mhurhangee/ep-ind-claims huggingface dataset:
Method for treating algae, comprising: (a) providing an ionic liquid, which is a conjugate of an organic base with pK a at least 6 and an acid, (b) providing algae, (c) subjecting algae to cell lysis with the ionic liquid, whereby at least two phases are formed, including a hydrophobic phase and a hydrophilic phase, and (d) separating the hydrophobic phase containing lipids. (a) providing an ionic liquid, which is a conjugate of an organic base with pK a at least 6 and an acid, (b) providing algae, (c) subjecting algae to cell lysis with the ionic liquid, whereby at least two phases are formed, including a hydrophobic phase and a hydrophilic phase, and (d) separating the hydrophobic phase containing lipids.
A yaw stability control system for a vehicle comprising: at least one body-force-disturbance detection unit; and at least one yaw rate sensor arranged to generate a signal ( ψ̇ veh) indicative of the vehicle yaw rate; and a controller responsive to a yaw rate error and arranged to provide an input to a system for performing vehicle yaw stability control operations, characterized in that the controller, in response to a detected body-force-disturbance further is arranged to: activate a yaw angle control part of the controller to start performing control of the yaw angle error ( ψ err) through performing an integration of the yaw rate, from degrees/second to degrees, where the yaw angle error ( ψ err) is obtained as the difference between an integration of a sensed yaw rate ( ψ̇ veh) and an integration of a yaw rate target ( ψ̇ ref) provided from a yaw rate reference model to which a steering wheel angle( δ) is input, in order to obtain a correction of the vehicle yaw angle resulting from the body-force-disturbance; and input to the system for performing vehicle yaw stability control operations a signal to perform a body-force-disturbance yaw stability control operation for eliminating the vehicle yaw angle resulting from the body-force-disturbance and returning the vehicle to a pre body-force-disturbance heading. activate a yaw angle control part of the controller to start performing control of the yaw angle error ( ψ err) through performing an integration of the yaw rate, from degrees/second to degrees, where the yaw angle error ( ψ err) is obtained as the difference between an integration of a sensed yaw rate ( ψ̇ veh) and an integration of a yaw rate target ( ψ̇ ref) provided from a yaw rate reference model to which a steering wheel angle( δ) is input, in order to obtain a correction of the vehicle yaw angle resulting from the body-force-disturbance; and input to the system for performing vehicle yaw stability control operations a signal to perform a body-force-disturbance yaw stability control operation for eliminating the vehicle yaw angle resulting from the body-force-disturbance and returning the vehicle to a pre body-force-disturbance heading.
A fluid communication device comprising a tubular body permitting circulation of a fluid and having a tubular end piece extending in a given axial direction, said tubular end piece being intended to be connected by axial insertion into a plug-in pipe having an outer annular locking neck, the device further comprising an assembly head in which the tubular end piece is mounted, this assembly head comprising a receiving chamber that is coaxial with the tubular end piece and is adapted to receive said plug-in pipe so as to connect it to the tubular end piece, the assembly head also comprising a U-shaped locking element with two arms that insert into said receiving chamber in an insertion direction that is perpendicular to said axial direction, the two arms being adapted to spread apart elastically in said receiving chamber in a direction transverse to said axial direction when the pipe is displaced axially in the receiving chamber to a position of abutment in which it is fully connected to the tubular end piece, said arms further being adapted to engage in said annular neck of the plug-in pipe by moving closer together when said plug-in pipe has reached its position of abutment with respect to the tubular end piece, so as to lock the plug-in pipe in position in the assembly head, characterized in that further provided is an intermediate ring, which is mounted in said receiving chamber so as to be able to slide in said axial direction in order to effect a pre-opening of the locking element, said intermediate ring being adapted to be pushed axially by said plug-in pipe when the latter is displaced in said receiving chamber toward the tubular end piece, said intermediate ring having chamfers that act to elastically spread apart the two arms of the locking element just before said plug-in pipe reaches its position of abutment.
A method of manufacturing an electrolytic capacitor element, including the steps of: forming a dielectric layer on surfaces of a plurality of anode bodies by anodic oxidation at one time; and forming a semiconductor layer on the dielectric layer, in which the anodic oxidation is carried out by limiting a value of the current for the anodic oxidation with respect to the individual anode bodies.
A method for controlling delivery of media data to a plurality of target devices (104, 106, 108) in a target network, the target network being connected to a communications control system (100, 110) via an access network, said method comprising, in the communications control system, the steps of: storing, in a database, target device group control data for controlling the transmission of media data to at least a first plurality of target devices in said target network; receiving a media data delivery initiation request from a source device, said request comprising a target device group indicator; said method being characterized by the steps of: retrieving target device group control data, from said database, on the basis of the target device group indicator contained in said media data delivery initiation request; and transmitting a media data delivery initiation response to said source device, said response comprising said retrieved target device group control data, said retrieved target device group control data identifying at least one network address in said target network to which media data is to be transmitted by said source device, whereby to deliver media data to the first plurality of target devices. storing, in a database, target device group control data for controlling the transmission of media data to at least a first plurality of target devices in said target network; receiving a media data delivery initiation request from a source device, said request comprising a target device group indicator; said method being characterized by the steps of: retrieving target device group control data, from said database, on the basis of the target device group indicator contained in said media data delivery initiation request; and transmitting a media data delivery initiation response to said source device, said response comprising said retrieved target device group control data, said retrieved target device group control data identifying at least one network address in said target network to which media data is to be transmitted by said source device, whereby to deliver media data to the first plurality of target devices. retrieving target device group control data, from said database, on the basis of the target device group indicator contained in said media data delivery initiation request; and transmitting a media data delivery initiation response to said source device, said response comprising said retrieved target device group control data, said retrieved target device group control data identifying at least one network address in said target network to which media data is to be transmitted by said source device, whereby to deliver media data to the first plurality of target devices.
A combustion device which burns fuel ammonia with combustion air in a combustion chamber, the combustion device comprising: a combustor liner which forms the combustion chamber; a burner which is installed at one end of the combustor liner, and is configured to supply natural gas as fuel; a deflection member which is provided on a downstream side of the combustor liner in a flow direction of the combustion gas, and is configured to deflect the flow direction of the combustion gas; and at least one ammonia injection hole which is provided between the burner and an outlet of the deflection member and is configured to supply the fuel ammonia into the combustion chamber, characterized in that an arrangement of the at least one ammonia injection hole or a supply amount of the fuel ammonia supplied from the at least one ammonia injection hole is adjusted to form an ammonia combustion field such that the ammonia combustion field pushes away the combustion gas and the at least one ammonia injection hole supplies the fuel ammonia toward an inner wall surface of the combustor liner facing the at least one ammonia injection hole such that a cross section of the combustor liner after the fuel ammonia is injected from the at least one ammonia injection hole has a biased temperature distribution in which a high temperature portion formed by the combustion gas pushed away by the ammonia combustion field, and a low temperature portion formed by the ammonia combustion field are present. a combustor liner which forms the combustion chamber; a burner which is installed at one end of the combustor liner, and is configured to supply natural gas as fuel; a deflection member which is provided on a downstream side of the combustor liner in a flow direction of the combustion gas, and is configured to deflect the flow direction of the combustion gas; and at least one ammonia injection hole which is provided between the burner and an outlet of the deflection member and is configured to supply the fuel ammonia into the combustion chamber, characterized in that an arrangement of the at least one ammonia injection hole or a supply amount of the fuel ammonia supplied from the at least one ammonia injection hole is adjusted to form an ammonia combustion field such that the ammonia combustion field pushes away the combustion gas and the at least one ammonia injection hole supplies the fuel ammonia toward an inner wall surface of the combustor liner facing the at least one ammonia injection hole such that a cross section of the combustor liner after the fuel ammonia is injected from the at least one ammonia injection hole has a biased temperature distribution in which a high temperature portion formed by the combustion gas pushed away by the ammonia combustion field, and a low temperature portion formed by the ammonia combustion field are present.
Roller tape cover for the protective coverage of a working space of a machine, having a housing which houses a winding shaft, mounted about a rotation axis, having a cover tape wound on the winding shaft, wherein the housing has at least two side elements which extend parallel to the rotation axis and the housing has in longitudinal direction at a first end and at a second end of the winding shaft in each case an end face element, wherein the side elements are connected by means of at least one connecting element, wherein the connecting element extends across the entire length of the side elements, is formed as a separate, strip-shaped part, and has a continuous cross-sectional shape in longitudinal direction, wherein the at least one connecting element is arranged in each case against a longitudinal edge of the housing, which longitudinal edge extends in longitudinal direction, characterized in that the winding shaft is supported at the end face at the end face elements and the at least one connecting element has in each case at the end face element a cutout for receiving a fastening means and the respective end face element can be fixed at the respective connecting element by means of the fastening means, wherein the cutout is in the form of a continuous channel, into which the fastening means in the form of screws are screwed in from the end face element axially into the continuous channel.
Cover to be arranged on a multi-pole connector element, having a first housing part, a second housing part, implemented as a cover element, a first opening (3a, 3b) for passing through cables attached to the connector element, wherein the first opening (3a, 3b) extends over the first housing part and the second housing part, and a second opening (4a, 4b) for passing through cables attached to the connector element, wherein the second opening (4a, 4b) extends over the first housing part and the second housing part, wherein in the assembled condition of the cover on the multi-pole connector element, the first opening (3a, 3b) immediately adjoins the connector element, wherein the second opening (4a, 4b) is spaced apart from the first opening (3a, 3b), wherein a plane defined by the first opening (3a, 3b) is inclined relative to a plane defined by the second opening (4a, 4b) at an angle (α) between 40° and 90°, preferably at an angle (α) between 50° and 80°, characterized in that the cover has a cable bundling element, wherein the cable bundling element is attached to the first housing part and to the second housing part, wherein the cable bundling element is guided through a through-passage opening constructed on the first housing part and through a through-passage opening constructed on the second housing part.
A neural stimulator adapted to stimulate the brain comprising: a hermetic package enclosing electronics, the package including a flange defining holes suitable for accommodating screws for mounting the hermetic package to the cranium; a flexible thin film lead with a first end having bond pads connected to the electronics and a second end having electrodes suitable to stimulate brain tissue, the flexible thin film lead including: a base polymer layer, an interlayer of patterned metal comprising traces and electrodes, and a top polymer layer patterned so as to expose the bond pads and electrodes but insulating the traces. a hermetic package enclosing electronics, the package including a flange defining holes suitable for accommodating screws for mounting the hermetic package to the cranium; a flexible thin film lead with a first end having bond pads connected to the electronics and a second end having electrodes suitable to stimulate brain tissue, the flexible thin film lead including: a base polymer layer, an interlayer of patterned metal comprising traces and electrodes, and a top polymer layer patterned so as to expose the bond pads and electrodes but insulating the traces.
A first wireless communication device comprising: a receiving unit configured to receive a first signal storing first information, said first information including information regarding an information indicating a grade classified in accordance with a numerical value of an error between a setting value and an actual value of transmission power; and a transmission unit configured to transmit a second signal regarding permission of multiple access that allows simultaneous communication of the first wireless communication device with at least one second wireless communication device identified based on the first information, wherein the receiving unit is configured to receive a third signal transmitted by at least one second wireless communication device based on the second signal. a receiving unit configured to receive a first signal storing first information, said first information including information regarding an information indicating a grade classified in accordance with a numerical value of an error between a setting value and an actual value of transmission power; and a transmission unit configured to transmit a second signal regarding permission of multiple access that allows simultaneous communication of the first wireless communication device with at least one second wireless communication device identified based on the first information, wherein the receiving unit is configured to receive a third signal transmitted by at least one second wireless communication device based on the second signal.
Process for a non-catalytic oxidative coupling of methane reaction characterized in that the process comprises: - a step of providing a counter-current shell-tube reactor comprising at least two tubes (3, 5) defining a tubular part and a shell part surrounding the tubular part and at least one inlet (7, 9) to feed a gaseous feed stream and at least one outlet (13, 15) to discharge a product stream; - a step of providing a gaseous feed stream comprising a gas mixture of methane (CH 4) and oxygen (O 2) in a defined molar ratio and preheated to a defined operating inlet temperature; - a step of feeding the gaseous feed stream at least in the tubular part or at least in the shell part of the counter-current shell-tube reactor; and - a step of recovering a product stream. - a step of providing a counter-current shell-tube reactor comprising at least two tubes (3, 5) defining a tubular part and a shell part surrounding the tubular part and at least one inlet (7, 9) to feed a gaseous feed stream and at least one outlet (13, 15) to discharge a product stream; - a step of providing a gaseous feed stream comprising a gas mixture of methane (CH 4) and oxygen (O 2) in a defined molar ratio and preheated to a defined operating inlet temperature; - a step of feeding the gaseous feed stream at least in the tubular part or at least in the shell part of the counter-current shell-tube reactor; and - a step of recovering a product stream.
An electrode plate comprising a current collector, an electrode active material layer and a safety coating disposed between the current collector and the electrode active material layer, wherein the safety coating comprises a polymer matrix, a conductive material and an inorganic filler, wherein the amount of other components is less than or equal to 3wt% and wherein the polymer matrix is fluorinated polyolefin and/or chlorinated polyolefin polymer matrix, wherein based on the total weight of the safety coating, the weight percentage of the polymer matrix is from 35 wt% to 75 wt%; the weight percentage of the inorganic filler is from 10 wt% to 60 wt%.
An aircraft comprising: a first wing, a second wing, and a fuselage, the first wing and a portion of the fuselage defining a first side, and the second wing and another portion of the fuselage defining a second side; and an asymmetric propulsion system, the asymmetric propulsion system comprising: an electric generator; a single turbomachine with a turbine section and a shaft rotatable with at least a portion of the turbine section, the single turbomachine being operable to drive the electric generator and a first propulsor mechanically coupled to the shaft of the single turbomachine, the single turbomachine being mounted to the first side of the aircraft; and a second propulsor assembly mounted to the second side at a location away from the single turbomachine and the first propulsor, the electric generator in electrical communication with the second propulsor assembly for powering the second propulsor assembly. a first wing, a second wing, and a fuselage, the first wing and a portion of the fuselage defining a first side, and the second wing and another portion of the fuselage defining a second side; and an asymmetric propulsion system, the asymmetric propulsion system comprising: an electric generator; a single turbomachine with a turbine section and a shaft rotatable with at least a portion of the turbine section, an electric generator; a single turbomachine with a turbine section and a shaft rotatable with at least a portion of the turbine section, the single turbomachine being operable to drive the electric generator and a first propulsor mechanically coupled to the shaft of the single turbomachine, the single turbomachine being mounted to the first side of the aircraft; and a second propulsor assembly mounted to the second side at a location away from the single turbomachine and the first propulsor, the electric generator in electrical communication with the second propulsor assembly for powering the second propulsor assembly. a first propulsor mechanically coupled to the shaft of the single turbomachine, the single turbomachine being mounted to the first side of the aircraft; and a second propulsor assembly mounted to the second side at a location away from the single turbomachine and the first propulsor, the electric generator in electrical communication with the second propulsor assembly for powering the second propulsor assembly.
Position/displacement measuring system, comprising a sensor head and an encoded scale body (12; 42; 60; 75; 86; 96; 106), the scale body (12; 42; 60; 75; 86; 96; 106) extending in a first direction (x) and in a second direction (y) lying transversely to the first direction (x), and having a region for absolute position determination and a region for incremental position determination with an encoding in the first direction (x), and the region for absolute position determination having an encoding in the second direction (y), the sensor head having a first sensor device with a sensor resolution parallel to the first direction (x), which is associated with the region for incremental position determination, and a second sensor device with a sensor resolution in a second direction (y), which is associated with the region for absolute position determination, characterized in that the scale body is magnetically encoded, in that the region for absolute position determination and the region for incremental position determination are arranged next to each other or are combined with each other in the second direction (y), pole fields (46a, 46b) of the region for incremental position determination and pole fields of the region for absolute position determination being arranged next to one another in the second direction (y) without any spacing between them, in that one or more pole fields (46a; 76a, 76b) of the region for incremental position determination and one or more pole fields (54; 80a, 80b) of the region for absolute position determination are arranged in a strip (48; 78), and the scale body (12; 42; 60; 75; 86; 96; 106) comprises a plurality of strips (48; 78) arranged next to one another in the first direction (x), and in that a strip comprises a first pole field and a second pole field, with the ratio of the length (L 2) of the second pole field to the length (L 1) of the first pole field in the second direction (y) varying for different strips.
A solar cell comprising: a semiconductor substrate; a tunneling layer formed on a surface of the semiconductor substrate; a p-type region and a n-type region formed on the tunneling layer, the p- and n-type regions being disposed next to each other in a direction parallel to the surface of the semiconductor substrate and being separated by a barrier region; an electrode structure (42, 44) electrically connected to the p- and n-type regions, characterised in that the barrier region includes an intrinsic semiconductor portion and a buffer portion located between the intrinsic semiconductor portion and the tunneling layer, the buffer portion having stronger electrical insulating property than the intrinsic semiconductor portion. a semiconductor substrate; a tunneling layer formed on a surface of the semiconductor substrate; a p-type region and a n-type region formed on the tunneling layer, the p- and n-type regions being disposed next to each other in a direction parallel to the surface of the semiconductor substrate and being separated by a barrier region; an electrode structure (42, 44) electrically connected to the p- and n-type regions, characterised in that the barrier region includes an intrinsic semiconductor portion and a buffer portion located between the intrinsic semiconductor portion and the tunneling layer, the buffer portion having stronger electrical insulating property than the intrinsic semiconductor portion.