mhurhangee/ep-ind-claims huggingface dataset:
A device comprising: a semiconductor structure comprising a III-nitride structure with a light emitting layer disposed between an n-type region and a p-type region, the light emitting layer being configured to emit light having a first peak wavelength; a first phosphor disposed in a path of light emitted by the light emitting layer, the first phosphor being configured to emit light having a second peak wavelength; and a second phosphor disposed in a path of light emitted by the light emitting layer, the second phosphor being configured to emit light having a third peak wavelength, wherein: the second phosphor comprises Eu 3 +-activated red phosphor, and the second phosphor is selected from a group comprising oxides, oxyhalogenides, garnets, vanadates, tungstates, borates, silicates, germanates and mixtures thereof and in the excitation spectrum of the second phosphor at 298K and 1.013 bar, a maximum intensity in a wavelength range between 460 nm and 470 nm is at least 5% of a maximum intensity in a wavelength range between 220 nm to 320 nm. a semiconductor structure comprising a III-nitride structure with a light emitting layer disposed between an n-type region and a p-type region, the light emitting layer being configured to emit light having a first peak wavelength; a first phosphor disposed in a path of light emitted by the light emitting layer, the first phosphor being configured to emit light having a second peak wavelength; and a second phosphor disposed in a path of light emitted by the light emitting layer, the second phosphor being configured to emit light having a third peak wavelength, wherein: the second phosphor comprises Eu 3 +-activated red phosphor, and the second phosphor is selected from a group comprising oxides, oxyhalogenides, garnets, vanadates, tungstates, borates, silicates, germanates and mixtures thereof and in the excitation spectrum of the second phosphor at 298K and 1.013 bar, a maximum intensity in a wavelength range between 460 nm and 470 nm is at least 5% of a maximum intensity in a wavelength range between 220 nm to 320 nm. the second phosphor comprises Eu 3 +-activated red phosphor, and the second phosphor is selected from a group comprising oxides, oxyhalogenides, garnets, vanadates, tungstates, borates, silicates, germanates and mixtures thereof and in the excitation spectrum of the second phosphor at 298K and 1.013 bar, a maximum intensity in a wavelength range between 460 nm and 470 nm is at least 5% of a maximum intensity in a wavelength range between 220 nm to 320 nm.
A sole structure comprising: a plate having an upper surface and a lower surface; a first cleat (106, 170, 172, 174, 176) extending from the lower surface, the first cleat (106, 170, 172, 174, 176) having a first height and having a first tip surface; an auxetic structure having an inner surface affixed to the lower surface and having an outer surface; wherein the inner surface is constrained by the lower surface; and wherein the outer surface is spaced closer to the lower surface than to the first tip surface. a plate having an upper surface and a lower surface; a first cleat (106, 170, 172, 174, 176) extending from the lower surface, the first cleat (106, 170, 172, 174, 176) having a first height and having a first tip surface; an auxetic structure having an inner surface affixed to the lower surface and having an outer surface; wherein the inner surface is constrained by the lower surface; and wherein the outer surface is spaced closer to the lower surface than to the first tip surface.
Safe method for controlling a position of an aircraft in relation to an authorised flight envelope, said method comprising the following steps: - measuring a first value of at least one flight characteristic of said aircraft via a main measurement chain of said aircraft, said at least one flight characteristic being used by a flight control system of said aircraft to automatically pilot said aircraft in the authorised flight envelope, - emitting at least one analogue signal which is a function of said at least one flight characteristic of said aircraft via an analogue backup measurement chain of said aircraft, - applying a first autopilot mode of said aircraft, the application being carried out by default by said flight control system by using said first value of at least one flight characteristic of said aircraft to automatically pilot said aircraft, the method being characterised by the following steps: - applying a second autopilot mode of said aircraft, the application being carried out by said flight control system by using said at least one analogue signal to automatically pilot said aircraft as soon as at least one of said at least one flight characteristic of said aircraft exceeds a predetermined limit or as soon as at least one difference between said first value of a flight characteristic and a second value of said flight characteristic determined from of said analogue signal is greater than or equal to a predetermined value, in order to maintain the aircraft in the authorised flight envelope or bring said aircraft back into said envelope. - measuring a first value of at least one flight characteristic of said aircraft via a main measurement chain of said aircraft, said at least one flight characteristic being used by a flight control system of said aircraft to automatically pilot said aircraft in the authorised flight envelope, - emitting at least one analogue signal which is a function of said at least one flight characteristic of said aircraft via an analogue backup measurement chain of said aircraft, - applying a first autopilot mode of said aircraft, the application being carried out by default by said flight control system by using said first value of at least one flight characteristic of said aircraft to automatically pilot said aircraft, - applying a second autopilot mode of said aircraft, the application being carried out by said flight control system by using said at least one analogue signal to automatically pilot said aircraft as soon as at least one of said at least one flight characteristic of said aircraft exceeds a predetermined limit or as soon as at least one difference between said first value of a flight characteristic and a second value of said flight characteristic determined from of said analogue signal is greater than or equal to a predetermined value, in order to maintain the aircraft in the authorised flight envelope or bring said aircraft back into said envelope.
A computer system where agents function on a set of devices, each device having a set of resources (4, 5, 7), the system comprising: a set of agents (110, 120); for each device, an environment on which agents run; and for each device, a set of services (102, 104, 106, 108) each service providing access by an agent to a resource, each agent having an associated permission list indicating which service the agent may access; wherein each type of service (102, 104, 106, 108) provides a standardized interface to all agents (110, 120) so that each type of service (102, 104, 106, 108) is accessed by all agents (110, 120) in a manner standard to that service type and where each agent may move from an environment on one device to an environment on another device. a set of agents (110, 120); for each device, an environment on which agents run; and for each device, a set of services (102, 104, 106, 108) each service providing access by an agent to a resource, each agent having an associated permission list indicating which service the agent may access; wherein each type of service (102, 104, 106, 108) provides a standardized interface to all agents (110, 120) so that each type of service (102, 104, 106, 108) is accessed by all agents (110, 120) in a manner standard to that service type and where each agent may move from an environment on one device to an environment on another device.
An apparatus comprising: a controller integrated circuit, IC, configured to couple to a circuit board; a microelectromechanical system, MEMS, IC mounted to a first side of the controller IC, the MEMS IC including: a device layer having a plurality of gaps, the plurality of gaps forming multiple moveable portions and a single anchor, the single anchor configured to support the multiple moveable portions; and a cap layer coupled to the device layer and configured to maintain a vacuum about the multiple moveable portions and to limit out-of-plane movement of the multiple moveable portions; and wherein the controller IC includes the first side coupled to the MEMS IC opposite the cap layer, and a through silicon via extending through the controller IC from the first side to a second side of the controller IC, the through silicon via configured to electrically couple contacts located on the first side of the controller IC with contacts located on the second side of the controller IC; and wherein the MEMS IC is coupled to the through silicon via. a controller integrated circuit, IC, configured to couple to a circuit board; a microelectromechanical system, MEMS, IC mounted to a first side of the controller IC, the MEMS IC including: a device layer having a plurality of gaps, the plurality of gaps forming multiple moveable portions and a single anchor, the single anchor configured to support the multiple moveable portions; and a cap layer coupled to the device layer and configured to maintain a vacuum about the multiple moveable portions and to limit out-of-plane movement of the multiple moveable portions; and a device layer having a plurality of gaps, the plurality of gaps forming multiple moveable portions and a single anchor, the single anchor configured to support the multiple moveable portions; and a cap layer coupled to the device layer and configured to maintain a vacuum about the multiple moveable portions and to limit out-of-plane movement of the multiple moveable portions; and wherein the controller IC includes the first side coupled to the MEMS IC opposite the cap layer, and a through silicon via extending through the controller IC from the first side to a second side of the controller IC, the through silicon via configured to electrically couple contacts located on the first side of the controller IC with contacts located on the second side of the controller IC; and wherein the MEMS IC is coupled to the through silicon via.
A smart card reader for generating electronic signatures in conjunction with an inserted smart card comprising: - a communication interface for communicating with a host computer; - a smart card connector for communicating with the smart card; - a first memory component for securely storing one or more cryptographic keys; - a user interface comprising a user output interface for presenting information to a user; - a data processing component for communicating with the host computer, communicating with the smart card and driving the user interface; said smart card reader being adapted to exchange smart card commands with a smart card using the smart card connector; said smart card reader being further adapted to present to the user data for review and approval using the output interface; wherein said smart card reader further comprises a second memory component having a log file stored therein; wherein said smart card reader is further adapted to operate in a secure logging mode in which the smart card reader logs in said log file security related events relative to the reader or the reader's usage; wherein said smart card reader is characterised in that it is further adapted to log in said log file data representative of the data for review and approval; and wherein said smart card reader is further adapted to generate a reader signature on said log file using at least one of the one or more cryptographic keys stored in said first memory. - a communication interface for communicating with a host computer; - a smart card connector for communicating with the smart card; - a first memory component for securely storing one or more cryptographic keys; - a user interface comprising a user output interface for presenting information to a user; - a data processing component for communicating with the host computer, communicating with the smart card and driving the user interface;
Profile clamp for connecting two tubular bodies, wherein the profile clamp has a clamp band having a profile cross section open radially on the inside, wherein the clamp band has a first transition section at at least one end and an adjoining, radially projecting clamping element, and wherein the clamping element can be clamped in the circumferential direction in order to tighten the profile clamp, wherein the width of a base of the profile cross section increases uniformly towards the clamping element from the end of the first transition section remote from the clamping element, wherein the profile cross section has two opposite end edges, the tangents of which enclose a second angle (β) with respect to one another, characterized in that the second angle (β) is approximately 90°, resulting in an opening angle of approximately 45°, into which a flange can be inserted, on each side of the profile cross section, wherein the second angle (β) is substantially constant in the first transition section.
A method (300, 400) to program a Media Access Control, MAC, address table, the method comprising: obtaining information identifying one or more Virtual Tunnel End Point, VTEP, Affinity Groups, VAGs, each of the one or more VAGs including an identification of only one VTEP per leaf node comprising one or more VTEPs; generating a unique Filtering Identifier, FID, for each of the one or more VAGs; obtaining information identifying assignment of each Virtual Routing and Forwarding element, VRF, of a plurality of VRFs instantiated on each leaf node to one of the one or more VAGs; based on the obtained information identifying assignment of each VRF of the plurality of VRFs to one of the one or more VAGs, grouping VRFs assigned to each VAG into a different VRF subset, thereby generating one or more VRF subsets; and populating the MAC address table with at least one entry having one of the FIDs, a MAC address of a leaf node, and the one or more VRF subsets. obtaining information identifying one or more Virtual Tunnel End Point, VTEP, Affinity Groups, VAGs, each of the one or more VAGs including an identification of only one VTEP per leaf node comprising one or more VTEPs; generating a unique Filtering Identifier, FID, for each of the one or more VAGs; obtaining information identifying assignment of each Virtual Routing and Forwarding element, VRF, of a plurality of VRFs instantiated on each leaf node to one of the one or more VAGs; based on the obtained information identifying assignment of each VRF of the plurality of VRFs to one of the one or more VAGs, grouping VRFs assigned to each VAG into a different VRF subset, thereby generating one or more VRF subsets; and populating the MAC address table with at least one entry having one of the FIDs, a MAC address of a leaf node, and the one or more VRF subsets.
A method for assembling a plug assembly for plugging one or more ports (66, 62) of a gas turbine engine, the method comprising: inserting a first arm into a sheath through-passage of a sheath, the first arm comprising a first longitudinal portion and a first projection portion, inserting the first projection portion through a first opening in a passageway portion of the sheath; inserting a second arm into the sheath through-passage), the second arm comprising a second longitudinal portion and a second projection portion; inserting the second projection portion through a second opening in the passageway portion; inserting a separating mechanism (160; 160b; 157; 160c) into the sheath through-passage between the first arm and the second arm; installing a biasing mechanism; sliding a top housing over the biasing mechanism such that the biasing mechanism is located in a cavity defined within the top housing, the biasing mechanism being configured to apply a force to the first arm and the second arm when the biasing mechanism is located in the cavity; and securing the top housing together with the sheath. inserting a first arm into a sheath through-passage of a sheath, the first arm comprising a first longitudinal portion and a first projection portion, inserting the first projection portion through a first opening in a passageway portion of the sheath; inserting a second arm into the sheath through-passage), the second arm comprising a second longitudinal portion and a second projection portion; inserting the second projection portion through a second opening in the passageway portion; inserting a separating mechanism (160; 160b; 157; 160c) into the sheath through-passage between the first arm and the second arm; installing a biasing mechanism; sliding a top housing over the biasing mechanism such that the biasing mechanism is located in a cavity defined within the top housing, the biasing mechanism being configured to apply a force to the first arm and the second arm when the biasing mechanism is located in the cavity; and securing the top housing together with the sheath.
An optically transparent conductor assembly comprising a transparent substrate defining perpendicular directions X and Y in a plane of said substrate, a plurality of conducting tracks (3a, 3b) of a non-transparent material positioned by said substrate, wherein some of said tracks (3a, 3b) are members of a first set of tracks and are parallel to each other along said direction X, wherein some of said tracks are members of a second set of tracks, wherein the tracks of said second set of tracks are parallel to each other and wherein said first and second sets of tracks (3a, 3b) intersect and form individually addressable sensing regions (8aa, 8ab, 8ba, 8bb), wherein the tracks (3a, 3b) have a width of less than 10 μm and wherein, for each of said tracks, and along both said directions X and Y, a distance between said track and a next one of said tracks is less than 200 μm, in particular less than 150 μm, wherein a plurality of crossing points are formed where the tracks (3a, 3b) of the first and the second set interact, wherein at a first set of said crossing points, said conductor assembly comprises a dielectric insulator electrically insulating the tracks (3a, 3b) of the first and the second sets, characterized in that at a second set of said crossing points, the tracks of one set of tracks are electrically connected to the tracks of the other set of tracks. a transparent substrate defining perpendicular directions X and Y in a plane of said substrate, a plurality of conducting tracks (3a, 3b) of a non-transparent material positioned by said substrate, wherein some of said tracks (3a, 3b) are members of a first set of tracks and are parallel to each other along said direction X, wherein some of said tracks are members of a second set of tracks, wherein the tracks of said second set of tracks are parallel to each other and wherein said first and second sets of tracks (3a, 3b) intersect and form individually addressable sensing regions (8aa, 8ab, 8ba, 8bb), wherein the tracks (3a, 3b) have a width of less than 10 μm and wherein, for each of said tracks, and along both said directions X and Y, a distance between said track and a next one of said tracks is less than 200 μm, in particular less than 150 μm, wherein a plurality of crossing points are formed where the tracks (3a, 3b) of the first and the second set interact, wherein at a first set of said crossing points, said conductor assembly comprises a dielectric insulator electrically insulating the tracks (3a, 3b) of the first and the second sets, characterized in that at a second set of said crossing points, the tracks of one set of tracks are electrically connected to the tracks of the other set of tracks.
Pre-coated, cold-rolled and annealed sheet for the fabrication of press-hardened parts, composed of a steel substrate for heat treatment with a carbon content C 0 between 0.07% and 0.5%, said content being expressed by weight, and a metal pre-coating at least on the two principal faces of said steel substrate, said metal pre-coating being aluminium or an aluminium alloy or zinc or a zinc alloy or is composed of a layer of aluminium or of an aluminium alloy surmounted by a layer of zinc or of a zinc alloy, the composition of said steel substrate comprising, the contents being expressed by weight: 0.07 % ≤ C ≤ 0.5 % 0.5 % ≤ Mn ≤ 3 % 0.02 % ≤ Si ≤ 0.5 % 0.01 % ≤ Cr ≤ 1 % Ti ≤ 0.2 % Al ≤ 0.25 % S ≤ 0.05 % P ≤ 0.1 % 0.0005 % ≤ B ≤ 0.010 %, optionally 0,0005 % ≤ Ca ≤ 0,005 %, the remainder of the composition being composed of iron and unavoidable impurities resulting from processing, characterised in that said substrate comprises a decarburised area on the surface of each of said two principal faces, the depth p 50% of the decarburised area being between 6 and 30 micrometres, p 50% being the depth at which the carbon content is equal to 50% of said content C 0, the depth p 50% being measured by Glow Discharge Spectrometry, and in that said sheet does not contain a layer of iron oxide between said substrate and said metal pre-coating,. the remainder of the composition being composed of iron and unavoidable impurities resulting from processing, characterised in that said substrate comprises a decarburised area on the surface of each of said two principal faces, the depth p 50% of the decarburised area being between 6 and 30 micrometres, p 50% being the depth at which the carbon content is equal to 50% of said content C 0, the depth p 50% being measured by Glow Discharge Spectrometry, and in that said sheet does not contain a layer of iron oxide between said substrate and said metal pre-coating,.
Hydraulic brake unit comprising - a brake booster comprising a body and a feeler piston, the feeler piston sliding in a bore formed in the body and connected by a first end to a brake pedal, the feeler piston delimiting a thrust chamber with the bore of the body, - a master cylinder comprising a primary chamber and a primary piston, the primary chamber being connected internally to a hydraulic brake circuit, the primary piston being connected to a second end of the feeler piston that is opposite to its first end, - a first hydraulic fluid reservoir supplying the primary chamber via a first duct, - a hydraulic fluid supplying the sealed thrust chamber via a third duct and by means of a hydraulic pump (25, 27), characterized in that it comprises - a fourth duct receiving hydraulic fluid and opening into the primary chamber of the master cylinder, and - the hydraulic pump (25, 27) being connected to the fourth duct, the filling of fluid into the primary chamber via the fourth duct being controlled by a sensor which activates the pump at the moment of a press on the brake pedal and prior to the filling of the thrust chamber via the third duct. - a brake booster comprising a body and a feeler piston, the feeler piston sliding in a bore formed in the body and connected by a first end to a brake pedal, the feeler piston delimiting a thrust chamber with the bore of the body, - a master cylinder comprising a primary chamber and a primary piston, the primary chamber being connected internally to a hydraulic brake circuit, the primary piston being connected to a second end of the feeler piston that is opposite to its first end, - a first hydraulic fluid reservoir supplying the primary chamber via a first duct, - a hydraulic fluid supplying the sealed thrust chamber via a third duct and by means of a hydraulic pump (25, 27), - a fourth duct receiving hydraulic fluid and opening into the primary chamber of the master cylinder, and - the hydraulic pump (25, 27) being connected to the fourth duct, the filling of fluid into the primary chamber via the fourth duct being controlled by a sensor which activates the pump at the moment of a press on the brake pedal and prior to the filling of the thrust chamber via the third duct.