mhurhangee/ep-ind-claims huggingface dataset:
A lamp constructed as a hand lamp and for static use, the lamp comprising: a lamp housing, a first light source in the lamp housing, a lamp mounting for mounting the lamp in a desired position on a surface and a universal joint (24, 26) coupling the lamp housing and the lamp mounting together, whereby the lamp housing is universally adjustable in attitude relative to the lamp mounting, and means coupling the universal coupling to the lamp housing and lamp mounting such that the lamp housing and lamp mounting can be spaced apart and brought together, and in that the lamp housing and lamp mounting being universally adjustable in relative attitude when the lamp housing and lamp mounting are spaced apart, wherein the light source is located on a side of the lamp housing, wherein the universal joint comprises a ball and socket joint, wherein the ball part of the ball and socket joint is coupled to a shaft, which shaft is mounted in the lamp housing, characterised in that the arrangement is such that the ball part can be moved axially from a first position in which the lamp housing and the mounting lie closely adjacent to one-another to a second position in which the lamp housing and mounting are spaced apart, the second position permitting articulation of the ball and socket joint, the lamp further comprising detent means coupled between the lamp housing and the shaft to tend to retain the shaft in the first and second positions. a lamp housing, a first light source in the lamp housing, a lamp mounting for mounting the lamp in a desired position on a surface and a universal joint (24, 26) coupling the lamp housing and the lamp mounting together, whereby the lamp housing is universally adjustable in attitude relative to the lamp mounting, and means coupling the universal coupling to the lamp housing and lamp mounting such that the lamp housing and lamp mounting can be spaced apart and brought together, and in that the lamp housing and lamp mounting being universally adjustable in relative attitude when the lamp housing and lamp mounting are spaced apart, wherein the light source is located on a side of the lamp housing, wherein the universal joint comprises a ball and socket joint, wherein the ball part of the ball and socket joint is coupled to a shaft, which shaft is mounted in the lamp housing, characterised in that the arrangement is such that the ball part can be moved axially from a first position in which the lamp housing and the mounting lie closely adjacent to one-another to a second position in which the lamp housing and mounting are spaced apart, the second position permitting articulation of the ball and socket joint, the lamp further comprising detent means coupled between the lamp housing and the shaft to tend to retain the shaft in the first and second positions.
Tyre comprising a tread, a crown with a crown reinforcement, two sidewalls, two beads, a carcass reinforcement anchored to the two beads and extending from one sidewall to the other, characterized in that the tread comprises a composition based on at least: - a diene elastomer, at a content of between 35 and 99 phr (parts by weight per hundred parts of elastomer), - a thermoplastic elastomer system, at a total content of between 1 and 65 phr, said thermoplastic elastomer system comprising at least two block copolymers, referred to as polystyrene and poly(butadiene/styrene) block copolymers, each comprising: - at least one elastomer block of optionally hydrogenated butadiene/styrene random copolymer type, and - at least one thermoplastic block of styrene type, one of the two polystyrene and poly(butadiene/styrene) block copolymers being hydrogenated such that a proportion ranging from 95 to 100 mol% of the double bonds in the butadiene portion is hydrogenated, the latter being referred to as an essentially hydrogenated polystyrene and poly(butadiene/styrene) block copolymer. - a diene elastomer, at a content of between 35 and 99 phr (parts by weight per hundred parts of elastomer), - a thermoplastic elastomer system, at a total content of between 1 and 65 phr, said thermoplastic elastomer system comprising at least two block copolymers, referred to as polystyrene and poly(butadiene/styrene) block copolymers, each comprising: - at least one elastomer block of optionally hydrogenated butadiene/styrene random copolymer type, and - at least one thermoplastic block of styrene type, - at least one elastomer block of optionally hydrogenated butadiene/styrene random copolymer type, and - at least one thermoplastic block of styrene type,
A method for forming a three dimensional printed product, comprising: forming a sacrificial support structure using a method comprising: ejecting only a first drop of a print material sequentially at each of a plurality of pillar locations from a print head; curing each first drop; then ejecting only a second drop of the print material sequentially onto the first drop at each of the plurality of pillar locations from the print head after curing each first drop; curing each second drop; then ejecting additional drops of the print material sequentially at two or more of the pillar locations to form a plurality of pillars after curing each second drop; forming the three dimensional printed product using a method comprising ejecting a plurality of third drops onto a plurality of fourth drops while the plurality of fourth drops are uncured; and separating the sacrificial support structure from the three dimensional printed product. ejecting only a first drop of a print material sequentially at each of a plurality of pillar locations from a print head; curing each first drop; then ejecting only a second drop of the print material sequentially onto the first drop at each of the plurality of pillar locations from the print head after curing each first drop; curing each second drop; then ejecting additional drops of the print material sequentially at two or more of the pillar locations to form a plurality of pillars after curing each second drop; forming the three dimensional printed product using a method comprising ejecting a plurality of third drops onto a plurality of fourth drops while the plurality of fourth drops are uncured; and separating the sacrificial support structure from the three dimensional printed product.
A toy comprising a transforming toy, lock releasing means and an item, the transforming toy comprising a locking part adapted to maintain a first form of the transforming toy in a locked state to allow the item accommodated in the transforming toy to be fixed to the transforming toy, wherein if the lock releasing means is attached to the transforming toy, the transforming toy transforms into a second form to allow the item accommodated therein to be released from a fixed state, so that the item is discharged to the outside; wherein the transforming toy further comprises: an upper housing having a plurality of housings (110' and 110") foldable to each other in such a manner as to have accommodation spaces formed at the inside thereof and adapted to maintain any one selected from the first form and the second form; a lower housing located under the upper housing to supportingly maintain the upper housing to the first form; a throwing part rotatably coupled to the lower housing by means of a support stand hinge and a rotary shaft in such a manner as to pressurize the item by means of the elastic force of a spring mounted on the rotary shaft and thus to throw the item to the outside; a latch part located on the lower housing in such a manner as to operate to allow the throwing part to be rotated and thus released from the locked state if the upper housing transforms into the second form; and the locking part located in the upper housing in such a manner as to be changed to a lock releasing position by means of the formation of a magnetic force together with the lock releasing means so that the upper housing is separated from the lower housing and transforms into the second form. an upper housing having a plurality of housings (110' and 110") foldable to each other in such a manner as to have accommodation spaces formed at the inside thereof and adapted to maintain any one selected from the first form and the second form; a lower housing located under the upper housing to supportingly maintain the upper housing to the first form; a throwing part rotatably coupled to the lower housing by means of a support stand hinge and a rotary shaft in such a manner as to pressurize the item by means of the elastic force of a spring mounted on the rotary shaft and thus to throw the item to the outside; a latch part located on the lower housing in such a manner as to operate to allow the throwing part to be rotated and thus released from the locked state if the upper housing transforms into the second form; and the locking part located in the upper housing in such a manner as to be changed to a lock releasing position by means of the formation of a magnetic force together with the lock releasing means so that the upper housing is separated from the lower housing and transforms into the second form.
A method of producing an atomic force probe for a metrology instrument, the method comprising: providing a substrate; forming a flat cap stock which is a pedestal, which extends upwardly from the substrate and which has a base which is conical, and a body extending generally orthogonally to the substrate to define a distal end, wherein the distal end has a substantially flat surface the area of which ranges between about 300 nm 2 and 15μm 2; wherein the distal end is substantially circular in cross-section and is a cylinder distal end, wherein a dimension (di) of the cross-section of the distal end of the flat cap stock is consistent along the length (d 4) of the distal end and is substantially the same as the dimension of a cross-section of the top of the base of the cap stock; characterized by FIB milling the flat cap stock by milling away material of the cap stock in a ring about a center of the distal end to form a tip of the probe having a height that is at least about 500 nm, wherein one milling operation machines substantially the entire length of the resultant tip as the beam makes its way around the circumference of the cap stock under suitable control so that the probe is usable for AFM imaging. providing a substrate; forming a flat cap stock which is a pedestal, which extends upwardly from the substrate and which has a base which is conical, and a body extending generally orthogonally to the substrate to define a distal end, wherein the distal end has a substantially flat surface the area of which ranges between about 300 nm 2 and 15μm 2; wherein the distal end is substantially circular in cross-section and is a cylinder distal end, wherein a dimension (di) of the cross-section of the distal end of the flat cap stock is consistent along the length (d 4) of the distal end and is substantially the same as the dimension of a cross-section of the top of the base of the cap stock; characterized by FIB milling the flat cap stock by milling away material of the cap stock in a ring about a center of the distal end to form a tip of the probe having a height that is at least about 500 nm, wherein one milling operation machines substantially the entire length of the resultant tip as the beam makes its way around the circumference of the cap stock under suitable control so that the probe is usable for AFM imaging.
A method of improving the stability of an aircraft during flight, the method comprising: using data indicative of a speed of the aircraft during flight, automatically causing a deployment of spoilers movably attached to wings of the aircraft when the speed of the aircraft is equal to or exceeds a spoiler-deployment trigger speed that is lower than a maximum operating Mach number of the aircraft; and causing the spoilers to remain deployed when the speed of the aircraft is between the spoiler-deployment trigger speed and the maximum operating Mach number of the aircraft. using data indicative of a speed of the aircraft during flight, automatically causing a deployment of spoilers movably attached to wings of the aircraft when the speed of the aircraft is equal to or exceeds a spoiler-deployment trigger speed that is lower than a maximum operating Mach number of the aircraft; and causing the spoilers to remain deployed when the speed of the aircraft is between the spoiler-deployment trigger speed and the maximum operating Mach number of the aircraft.
An in-vehicle apparatus comprising: a vehicle information collection device configured to collect vehicle information, which is information relating to an emission amount of at least one vehicle at any of a predetermined point, a predetermined section, and a predetermined period of time; a traveling history database configured to accumulate the vehicle information collected by the vehicle information collection device along with a point through which the vehicle has traveled; and a display device configured to display the vehicle information accumulated in the traveling history database for each point through which the vehicle has traveled, wherein the display device is configured to display, by an image on a map including each point for each point through which the vehicle has traveled, the vehicle information accumulated in the traveling history database with a respective one of a plurality of predetermined symbols, according to a cumulative result of the vehicle information for the respective point through which the vehicle has traveled, and wherein the display device is configured to display the symbol on the map at a magnified scale when: a discharge amount of the exhaust gas in the vehicle information is smaller, when a amount of fuel consumption in the vehicle information is smaller, when a vehicle speed in the vehicle information is lower, when an acceleration in the vehicle information is lower, or when the reduction ratio of the use gear of the transmission in the vehicle information is smaller. a vehicle information collection device configured to collect vehicle information, which is information relating to an emission amount of at least one vehicle at any of a predetermined point, a predetermined section, and a predetermined period of time; a traveling history database configured to accumulate the vehicle information collected by the vehicle information collection device along with a point through which the vehicle has traveled; and a display device configured to display the vehicle information accumulated in the traveling history database for each point through which the vehicle has traveled,
Drug eluting device for preventing and treating restenosis and neointimal formation after vascular procedures and/or implantation of implants comprising an implantable and non-implantable stent, wherein said device comprises a therapeutically effective amount of at least one retinoid receptors ligand as active ingredient and a coating matrix, wherein said device is coated with a mixture of all trans- retinoic acid and polylactide-co-glycolide, wherein the ratio of retinoic acid polymer by weight is 25% and the overall dose of all trans-retinoic acid is 2.5 micrograms per millimeter of stent length.
Roller straightening machine for straightening target material, in particular strips and parts made of metal, having a machine frame, an upper and a lower straightening unit, wherein the upper or lower straightening unit each comprises a plurality of upper or lower straightening rollers (7 or 9), wherein the upper straightening rollers are mounted in upper bearing slats and the lower straightening rollers are mounted in lower bearing slats, and at least one collector to collect impurities, in particular those caused by scale, which come off or are removed when the surface of the target material is straightened, which essentially comprises a trough-shaped collection device and is arranged between two adjacent lower straightening rollers of the roller straightening machine, wherein the trough-shaped collection device comprises a base section and a first inclined contact surface, characterised in that, the at least one collector can be inserted and removed again from above between the lower straightening rollers, and the first inclined contact surface comprises a stripper edge, which touches the assigned straightening roller.
Electrical heating device for evaporating volatile substances with adjustable evaporation rate, comprising at least one heating resistor arranged in the device for heating a volatile substance, wherein the device further comprises a rigid substrate, and wherein a potentiometer is formed on said rigid substrate, and wherein the substrate is a printed circuit board incorporating said potentiometer, and wherein the potentiometer is a planar potentiometer having two conductive tracks and a cursor arranged for sliding along said tracks connecting them, wherein said conductive tracks are formed on one surface of the printed circuit board, wherein said potentiometer is electrically associated with said heating resistor for regulating the electric current passing through the resistor for manually regulating the evaporation rate, characterised in that the device further comprises: two wicks and two associated containers, two corresponding heating resistors (3,3'), two potentiometers (4,4') arranged side by side, and a single cursor provided in common for regulating the resistive value of the two potentiometers (4,4'), so that the cursor slides only on the tracks of one potentiometer at a time to set a resistive value only for one potentiometer, whereas the other potentiometer is open.
Use of a plasticizer selected from Alkylsulfonic phenyl ester and/or 2-(octyloxy)benzonitrile in an ion-selective polymeric matrix sensitive to organic ions and ionisable organic molecules with logP values above 0; wherein the polymeric component of said polymeric matrix is made from a polymer selected from the group consisting of poly (n-butylacrylate), cross-linked poly(butylacrylate), polycarbonate, polystyrene, polymethylmethacrylate, poly(vinylchloride-co-vinylacetate-covinylalcohol), polysiloxane, polyvinyl chloride, high molecular weight polyvinyl chloride, or combinations thereof; wherein the polymeric matrix comprises of about 20 to about 40% of polymer; wherein the polymeric matrix comprises of about 50 to about 70% of said plasticizer; and wherein the matrix is not preloaded with the ionophore of the ion of interest.
An apparatus comprising: a torque tube (100;200;300;420) having an axis, a proximal terminus and a distal back leg (102;202); a first spline (106;308) circumferentially disposed on the torque tube (100;200;300;420); a second spline (108;208;302,304,306;416) circumferentially disposed on the torque tube (100;200;300;420); the first spline (106;308) extending from a first location proximal to the distal back leg (102;202) to a first terminal point; and characterised in that: the second spline (108;208;302,304,306;416) extends from a second location proximal to the distal back leg (102;202) to a second terminal point, the second terminal point being distal to the first terminal point. a torque tube (100;200;300;420) having an axis, a proximal terminus and a distal back leg (102;202); a first spline (106;308) circumferentially disposed on the torque tube (100;200;300;420); a second spline (108;208;302,304,306;416) circumferentially disposed on the torque tube (100;200;300;420); the first spline (106;308) extending from a first location proximal to the distal back leg (102;202) to a first terminal point; and characterised in that: the second spline (108;208;302,304,306;416) extends from a second location proximal to the distal back leg (102;202) to a second terminal point, the second terminal point being distal to the first terminal point. the second spline (108;208;302,304,306;416) extends from a second location proximal to the distal back leg (102;202) to a second terminal point, the second terminal point being distal to the first terminal point.
An interceptor UAV for disabling a target UAV, the interceptor UAV comprising: a flight vehicle having: a generally cylindrical fuselage elongated along a fuselage axis; a propulsion system that includes: a first propeller positioned along the fuselage axis; a second propeller positioned along the fuselage axis; and a power source coupled to the first and second propellers to rotate the first propeller in a first direction and rotate the second propeller in a second direction opposite the first direction; a fin carried by the fuselage and being one of three fins, wherein each fin includes a slot that receives the first and second propellers as the propellers rotate; at least one control surface; a guidance system carried by the flight vehicle and coupled to the at least one control surface; and a disabling system carried by the flight vehicle and having a first, inactive mode and a second, active mode, wherein in the second mode, the disabling system is positioned to disable the target UAV. a generally cylindrical fuselage elongated along a fuselage axis; a propulsion system that includes: a first propeller positioned along the fuselage axis; a second propeller positioned along the fuselage axis; and a power source coupled to the first and second propellers to rotate the first propeller in a first direction and rotate the second propeller in a second direction opposite the first direction; a first propeller positioned along the fuselage axis; a second propeller positioned along the fuselage axis; and a power source coupled to the first and second propellers to rotate the first propeller in a first direction and rotate the second propeller in a second direction opposite the first direction; a fin carried by the fuselage and being one of three fins, wherein each fin includes a slot that receives the first and second propellers as the propellers rotate; at least one control surface; a guidance system carried by the flight vehicle and coupled to the at least one control surface; and a disabling system carried by the flight vehicle and having a first, inactive mode and a second, active mode, wherein in the second mode, the disabling system is positioned to disable the target UAV.
A multi-stage missile system comprising: plural stages adapted to be physically coupled to and decoupled from adjacent stages and processor means disposed on a single stage for controlling each stage, said processor means including a guidance processor, a field programmable gate array and serial bus interface means for coupling said processor means to electronic circuitry on said plural stages, said interface means including a physical layer interface and a link interface characterised by providing a daisy chain interconnection between said plural stages. plural stages adapted to be physically coupled to and decoupled from adjacent stages and processor means disposed on a single stage for controlling each stage, said processor means including a guidance processor, a field programmable gate array and serial bus interface means for coupling said processor means to electronic circuitry on said plural stages, said interface means including a physical layer interface and a link interface characterised by providing a daisy chain interconnection between said plural stages.