against a front face of the fixed frame with a flat side and the outer and inner channel sections (10, 12), respectively located on both sides of the first channel section, form a flow opening (15, 16), characterized in that the outer and inner channel sections (10, 12) are arcuately formed, with the flow opening (15, 16) directed towards the window or the door and respectively provided with a radius (17, 18) towards the flat side of the flat channel, wherein at least the inner channel section extends from the flat side at an obtuse angle of more than 90 ° and diverges facing away from a front side of the window or the door, and wherein the flow opening of the inner channel section terminates at an inner side of the wall arranged at the window or at the door and wherein the flow opening of the inner channel section has the biggest possible distance from the fixed frame at the inner side of the wall away from the window or the door. the outer and inner channel sections (10, 12) are arcuately formed, with the flow opening (15, 16) directed towards the window or the door and respectively provided with a radius (17, 18) towards the flat side of the flat channel, wherein at least the inner channel section extends from the flat side at an obtuse angle of more than 90 ° and diverges facing away from a front side of the window or the door, and wherein the flow opening of the inner channel section terminates at an inner side of the wall arranged at the window or at the door and wherein the flow opening of the inner channel section has the biggest possible distance from the fixed frame at the inner side of the wall away from the window or the door.
A method comprising: obtaining a first non-zero set of coefficients of a vector representative of a foreground component of a sound field, the vector having been decomposed from a plurality of spherical harmonic coefficients that describe the sound field according to a decomposition that provides linearly uncorrelated output; obtaining one of a plurality of configuration modes by which to extract the non-zero set of coefficients of the vector in accordance with the one of the plurality of configuration modes, wherein the one of the plurality of configuration modes indicates that the non-zero set of the coefficients includes all of the coefficients except for at least one of the coefficients; and extracting the non-zero set of the coefficients of the vector based on the obtained one of the plurality of configuration modes. obtaining a first non-zero set of coefficients of a vector representative of a foreground component of a sound field, the vector having been decomposed from a plurality of spherical harmonic coefficients that describe the sound field according to a decomposition that provides linearly uncorrelated output; obtaining one of a plurality of configuration modes by which to extract the non-zero set of coefficients of the vector in accordance with the one of the plurality of configuration modes, wherein the one of the plurality of configuration modes indicates that the non-zero set of the coefficients includes all of the coefficients except for at least one of the coefficients; and extracting the non-zero set of the coefficients of the vector based on the obtained one of the plurality of configuration modes.
A special-purpose bench for the maintenance of axles and/or transmissions and/or differentials, comprising a support structure carrying a table and special support means associated with the support structure and/or the table, characterized in that the special support means comprise at least two forks mounted on the table and spaced apart in positions such that the forks jointly form a support cradle for an axle, wherein the forks are selectively fastened to the table in at least two operative positions, namely a working position in which the forks extend from the table by projecting from the opposite side to the support structure and a rest position in which the forks extend entirely below a plane defined by a planar development of the table.
An emergency oxygen supply for passengers in an aircraft, with an oxygen source and with a number of pulse breathing masks which are conductively connected to the oxygen source, wherein an individual shut-off valve which in the non-actuated condition is switched to block is provided in each conduit to a breathing mask, with an impulse breathing control for actuating each individual shut-off valve, and characterised by an auxiliary conduit which connects the oxygen source to the breathing masks whilst bypassing the individual shut-off valves and which in each case via a check valve is connected to the respective conduit which leads to the breathing mask or is connected to the breathing mask itself, wherein the auxiliary conduit is connected to the oxygen source via a central shut-off valve which is switched to open in the non-actuated condition, and is activated to block in normal emergency operation as long as an electricity supply or emergency electricity supply exists.
A screw compressor, including a compressor housing having a screw rotor chamber arranged therein, two screw rotors (26, 28) that are arranged in the screw rotor chamber and are mounted on the compressor housing, each rotatably about a respective screw rotor axis (22, 24), and engage in each other by means of their helical contours (32, 34) and each cooperate with compression wall surfaces (36, 38) which are adjacent thereto and partly surround them in order to receive gaseous medium that is supplied by way of a low-pressure chamber arranged in the compressor housing and to discharge it in the region of a highpressure chamber that is arranged in the compressor housing, wherein the gaseous medium is enclosed in compression chambers that are formed between the helical contours (32, 34) and compression wall surfaces (36, 38) that are adjacent thereto with an inflow volume at low pressure and is compressed to a final volume at high pressure, and including two control sliders (52, 54) that are arranged one behind the other in a slider channel of the compressor housing in a direction of displacement parallel to the screw rotor axes (22, 24) and are adjacent to both screw rotors (26, 28) by means of slider compression wall surfaces (62, 64) and are movable in the direction of displacement, wherein a first control slider is arranged such that it affects the final volume and a second control slider is arranged such that it affects the initial volume, wherein, in a combined position with mutually facing end surfaces (86, 88) the first control slider and the second control slider are sealed tightly with each other and are movable together in the direction of displacement and, in a separated position, are positionable at a spacing from one another, forming an intermediate space, characterised in that, at least in a transfer position located between the combined position and the separated position, the control sliders (52, 54) form an inflow chamber into which the medium to be compressed flows out of one of the compression chambers by passing between the mutually facing end surfaces (86, 88) of the control sliders (52, 54), and in that one of the control sliders is provided with at least one outflow outlet that is adjacent to the inflow chamber and through which the medium from the inflow chamber enters an outflow opening in the slider channel that overlaps with the outflow outlet in this transfer position.
A vented upper body garment, comprising: a back panel comprising an inner surface intended for contacting the skin of a user and an outer surface, a top edge, a bottom edge, a right edge and a left edge, a first region and a second region; the first region comprising a plurality of adhesive overlay film structures (210, 710) affixed to the back panel, each adhesive overlay film structure (210, 710) in the plurality of adhesive overlay film structures (210, 710) having a shape; a plurality of perforations (300, 720) aligning with the plurality of adhesive overlay film structures (210, 710), each of the perforations (300, 720) extending through each adhesive overlay film structure (210, 710) and the back panel; each adhesive overlay film structure (210, 710) defining a reinforcing perimeter for each of the perforations (300, 720) in the plurality of perforations (300, 720) on the back panel; and a flocked silicone pattern on the inner surface aligned with a perimeter of each perforation (300, 720) in the plurality of perforations (300, 720) in the first region, the flocked silicone pattern extending into the second region. a back panel comprising an inner surface intended for contacting the skin of a user and an outer surface, a top edge, a bottom edge, a right edge and a left edge, a first region and a second region; the first region comprising a plurality of adhesive overlay film structures (210, 710) affixed to the back panel, each adhesive overlay film structure (210, 710) in the plurality of adhesive overlay film structures (210, 710) having a shape; a plurality of perforations (300, 720) aligning with the plurality of adhesive overlay film structures (210, 710), each of the perforations (300, 720) extending through each adhesive overlay film structure (210, 710) and the back panel; each adhesive overlay film structure (210, 710) defining a reinforcing perimeter for each of the perforations (300, 720) in the plurality of perforations (300, 720) on the back panel; and a flocked silicone pattern on the inner surface aligned with a perimeter of each perforation (300, 720) in the plurality of perforations (300, 720) in the first region, the flocked silicone pattern extending into the second region.