mhurhangee/ep-ind-claims huggingface dataset:
An electromagnetic interference shielding arrangement comprising a first and a second electro-conductive component (2,3) arranged to be joined, wherein; the first electro-conductive component comprises a first wall and a peripheral flange located at the periphery of the first wall and which projects perpendicularly from the first wall, and a first electro-conductive contact surface on the peripheral flange; and the second electro-conductive component comprises a second wall having a boundary edge, a second electro-conductive contact surface; the arrangement being such that, in the joined configuration of the first and the second electro-conductive components (2,3) the boundary edge of the second wall of the second electro-conductive component is aligned with the first wall of the first component, the first and the second electro-conductive surfaces (6,9) abut to create an electro-conductive engagement region; characterized in that said second electro-conductive component comprises a shielding member extending from the second wall at a location adjacent the second electro-conductive contact surface and projecting perpendicularly to the second wall and separated from the boundary edge by the second electro-conductive contact surface; wherein said electro-conductive engagement region is adjacent the shielding member and the shielding member is disposed adjacently an entrance edge of the electro-conductive engagement region to shield the entrance edge of the engagement region from outgoing electromagnetic waves, the electro-conductive engagement region providing electrical connection between the first and the second electro-conductive components (2,3).
Method for aligning an earth station antenna with a satellite antenna, the method comprising the following steps: - a. sending an uplink signal from the earth station antenna to the satellite antenna; - b. measuring at least a strength of the uplink signal received by the satellite antenna; - c. sending by telemetry the measured strength to a telemetry station: characterised by - d. adjusting an orientation of the earth station antenna in order to maximize the measured strength. - a. sending an uplink signal from the earth station antenna to the satellite antenna; - b. measuring at least a strength of the uplink signal received by the satellite antenna; - c. sending by telemetry the measured strength to a telemetry station: characterised by - d. adjusting an orientation of the earth station antenna in order to maximize the measured strength.
Hub bearing/constant velocity joint assembly (1;1b;1c;1d) for vehicles, comprising: - a hub bearing unit with a radially outer ring or housing, a radially inner, annular, flanged hub, and a plurality of rolling bodies arranged between the annular housing and the flanged hub; - an annular element of a constant velocity joint, configured to engage with the flanged hub by means of an axial splined coupling arranged between the annular element and the flanged hub; and - a clamping system comprising a screw element configured to engage with a threaded section formed on the flanged hub, and provided with a flange-shaped head configured to cooperate with the annular element and axially constrain the flanged hub and the annular element; the assembly being characterized in that the clamping system further comprises an elastic ring and at least one annular seat (27;30) for the elastic ring, formed radially on the inside of the annular element and/or formed radially on the outside of the flange-shaped head, along a radially outer peripheral edge of the flange-shaped head. - a hub bearing unit with a radially outer ring or housing, a radially inner, annular, flanged hub, and a plurality of rolling bodies arranged between the annular housing and the flanged hub; a radially outer ring or housing, a radially inner, annular, flanged hub, and a plurality of rolling bodies arranged between the annular housing and the flanged hub; - an annular element of a constant velocity joint, configured to engage with the flanged hub by means of an axial splined coupling arranged between the annular element and the flanged hub; and - a clamping system comprising a screw element configured to engage with a threaded section formed on the flanged hub, and provided with a flange-shaped head configured to cooperate with the annular element and axially constrain the flanged hub and the annular element; the assembly being characterized in that the clamping system further comprises an elastic ring and at least one annular seat (27;30) for the elastic ring, formed radially on the inside of the annular element and/or formed radially on the outside of the flange-shaped head, along a radially outer peripheral edge of the flange-shaped head. a screw element configured to engage with a threaded section formed on the flanged hub, and provided with a flange-shaped head configured to cooperate with the annular element and axially constrain the flanged hub and the annular element; the assembly being characterized in that the clamping system further comprises an elastic ring and at least one annular seat (27;30) for the elastic ring, formed radially on the inside of the annular element and/or formed radially on the outside of the flange-shaped head, along a radially outer peripheral edge of the flange-shaped head.
A method for injecting a plurality of spacecrafts escaping from a gravitational sphere of the earth, into at least two different orbits in a single launch and then loosing said plurality of spacecrafts, respectively, toward different targets, comprising the steps of: mounting the plurality of the spacecrafts (1 - 4) on a single assist module for assisting a space flight; injecting said single assist module mounting the plurality of spacecrafts, into an interplanetary orbit having a periodicity synchronous with the earth's revolution period; and performing a swing-by maneuver of the single assist module relative to the earth, wherein the orbit of said assist module is changed in a sequential order with respect to each of said plurality of spacecrafts (1 - 4) a half month to several days before said swing-by maneuver is performed. mounting the plurality of the spacecrafts (1 - 4) on a single assist module for assisting a space flight; injecting said single assist module mounting the plurality of spacecrafts, into an interplanetary orbit having a periodicity synchronous with the earth's revolution period; and performing a swing-by maneuver of the single assist module relative to the earth, wherein the orbit of said assist module is changed in a sequential order with respect to each of said plurality of spacecrafts (1 - 4) a half month to several days before said swing-by maneuver is performed.
A centrifugal compressor, comprising: a first stage impeller; a second stage impeller; a side stream injection port located between the first stage impeller and the second stage impeller, the side stream injection port configured to receive a side stream of a fluid; and a capacity control valve, the capacity control valve configured to extend and retract through the side stream injection port, wherein: the capacity control valve has a curved surface facing a direction of flow from the first stage impeller to the second stage impeller; and the capacity control valve is configured to be extended through the side stream injection port between an open position where the side stream of the fluid can flow through the side stream injection port and a closed position where the capacity control valve obstructs flow of the side stream of the fluid through the side stream injection port. a first stage impeller; a second stage impeller; a side stream injection port located between the first stage impeller and the second stage impeller, the side stream injection port configured to receive a side stream of a fluid; and a capacity control valve, the capacity control valve configured to extend and retract through the side stream injection port, wherein: the capacity control valve has a curved surface facing a direction of flow from the first stage impeller to the second stage impeller; and the capacity control valve is configured to be extended through the side stream injection port between an open position where the side stream of the fluid can flow through the side stream injection port and a closed position where the capacity control valve obstructs flow of the side stream of the fluid through the side stream injection port. the capacity control valve has a curved surface facing a direction of flow from the first stage impeller to the second stage impeller; and the capacity control valve is configured to be extended through the side stream injection port between an open position where the side stream of the fluid can flow through the side stream injection port and a closed position where the capacity control valve obstructs flow of the side stream of the fluid through the side stream injection port.
Antenna system comprising: a first antenna element adapted to a first frequency band; a second antenna element adapted to a second frequency band which is different from the first frequency band; wherein: the first antenna element comprises: • a radiating structure provided on a first side of a dielectric substrate of the antenna system, and • at least one resonant structure provided, at least in part, on a second, reverse side of the dielectric substrate; the at least one resonant structure is an open-loop type resonator adapted to resonate at a frequency in the second frequency band; the at least one resonant structure is provided at close proximity to the radiating structure on the reverse side of the dielectric substrate, occupying, on the second side of the dielectric substrate, an area which is only in part covered by the radiating structure on the first side of the dielectric substrate. a first antenna element adapted to a first frequency band; a second antenna element adapted to a second frequency band which is different from the first frequency band; wherein: the first antenna element comprises: • a radiating structure provided on a first side of a dielectric substrate of the antenna system, and • at least one resonant structure provided, at least in part, on a second, reverse side of the dielectric substrate; the at least one resonant structure is an open-loop type resonator adapted to resonate at a frequency in the second frequency band; the at least one resonant structure is provided at close proximity to the radiating structure on the reverse side of the dielectric substrate, occupying, on the second side of the dielectric substrate, an area which is only in part covered by the radiating structure on the first side of the dielectric substrate. the first antenna element comprises: • a radiating structure provided on a first side of a dielectric substrate of the antenna system, and • at least one resonant structure provided, at least in part, on a second, reverse side of the dielectric substrate; • a radiating structure provided on a first side of a dielectric substrate of the antenna system, and • at least one resonant structure provided, at least in part, on a second, reverse side of the dielectric substrate; the at least one resonant structure is an open-loop type resonator adapted to resonate at a frequency in the second frequency band; the at least one resonant structure is provided at close proximity to the radiating structure on the reverse side of the dielectric substrate, occupying, on the second side of the dielectric substrate, an area which is only in part covered by the radiating structure on the first side of the dielectric substrate.
An electrical machine for converting rotational energy into electrical energy, the machine comprising a stator, a winding (110, 211, 311) arranged at the stator, a frame (130, 231, 331, 431) adapted to support the winding and comprising a first wall and a second wall opposing the first wall, a rotor (120, 221) arranged to be rotatable relative to the stator and adapted to induce an electric current in the winding during rotation, and an electrically conductive structure (240, 340, 441, 442) arranged between the winding and the rotor to reduce a capacitance (C wr) between the winding and the rotor, characterized in that the electrically conductive structure comprises a first set of strips extending in parallel from the first wall of the frame towards the second wall of the frame and a second set of strips extending in parallel from the second wall of the frame towards the first wall of the frame, wherein each strip of one of the first set of strips and second set of strips covers a part of a space between two strips of the other one of the first set of strips and second set of strips when viewed in a direction from the winding towards the rotor.
Production plant for workpieces, in particular bodywork components, wherein the production plant has a production zone with a plurality of automatic, programme-controlled production devices (18, 22) and also has a supply station for workpieces, wherein the production plant has a supply station for various application-specific tools and also a conveyor, characterized in that the conveyor connects the production devices to one another and to the external supply stations (10, 11) in a flexible manner, wherein the conveyor has a network of conveying paths and a multiplicity of individually controllable conveying means, which travel over freely programmable conveying tracks in the network of conveying paths, wherein a conveying path extends into, and preferably through, a production device.
A process comprising: contacting at least a portion of a recycle gas stream comprising an alkyl iodide impurity and a vinyl iodide impurity with a first guard bed material to yield a partially treated recycle gas stream, wherein the first guard bed material comprises a first support material, and deposited on the first support material, silver in an amount of from 2% to 10% by weight; contacting at least a portion of the partially treated recycle gas stream with a second guard bed material to yield a treated recycle gas stream, wherein the second guard bed material comprises a second support material, palladium and gold; and contacting an epoxidation feed gas comprising ethylene, oxygen and at least a portion of the treated recycle gas stream with an epoxidation catalyst to yield an epoxidation reaction product comprising ethylene oxide. contacting at least a portion of a recycle gas stream comprising an alkyl iodide impurity and a vinyl iodide impurity with a first guard bed material to yield a partially treated recycle gas stream, wherein the first guard bed material comprises a first support material, and deposited on the first support material, silver in an amount of from 2% to 10% by weight; contacting at least a portion of the partially treated recycle gas stream with a second guard bed material to yield a treated recycle gas stream, wherein the second guard bed material comprises a second support material, palladium and gold; and contacting an epoxidation feed gas comprising ethylene, oxygen and at least a portion of the treated recycle gas stream with an epoxidation catalyst to yield an epoxidation reaction product comprising ethylene oxide.
A device, comprising: a processor; memory (62, 70) connected to the processor, the memory comprising instructions that when executed cause the device to: receive, from a server, a signed server key; reboot a first time; verify the signed server key in a DXE, driver execution environment, of the device's firmware; send a nonce to the server, the nonce being encrypted by the signed server key; receive a message from the server that includes a first portion with a secure command and a second portion that is based on a hash of the nonce; reboot a second time; verify the message in the DXE of the device's firmware; and execute the secure command. a processor; memory (62, 70) connected to the processor, the memory comprising instructions that when executed cause the device to: receive, from a server, a signed server key; reboot a first time; verify the signed server key in a DXE, driver execution environment, of the device's firmware; send a nonce to the server, the nonce being encrypted by the signed server key; receive a message from the server that includes a first portion with a secure command and a second portion that is based on a hash of the nonce; reboot a second time; verify the message in the DXE of the device's firmware; and execute the secure command. receive, from a server, a signed server key; reboot a first time; verify the signed server key in a DXE, driver execution environment, of the device's firmware; send a nonce to the server, the nonce being encrypted by the signed server key; receive a message from the server that includes a first portion with a secure command and a second portion that is based on a hash of the nonce; reboot a second time; verify the message in the DXE of the device's firmware; and execute the secure command.
An electric vehicle comprising: an electric motor for generating driving power for moving a vehicle body of the electric vehicle; a battery for supplying electric power to the electric motor; an outside electric power supply connection unit configured to be connected to an outside electric power supply for supplying the electric power to be charged; a control device for controlling switching between a first connection state in which the battery is connected to the electric motor and a second connection state in which the battery is connected to the outside electric power supply connection unit; and a switch for opening and closing a power supply path connected to the control device; characterized in that the electric vehicle comprises an input device which is configured to be operated by a user to command the control device to perform switching between the first connection state and the second connection state, and when one of the first connection state and the second connection state is switched to the other connection state, the switch opens the power supply path to cut-off electric power supply to the control device for a specified time and the control device is reset, and the control device performs control in the other connection state after the reset of the control device. an electric motor for generating driving power for moving a vehicle body of the electric vehicle; a battery for supplying electric power to the electric motor; an outside electric power supply connection unit configured to be connected to an outside electric power supply for supplying the electric power to be charged; a control device for controlling switching between a first connection state in which the battery is connected to the electric motor and a second connection state in which the battery is connected to the outside electric power supply connection unit; and a switch for opening and closing a power supply path connected to the control device; characterized in that the electric vehicle comprises an input device which is configured to be operated by a user to command the control device to perform switching between the first connection state and the second connection state, and when one of the first connection state and the second connection state is switched to the other connection state, the switch opens the power supply path to cut-off electric power supply to the control device for a specified time and the control device is reset, and the control device performs control in the other connection state after the reset of the control device.
A method for producing a modified conjugated diene rubber, comprising a step of obtaining a modified conjugated diene rubber by reacting a conjugated diene polymer having an alkali metal or alkaline-earth metal active end which is obtained by polymerizing a conjugated diene compound or a conjugated diene compound and an aromatic vinyl compound with at least one of an alkali metal compound and an alkaline-earth metal compound used as a polymerization initiator, with a first hydrocarbyloxysilane compound having the following functional groups (a) and (b): Functional group (a): an alkyl polyether group Functional group (b): a group convertible into an onium. Functional group (a): an alkyl polyether group Functional group (b): a group convertible into an onium.
A method for shimming a magnetic field in which there is an inhomogeneity having more than one functional magnetic component in an expansion of the magnetic field on a set of functions, the magnetic field being produced by a magnet assembly (27, 610) having two distanced assembly ends and an assembly axis, the method comprising: providing a plurality of commonly oriented shim paths (101, 201, 202, 330), said shim paths disposed on a common surface having first and second distanced ends (110, 120, 301, 302), each of said first and second distanced ends having at least one associated connector (103, 104); applying a plurality of coordinately modulated single shim currents along corresponding ones of the plurality of shim paths, each of said shim currents entering said connector at the first end (110, 301), flowing from said connector at the first end to said connector at the second end (120, 302), and exiting said connector at the second end; and suppressing the more than one functional magnetic component of the inhomogeneity in the magnetic field using the plurality of shim currents, wherein the magnet assembly is that of a device for measurement of magnetic resonance of a sample, wherein the magnet assembly further comprises a cavity extending along the assembly axis, wherein the sample is positioned in the cavity along the assembly axis, wherein the magnet assembly comprises mutually opposing pole pieces (28, 80, 630) in the cavity, wherein one of at least two shim panels (18, 18', 90, 100, 200, 300, 400, 640, 642) is placed at or near the surface of each pole piece, wherein the plurality of shim paths is placed on said at least two shim panels, and wherein a portion of each shim path is located within the magnet assembly. providing a plurality of commonly oriented shim paths (101, 201, 202, 330), said shim paths disposed on a common surface having first and second distanced ends (110, 120, 301, 302), each of said first and second distanced ends having at least one associated connector (103, 104); applying a plurality of coordinately modulated single shim currents along corresponding ones of the plurality of shim paths, each of said shim currents entering said connector at the first end (110, 301), flowing from said connector at the first end to said connector at the second end (120, 302), and exiting said connector at the second end; and suppressing the more than one functional magnetic component of the inhomogeneity in the magnetic field using the plurality of shim currents, wherein the magnet assembly is that of a device for measurement of magnetic resonance of a sample, wherein the magnet assembly further comprises a cavity extending along the assembly axis, wherein the sample is positioned in the cavity along the assembly axis, wherein the magnet assembly comprises mutually opposing pole pieces (28, 80, 630) in the cavity, wherein one of at least two shim panels (18, 18', 90, 100, 200, 300, 400, 640, 642) is placed at or near the surface of each pole piece, wherein the plurality of shim paths is placed on said at least two shim panels, and wherein a portion of each shim path is located within the magnet assembly.