mhurhangee/ep-ind-claims huggingface dataset:
A control method for transmitting charging power to a wireless power receiver in a wireless power transmitter, the control method comprising: receiving an advertisement signal from a wireless power receiver, the advertisement signal including a first handle value and a preset universally unique identifier, UUID; obtaining a second handle value by adding a predetermined number to the first handle value; identifying a characteristic assigned to the second handle value; transmitting a connection request signal to the wireless power receiver for establishing a communication connection with the wireless power receiver, in response to the advertisement signal; transmitting, over the communication connection, a read request signal based on the second handle value to the wireless power receiver; and receiving, over the communication connection, a read response signal corresponding to the read request signal from the wireless power receiver. receiving an advertisement signal from a wireless power receiver, the advertisement signal including a first handle value and a preset universally unique identifier, UUID; obtaining a second handle value by adding a predetermined number to the first handle value; identifying a characteristic assigned to the second handle value; transmitting a connection request signal to the wireless power receiver for establishing a communication connection with the wireless power receiver, in response to the advertisement signal; transmitting, over the communication connection, a read request signal based on the second handle value to the wireless power receiver; and receiving, over the communication connection, a read response signal corresponding to the read request signal from the wireless power receiver.
A hand-operated work apparatus comprising an internal combustion engine and an air filter, the air filter having a cylindrical filter element, which is permanently connected at its end faces to end plates, the filter element and the end plates separating a dirty side of the air filter from a clean side, the clean side of the air filter being connected by at least one channel to the internal combustion engine, a first end plate being embodied as an air filter base, the air filter base and an intermediate flange arranged on the air filter base delimiting an inner chamber in which a section of the channel runs, the intermediate flange being arranged between the air filter and the internal combustion engine in the direction of flow, there being moulded on the air filter base at least one seal (54, 55), which abuts the intermediate flange and seals the inner chamber, the channel in the inner chamber being delimited by at least one boundary wall, which projects into the inner chamber transverse to the air filter base, the boundary wall being formed on the intermediate flange and/or on the air filter base and the distance (a) between the air filter base and the base opposite the air filter base bridging the intermediate flange.
An active clearance control system for a gas turbine engine, comprising: a turbine section comprising: blade outer air seals and stator vanes providing a core flow path; a turbine case supporting the blade outer air seals and the stator vanes, an annular space provided between an interior surface of the turbine case and the blade outer air seals and the stator vanes, and at least one hole extending through the turbine case from an exterior surface to the interior surface, the annular space extending axially to an exit; and a manifold circumscribing the exterior surface of the turbine case and providing an annular cavity therebetween, the annular cavity in fluid communication with the exit of the annular space via the at least one hole; characterised by: an inlet including an inlet particle separator configured to separate debris from inlet air entering the inlet and for supplying debris-laden air to the manifold of the active clearance control system; and an exhaust case secured to the turbine case, wherein the annular cavity is in fluid communication with the inlet particle separator and the exit is in fluid communication with the exhaust case. blade outer air seals and stator vanes providing a core flow path; a turbine case supporting the blade outer air seals and the stator vanes, an annular space provided between an interior surface of the turbine case and the blade outer air seals and the stator vanes, and at least one hole extending through the turbine case from an exterior surface to the interior surface, the annular space extending axially to an exit; and a manifold circumscribing the exterior surface of the turbine case and providing an annular cavity therebetween, the annular cavity in fluid communication with the exit of the annular space via the at least one hole; characterised by: an inlet including an inlet particle separator configured to separate debris from inlet air entering the inlet and for supplying debris-laden air to the manifold of the active clearance control system; and an exhaust case secured to the turbine case, wherein the annular cavity is in fluid communication with the inlet particle separator and the exit is in fluid communication with the exhaust case. an inlet including an inlet particle separator configured to separate debris from inlet air entering the inlet and for supplying debris-laden air to the manifold of the active clearance control system; and an exhaust case secured to the turbine case, wherein the annular cavity is in fluid communication with the inlet particle separator and the exit is in fluid communication with the exhaust case.
A controller configured to be coupled to a plurality of millimeter-wave radars mounted on a device having a screen, the controller configured to: at a first time, detect a first presence of an object in a field of view of a first millimeter-wave radar of the plurality of millimeter-wave radars; at a second time, detect a second presence of the object in a field of view of a second millimeter-wave radar of the plurality of millimeter-wave radars, the second time occurring after the first time; determine a gesture signature (408, 414 420, 422, 424, 446, 448, 612, 16, 818, 820, 916, 918, 920) based on detecting the first presence of the object in the field of view of the first millimeter-wave radar at the first time and detecting the second presence of the object in the field of view of the second millimeter-wave radar at the second time; and execute a command based on the determined gesture signature (408, 414 420, 422, 424, 446, 448, 612, 16, 818, 820, 916, 918, 920), select a first set of millimeter-wave radars from the plurality of millimeter-wave radars, wherein the first set comprises the first and second millimeter-wave radars, wherein each millimeter-wave radar of the plurality of millimeter-wave radars is configured to generate a signal associated with a presence of an object in respective fields of view at respective outputs, and wherein determining the gesture signature (408, 414 420, 422, 424, 446, 448, 612, 16, 818, 820, 916, 918, 920) is further based on outputs of each millimeter-wave radar of the first set, wherein the first set is a subset of millimeter-wave radars from the plurality of millimeter-wave radars. at a first time, detect a first presence of an object in a field of view of a first millimeter-wave radar of the plurality of millimeter-wave radars; at a second time, detect a second presence of the object in a field of view of a second millimeter-wave radar of the plurality of millimeter-wave radars, the second time occurring after the first time; determine a gesture signature (408, 414 420, 422, 424, 446, 448, 612, 16, 818, 820, 916, 918, 920) based on detecting the first presence of the object in the field of view of the first millimeter-wave radar at the first time and detecting the second presence of the object in the field of view of the second millimeter-wave radar at the second time; and execute a command based on the determined gesture signature (408, 414 420, 422, 424, 446, 448, 612, 16, 818, 820, 916, 918, 920), select a first set of millimeter-wave radars from the plurality of millimeter-wave radars, wherein the first set comprises the first and second millimeter-wave radars, wherein each millimeter-wave radar of the plurality of millimeter-wave radars is configured to generate a signal associated with a presence of an object in respective fields of view at respective outputs, and wherein determining the gesture signature (408, 414 420, 422, 424, 446, 448, 612, 16, 818, 820, 916, 918, 920) is further based on outputs of each millimeter-wave radar of the first set, wherein the first set is a subset of millimeter-wave radars from the plurality of millimeter-wave radars.
A method of forming an electro-optic display comprising: forming a front plane laminate comprising, in this order, a first substrate, a first conductive layer, a layer of electro-optic medium, and an adhesive, the first substrate and first conductive layer being transparent; providing a backplane comprising a conductor (1140, 1160) located on a surface of the backplane; and applying a conductive material to at least one of the conductor and the adhesive; characterised in that the method includes: laminating the front plane laminate to the backplane such that the conductive material penetrates the layer of electro-optic medium to provide an electrical connection between the first conductive layer and the conductor, wherein the conductive material contacts the first conductive layer only after the laminating step. forming a front plane laminate comprising, in this order, a first substrate, a first conductive layer, a layer of electro-optic medium, and an adhesive, the first substrate and first conductive layer being transparent; providing a backplane comprising a conductor (1140, 1160) located on a surface of the backplane; and applying a conductive material to at least one of the conductor and the adhesive; characterised in that the method includes: laminating the front plane laminate to the backplane such that the conductive material penetrates the layer of electro-optic medium to provide an electrical connection between the first conductive layer and the conductor, wherein the conductive material contacts the first conductive layer only after the laminating step.
A universal surgical guide system, comprising: a guide arm (120, 220) having a first portion (122, 222) configured to define a trajectory at which a bore is to be drilled into bone and a second portion (124, 224) configured to define a location of a distal end of the bore to be drilled into bone, the first portion (122, 222) having opposed surfaces thereof; and a carriage (140, 240) disposed on the first portion (122, 222) of the guide arm, the carriage (140, 240) being configured to translate along a length of the first portion (122, 222); characterised in that each of the opposed surfaces of the first portion (122, 222) of the guide arm (120, 220) has formed therein a plurality of slots, and each slot being indicative of an intended trajectory for the bore to be drilled into bone, the carriage (140, 240) being configured to selectively lock within a slot of the plurality of slots to set the intended trajectory at which the bore is to be drilled into bone. a guide arm (120, 220) having a first portion (122, 222) configured to define a trajectory at which a bore is to be drilled into bone and a second portion (124, 224) configured to define a location of a distal end of the bore to be drilled into bone, the first portion (122, 222) having opposed surfaces thereof; and a carriage (140, 240) disposed on the first portion (122, 222) of the guide arm, the carriage (140, 240) being configured to translate along a length of the first portion (122, 222); characterised in that each of the opposed surfaces of the first portion (122, 222) of the guide arm (120, 220) has formed therein a plurality of slots, and each slot being indicative of an intended trajectory for the bore to be drilled into bone, the carriage (140, 240) being configured to selectively lock within a slot of the plurality of slots to set the intended trajectory at which the bore is to be drilled into bone.
An abuse-deterrent formulation, comprising medicament, poloxamer, water-soluble anionic polysaccharide, and PEG ester; wherein: the medicament is or a pharmaceutically acceptable salt thereof; the poloxamer is poloxamer 124, the water-soluble anionic polysaccharide is gellan gum, and the PEG ester is polyoxyl stearate; wherein the weight ratio of poloxamer 124:gellan gum:polyoxyl stearate is about 40:30:30. the poloxamer is poloxamer 124, the water-soluble anionic polysaccharide is gellan gum, and the PEG ester is polyoxyl stearate; wherein the weight ratio of poloxamer 124:gellan gum:polyoxyl stearate is about 40:30:30.
A system for spinal cord stimulation of a subject comprising: a) a programmable implantable pulse generator, b) one or more multi-electrode arrays suitable to cover at least a portion of the spinal cord of said subject and configured to apply a selective stimulation to the dorsal roots of the spinal cord of said subject, wherein said IPG is operatively connected to said multi-electrode array and adapted to deliver to said multi-electrode array a stimulation characterized by a frequency comprised between 20 and 1200 Hz and an amplitude comprised between 0.1 motor threshold amplitude and 1.5 motor threshold amplitude, and wherein the stimulation is delivered at bursts of pulses, each burst of pulses occurring with a frequency comprised between 20 Hz and 100 Hz a) a programmable implantable pulse generator, b) one or more multi-electrode arrays suitable to cover at least a portion of the spinal cord of said subject and configured to apply a selective stimulation to the dorsal roots of the spinal cord of said subject, wherein said IPG is operatively connected to said multi-electrode array and adapted to deliver to said multi-electrode array a stimulation characterized by a frequency comprised between 20 and 1200 Hz and an amplitude comprised between 0.1 motor threshold amplitude and 1.5 motor threshold amplitude, and wherein the stimulation is delivered at bursts of pulses, each burst of pulses occurring with a frequency comprised between 20 Hz and 100 Hz wherein said IPG is operatively connected to said multi-electrode array and adapted to deliver to said multi-electrode array a stimulation characterized by a frequency comprised between 20 and 1200 Hz and an amplitude comprised between 0.1 motor threshold amplitude and 1.5 motor threshold amplitude, and wherein the stimulation is delivered at bursts of pulses, each burst of pulses occurring with a frequency comprised between 20 Hz and 100 Hz
A device comprising: an adjustable frame comprising three support stanchions (160, 170, 180), the first and second support stanchions (160, 170) of the three support stanchions (160, 170, 180) being configured to rest on cutaneous surfaces immediately superficial to anterior superior iliac spine prominences (120, 130), and the third stanchion of the three support stanchions (160, 170, 180) being configured to be supported by the skin and subcutaneous tissue immediately superficial to the symphysis pubis; the device being characterized by: a surgical guide (190a, 190b) associated with the adjustable frame; and at least two guide pins (110a, 110b), wherein the surgical guide (190a, 190b) is configured to position the at least two guide pins (110a, 110b) in the lateral pelvis superior to the acetabular cavity and comprises one or more guide holes for such positioning, and wherein the at least two guide pins (110a, 110b) are configured to be inserted into the pelvis along axes that are each parallel with a line defined by the anterior superior iliac spine prominences (120, 130), such that a plane containing both of the pin axes is parallel or angularly referenced to an anterior pelvic plane defined by the anterior superior iliac spine prominences (120, 130) and the symphysis pubis. a surgical guide (190a, 190b) associated with the adjustable frame; and at least two guide pins (110a, 110b), wherein the surgical guide (190a, 190b) is configured to position the at least two guide pins (110a, 110b) in the lateral pelvis superior to the acetabular cavity and comprises one or more guide holes for such positioning, and wherein the at least two guide pins (110a, 110b) are configured to be inserted into the pelvis along axes that are each parallel with a line defined by the anterior superior iliac spine prominences (120, 130), such that a plane containing both of the pin axes is parallel or angularly referenced to an anterior pelvic plane defined by the anterior superior iliac spine prominences (120, 130) and the symphysis pubis.
A liquid container system for a spray gun including: a cup including a closed end and an open top, the top including a cup lip, the cup lip including a cup lip recess; a ring, the ring including a peripheral flange and a ring recess in the flange, the peripheral flange for insertion into the cup lip recess; a liner (130, 600) including a liner lip at an open end, the liner (130, 600) insertable through the ring into the cup, the bottom side of the liner lip adapted for insertion into the ring recess; and a lid (200, 340) for closing the top of the cup, the lid (200, 340) including a flexible gasket extending from a flange on the periphery of the lid (200, 340) such that the lid (200, 340), liner (130, 600) and ring form a liquid tight unit. a cup including a closed end and an open top, the top including a cup lip, the cup lip including a cup lip recess; a ring, the ring including a peripheral flange and a ring recess in the flange, the peripheral flange for insertion into the cup lip recess; a liner (130, 600) including a liner lip at an open end, the liner (130, 600) insertable through the ring into the cup, the bottom side of the liner lip adapted for insertion into the ring recess; and a lid (200, 340) for closing the top of the cup, the lid (200, 340) including a flexible gasket extending from a flange on the periphery of the lid (200, 340) such that the lid (200, 340), liner (130, 600) and ring form a liquid tight unit.
A method of forming a shaped chocolate product comprising the steps of: (a) depositing an edible mass comprising a chocolate composition having a liquid fat phase onto a deposit surface, wherein an area of contact of said deposited chocolate composition with said deposit surface is bounded by a containment means selected from: (i) a recess volume on said deposit surface, provided that said deposited chocolate composition extends above the depth of said recess volume; (ii) a texturing of said deposit surface effective to retard the spreading of said chocolate composition; (iii) a raised ridge on said deposit surface, provided that said deposited chocolate composition extends above said raised ridge; and (iv) one or more containment members which contact said deposit surface, said method further including a step of engaging the one or more containment members with said deposit surface to retard the spreading of said deposited chocolate composition; and then (b) contacting at least one surface of said chocolate composition with a chilled forming device having a contacting surface at a temperature below 10°C thereby at least partially solidifying at least one outer surface layer of said chocolate composition in a form corresponding to said forming device, forming a shaped chocolate product. (a) depositing an edible mass comprising a chocolate composition having a liquid fat phase onto a deposit surface, wherein an area of contact of said deposited chocolate composition with said deposit surface is bounded by a containment means selected from: (i) a recess volume on said deposit surface, provided that said deposited chocolate composition extends above the depth of said recess volume; (ii) a texturing of said deposit surface effective to retard the spreading of said chocolate composition; (iii) a raised ridge on said deposit surface, provided that said deposited chocolate composition extends above said raised ridge; and (iv) one or more containment members which contact said deposit surface, said method further including a step of engaging the one or more containment members with said deposit surface to retard the spreading of said deposited chocolate composition; and then (i) a recess volume on said deposit surface, provided that said deposited chocolate composition extends above the depth of said recess volume; (ii) a texturing of said deposit surface effective to retard the spreading of said chocolate composition; (iii) a raised ridge on said deposit surface, provided that said deposited chocolate composition extends above said raised ridge; and (iv) one or more containment members which contact said deposit surface, said method further including a step of engaging the one or more containment members with said deposit surface to retard the spreading of said deposited chocolate composition; and then (b) contacting at least one surface of said chocolate composition with a chilled forming device having a contacting surface at a temperature below 10°C thereby at least partially solidifying at least one outer surface layer of said chocolate composition in a form corresponding to said forming device, forming a shaped chocolate product.
A polymer electrolyte fuel cell separator made of pure titanium or a titanium alloy having a surface layer part to which conductive compound particles are affixed, said polymer electrolyte fuel cell separator made of pure titanium or a titanium alloy characterized in that the pure titanium or titanium alloy has surface oxide of a thickness of 3 to 15 nm in range, an average carbon concentration in a range from an outermost surface, including the oxide layer of the pure titanium or titanium alloy, to a depth of 100 nm is 0.02 to 6 at%, and said conductive compound particles have an average particle size of 0.01 to 20 μm, wherein said conductive compound particles are comprised of one or more of Cr 2 N, CrSi 2, VB, V 8 C 7, VN, TaN, TaC, WC, and WN.
A composite metal powder for diffusion-brazing assembly or resurfacing of parts (1, 2) made of superalloy, the powder being formed by mixing a powder of an Astroloy type base metal with a powder of an NiCrB1055 type diffusion-brazing metal, the powder being characterized in that it is free of silicon and in that it comprises in the range 65% to 70% by weight of Astroloy and in the range 30% to 35% by weight of NiCrB1055, wherein both the Astroloy powder and the NiCrB1055 powder present grain size lying in the range 60 μm to 70 μm, and preferably of the order of 63 μm.