mhurhangee/ep-ind-claims huggingface dataset:
A brake system of an aircraft, the brake system comprising: a first brake control assembly; a second brake control assembly; a first brake control unit electrically coupled to the first brake control assembly; a second brake control unit electrically coupled to the second brake control assembly; characterised by an arbitration control module configured to determine an operational integrity of the first brake control unit and the second brake control unit, wherein, in response to determining that one of the first brake control unit and the second brake control unit does not have sufficient operational integrity, the arbitration control module enables the other of the first brake control unit and the second brake control unit to control both the first brake control assembly and the second brake control assembly. a first brake control assembly; a second brake control assembly; a first brake control unit electrically coupled to the first brake control assembly; a second brake control unit electrically coupled to the second brake control assembly; characterised by an arbitration control module configured to determine an operational integrity of the first brake control unit and the second brake control unit, wherein, in response to determining that one of the first brake control unit and the second brake control unit does not have sufficient operational integrity, the arbitration control module enables the other of the first brake control unit and the second brake control unit to control both the first brake control assembly and the second brake control assembly.
An actuator for an automated or an automatic transmission, which has a cylinder housing, a piston unit and a piston rod, in which the piston unit is coupled to the piston rod and is arranged in the cylinder housing in a movable manner along an axial longitudinal axis, in which the piston unit separates two pressure chambers (8, 9) which have a variable volume, in the cylinder housing, said pressure chambers being used to supply the piston unit with compressed air on both sides, in which the two pressure chambers (8, 9) are connected to a valve unit, by means of which the application of pressure or the ventilation of each of the two pressure chambers (8, 9) can be switched, and in which an end stop damping device for damping at least one end stop of the piston unit is arranged in the actuator, wherein the end stop damping device is configured to be two-stage, namely, with a first, pneumatically operating damping stage and with a second, mechanically operating damping stage, wherein by means of the pneumatic damping stage the kinetic energy of the piston unit in at least one direction of movement of the same is reducible coaxially to the longitudinal axis in the event of an approach of the piston unit to an end stop surface (5, 6) formed on the cylinder housing by means of a pneumatic damping element (19, 20), wherein the pneumatic damping element (19, 20) has an air outlet (34, 35) that can be changed with respect to its capacity for compressed air, which is pneumatically connectible to one of the two pressure chambers (8, 9) by switching the valve unit to a ventilating position, wherein the operating cross-sectional surface (28, 29) of the air outlet (34, 35) is variably adjustable depending on the pressure in the pressure chamber (8, 9) connected to it, and in which, by means of the mechanical damping stage, a remaining kinetic energy of the piston unit after braking by the pneumatic damping element (19, 20) can be reduced upon its reaching the end stop surface (5, 6) by means of a mechanical damping element (40, 41).
An apparatus of a collection of computing systems, to prepare memory for reuse, comprising: a first memory (126, 220, 320) that is accessible to a first client device of a first user during a usage period of the first user; a service processor (124, 204, 304, 404) coupled to a switch (160, 202, 302, 402), wherein the service processor is in communication with the first memory during the usage period; a root of trust processor (144, 214, 314, 414) coupled to the switch, wherein the root of trust processor is inaccessible to the first client device of the first user during the usage period; a second memory (146, 222, 322) that is inaccessible to the first client device of the first user during the usage period of the first user; and a controller configured to send one or more control signals to the root of trust processor to trigger the root of trust processor to prepare the second memory for deployment while the service processor is in communication with the first memory. a first memory (126, 220, 320) that is accessible to a first client device of a first user during a usage period of the first user; a service processor (124, 204, 304, 404) coupled to a switch (160, 202, 302, 402), wherein the service processor is in communication with the first memory during the usage period; a root of trust processor (144, 214, 314, 414) coupled to the switch, wherein the root of trust processor is inaccessible to the first client device of the first user during the usage period; a second memory (146, 222, 322) that is inaccessible to the first client device of the first user during the usage period of the first user; and a controller configured to send one or more control signals to the root of trust processor to trigger the root of trust processor to prepare the second memory for deployment while the service processor is in communication with the first memory.
A fan annulus filler (28, 128) for mounting on a turbine engine, the annulus filler (28, 128) comprising: a filler body (36, 136) including a hook extending therefrom for coupling to a rotor disc, the filler body (36, 136) being made of a polymer; and a nanocrystalline coating (30, 130) being disposed on an exterior surface (38, 138) of the filler body (36, 136), wherein nanocrystalline is defined as a polycrystalline having a grain size generally of 100 nm or less, characterized in that the body (36, 136) includes a plurality of bores defined therein and extending through the body (36, 136) between one portion of the exterior surface (38, 138) and another portion of the exterior surface (38, 138), and the coating (30, 130) is disposed within the bores to fill the bores and provide reinforcement pins that extend through the body (36, 136). a filler body (36, 136) including a hook extending therefrom for coupling to a rotor disc, the filler body (36, 136) being made of a polymer; and a nanocrystalline coating (30, 130) being disposed on an exterior surface (38, 138) of the filler body (36, 136), wherein nanocrystalline is defined as a polycrystalline having a grain size generally of 100 nm or less, characterized in that the body (36, 136) includes a plurality of bores defined therein and extending through the body (36, 136) between one portion of the exterior surface (38, 138) and another portion of the exterior surface (38, 138), and the coating (30, 130) is disposed within the bores to fill the bores and provide reinforcement pins that extend through the body (36, 136).
An electronic flight bag for an aircraft that has an associated flight manual, the electronic flight bag comprising: a display device coupled to receive display commands and operable, in response thereto, to render various images; a processing system in operable communication with the display, the processing system configured to receive fault data from one or more aircraft systems and operable, upon receipt of the fault data to (i) determine a page in the associated flight manual that corresponds to the received fault data and (ii) supply display commands to the display device that cause the display device to automatically render an image of the determined page in the associated flight manual; characterised in that the processing system is further configured to receive health data, from a plurality of aircraft displays and aircraft avionics that are representative of flight deck operability, and is operable to determine whether one or more flight deck functions are degraded; and the processing system further operable, upon determining that one or more flight deck functions are degraded, to selectively supply display commands to the display device that cause the display device to render images representative of a standby indicator. a display device coupled to receive display commands and operable, in response thereto, to render various images; a processing system in operable communication with the display, the processing system configured to receive fault data from one or more aircraft systems and operable, upon receipt of the fault data to (i) determine a page in the associated flight manual that corresponds to the received fault data and (ii) supply display commands to the display device that cause the display device to automatically render an image of the determined page in the associated flight manual; characterised in that the processing system is further configured to receive health data, from a plurality of aircraft displays and aircraft avionics that are representative of flight deck operability, and is operable to determine whether one or more flight deck functions are degraded; and the processing system further operable, upon determining that one or more flight deck functions are degraded, to selectively supply display commands to the display device that cause the display device to render images representative of a standby indicator.
A wire-tensioning mechanism of a steerable catheter, the mechanism comprising: at least a first wire and at least a second wire; where the first wire includes a first wire proximal end and a first wire distal end, and the second wire includes a second wire proximal end and a second wire distal end; at least a first spool including at least one outer circumferential surface surrounding and defining a first spool body; a first gear and a second gear disposed rotatably in the first spool body, each of the first gear and second gear being rotatable around a gear-rotation axis generally orthogonal to a plane defined by the first spool body; where at least first and second apertures (126a, 126b) each provide a path of mechanical communication through the at least one circumferential surface to, respectively, the first gear and the second gear; a first detent releasably engaging the first gear and a second detent releasably engaging the second gear; where the first wire is disposed through the first aperture, is securely attached to and is windable around the first gear; and where the second wire is disposed through the second aperture, is securely attached to and is windable around the second gear. at least a first wire and at least a second wire; where the first wire includes a first wire proximal end and a first wire distal end, and the second wire includes a second wire proximal end and a second wire distal end; at least a first spool including at least one outer circumferential surface surrounding and defining a first spool body; a first gear and a second gear disposed rotatably in the first spool body, each of the first gear and second gear being rotatable around a gear-rotation axis generally orthogonal to a plane defined by the first spool body; where at least first and second apertures (126a, 126b) each provide a path of mechanical communication through the at least one circumferential surface to, respectively, the first gear and the second gear; a first detent releasably engaging the first gear and a second detent releasably engaging the second gear; where the first wire is disposed through the first aperture, is securely attached to and is windable around the first gear; and where the second wire is disposed through the second aperture, is securely attached to and is windable around the second gear.
A gas oven range comprising: an oven chamber in which food is cooked; an upper burner inside the oven chamber; and a reflector (600; 700; 800; 900) disposed above the burner; the reflector comprising a reflection part (610; 710; 810; 910) configured to reflect flame and heat generated by combustion of gas at the burner, and an exhaust hole (620; 730; 830; 930) configured to discharge combustion gas generated by combustion of gas at the burner toward a side opposite to the burner; characterized by a cover part (750; 950) spaced apart from the exhaust hole (730; 930) in a direction where combustion gas is discharged through the exhaust hole (730; 930), the cover part (750, 950) is disposed directly above the exhaust hole (730; 930), and the cover part (750, 950) has a plate shape with a size corresponding to the size of the exhaust hole (730, 930), wherein fixing ribs (751, 951) are provided at front and rear end portions of each cover part (750, 950), and wherein the fixing ribs (751, 951) are provided to fix the cover part (750, 950) to the reflection part (710, 910). an oven chamber in which food is cooked; an upper burner inside the oven chamber; and a reflector (600; 700; 800; 900) disposed above the burner; the reflector comprising a reflection part (610; 710; 810; 910) configured to reflect flame and heat generated by combustion of gas at the burner, and an exhaust hole (620; 730; 830; 930) configured to discharge combustion gas generated by combustion of gas at the burner toward a side opposite to the burner; characterized by a cover part (750; 950) spaced apart from the exhaust hole (730; 930) in a direction where combustion gas is discharged through the exhaust hole (730; 930), the cover part (750, 950) is disposed directly above the exhaust hole (730; 930), and the cover part (750, 950) has a plate shape with a size corresponding to the size of the exhaust hole (730, 930), wherein fixing ribs (751, 951) are provided at front and rear end portions of each cover part (750, 950), and wherein the fixing ribs (751, 951) are provided to fix the cover part (750, 950) to the reflection part (710, 910).
A medicament for use in treating moderate or severe osteoarthritis or moderate or severe rheumatoid arthritis, wherein the medicament comprises a combination composition comprising ibuprofen and paracetamol to be administered in doses of 250 mg to 300 mg ibuprofen and 950 mg to 1,000 mg paracetamol per dosage event.
A double-prism assembly, comprising a first prism and a second prism arranged in a coaxial manner, wherein the first prism has a first prism face structure, the second prism has a second prism face structure, and the first prism face structure and the second prism face structure are arranged in a same direction or in different directions, wherein the first prism is a conical structure, the first prism face structure is arranged on a lateral side of the conical structure, and the first prism face structure includes a plurality of first prism face units extending from a bottom face of the conical structure to a vertex of the conical structure, characterized in that the second prism is a truncated conical structure, the second prism face structure is arranged on a lateral side of the truncated conical structure, and the second prism face structure includes a plurality of second prism face units extending from a bottom face of the truncated conical structure to a top face of the truncated conical structure.
A processing machine with a plurality of processing stations (02; 03; 04; 06) for processing bodies, wherein the processing stations (02; 03; 04; 06) provided for processing the bodies are arranged in a working space in each case at positions different from one another in the transport direction of the bodies to be processed, wherein the respective position of the relevant processing station (02; 03; 04; 06) is adjusted for the execution of a specified processing procedure, wherein the respective positions of the processing stations (02; 03; 04; 06) adjusted in each case for the execution of their specified processing procedures are arranged in the working space on a same horizontal plane, wherein a transport of a body that has been or will be processed occurs from one processing station (02; 03; 04; 06) to the next below its horizontal plane, in which the respective positions of the individual processing stations (02; 03; 04; 06) adjusted in each case for the execution of their processing procedures are arranged, wherein in the working space a plurality of simultaneously handling devices that are operated or at least can be operated simultaneously are provided, wherein every handling device is provided in each case for transport of at least body that has been or will be processed, wherein at least two handling devices arranged in the same working space and which are simultaneously operated or at least can be simultaneously operated are arranged vertically one above the other on different horizontal planes and are each moved horizontally or at least can be moved horizontally on their respective plane, wherein a movement path of the relevant handling device provided for the transport of the bodies that have been or will be processed is arranged on a vertical transport plane, wherein the vertical transport plane having the movement path of the relevant handling device is arranged in each case lengthwise to the positions of the processing stations (02; 03; 04; 06) provided for processing the bodies, characterized in that the handling devices are each moved or at least can be moved horizontally on their respective plane along a rail system.
A blow molded article having at least one layer comprising: a) a thermoplastic resin; b) between 0.1% and 20% of an additive having a kinematic viscosity of greater than 1 m 2 /s (1,000,000 cst) as measured according to the Viscosity Measurement as disclosed herein, wherein the kinematic viscosity is measured using a TA Instruments DHR2 or equivalent rheometer at 23 ± 1°C, using 25 mm parallel plates, at a frequency measurement 0.5 Hz at 1 % strain and with a sample gap of 0.7 ± 0.2 mm, wherein there is a refractive index difference of at least 0.04 between the additive and the thermoplastic resin. a) a thermoplastic resin; b) between 0.1% and 20% of an additive having a kinematic viscosity of greater than 1 m 2 /s (1,000,000 cst) as measured according to the Viscosity Measurement as disclosed herein, wherein the kinematic viscosity is measured using a TA Instruments DHR2 or equivalent rheometer at 23 ± 1°C, using 25 mm parallel plates, at a frequency measurement 0.5 Hz at 1 % strain and with a sample gap of 0.7 ± 0.2 mm,
Process for preparing an inorganic aerogel, the process comprising the steps (i) providing a composition suitable to form an inorganic gel with a gelation time t G, (ii) spraying the composition into supercritical carbon dioxide at a spraying time ts to obtain gel particles, (iii) drying the gel particles obtained in step (ii) by supercritical liquid extraction, wherein the ratio t S: t G is in the range of from 0.2 to 0.99, wherein the gelation time t G is the time from mixing the components which form the gel until a gel has been formed and the spraying time t S is defined as the time from mixing the components until composition is sprayed into supercritical carbon dioxide and wherein the reacting sol is injected into the autoclave with a flow rate in the range from 10 to 999 mL/minute. (i) providing a composition suitable to form an inorganic gel with a gelation time t G, (ii) spraying the composition into supercritical carbon dioxide at a spraying time ts to obtain gel particles, (iii) drying the gel particles obtained in step (ii) by supercritical liquid extraction, wherein the ratio t S: t G is in the range of from 0.2 to 0.99, wherein the gelation time t G is the time from mixing the components which form the gel until a gel has been formed and the spraying time t S is defined as the time from mixing the components until composition is sprayed into supercritical carbon dioxide and wherein the reacting sol is injected into the autoclave with a flow rate in the range from 10 to 999 mL/minute.
An electronic device of a user equipment, which is adapted to keep a first wireless communication channel with a first base station after a second wireless communication channel with a second base station is established, comprising: processing circuitry configured to, receive, from the first base station, information for measuring a signal of the second base station; send measuring result to the first base station in response to the instruction information for measuring a signal of the second base station; establish the second wireless communication channel with the second base station, wherein the frequency bands used for communicating with the first base station are different from the frequency bands used by the the electronic device for communicating with the second base station, wherein the second wireless communication channel is established after receiving, from the first base station, Radio Resource Control, RRC, connection reconfiguration information which includes acknowledge information, comprising information for establishing communication with the second base station. processing circuitry configured to, receive, from the first base station, information for measuring a signal of the second base station; send measuring result to the first base station in response to the instruction information for measuring a signal of the second base station; establish the second wireless communication channel with the second base station, wherein the frequency bands used for communicating with the first base station are different from the frequency bands used by the the electronic device for communicating with the second base station, wherein the second wireless communication channel is established after receiving, from the first base station, Radio Resource Control, RRC, connection reconfiguration information which includes acknowledge information, comprising information for establishing communication with the second base station.
A lubricating composition comprising an oil of lubricating viscosity and an ashless ketone compound represented by the formula: wherein: R 1 is nitrogen-free alkyl group containing 8 to 20 carbon atoms; and R 2, R 3 and R 4 are each independently hydrogen or a hydrocarbyl group. R 1 is nitrogen-free alkyl group containing 8 to 20 carbon atoms; and R 2, R 3 and R 4 are each independently hydrogen or a hydrocarbyl group.