mhurhangee/ep-ind-claims huggingface dataset:
A system (450, 500, 600) for mass spectrometry comprising: a curtain gas chamber defined by a curtain plate (454, 504, 604) having an aperture (456, 506, 606) for receiving ions from an ion source and an orifice plate (458, 508, 608) having an inlet (460, 510, 610) into a mass spectrometer; at least one barrier (512, 612) for separating the curtain gas chamber into a first curtain gas chamber region (452A, 502A, 602A) and a second curtain gas chamber region (452B, 502B, 602B); wherein the second curtain gas chamber region (452B, 502B, 602B) comprises a differential mobility spectrometer at least partially sealed to the inlet (460, 510, 610); a first gas source (464B, 514B, 614B) configured to provide a first gas flow into the first curtain gas chamber region (452A, 502A, 602A), wherein a portion of the first gas flow forms a gas outflow (468, 518, 618) directed out of the aperture (456, 506, 606) and into an ion source region; and a second gas source (464A, 514A, 614A) configured to provide a second gas flow into the second curtain gas chamber region (452B, 502B, 602B), wherein the second gas flow to the second curtain gas chamber region (452B, 502B, 602B) forms a gas inflow (466, 516, 616) into the differential mobility spectrometer and inlet (460, 510, 610); and a heating element (470, 620) configured to heat the gas inflow (466, 516, 616), a portion of the heated gas inflow (466, 516, 616) directed into the inlet (460, 510, 610) of the mass spectrometer wherein the portion of the heated gas inflow (466, 516, 616) is at a substantially higher temperature than the gas outflow (468, 518, 618). a curtain gas chamber defined by a curtain plate (454, 504, 604) having an aperture (456, 506, 606) for receiving ions from an ion source and an orifice plate (458, 508, 608) having an inlet (460, 510, 610) into a mass spectrometer; at least one barrier (512, 612) for separating the curtain gas chamber into a first curtain gas chamber region (452A, 502A, 602A) and a second curtain gas chamber region (452B, 502B, 602B); wherein the second curtain gas chamber region (452B, 502B, 602B) comprises a differential mobility spectrometer at least partially sealed to the inlet (460, 510, 610); a first gas source (464B, 514B, 614B) configured to provide a first gas flow into the first curtain gas chamber region (452A, 502A, 602A), wherein a portion of the first gas flow forms a gas outflow (468, 518, 618) directed out of the aperture (456, 506, 606) and into an ion source region; and a second gas source (464A, 514A, 614A) configured to provide a second gas flow into the second curtain gas chamber region (452B, 502B, 602B), wherein the second gas flow to the second curtain gas chamber region (452B, 502B, 602B) forms a gas inflow (466, 516, 616) into the differential mobility spectrometer and inlet (460, 510, 610); and a heating element (470, 620) configured to heat the gas inflow (466, 516, 616), a portion of the heated gas inflow (466, 516, 616) directed into the inlet (460, 510, 610) of the mass spectrometer wherein the portion of the heated gas inflow (466, 516, 616) is at a substantially higher temperature than the gas outflow (468, 518, 618).
A polyester binder fiber comprising: a polyester and a polymer having a repeating unit represented by the following formula in a proportion of 0.1 to 5.0 mass% based on the mass of the polyester, the polyester binder fiber having a crystallization temperature measured by differential calorimetry in a range of 100°C or higher and 250°C or lower, the polyester binder fiber having a fiber length of 0.5 to 50 mm where R 1 and R 2 are substituents each comprising arbitrary atoms chosen from C, H, N, O, S, P, and a halogen atom, the sum of the molecular weights of R 1 and R 2 is 40 or more, and n is a positive integer. a polyester and a polymer having a repeating unit represented by the following formula in a proportion of 0.1 to 5.0 mass% based on the mass of the polyester, the polyester binder fiber having a crystallization temperature measured by differential calorimetry in a range of 100°C or higher and 250°C or lower, the polyester binder fiber having a fiber length of 0.5 to 50 mm where R 1 and R 2 are substituents each comprising arbitrary atoms chosen from C, H, N, O, S, P, and a halogen atom, the sum of the molecular weights of R 1 and R 2 is 40 or more, and n is a positive integer.
A process for the production of a mono-olefin by reacting an oxygen containing gas with a gaseous paraffinic hydrocarbon to form said mono-olefin, which process utilizes an apparatus which comprises a first supply means which comprises a plurality of first outlets for delivery of the oxygen containing gas, and a second supply means which comprises a plurality of second outlets for delivery of the gaseous paraffinic hydrocarbon, a resistance zone and a reaction zone, wherein the resistance zone is porous, is positioned downstream of the first and second supply means with respect to the flow of the oxygen containing gas and the gaseous paraffinic hydrocarbon and is in fluid communication with the first and second supply means, the reaction zone is positioned downstream of the resistance zone with respect to the flow of the oxygen containing gas and the gaseous paraffinic hydrocarbon and is fluid communication with the resistance zone, and wherein the first supply means and the second supply means are arranged such that the first gas and the second gas are contacted in an essentially parallel manner and mixed prior to contacting the resistance zone, which process comprises: passing oxygen containing gas into said first supply means and passing gaseous paraffinic hydrocarbon into said second supply means, such that the gaseous paraffinic hydrocarbon is contacted in an essentially parallel manner and mixed with the oxygen-containing gas, passing the gaseous mixture to the reaction zone via the porous resistance zone and partially combusting the gaseous mixture in the reaction zone in the presence of a catalyst which is capable of supporting combustion beyond the fuel rich limit of flammability, to produce the mono-olefin. passing oxygen containing gas into said first supply means and passing gaseous paraffinic hydrocarbon into said second supply means, such that the gaseous paraffinic hydrocarbon is contacted in an essentially parallel manner and mixed with the oxygen-containing gas, passing the gaseous mixture to the reaction zone via the porous resistance zone and partially combusting the gaseous mixture in the reaction zone in the presence of a catalyst which is capable of supporting combustion beyond the fuel rich limit of flammability, to produce the mono-olefin.
Support member for air-carrying pipes of portable air conditioners which can be applied to windows comprising a frame and respective guides (G1, G2), the support member comprising a first module provided with a slit adapted to accommodate the air pipe and at least one second module adapted to be coaxially sliding on said first module, wherein said at least one second module is continuously slideable with respect to said first module in order to make the length of said support member modifiable, and said first module and said at least one second module are provided, in correspondence with respective ends (12a, 14a), with respective stabilizing members (11, 13), configured to be inserted into and to cooperate with the sliding guides (G1, G2) provided on the frame of the window, characterized in that said support member comprises clamping members suitable to reciprocally clamp the first module and the at least one second module into a reciprocal stable sliding position and comprising at least one hole provided on a first sliding surface of the first module and a groove provided on a second sliding surface of the at least one second module and facing said first sliding surface, said at least one hole being configured to cooperate, during use, with said groove to allow fixing means to block the position of said second module with respect to said at least one first module and in that said stabilizing members (11, 13) are integrated in said first module and second module, wherein said respective ends (12a, 14a) are tapered and have respective substantially flat terminal portions (15a, 15b), with a constant thickness, which define said stabilizing members (11, 13).
An explosion-proof housing which forms an interior for accommodating components that can form ignition sources, with a first housing part that has a first section that comprises a first surface and a second housing part that has a second section that comprises a second surface, wherein the first section and/or the second section is a wall section, wherein the first surface and the second surface delimit an intermediate region, wherein the first section and the second section are pressed against one another by means of a clamping device under elastic deformation of the wall section (13, 20), so that the intermediate region is geometrically closed in a flameproof manner by the elastic deformation of the wall section (13, 20).
A method for producing a component for a turbomachine, in which a component is provided which comprises at least one region made of an intermetallic material which is formed from an intermetallic compound or comprises an intermetallic phase as the largest constituent, in particular representing more than 50 vol.%, microplasticization being carried out in the intermetallic material at least partially at a surface or interface in a region (14, 17) close to the surface or close to the interface, characterized in that before the microplasticization, a plate is applied to the region subjected to the microplasticization.
A pixel (10, 12, 14, 16) comprising: a CMOS support; exactly a first organic photodetector (10A, 12A, 14A, 16A), a second organic photodetector (10B, 12B, 14B, 16B) and a third organic photodetector (10C, 12C, 14C, 16C); and a same lens vertically in line with said first, second and third organic photodetectors, wherein the first and second organic photodetectors comprise a first active layer (120, 100A, 120A, 120B, 160A), made of a same first material, and the third organic photodetector comprises a second active layer, made of a second material, different from the first material, capable of absorbing the electromagnetic waves of the visible spectrum, characterized in that the first material is capable of absorbing the electromagnetic waves of part of the infrared spectrum. a CMOS support; exactly a first organic photodetector (10A, 12A, 14A, 16A), a second organic photodetector (10B, 12B, 14B, 16B) and a third organic photodetector (10C, 12C, 14C, 16C); and a same lens vertically in line with said first, second and third organic photodetectors, wherein the first and second organic photodetectors comprise a first active layer (120, 100A, 120A, 120B, 160A), made of a same first material, and the third organic photodetector comprises a second active layer, made of a second material, different from the first material, capable of absorbing the electromagnetic waves of the visible spectrum, characterized in that the first material is capable of absorbing the electromagnetic waves of part of the infrared spectrum.
A gas turbine engine component comprising: a ceramic matrix composite body including an interior surface characterized by defining a blind cavity; a barrier coating disposed on an exterior of the CMC body; and by a ceramic body (80; 180) in the blind cavity and lining at least a portion of the interior surface of the CMC body, the ceramic body (80; 180) defining an open, interconnected network of pores. a ceramic matrix composite body including an interior surface characterized by defining a blind cavity; a barrier coating disposed on an exterior of the CMC body; and by a ceramic body (80; 180) in the blind cavity and lining at least a portion of the interior surface of the CMC body, the ceramic body (80; 180) defining an open, interconnected network of pores.
Process of producing a clad plate comprising a first, structural-strength-providing base layer of a first material and on at least one side thereof a second, wear-resistance-providing cladding layer of a second material, wherein the first material and the second material are relatively ductile and brittle, respectively, whereby the process comprises the steps of: - placing the second layer onto the first layer to form a multilayer plate assembly; - making slits (6, 6a, 6b) in the second layer, - wherein the slits (6, 6a, 6b) are made as to extend from the outer surface of the second layer towards the boundary with the first layer, preferably to extend throughout the whole thickness of the second layer. - placing the second layer onto the first layer to form a multilayer plate assembly; - making slits (6, 6a, 6b) in the second layer, - wherein the slits (6, 6a, 6b) are made as to extend from the outer surface of the second layer towards the boundary with the first layer, preferably to extend throughout the whole thickness of the second layer.
A method comprising: obtaining data associated with aircraft flight parameters pertaining to collective input, engine power, and shaft torque when an aircraft is being operated in flight; processing the data to determine that at a weighted combination of the collective input, engine power, and shaft torque indicates a step change in value in an amount greater than a threshold magnitude as a function of time during flight; and decoupling a load from the aircraft based at least in part on determining that the weighted combination of the collective input, engine power, and shaft torque indicates the step change in value. obtaining data associated with aircraft flight parameters pertaining to collective input, engine power, and shaft torque when an aircraft is being operated in flight; processing the data to determine that at a weighted combination of the collective input, engine power, and shaft torque indicates a step change in value in an amount greater than a threshold magnitude as a function of time during flight; and decoupling a load from the aircraft based at least in part on determining that the weighted combination of the collective input, engine power, and shaft torque indicates the step change in value.
A pharmaceutical composition comprising a pharmaceutically acceptable carrier and activated protein C for use in the therapy of retinal leakage and choroidal neovascularization.
System for mounting a refrigerant compressor housing to a base plate having threaded holes, the system comprising at least two screw pins and one clip to connect the two screw pins, wherein each screw pin, as seen in its longitudinal direction, has a threaded portion for screwing the screw pin into a threaded hole of a base plate, the threaded portion being followed by a middle portion to be inserted into a respective opening of a refrigerant compressor housing, the middle portion being followed by a neck portion having a smaller diameter than the middle portion, the neck portion being followed by a head portion, the head portion having a larger diameter than the neck portion, wherein the elongate clip has one slot (7,8) in each of its two end portions, the first slot having a width equal to the diameter of the neck portion of the screw pin and being oriented in longitudinal direction of the clip, the second slot narrowing to a width smaller than the diameter of the neck portion of the screw pin and then enlarging to a diameter equal to the diameter of the neck portion and the second slot being oriented normal to the longitudinal direction of the clip.
A data structure recorded in a recording medium conforming to the Blu-ray Disc standard including: image data adapted for 2D (2 Dimensional) display of a sub-image corresponding to said image data and made up of a caption or menu button; and a table in which is arranged, with regard to said sub-image corresponding to said image data, offset information which is made up of - an offset direction (offset_flag) representing a direction of shift of an L image for a left eye and R image for a right eye, adapted for 3D display of the sub-image on a display unit, and - an offset value (offset_value) representing an amount of shift, wherein said offset information is arranged along with a playing point-in-time (offset_pts) of the sub-image, said playing point-in-time (offset_pts) being comprised in the table, wherein the table is arranged in an offset_metadata() field located in a data_block() field of an ExtensionData() field of a playlist file of the recording medium. image data adapted for 2D (2 Dimensional) display of a sub-image corresponding to said image data and made up of a caption or menu button; and a table in which is arranged, with regard to said sub-image corresponding to said image data, offset information which is made up of - an offset direction (offset_flag) representing a direction of shift of an L image for a left eye and R image for a right eye, adapted for 3D display of the sub-image on a display unit, and - an offset value (offset_value) representing an amount of shift, - an offset direction (offset_flag) representing a direction of shift of an L image for a left eye and R image for a right eye, adapted for 3D display of the sub-image on a display unit, and - an offset value (offset_value) representing an amount of shift,
A method for radio frequency secure communication performed by a terminal, comprising: generating magnetic channel data, and transmitting the magnetic channel data via a magnetic channel; establishing a radio frequency link with a peer device which feeds back response information of the magnetic channel data; and wherein: based on the magnetic channel data, calculating parameters of the radio frequency channel; and wherein based on the parameters of the radio frequency channel, receiving the response information of the magnetic channel data fed back from the peer device on a corresponding radio frequency channel; generating first radio frequency data, encrypting the first radio frequency data using the magnetic channel data, and transmitting the encrypted first radio frequency data to the peer device via the radio frequency link; and receiving encrypted second radio frequency data transmitted by the peer device via the radio frequency link and decrypting the encrypted second radio frequency data using the magnetic channel data. generating magnetic channel data, and transmitting the magnetic channel data via a magnetic channel; establishing a radio frequency link with a peer device which feeds back response information of the magnetic channel data; and wherein: based on the magnetic channel data, calculating parameters of the radio frequency channel; and wherein based on the parameters of the radio frequency channel, receiving the response information of the magnetic channel data fed back from the peer device on a corresponding radio frequency channel; based on the magnetic channel data, calculating parameters of the radio frequency channel; and wherein based on the parameters of the radio frequency channel, receiving the response information of the magnetic channel data fed back from the peer device on a corresponding radio frequency channel; generating first radio frequency data, encrypting the first radio frequency data using the magnetic channel data, and transmitting the encrypted first radio frequency data to the peer device via the radio frequency link; and receiving encrypted second radio frequency data transmitted by the peer device via the radio frequency link and decrypting the encrypted second radio frequency data using the magnetic channel data.
A method of a User Equipment, in the following also referred to as UE, configured with Discontinuous Reception, in the following also referred to as DRX, comprising: starting a period in response to start of an Uplink, in the following also referred to as UL, transmission; and monitoring a first downlink control signaling including a puncturing indication during the period; wherein the period ends in response to an end of the UL transmission, and the method further comprises suspending or stopping the UL transmission if the first downlink control signaling is received by the UE; and characterized by: stopping the period when the first downlink control signaling is received. starting a period in response to start of an Uplink, in the following also referred to as UL, transmission; and monitoring a first downlink control signaling including a puncturing indication during the period; wherein the period ends in response to an end of the UL transmission, and the method further comprises suspending or stopping the UL transmission if the first downlink control signaling is received by the UE; and characterized by: stopping the period when the first downlink control signaling is received.
An unmanned aerial vehicle comprising: - a self-contained electrical power source (12; 44A, 44B), - a housing in the interior volume of which electronic equipment (46, 48A, 48B, 48C, 48D, 50, 52, 54, 56) electrically powered by the power source (12; 44A, 44B) is arranged, including an electronic autopilot, at least one controller (48; 48A, 48B, 48C, 48D) of at least one propeller motor and a radio-frequency transmitter/receiver for remote-controlled propulsion or lift actuation of the aerial vehicle, the housing comprising an electrically conductive wall extending so as to protect this electronic equipment (46, 48A, 48B, 48C, 48D, 50, 52, 54, 56) from any electromagnetic field outside the housing, - at least one rotary wing (16A, 16B, 16C, 16D) with a motorized propeller (32; 32A, 32B, 32C, 32D) for maintaining flight by propulsion or lift on remote control of electronic equipment, and - for each motorized propeller (32; 32A, 32B, 32C, 32D), a mechanical protection structural element (34; 34A, 34B, 34C, 34D), characterized in that an electrically conductive strip electrically connected to the conductive wall of the housing extends at the periphery of each propeller's mechanical protection structural element (34; 34A, 34B, 34C, 34D) as an add-on element or formed by direct deposition of an electrically conductive material at the periphery of the mechanical protection structural element (34; 34A, 34B, 34C, 34D) by a surface treatment method. - a self-contained electrical power source (12; 44A, 44B), - a housing in the interior volume of which electronic equipment (46, 48A, 48B, 48C, 48D, 50, 52, 54, 56) electrically powered by the power source (12; 44A, 44B) is arranged, including an electronic autopilot, at least one controller (48; 48A, 48B, 48C, 48D) of at least one propeller motor and a radio-frequency transmitter/receiver for remote-controlled propulsion or lift actuation of the aerial vehicle, the housing comprising an electrically conductive wall extending so as to protect this electronic equipment (46, 48A, 48B, 48C, 48D, 50, 52, 54, 56) from any electromagnetic field outside the housing, - at least one rotary wing (16A, 16B, 16C, 16D) with a motorized propeller (32; 32A, 32B, 32C, 32D) for maintaining flight by propulsion or lift on remote control of electronic equipment, and - for each motorized propeller (32; 32A, 32B, 32C, 32D), a mechanical protection structural element (34; 34A, 34B, 34C, 34D),