mhurhangee/ep-ind-claims huggingface dataset:
A flexible lighting device, comprising: - a housing having a longitudinal direction, the housing comprising: reflective side walls extending in the longitudinal direction, a first cavity disposed between the reflective side walls, an opening for the passage of light from the first cavity; - light emitting diodes (LEDs), at least partially arranged, relative to each other, along the longitudinal direction of the housing, each LED having a light-emitting face and side faces; - an interposer structure for providing the electrical connection of the LEDs; and - a reflection element that covers a side of the interposer structure facing the opening and configured as strip comprising through holes in which the LEDs are arranged such that the reflection element surrounds the LEDs on the side faces and that the LEDs are arranged in the first cavity, characterized in that the interposer structure comprises separate interposers spaced apart from each other, and the LEDs are arranged on the separate interposers. - a housing having a longitudinal direction, the housing comprising: reflective side walls extending in the longitudinal direction, a first cavity disposed between the reflective side walls, an opening for the passage of light from the first cavity; - light emitting diodes (LEDs), at least partially arranged, relative to each other, along the longitudinal direction of the housing, each LED having a light-emitting face and side faces; - an interposer structure for providing the electrical connection of the LEDs; and - a reflection element that covers a side of the interposer structure facing the opening and configured as strip comprising through holes in which the LEDs are arranged such that the reflection element surrounds the LEDs on the side faces and that the LEDs are arranged in the first cavity,
Electric engine for a vertical take-off and landing aircraft, wherein the engine is configured to be movable with respect to an aircraft component (102, 342) of the aircraft between a hover position for take-off and landing, and a cruise position for forward flight, wherein the engine comprises a variable area exhaust nozzle mounted to an exhaust portion of the engine, said variable area exhaust nozzle comprising at least one aerodynamic element movable with respect to the engine between an open position and a closed position, characterized in that the engine comprises a transmission having a first end connected to the variable area exhaust nozzle and a second end adapted to be connected to the aircraft component, wherein the transmission is adapted to translate a movement of the engine with respect to the aircraft component into a movement of the at least one aerodynamic element. wherein the engine is configured to be movable with respect to an aircraft component (102, 342) of the aircraft between a hover position for take-off and landing, and a cruise position for forward flight, wherein the engine comprises a variable area exhaust nozzle mounted to an exhaust portion of the engine, said variable area exhaust nozzle comprising at least one aerodynamic element movable with respect to the engine between an open position and a closed position, characterized in that the engine comprises a transmission having a first end connected to the variable area exhaust nozzle and a second end adapted to be connected to the aircraft component, wherein the transmission is adapted to translate a movement of the engine with respect to the aircraft component into a movement of the at least one aerodynamic element.
Valve arrangement for a high pressure pump, having - a pump housing with a depression, - a valve housing which is configured so as to correspond with the depression in the pump housing, with the result that it can be inserted into the depression, and - a clamping disk, the valve housing having at least one radial projection with a first axial bounding face and a second axial bounding face which is arranged so as to lie opposite the former, the clamping disk extending radially over the radial projection of the valve housing and having a third axial bounding face which rests flush on the second axial bounding face of the valve housing, and the clamping disk having a thread on the circumferential side, which thread can be screwed into a thread on the inner side of the depression in such a way that the valve housing is braced in the pump housing via the clamping disk, characterized in that the valve housing and the clamping disk have in each case one bore (50, 52), the bores (50, 52) merging into one another and the diameters corresponding with one another, and in that the valve arrangement also has an actuator and an actuator housing of the valve actuator is plugged into the two bores (50, 52). - a pump housing with a depression, - a valve housing which is configured so as to correspond with the depression in the pump housing, with the result that it can be inserted into the depression, and - a clamping disk, the valve housing having at least one radial projection with a first axial bounding face and a second axial bounding face which is arranged so as to lie opposite the former, the clamping disk extending radially over the radial projection of the valve housing and having a third axial bounding face which rests flush on the second axial bounding face of the valve housing, and the clamping disk having a thread on the circumferential side, which thread can be screwed into a thread on the inner side of the depression in such a way that the valve housing is braced in the pump housing via the clamping disk, characterized in that the valve housing and the clamping disk have in each case one bore (50, 52), the bores (50, 52) merging into one another and the diameters corresponding with one another, and in that the valve arrangement also has an actuator and an actuator housing of the valve actuator is plugged into the two bores (50, 52).
A composition comprising: at least one of an emulsion, dispersion, and suspension comprising, a liquid carrier selected from the group consisting of oil, olefin oligomers, polybutene, polyisoprene, and combinations thereof, and a solid particle comprising an ethylene copolymer wherein the ethylene copolymer has a Melt Index as tested by ASTM D 1238 (190°C/2.16 kg) of no greater than about 2. at least one of an emulsion, dispersion, and suspension comprising, a liquid carrier selected from the group consisting of oil, olefin oligomers, polybutene, polyisoprene, and combinations thereof, and a solid particle comprising an ethylene copolymer wherein the ethylene copolymer has a Melt Index as tested by ASTM D 1238 (190°C/2.16 kg) of no greater than about 2. a liquid carrier selected from the group consisting of oil, olefin oligomers, polybutene, polyisoprene, and combinations a solid particle comprising an ethylene copolymer wherein the ethylene copolymer has a Melt Index as tested by ASTM D 1238 (190°C/2.16 kg) of no greater than about 2.
A method for the production of three-dimensional models by means of a layer application technique, wherein fluid construction material is applied onto a construction field and then a binder material is selectively applied onto the construction material by a printer, characterised in that after application of the fluid construction material, substantially a first half of the length of the construction field is printed on during a first displacement of a print head over the construction field, the printing width of said print head being smaller than the length of the construction field, and during a second displacement of the print head over the construction field the print head is offset and substantially a second half of the length of the construction field is printed on, wherein the print head is staggered by the printing width (sb) after the first displacement and the second half of the length of the construction field is printed on.
Multilayered metal cord with a plurality of concentric layers of wires, comprising one or more inner layer(s) and an outer layer, characterized in that all or some of the gaps situated between the wires of the different layers in the cord comprise an unsaturated thermoplastic elastomer.
An electrophotographic photosensitive member comprising: a support; and a photosensitive layer formed on the support; wherein a surface layer of the electrophotographic photosensitive member comprises particles which comprise: silica particles; and a compound-A adsorbed to each of the silica particles, the silica particles have a volume average particle diameter of 0.1 μm or more and 4 μm or less as measurable by light scattering diffraction on a 3% by mass dispersion of the silica particles in ion-exchanged water, and a specific surface area of 400 m 2 /g or more and 1000 m 2 /g or less as measurable by nitrogen adsorption according to the Brunauer-Emmett-Teller method in accordance with ASTM Standard D3663-78, the compound-A is at least one selected from the group consisting of a tertiary amine compound and a urea compound, and the compound-A has a molecular weight of 150 or more and 550 or less. a support; and a photosensitive layer formed on the support; silica particles; and a compound-A adsorbed to each of the silica particles,
A composition comprising oil obtained from Nigella sativa seeds and one or more surface-active agents, wherein the concentration of thymoquinone in said composition is at least 2 % (w/w), wherein the concentration of said surface-active agent(s) is at least 0.2 % (w/w), and wherein said one or more surface-active agents are selected from the group consisting of D-α-Tocopherol polyethylene glycol succinate (TPGS), lecithin and isolecithin.
A method for performing a quantum gate operation, characterised by: adjusting a first classical control parameter, configured to tune an associated frequency of a first qubit, from a first value to a second value, the first value being selected such that the first qubit is tuned to a first frequency far from a characteristic frequency of an associated resonator and the second value being selected such that the first qubit is tuned to a second frequency near to the characteristic frequency of the resonator; adjusting a second classical control parameter, configured to tune an associated frequency of a second qubit, from a third value to a fourth value, the third value being selected such that the second qubit is tuned to a third frequency far from the characteristic frequency of the resonator; and the fourth value is selected such that the second qubit is tuned to a fourth frequency near to the characteristic frequency of the resonator; and returning the first classical control parameter to the first value; and returning the second classical control parameter to the third value. adjusting a first classical control parameter, configured to tune an associated frequency of a first qubit, from a first value to a second value, the first value being selected such that the first qubit is tuned to a first frequency far from a characteristic frequency of an associated resonator and the second value being selected such that the first qubit is tuned to a second frequency near to the characteristic frequency of the resonator; adjusting a second classical control parameter, configured to tune an associated frequency of a second qubit, from a third value to a fourth value, the third value being selected such that the second qubit is tuned to a third frequency far from the characteristic frequency of the resonator; and the fourth value is selected such that the second qubit is tuned to a fourth frequency near to the characteristic frequency of the resonator; and returning the first classical control parameter to the first value; and returning the second classical control parameter to the third value.
A rocket motor nozzle comprising: a pair of relatively-low-erosion material layers (50, 54, 58); and a relatively-high-erosion material layer (52, 56) sandwiched between the relatively-low-erosion material layers; wherein the relatively-high-erosion material layer is made of a relatively-high-erosion material that erodes more quickly when exposed to flow through the nozzle than does a relatively-low-erosion material or materials of the relatively-low-erosion material layers; and wherein the relatively-low-erosion material layers include: an inner relatively-low-erosion material layer that radially inwardly overlaps the relatively-high-erosion material layer; and an outer relatively-low-erosion material layer that radially outwardly overlaps the relatively-high-erosion material layer, characterized in that each of the pair of relatively-low-erosion material layers and the relatively-high erosion material layers include resin-transfer molded materials. a pair of relatively-low-erosion material layers (50, 54, 58); and a relatively-high-erosion material layer (52, 56) sandwiched between the relatively-low-erosion material layers; wherein the relatively-high-erosion material layer is made of a relatively-high-erosion material that erodes more quickly when exposed to flow through the nozzle than does a relatively-low-erosion material or materials of the relatively-low-erosion material layers; and wherein the relatively-low-erosion material layers include: an inner relatively-low-erosion material layer that radially inwardly overlaps the relatively-high-erosion material layer; and an outer relatively-low-erosion material layer that radially outwardly overlaps the relatively-high-erosion material layer, characterized in that each of the pair of relatively-low-erosion material layers and the relatively-high erosion material layers include resin-transfer molded materials. an inner relatively-low-erosion material layer that radially inwardly overlaps the relatively-high-erosion material layer; and an outer relatively-low-erosion material layer that radially outwardly overlaps the relatively-high-erosion material layer, characterized in that each of the pair of relatively-low-erosion material layers and the relatively-high erosion material layers include resin-transfer molded materials.
A method for wireless communication, comprising: identifying sidelink control information, SCI, associated with a sidelink shared channel transmission to be transmitted to one or more receivers, the SCI comprising one or more fields; computing a cyclic redundancy check, CRC, for the one or more fields within the SCI; identifying a demodulation reference signal, DMRS, sequence for use in transmitting the sidelink shared channel transmission based at least in part on the computed CRC; transmitting a sidelink control channel transmission that includes the SCI and the computed CRC to the one or more receivers; and transmitting the sidelink shared channel transmission based at least in part on the identified DMRS sequence. identifying sidelink control information, SCI, associated with a sidelink shared channel transmission to be transmitted to one or more receivers, the SCI comprising one or more fields; computing a cyclic redundancy check, CRC, for the one or more fields within the SCI; identifying a demodulation reference signal, DMRS, sequence for use in transmitting the sidelink shared channel transmission based at least in part on the computed CRC; transmitting a sidelink control channel transmission that includes the SCI and the computed CRC to the one or more receivers; and transmitting the sidelink shared channel transmission based at least in part on the identified DMRS sequence.
Process to degrease a non-steel metal foil or sheet where the non-steel metal foil or sheet is contaminated with a lubricant, where the contaminated foil or sheet is coiled, characterized in, that the foil coil is first uncoiled and thereafter coiled in a continuous process, in that after having been uncoiled the metal foil or sheet is subjected to DFI burners (4,5) directed towards the foil or sheet on both sides of the foil or sheet so that the foil or sheet is heated from both sides of the foil or sheet, in that the distance from the burners (4, 5) to the foil or sheet, the fuel/oxidant ratio, the power of the burners (4,5) and the speed of the foil or sheet when passing the burners are chosen such that the temperature of the foil or sheet is caused not to exceed the annealing temperature of the foil or sheet and that the fuel/oxidant ratio is over stoichiometric in the interval 1.02 - 1.03.
An emulsified composition comprising 0.01 mass% or more and 1 mass% or less of an anionic surfactant comprising one or more selected from the group consisting of N-acylamino acids, fatty acids having 12 to 24 carbon atoms, alkyl ether carboxylic acids, diacyl glutamic acid lysine, alkylsulfosuccinic acids, N-acyl methyl taurine, alkyl sulfates, polyoxyethylene alkyl ether sulfuric acids, polyoxyethylene alkyl ether phosphoric acids, and salts thereof, a cationic surfactant comprising one or more selected from the group consisting of monoalkyl quaternary ammonium salts, dialkyl quaternary ammonium salts, diacylethyl hydroxyethylmonium methosulfates, and acyl arginine ethyl pyrrolidone carboxylic acid salts, a ceramide, and water, wherein the mass ratio of Component to Component, A/B, is 0.5 or more and 60 or less.
A pressure disinfestation assembly, comprising a pressure chamber for receiving at least one packaging unit with a product to be disinfested, an inert gas supply, which feeds pressurized inert gas into the pressure chamber, and a supply device for increasing an inert gas concentration in a product located in the packaging unit during a pressure disinfestation in the pressure chamber, wherein the supply device comprises an inert gas supply, which is connected to an inert gas discharge region, which in operation is placed inside the packaging unit and inside the product located therein and thus directly supplies inert gas supplied through at least one discharge opening via the inert gas supply to the product so as to increase the inert gas concentration within the packaging unit and/or accelerates an increase in the inert gas concentration.
A pharmaceutical composition comprising ezetimibe, or a pharmaceutically acceptable salt thereof, and curcumin for use in a method of treating a cancer in a patient in need thereof, wherein the cancer is characterized by overexpression of Mdm2.
Emulsion comprising a continuous aqueous phase and a dispersed fatty phase in the form of drops, or conversely, the drops comprising a shell formed of at least one anionic polymer comprising at least one carboxylic acid function and at least one cationic polymer comprising at least two amine functions, wherein the quantity of amine functions provided by the cationic polymer in the fatty phase is between 0.2 μmol and 2 μmol per gram of fatty phase, the cationic polymer being a silicone polymer modified with a primary, secondary or tertiary amine function, and wherein the fatty phase does not comprise polydimethylsiloxane. wherein the quantity of amine functions provided by the cationic polymer in the fatty phase is between 0.2 μmol and 2 μmol per gram of fatty phase, the cationic polymer being a silicone polymer modified with a primary, secondary or tertiary amine function, and wherein the fatty phase does not comprise polydimethylsiloxane.
A method for performing a wireless handoff for user equipment, UE as the UE performs a handoff from a source extended Node-B, e-NB to a target e-NB, the method comprising: detecting a radio link failure, RLF between the UE and the source e-NB by the UE; and maintaining an active communication service at a service layer of the UE after detecting the RLF and as the UE performs the handoff from the source e-NB to the target e-NB, the communication service supporting a first communication between the UE and a third party; wherein after detecting the RLF, the UE transitions to a service re-establishment sub-state such that a protocol layer of the UE is in an LTE_IDLE state, a NAS layer of the UE keeps the current status for the service, such that a radio resource connection, RRC of the UE enters an RRC_IDLE state, and such that a process supporting communication between the UE and the third party continues while payload data between the UE and the third party is unavailable. detecting a radio link failure, RLF between the UE and the source e-NB by the UE; and maintaining an active communication service at a service layer of the UE after detecting the RLF and as the UE performs the handoff from the source e-NB to the target e-NB, the communication service supporting a first communication between the UE and a third party; wherein after detecting the RLF, the UE transitions to a service re-establishment sub-state such that a protocol layer of the UE is in an LTE_IDLE state, a NAS layer of the UE keeps the current status for the service, such that a radio resource connection, RRC of the UE enters an RRC_IDLE state, and such that a process supporting communication between the UE and the third party continues while payload data between the UE and the third party is unavailable.
A pixel of a display device, consisting of: a first organic light emitting device that emits red light having a peak wavelength in the visible spectrum of 600 - 700 nm, further comprising a first emissive layer having a first emissive material, wherein the first emissive material is phosphorescent; a second organic light emitting device that emits green light having a peak wavelength in the visible spectrum of 500 - 600 nm, further comprising a second emissive layer having a second emissive material, wherein the second emissive material is phosphorescent; a third organic light emitting device that emits light blue light having a peak wavelength in the visible spectrum of 400 - 500 nm, further comprising a third emissive layer having a third emissive material, wherein the third emissive material is phosphorescent; and a fourth organic light emitting device that emits deep blue light having a peak wavelength in the visible spectrum of 400 to 500 nm, further comprising a fourth emissive layer having a fourth emissive material, wherein the fourth emissive material is fluorescent; wherein the peak wavelength in the visible spectrum of light emitted by the fourth organic light emitting device is at least 4 nm less than the peak wavelength in the visible spectrum of light emitted by the third organic light emitting device. a first organic light emitting device that emits red light having a peak wavelength in the visible spectrum of 600 - 700 nm, further comprising a first emissive layer having a first emissive material, wherein the first emissive material is phosphorescent; a second organic light emitting device that emits green light having a peak wavelength in the visible spectrum of 500 - 600 nm, further comprising a second emissive layer having a second emissive material, wherein the second emissive material is phosphorescent; a third organic light emitting device that emits light blue light having a peak wavelength in the visible spectrum of 400 - 500 nm, further comprising a third emissive layer having a third emissive material, wherein the third emissive material is phosphorescent; and a fourth organic light emitting device that emits deep blue light having a peak wavelength in the visible spectrum of 400 to 500 nm, further comprising a fourth emissive layer having a fourth emissive material, wherein the fourth emissive material is fluorescent;