mhurhangee/ep-ind-claims huggingface dataset:
A gas filling device comprising: a filling unit having a filling mechanism for transporting a gas from a gas supply source while measuring flow rate of the gas, a hose unit having a filling hose connected to a gas outlet pipe of the gas filling mechanism and a filling nozzle attached to a tip of the filling hose; and a display unit for displaying filling data measured by the filling mechanism, characterised in that said display unit has an internal pressure explosion-proof structure and is filled with an incombustible gas. a filling unit having a filling mechanism for transporting a gas from a gas supply source while measuring flow rate of the gas, a hose unit having a filling hose connected to a gas outlet pipe of the gas filling mechanism and a filling nozzle attached to a tip of the filling hose; and a display unit for displaying filling data measured by the filling mechanism, characterised in that said display unit has an internal pressure explosion-proof structure and is filled with an incombustible gas.
A method for performing co-registered optical imaging, the method comprising: acquiring a three-dimensional surface outline of the subject to be imaged; representing the three-dimensional surface outline as a discretized mesh; using two or more probes (100A, 100B) of a probe assembly to acquire an optical signal at a surface of the subject, each of the two or more probes being configured to independently function as an illumination source and as a detector, and to move independently with respect to one another to facilitate different types of co-registered optical imaging; tracking one or more markers on each probe (100A, 100B) of the probe assembly as the optical signal is acquired; receiving, via an imaging system coupled to the probe assembly, the optical signal captured by the probe assembly; converting the optical signal to image data; and co-registering to the discretized mesh the image data to form an image of the subject. acquiring a three-dimensional surface outline of the subject to be imaged; representing the three-dimensional surface outline as a discretized mesh; using two or more probes (100A, 100B) of a probe assembly to acquire an optical signal at a surface of the subject, each of the two or more probes being configured to independently function as an illumination source and as a detector, and to move independently with respect to one another to facilitate different types of co-registered optical imaging; tracking one or more markers on each probe (100A, 100B) of the probe assembly as the optical signal is acquired; receiving, via an imaging system coupled to the probe assembly, the optical signal captured by the probe assembly; converting the optical signal to image data; and co-registering to the discretized mesh the image data to form an image of the subject.
A multirotor aircraft that is adapted for vertical take-off and landing, comprising a fuselage, a thrust producing units assembly that is provided for producing thrust in operation, and a forward-swept wing that comprises a portside half wing and a starboard side half wing, each one of the portside and starboard side half wings (43, 44) comprising an inboard section that is connected to the fuselage and an outboard section that forms a wing tip, wherein the inboard sections of the portside and starboard side half wings (43, 44) form a central wing region, wherein each one of the portside and starboard side half wings (43, 44) is connected in the region of its wing tip to an associated outboard wing pod, wherein each one of the associated outboard wing pods supports at least two non-tiltably mounted thrust producing units (31, 32) of the thrust producing units assembly that are provided for generating lift at least during vertical taking-off and landing, wherein the associated outboard wing pod of the portside half wing is provided with a first and a second thrust producing unit (31, 32), the first thrust producing unit being arranged near a trailing edge of the portside half wing and the second thrust producing unit being arranged near a leading edge of the portside half wing, wherein the associated outboard wing pod of the starboard side half wing is provided with a third and a fourth thrust producing unit (31, 32), the third thrust producing unit being arranged near a trailing edge of the starboard side half wing and the fourth thrust producing unit being arranged near a leading edge of the starboard side half wing, wherein a thrust producing units sub-assembly of the thrust producing units assembly is provided in the central wing region near a trailing edge of the forward-swept wing for generating lift at least during vertical taking-off and landing, and characterised in that at least one thrust producing unit of the thrust producing units assembly is fixedly inclined with respect to a longitudinal axis of the multirotor aircraft for generating forward thrust at least during cruise operation of the multirotor aircraft.
An apparatus comprising: a deformable substrate (102, 202, 300a, 300b, 400a, 400b, 500a, 500b, 602, 902), the substrate configured to allow for electrical connection of one or more substrate electronic components (120, 220, 620) mounted on the deformable substrate to at least one of: one or more other electronic components (120, 220, 620) mounted on the deformable substrate, and one or more other electronic components (120, 220, 620) mounted on another connected substrate; and wherein the one or more substrate electronic components are mounted on the deformable substrate by an interconnect, the interconnect configured to electrically and mechanically interconnect the one or more substrate electronic components to the deformable substrate; wherein the interconnect comprises an ion gel (110, 210, 410a, 410b, 510a, 510b, 610, 910), the ion gel configured to: electrically interconnect the one or more substrate electronic components to the deformable substrate by capacitive coupling; mechanically interconnect the one or more substrate electronic components to the deformable substrate by adhesion, and maintain the electrical and mechanical interconnection of the one or more substrate electronic components under operational strains of the deformable substrate. a deformable substrate (102, 202, 300a, 300b, 400a, 400b, 500a, 500b, 602, 902), the substrate configured to allow for electrical connection of one or more substrate electronic components (120, 220, 620) mounted on the deformable substrate to at least one of: one or more other electronic components (120, 220, 620) mounted on the deformable substrate, and one or more other electronic components (120, 220, 620) mounted on another connected substrate; and one or more other electronic components (120, 220, 620) mounted on the deformable substrate, and one or more other electronic components (120, 220, 620) mounted on another connected substrate; and wherein the one or more substrate electronic components are mounted on the deformable substrate by an interconnect, the interconnect configured to electrically and mechanically interconnect the one or more substrate electronic components to the deformable substrate; wherein the interconnect comprises an ion gel (110, 210, 410a, 410b, 510a, 510b, 610, 910), the ion gel configured to: electrically interconnect the one or more substrate electronic components to the deformable substrate by capacitive coupling; mechanically interconnect the one or more substrate electronic components to the deformable substrate by adhesion, and maintain the electrical and mechanical interconnection of the one or more substrate electronic components under operational strains of the deformable substrate. electrically interconnect the one or more substrate electronic components to the deformable substrate by capacitive coupling; mechanically interconnect the one or more substrate electronic components to the deformable substrate by adhesion, and maintain the electrical and mechanical interconnection of the one or more substrate electronic components under operational strains of the deformable substrate.
An ablation device for treatment of tissue in body lumens with varying sizes, the device comprising: a catheter; an expansion member coupled with a distal portion of the catheter; an ablation structure comprising a plurality of longitudinal electrode regions (161,162,502,504,506,702-718,802-810,902-912,1006-1016) wherein each of the longitudinal electrode regions is controlled or wired separately, whereby each of the longitudinal electrode regions can be selectively enabled or disabled; and an ablation structure support coupled with the ablation structure, wherein the ablation structure and the ablation structure support are configured to at least partially unfurl or furl around the expansion member as the expansion member expands or contracts; characterized in that the ablation device further comprises one or more springs (1602,1600-a) coupled with the ablation structure support and configured to provide a force to cause the ablation structure to furl around the expansion member as the expansion member contracts, wherein the one or more springs comprise one or more strips of material coupled to the ablation structure laterally with respect to a longitudinal axis of the ablation structure, and wherein at least one of the strips of material comprises a tapered portion (1604,1606) such that the density of the said at least one strip of material proximal to a free end of the ablation structure support is less than the density of the said at least one strip of material distal to the free end of the ablation structure support. a catheter; an expansion member coupled with a distal portion of the catheter; an ablation structure comprising a plurality of longitudinal electrode regions (161,162,502,504,506,702-718,802-810,902-912,1006-1016) wherein each of the longitudinal electrode regions is controlled or wired separately, whereby each of the longitudinal electrode regions can be selectively enabled or disabled; and an ablation structure support coupled with the ablation structure, wherein the ablation structure and the ablation structure support are configured to at least partially unfurl or furl around the expansion member as the expansion member expands or contracts; characterized in that the ablation device further comprises one or more springs (1602,1600-a) coupled with the ablation structure support and configured to provide a force to cause the ablation structure to furl around the expansion member as the expansion member contracts, wherein the one or more springs comprise one or more strips of material coupled to the ablation structure laterally with respect to a longitudinal axis of the ablation structure, and wherein at least one of the strips of material comprises a tapered portion (1604,1606) such that the density of the said at least one strip of material proximal to a free end of the ablation structure support is less than the density of the said at least one strip of material distal to the free end of the ablation structure support.
A delivery device (10, 50) for delivering graft material to a target site, comprising: a hand piece (16, 52) maintaining an actuator mechanism (18, 52); a tube defining a lumen, an open end and a connection mechanism coupled to the hand piece, wherein the tube defines a bend portion along its length; and a plunger (14, 80) positioned within the lumen of the tube and coupled to the actuator mechanism, wherein the plunger includes a flexible distal portion having a plurality of cuts (76, 82), and further wherein a shape of the cuts is one of a spiral cut, a double spiral cut and a dovetail cut; wherein the actuator mechanism is configured to move the plunger relative to the open end within the lumen from a loading position to an extended position, with the plurality of cuts imparting flexibility in the flexible distal portion such that the plunger moves within the lumen along the bend portion when the actuator moves the plunger from the loading position to the extended position. a hand piece (16, 52) maintaining an actuator mechanism (18, 52); a tube defining a lumen, an open end and a connection mechanism coupled to the hand piece, wherein the tube defines a bend portion along its length; and a plunger (14, 80) positioned within the lumen of the tube and coupled to the actuator mechanism, wherein the plunger includes a flexible distal portion having a plurality of cuts (76, 82), and further wherein a shape of the cuts is one of a spiral cut, a double spiral cut and a dovetail cut; wherein the actuator mechanism is configured to move the plunger relative to the open end within the lumen from a loading position to an extended position, with the plurality of cuts imparting flexibility in the flexible distal portion such that the plunger moves within the lumen along the bend portion when the actuator moves the plunger from the loading position to the extended position.
Loudspeaker system having: multiple micro-electromechanical loudspeaker units, a drive circuit device for driving the loudspeaker units by means of electrical drive signals for emitting sound waves in an acoustic frequency range, characterized in that it has a frequency-selectively damping filter device which is at a distance from the loudspeaker units in the direction of sound propagation and damps sound waves in at least one ultrasound frequency range more strongly than the sound waves in the acoustic frequency range, it has a resonance tuning for sound waves in at least one specific ultrasound frequency range, to be specific the clock frequency of the drive signal and/or multiple frequencies thereof. multiple micro-electromechanical loudspeaker units, a drive circuit device for driving the loudspeaker units by means of electrical drive signals for emitting sound waves in an acoustic frequency range, it has a frequency-selectively damping filter device which is at a distance from the loudspeaker units in the direction of sound propagation and damps sound waves in at least one ultrasound frequency range more strongly than the sound waves in the acoustic frequency range, it has a resonance tuning for sound waves in at least one specific ultrasound frequency range, to be specific the clock frequency of the drive signal and/or multiple frequencies thereof.
Method for stunning an animal to be slaughtered, in particular a pig, by means of electrodes (18, 20) to be attached to an area of the head of said animal and that are supplied with a voltage to stun it, where said animal is restrained before being stunned and where said area is determined by means of a sensor device and the electrodes are then attached in that area, wherein the position of the ears (22, 24) of the animal to be slaughtered or at least of a reference point selected with reference to the ears is determined by means of an optical sensor of the sensor device and the area to which the electrodes are attached is determined depending on the position determined by image processing.
An operation-mode switching system for an elevator, which is provided to an elevator including a plurality of landing-door switches for detecting an open state of a plurality of landing doors, and which switches an operation mode during maintenance work, the operation-mode switching system for an elevator comprising: a maintenance-operation mode selector switch (9, 15) provided in a hoistway, for switching the operation mode to a maintenance-operation mode; a landing-door opening detection switch (7, 8) provided to the landing door independently of the landing-door switches, the landing-door opening detection switch (7, 8) being turned OFF when the landing door is intentionally opened; and a relay (35, 36) for inhibiting normal operation during maintenance, which is demagnetized when the landing-door opening detection switch (7, 8) is turned OFF to inhibit start of a car, wherein a maintenance operation of the car is enabled by switching the operation mode to the maintenance-operation mode through the maintenance-operation mode selector switch (9, 15) after the start of the car is inhibited by the relay (35, 36) for inhibiting normal operation during maintenance. a maintenance-operation mode selector switch (9, 15) provided in a hoistway, for switching the operation mode to a maintenance-operation mode; a landing-door opening detection switch (7, 8) provided to the landing door independently of the landing-door switches, the landing-door opening detection switch (7, 8) being turned OFF when the landing door is intentionally opened; and a relay (35, 36) for inhibiting normal operation during maintenance, which is demagnetized when the landing-door opening detection switch (7, 8) is turned OFF to inhibit start of a car, wherein a maintenance operation of the car is enabled by switching the operation mode to the maintenance-operation mode through the maintenance-operation mode selector switch (9, 15) after the start of the car is inhibited by the relay (35, 36) for inhibiting normal operation during maintenance.
A rotary catheter for opening an obstruction in a bodily vessel, comprising in combination; a motor-driven flexible hollow shaft rotatably disposed in a flexible tube, an aspiration channel defined between an internal diameter of said flexible tube and an external diameter of said hollow shaft, at least a distal portion of said hollow shaft being free to move radially in said aspiration channel enabling said aspiration channel to ingest particles which are as large as, or smaller than, a difference between said internal and external diameters, relative motion between said rotating hollow shaft and said flexible tube eases movement of the particles through said aspiration channel and impedes the particles from clogging said aspiration channel, a tip characterized in having a narrowed cross section wherein said tip is affixed to a distal end of said hollow shaft, said tip having a rounded distal end, wherein the rounded distal end of the tip defines a bore adapted to fit over a guidewire, said hollow shaft and said tip being rotatable and slideable over said guidewire, said tip also having a first side opposite a second side, said first side adapted to impact said obstruction when said tip rotates in a first direction, said first side and said second side being a cross sectional distance apart to define a width of said tip, said tip also having a base and an opposing crown that is adapted to atraumatically slide against a wall of said vessel as said tip rotates outside of said flexible tube, said base and said opposing crown being a cross sectional distance apart to define a height of said tip, said crown being offset away from a longitudinal axis of said hollow shaft further than said base is offset away from said longitudinal axis, said width being smaller than said height.
A display device comprising: a first substrate including a first contact hole; a first barrier insulating layer disposed on the first substrate and including a plurality of second contact holes; pad parts inserted into some of the plurality of second contact holes; fan-out lines formed of a first metal layer on the first barrier insulating layer and integral with the pad parts; a display layer disposed on the fan-out lines; and a flexible film (FPCB) disposed below the first substrate and inserted into the first contact hole to be electrically connected to the pad parts, wherein a maximum width of each of the pad parts is greater than a minimum width of each of the plurality of second contact holes, characterised by inspection pad parts inserted into other ones of the plurality of second contact holes; and a maximum width of each of the inspection pad parts being smaller than the minimum width of each of the second contact holes. a first substrate including a first contact hole; a first barrier insulating layer disposed on the first substrate and including a plurality of second contact holes; pad parts inserted into some of the plurality of second contact holes; fan-out lines formed of a first metal layer on the first barrier insulating layer and integral with the pad parts; a display layer disposed on the fan-out lines; and a flexible film (FPCB) disposed below the first substrate and inserted into the first contact hole to be electrically connected to the pad parts, wherein a maximum width of each of the pad parts is greater than a minimum width of each of the plurality of second contact holes, characterised by inspection pad parts inserted into other ones of the plurality of second contact holes; and a maximum width of each of the inspection pad parts being smaller than the minimum width of each of the second contact holes.
A method for wireless communications, comprising: identifying subframes with cell-specific reference signal, CRS, interference between transmissions of a serving Node B and one or more non-serving Node Bs (110b, 110c), wherein the subframes are identified based on cooperative partitioning of resources between the serving Node B and the one or more non-serving Node Bs (110b, 110c), and wherein the transmissions of the one or more non-serving Node Bs (110b, 110c) comprise CRS transmissions; obtaining a parameter related to the CRS interference, wherein the parameter comprises at least one of a number indicating a quantity of resource elements, REs, that are subject to the CRS interference or a transport block size, TBS, wherein the TBS corresponds to a number of code blocks; and determining whether to puncture REs of the subframes which are subject to the CRS interference or to perform CRS interference cancelation, CRS IC, to reduce the interference based on the obtained parameter or the number of code blocks. identifying subframes with cell-specific reference signal, CRS, interference between transmissions of a serving Node B and one or more non-serving Node Bs (110b, 110c), wherein the subframes are identified based on cooperative partitioning of resources between the serving Node B and the one or more non-serving Node Bs (110b, 110c), and wherein the transmissions of the one or more non-serving Node Bs (110b, 110c) comprise CRS transmissions; obtaining a parameter related to the CRS interference, wherein the parameter comprises at least one of a number indicating a quantity of resource elements, REs, that are subject to the CRS interference or a transport block size, TBS, wherein the TBS corresponds to a number of code blocks; and determining whether to puncture REs of the subframes which are subject to the CRS interference or to perform CRS interference cancelation, CRS IC, to reduce the interference based on the obtained parameter or the number of code blocks.