mhurhangee/ep-ind-claims huggingface dataset:
A method, comprising: retrieving, from one or more other systems, information about enforcements of Service Level Agreements for services provided to a plurality of tenants (122, 124, 126) by a cloud provider, wherein the Service Level Agreements are related to performance of the services and security of the services; detecting a possible Service Level Agreement violation for a service provided to one tenant of the plurality of tenants, wherein the possible Service Level Agreement violation is caused by a confliction between performance requirements and security requirements; deciding which of a cloud manager and a security management system of the cloud provider to trigger to mitigate the possible Service Level Agreement violation; and automatically mitigating the possible Service Level Agreement violation with cooperation with at least one of the cloud manager and the security management system of the cloud provider. retrieving, from one or more other systems, information about enforcements of Service Level Agreements for services provided to a plurality of tenants (122, 124, 126) by a cloud provider, wherein the Service Level Agreements are related to performance of the services and security of the services; detecting a possible Service Level Agreement violation for a service provided to one tenant of the plurality of tenants, wherein the possible Service Level Agreement violation is caused by a confliction between performance requirements and security requirements; deciding which of a cloud manager and a security management system of the cloud provider to trigger to mitigate the possible Service Level Agreement violation; and automatically mitigating the possible Service Level Agreement violation with cooperation with at least one of the cloud manager and the security management system of the cloud provider.
An aerofoil component defining an in use leading edge and a trailing edge, the leading edge comprising at least one serration defining an apex and a nadir, wherein the leading edge comprises a generally chordwise extending slot located at the nadir of each serration, wherein each serration comprises, in sequence in a spanwise direction extending from the apex: a rearwardly inclined relative to an in use flow direction first portion; a rearwardly inclined second portion (28, 228) joined with the first portion at a first internal angle (α) relative to the first portion of between 90° and 180°; a forwardly inclined relative to the in use flow direction third portion (30, 130), the second and third portions (28, 128, 30, 130) forming the slot; and a forwardly inclined fourth portion joined with the third portion (30, 130) at a second internal angle (β) relative to the third portion (30, 130) of between 90° and 180°, wherein either the second portion is joined to the third portion at an angle (γ) to form the slot, or the second and third portions (28, 30) are joined to one another by a fifth portion, the second, third and fifth portions defining the slot, the fifth portion extending in a generally spanwise direction, generally normal to the in use flow direction, characterised in that a chordwise distance between the apex and the nadir of each serration is at least twice the spanwise distance (λ) between apexes of adjacent serrations (22a, 22b). a rearwardly inclined relative to an in use flow direction first portion; a rearwardly inclined second portion (28, 228) joined with the first portion at a first internal angle (α) relative to the first portion of between 90° and 180°; a forwardly inclined relative to the in use flow direction third portion (30, 130), the second and third portions (28, 128, 30, 130) forming the slot; and a forwardly inclined fourth portion joined with the third portion (30, 130) at a second internal angle (β) relative to the third portion (30, 130) of between 90° and 180°, wherein either the second portion is joined to the third portion at an angle (γ) to form the slot, or the second and third portions (28, 30) are joined to one another by a fifth portion, the second, third and fifth portions defining the slot, the fifth portion extending in a generally spanwise direction, generally normal to the in use flow direction, characterised in that a chordwise distance between the apex and the nadir of each serration is at least twice the spanwise distance (λ) between apexes of adjacent serrations (22a, 22b).
Method for using an automated teller machine, wherein the automated teller machine is coupled to a mobile phone of a user of the automated teller machine via a Bluetooth Low Energy connection, the automated teller machine transmits a first string, the content of which relates to the use of the automated teller machine, to the mobile phone of the user via the Bluetooth Low Energy connection, the mobile phone reads aloud the content of the first string to the user by means of a text-to-speech function of the mobile phone, and the user is able to use the automated teller machine accordingly. the automated teller machine is coupled to a mobile phone of a user of the automated teller machine via a Bluetooth Low Energy connection, the automated teller machine transmits a first string, the content of which relates to the use of the automated teller machine, to the mobile phone of the user via the Bluetooth Low Energy connection, the mobile phone reads aloud the content of the first string to the user by means of a text-to-speech function of the mobile phone, and the user is able to use the automated teller machine accordingly.
A spacecraft comprising: a magnetic field source arranged to generate a shield magnetic field to protect the spacecraft from energetic charged particles, characterised in that the spacecraft further comprises: a source controller arranged to operate the magnetic field source so as to provide ongoing perturbation of the shield magnetic field, to thereby increase the effectiveness of the protection. a magnetic field source arranged to generate a shield magnetic field to protect the spacecraft from energetic charged particles, characterised in that the spacecraft further comprises: a source controller arranged to operate the magnetic field source so as to provide ongoing perturbation of the shield magnetic field, to thereby increase the effectiveness of the protection. a source controller arranged to operate the magnetic field source so as to provide ongoing perturbation of the shield magnetic field, to thereby increase the effectiveness of the protection.
A device for controlling levels of light output by a solid state lighting load (130, 230) at low dimming levels, the device comprising an AC voltage phase chopping dimmer and a bleed circuit (140, 240), - the bleed circuit (140, 240) being connected in parallel with the solid state lighting load (130, 230); - the bleed circuit (140, 240) comprising a resistor (141, 241) and a transistor (145, 245) connected in series; and - the transistor (145, 245) being configured to turn on and off in accordance with a digital control signal; characterized by - a detection circuit (110, 210) configured to detect the dimming level set by the AC voltage phase chopping dimmer, to set a duty cycle of the digital control signal based on the detected dimming level, and to output the digital control signal at the duty cycle to the transistor (145, 245), wherein the duty cycle is set to 0% when the detected dimming level is above a predetermined first dimming threshold, the duty cycle is set to 100% when the detected dimming level is below a predetermined second dimming threshold and the duty cycle is set to a value in between 0% and 100% when the detected dimming level is below the predetermined first dimming threshold and above the predetermined second dimming threshold; and - the bleed circuit (140, 240) having a lower effective resistance at a higher duty cycle than at a lower duty cycle of the digital control signal. - the bleed circuit (140, 240) being connected in parallel with the solid state lighting load (130, 230); - the bleed circuit (140, 240) comprising a resistor (141, 241) and a transistor (145, 245) connected in series; and - the transistor (145, 245) being configured to turn on and off in accordance with a digital control signal; - a detection circuit (110, 210) configured to detect the dimming level set by the AC voltage phase chopping dimmer, to set a duty cycle of the digital control signal based on the detected dimming level, and to output the digital control signal at the duty cycle to the transistor (145, 245), wherein the duty cycle is set to 0% when the detected dimming level is above a predetermined first dimming threshold, the duty cycle is set to 100% when the detected dimming level is below a predetermined second dimming threshold and the duty cycle is set to a value in between 0% and 100% when the detected dimming level is below the predetermined first dimming threshold and above the predetermined second dimming threshold; and - the bleed circuit (140, 240) having a lower effective resistance at a higher duty cycle than at a lower duty cycle of the digital control signal.
A construction machine comprising: an engine; a radiator that cools through heat exchange cooling water heated by the engine; a cooling fan disposed between the radiator and the engine, the cooling fan sending air drawn in via the radiator to the engine; a shroud disposed on an outer peripheral side of the cooling fan, the shroud forming a passage for air to be drawn in via the radiator; characterized in further comprising a tank disposed superior to an upper end portion of the radiator, the tank storing cooling water to be supplied to the radiator and the engine; and a cover disposed openably in an opening formed in an upper surface of the shroud, wherein the tank is disposed at a position adjacent to the shroud on a side closer to the engine than the cover is. an engine; a radiator that cools through heat exchange cooling water heated by the engine; a cooling fan disposed between the radiator and the engine, the cooling fan sending air drawn in via the radiator to the engine; a shroud disposed on an outer peripheral side of the cooling fan, the shroud forming a passage for air to be drawn in via the radiator; characterized in further comprising a tank disposed superior to an upper end portion of the radiator, the tank storing cooling water to be supplied to the radiator and the engine; and a cover disposed openably in an opening formed in an upper surface of the shroud, wherein the tank is disposed at a position adjacent to the shroud on a side closer to the engine than the cover is.
A continuous process for the production of hydrogen peroxide by the anthraquinone process, comprising the steps of: (i) hydrogenating an organic working solution containing one or more anthraquinone derivatives in the presence of a heterogeneous catalyst to form a hydrogenated working solution, (ii) oxidizing the hydrogenated working solution by introducing an oxygen-containing oxidizing gas at an overpressure into an oxidation reactor, and contacting the oxidizing gas with the hydrogenated working solution to form an oxidized working solution, whereby hydrogen peroxide is formed, (iii) withdrawing oxidation off gas from the oxidation reactor, and (iv) recovering the hydrogen peroxide from the oxidized working solution, characterized in that the process comprises the steps of (v) subjecting the oxidation off gas leaving the oxidation reactor, which has an excess pressure over the atmospheric pressure, to a demisting treatment to obtain a demisted oxidation off gas, and (vi) feeding the demisted oxidation off gas as propellant gas into a gas ejector to produce a vacuum. (i) hydrogenating an organic working solution containing one or more anthraquinone derivatives in the presence of a heterogeneous catalyst to form a hydrogenated working solution, (ii) oxidizing the hydrogenated working solution by introducing an oxygen-containing oxidizing gas at an overpressure into an oxidation reactor, and contacting the oxidizing gas with the hydrogenated working solution to form an oxidized working solution, whereby hydrogen peroxide is formed, (iii) withdrawing oxidation off gas from the oxidation reactor, and (iv) recovering the hydrogen peroxide from the oxidized working solution, characterized in that the process comprises the steps of (v) subjecting the oxidation off gas leaving the oxidation reactor, which has an excess pressure over the atmospheric pressure, to a demisting treatment to obtain a demisted oxidation off gas, and (vi) feeding the demisted oxidation off gas as propellant gas into a gas ejector to produce a vacuum.
A series comprising two or more reinforcing elements for geo-technical applications each of a type comprising a monolithic net structure made of a plastic material, having: a plurality of first elements distanced from one another and having an elongate conformation in a respective prevalent development direction, a plurality of second elements distanced from one another which develop substantially in a transversal direction to the first elements, the second elements also having an elongate conformation according to a respective prevalent development direction, the net structure exhibiting a length, measured in a direction of the first elements, having a considerably greater extension than a width measured in a direction of the second elements, following the formation of the net structure, the second elements being stretched along the prevalent development direction thereof, giving the net structure a width in a direction of the second elements that is greater than 2 meters, said first elements do not exhibit a stretching following formation thereof or exhibit a stretching ratio defined as a ratio between a final length of the first elements once the stretching has been carried out and an initial length of the first elements before a stretching action thereon, that is comprised between 1 and 1.5; the reinforcing elements being transversally flanked and arranged longitudinally according to a direction parallel to a direction of the first elements, wherein the reinforcing elements are connected by blocking elements which constrain longitudinally flanked edges of adjacent reinforcing elements, wherein the reinforcing elements are arranged such as to define an overlap zone which comprises a plurality of slots which form passage openings delimited by segments of the second elements of mutually overlapping flaps (13, 14), the slots being aligned in a direction parallel to the first elements, forming a coupling area, a blocking element, comprising a cylindrical body or a bar, being inserted through the slots such as to cooperate with portions of the second elements of the two overlapping flaps (13, 14). a plurality of first elements distanced from one another and having an elongate conformation in a respective prevalent development direction, a plurality of second elements distanced from one another which develop substantially in a transversal direction to the first elements, the second elements also having an elongate conformation according to a respective prevalent development direction,
Spectacle lens for a display device that can be fitted on the head of a user and generates an image, with a spectacle lens body comprising a front side and a rear side, wherein the front side and/or the rear side is/are curved and the spectacle lens body comprises at least a first and a second partial body (35, 36), and with, seen in top view onto the spectacle lens (3, 4), a coupling-in section in an edge area of the spectacle lens (3, 4) and a coupling-out section in a central area of the spectacle lens (3, 4), wherein the spectacle lens (3, 4) is suitable for guiding light bundles of pixels of the generated image, which are coupled into the spectacle lens (3, 4) via the coupling-in section of the spectacle lens, in the spectacle lens (3, 4) to the coupling-out section and coupling them out of the spectacle lens (3, 4) via the coupling-out section, wherein a flat first reflecting surface (18, 31) and a flat second reflecting surface (19, 32) spaced apart from the first reflecting surface (18, 31) are provided in the spectacle lens body, which extend, in each case, in a direction from the coupling-in section to the coupling-out section and which are, in each case, spaced apart from the front and rear side (8, 9) of the spectacle lens body, wherein the light bundles are guided by means of reflections at the two reflecting surfaces (18, 31; 19, 32) in the direction from the coupling-in section to the coupling-out section, and wherein at least one of the first and second reflecting surfaces (18, 31; 19, 32) is provided in the first or second partial body (35, 36) and is offset from the boundary surface (38, 39) of the corresponding partial body (35, 36) in the direction from the first to the second partial body (35, 36), characterized in that the mutually facing boundary surfaces (38, 39) of the first and second partial body (35, 36) are in direct contact.
Method for manufacturing a heavy-duty laundry detergent wipe, characterized by the following steps: (a) incorporating oxygen donors and their activators in a waxy matrix which is surrounded by an ionic polymer layer for providing a capsule system, (b) incorporating the capsule system into a dispersion comprising a liquid washing detergent and a water insoluble functional additive, (c) applying the dispersion provided with the capsule system to a carrier material which is solid at ambient temperature. (a) incorporating oxygen donors and their activators in a waxy matrix which is surrounded by an ionic polymer layer for providing a capsule system, (b) incorporating the capsule system into a dispersion comprising a liquid washing detergent and a water insoluble functional additive, (c) applying the dispersion provided with the capsule system to a carrier material which is solid at ambient temperature.
A test element for qualifying an apparatus for electrically characterising fuel cell elements and/or fuel cells, said test element being characterised in that it includes: - a first and a second contact face (131, 132) respectively including a first and a second metal layer occupying all or part of the area of the corresponding contact face (131, 132) and respectively forming a first and a second contact zone (135, 136), the first and the second contact faces (131, 132) delimiting an internal volume between them, - a passive equivalent circuit configured to exhibit an impedance equivalent to at least one fuel cell element, said equivalent circuit including a first and a second output terminal (111, 112) respectively connected to the first and the second contact zones (135, 136), the equivalent circuit being housed in the internal volume. - a first and a second contact face (131, 132) respectively including a first and a second metal layer occupying all or part of the area of the corresponding contact face (131, 132) and respectively forming a first and a second contact zone (135, 136), the first and the second contact faces (131, 132) delimiting an internal volume between them, - a passive equivalent circuit configured to exhibit an impedance equivalent to at least one fuel cell element, said equivalent circuit including a first and a second output terminal (111, 112) respectively connected to the first and the second contact zones (135, 136), the equivalent circuit being housed in the internal volume.
Device for the opening of ampoules, comprising an external container (7, 17, 27), in which is arranged a closed ampoule (4, 14, 24) having an ampoule body and an ampoule head (2, 12, 22), and comprising a hollow space (3, 13, 23) in the region of the ampoule head (2, 12, 22), whereby the external container (7, 17, 27) is attached to a hollow body, in which the hollow space (3, 13, 23) is formed, the hollow body being limited on the upper side by an ampoule support (6, 16, 26), in which a connection (1, 11, 21) to the ampoule (4, 14, 24) is arranged, and the hollow body consists of a solid material that cannot be deformed by hand, the ampoule head (2, 12, 22), at least regions thereof, is arranged in the connection (1, 11, 21) of the hollow space (3, 13, 23) to the ampoule (4, 14, 24), and the walls of the external container (7, 17, 27) comprise at least one deformable region (19, 29) or are altogether made of a deformable material, whereby tilting of the ampoule (4, 14, 24) with respect to the connection (1, 11, 11.21) is made feasible, and in that the diameter of the connection (1, 11, 21) is adapted appropriately to the dimensions of the ampoule head (2, 12, 22) such that the ampoule head (2, 12, 22) can be fractured or broken off the ampoule body when the ampoule (4, 14, 24) is being tilted with respect to the connection (1, 11, 21). the height and cross-section of the hollow space (3, 13, 23) are at least of the same size as the height of the ampoule head (2, 12, 22) up to the breaking edge of the ampoule (4, 14, 24) such that the hollow space is suitable to facilitate a rotation of the broken-off ampoule head in the hollow space.
A nozzle assembly (10, 10', 10") with a self-cleaning face, comprising: a nozzle body with a liquid flow path defined therethrough having an inlet and a spray outlet; a carrier body (20, 20') that surrounds the nozzle body, with an annular gas flow channel with a gas discharge outlet located around the spray outlet; a porous surface located around the gas flow channel at the gas discharge outlet; a pathway in communication with the porous surface and adapted to provide a low velocity fluid discharge from the porous surface; a radiused surface formed in the carrier body (20, 20') around the gas discharge outlet; and a stator located in the annular gas flow channel that includes a plurality of guide vanes oriented angularly to the liquid flow path; wherein liquid from a liquid chamber (66A, 66B) is adapted to be sprayed through the nozzle body while pressurised fluid is simultaneously supplied to the porous surface to create a low velocity fluid discharge from the porous surface, wherein the fluid transported through the porous surface and a radially outwardly expanding flow of gas with an imparted swirling generated by the stator exiting from the annular gas flow channel and moving outwardly over the radiused surface to the porous surface are adapted to keep a discharge end surface of the nozzle body clean. a nozzle body with a liquid flow path defined therethrough having an inlet and a spray outlet; a carrier body (20, 20') that surrounds the nozzle body, with an annular gas flow channel with a gas discharge outlet located around the spray outlet; a porous surface located around the gas flow channel at the gas discharge outlet; a pathway in communication with the porous surface and adapted to provide a low velocity fluid discharge from the porous surface; a radiused surface formed in the carrier body (20, 20') around the gas discharge outlet; and a stator located in the annular gas flow channel that includes a plurality of guide vanes oriented angularly to the liquid flow path; wherein liquid from a liquid chamber (66A, 66B) is adapted to be sprayed through the nozzle body while pressurised fluid is simultaneously supplied to the porous surface to create a low velocity fluid discharge from the porous surface, wherein the fluid transported through the porous surface and a radially outwardly expanding flow of gas with an imparted swirling generated by the stator exiting from the annular gas flow channel and moving outwardly over the radiused surface to the porous surface are adapted to keep a discharge end surface of the nozzle body clean.