mhurhangee/ep-ind-claims huggingface dataset:
A microprocessor comprising: a central processing unit; an on-chip memory array for storing instructions executable on said central processing unit; an external memory interface capable of reading from and writing to an off-chip memory instructions executable on said central processing unit; a control status register having a data field indicative of a desired program memory mode; and a configurable program memory controller in communication with said central processing unit, said on-chip memory array and said external memory interface, said configurable program memory controller having a plurality of operating modes corresponding to said data field of said control status register including a memory-mapped mode controlling said on-chip memory array as a memory-mapped on-chip memory and a cache mode controlling said on-chip memory array as a cache on-chip memory, characterized in that said configurable program memory controller operable in response to a memory-mapped write to said data field of said configuration register to transition from said cache mode to said memory-mapped mode only following a cache miss. a central processing unit; an on-chip memory array for storing instructions executable on said central processing unit; an external memory interface capable of reading from and writing to an off-chip memory instructions executable on said central processing unit; a control status register having a data field indicative of a desired program memory mode; and a configurable program memory controller in communication with said central processing unit, said on-chip memory array and said external memory interface, said configurable program memory controller having a plurality of operating modes corresponding to said data field of said control status register including a memory-mapped mode controlling said on-chip memory array as a memory-mapped on-chip memory and a cache mode controlling said on-chip memory array as a cache on-chip memory, characterized in that said configurable program memory controller operable in response to a memory-mapped write to said data field of said configuration register to transition from said cache mode to said memory-mapped mode only following a cache miss.
A wind turbine blade extending in a longitudinal direction from a root end to a tip end and defining an aerodynamic airfoil cross-section between a leading edge and a trailing edge in a chordwise direction transverse to the longitudinal direction, the aerodynamic airfoil cross-section having an effective camber in the chordwise direction; the wind turbine blade comprising: a blade body; a first device for modifying the aerodynamic surface or shape of the blade, the position and/or movement of the first device relative to the blade body being controlled by a first actuation mechanism; a second device for modifying the effective camber of the airfoil cross section; characterised in that: the first device and the second device are disposed adjacent to each other on the trailing edge, or the first device and the second device form part of the trailing edge and they are disposed separate from each other on the trailing edge, or the first device forms part of the trailing edge and the first device surrounds the second device; and the first device is configured to modify the aerodynamic surface or shape of the blade at a frequency up to a first maximum frequency and the second device is configured to modify the effective camber of the airfoil cross section at a frequency up to a second maximum frequency, the second maximum frequency being higher than the first maximum frequency. a blade body; a first device for modifying the aerodynamic surface or shape of the blade, the position and/or movement of the first device relative to the blade body being controlled by a first actuation mechanism; a second device for modifying the effective camber of the airfoil cross section; characterised in that: the first device and the second device are disposed adjacent to each other on the trailing edge, or the first device and the second device form part of the trailing edge and they are disposed separate from each other on the trailing edge, or the first device forms part of the trailing edge and the first device surrounds the second device; and the first device is configured to modify the aerodynamic surface or shape of the blade at a frequency up to a first maximum frequency and the second device is configured to modify the effective camber of the airfoil cross section at a frequency up to a second maximum frequency, the second maximum frequency being higher than the first maximum frequency. the first device and the second device are disposed adjacent to each other on the trailing edge, or the first device and the second device form part of the trailing edge and they are disposed separate from each other on the trailing edge, or the first device forms part of the trailing edge and the first device surrounds the second device; and the first device is configured to modify the aerodynamic surface or shape of the blade at a frequency up to a first maximum frequency and the second device is configured to modify the effective camber of the airfoil cross section at a frequency up to a second maximum frequency, the second maximum frequency being higher than the first maximum frequency.
Apparatus for the pretreatment and subsequent conveying, plastification or agglomeration of plastics, in particular of thermoplastics waste for recycling purposes, with a container for the material to be processed, where the arrangement has, in the container, at least one mixing and/or comminution implement which rotates around an axis of rotation and which is intended for the mixing, heating and optionally comminution of the plastics material, where an aperture through which the pretreated plastics material can be removed from the interior of the container is formed in a side wall of the container in the region of the level of the, or of the lowest, mixing and/or comminution implement that is closest to the base, where at least one conveyor, in particular one extruder, is provided to receive the pretreated material, and has at least one screw which rotates in a housing and which in particular has plastifying or agglomerating action, where the housing has, located at its end or in its jacket wall, an intake aperture for the material to be received by the screw, and there is a connection between the intake aperture and the aperture, where the imaginary continuation of the central longitudinal axis of the conveyor or of the screw closest to the intake aperture, in a direction opposite to the direction of conveying of the conveyor, passes, and does not intersect, the axis of rotation, characterized in that, on the outflow side or in the direction of rotation or of movement of the mixing and/or comminution implement, there is an offset distance between the longitudinal axis of the conveyor or of the screw closest to the intake aperture, and the radius that is associated with the container and that is parallel to the longitudinal axis and that proceeds outwards from the axis of rotation of the mixing and/or comminution implement in the direction of conveying of the conveyor, and in that the radial distance (mb), between the implement and the inner surface of the side wall of the container, measured from the radially outermost point of the mixing and/or comminution implement closest to the base, or implements and/or blades provided there, or from the circle defined as being described by that point, is in the range from 15 mm to 120 mm, preferably in the range from 20 mm to 80 mm, and complies with the following relationship: mb = k * D B where D B is the internal diameter of a cylindrical container with circular cross section in mm or the internal diameter in mm of an imaginary cylindrical container of the same height with cylindrical cross section calculated to have the same volume capacity, and k is a constant in the range from 0.006 to 0.16. D B is the internal diameter of a cylindrical container with circular cross section in mm or the internal diameter in mm of an imaginary cylindrical container of the same height with cylindrical cross section calculated to have the same volume capacity, and k is a constant in the range from 0.006 to 0.16.
Cooling module for a motor vehicle, comprising at least first heat exchanger (3, 4) and at least one duct comprising an air inlet of the cooling module, the duct being configured to convey cooling air from the air inlet to the heat exchanger (3, 4), the duct comprises fixing elements (24, 24', 25, 26, 27, 28, 29) configured to fix the first heat exchanger (3, 4) to the duct, said duct comprising an air outlet, extending in a plane parallel to a plane of extension of the cooling module, and a cover wall bordering the air outlet and defined by a plurality of panels (20a, 20b, 20c, 20d) extending perpendicularly to the plane of extension of the cooling module, and characterised in that the first fastening elements (26, 27, 28, 29) project from an internal face of the duct so as to house the first heat exchanger in a housing defined at least in part by the covering wall of the duct.
Monolayer blown film comprising at least 80.0 wt% of a trimodal metallocene-catalysed polymer of ethylene with at least two different comonomers selected from alpha-olefins having from 4 to 10 carbon atoms, which has a) MFR 2 of 0.5 to 5 g/10 min (ISO1133, 190°C, 2.16 kg load), b) MFR 21 / MFR 2 of 10 to 25 (MFR 21 determined according to ISO1133, 190°C, 21.6 kg load) c) a density of 910 to 925 kg/m 3 determined according to ISO 1183 d) a MWD (ISO 16014-4:2003) in the range of from 3.0 to 5.0 and which consists of (i) an ethylene polymer component, comprising ethylene polymer fraction (A-1) and ethylene polymer fraction (A-2) and (ii) an ethylene polymer component, wherein the MFR 2 of the ethylene polymer components and are different from each other, wherein the monolayer blown film is characterized by a relative Elmendorf tear resistance measured according to ISO 6383/2 on a blown film with a film thickness of 40 μm in machine direction of at least 125 N/mm and in transversal direction of at least 165 N/mm. a) MFR 2 of 0.5 to 5 g/10 min (ISO1133, 190°C, 2.16 kg load), b) MFR 21 / MFR 2 of 10 to 25 (MFR 21 determined according to ISO1133, 190°C, 21.6 kg load) c) a density of 910 to 925 kg/m 3 determined according to ISO 1183 d) a MWD (ISO 16014-4:2003) in the range of from 3.0 to 5.0 and which consists of (i) an ethylene polymer component, comprising ethylene polymer fraction (A-1) and ethylene polymer fraction (A-2) and (ii) an ethylene polymer component, (i) an ethylene polymer component, comprising ethylene polymer fraction (A-1) and ethylene polymer fraction (A-2) and (ii) an ethylene polymer component, wherein the MFR 2 of the ethylene polymer components and are different from each other, wherein the monolayer blown film is characterized by a relative Elmendorf tear resistance measured according to ISO 6383/2 on a blown film with a film thickness of 40 μm in machine direction of at least 125 N/mm and in transversal direction of at least 165 N/mm.
A process for manufacturing a reflector antenna comprising: providing a support structure; placing a reflector surface on a mold; directly attaching the support structure to the reflector surface; removing the reflector surface and support structure assembly from the mold; measuring the geometry of the reflector surface; adjusting the surface geometry of the reflector if appropriate to obtain improved accuracy for the reflector surface; and fixedly connecting the support structure and the reflector surface. providing a support structure; placing a reflector surface on a mold; directly attaching the support structure to the reflector surface; removing the reflector surface and support structure assembly from the mold; measuring the geometry of the reflector surface; adjusting the surface geometry of the reflector if appropriate to obtain improved accuracy for the reflector surface; and fixedly connecting the support structure and the reflector surface.
Follower aircraft in formation flying comprising a flight command management system having at least one information source and a system for aiding formation flying of the follower aircraft with respect to a wake vortex from a leader aircraft, the system for aiding formation flying being independent of the at least one information source of the flight command management system, characterized in that the system for aiding formation flying comprises a controller and at least one accelerometer installed on the follower aircraft, the controller comprising electronic circuitry configured so as to: - receive (501, 601; 701, 703, 801, 802) acceleration measurements performed by said at least one accelerometer; - process (502, 602; 702, 704, 803, 804) the received measurements so as to obtain therefrom a value representative of vibrations generated by the wake vortex from the leader aircraft; - compare (503, 603; 706, 806) the obtained value with a predetermined threshold representative of excessive vibrations with regard to the location of said at least one accelerometer on the follower aircraft; - generate (504, 604; 707, 807) a notification when the comparison shows that the obtained value is greater than the predetermined threshold, the notification being a message sent to the flight command management system, and in that the flight command management system is configured so as to make adjustments to the trajectory of the follower aircraft based on said message. - receive (501, 601; 701, 703, 801, 802) acceleration measurements performed by said at least one accelerometer; - process (502, 602; 702, 704, 803, 804) the received measurements so as to obtain therefrom a value representative of vibrations generated by the wake vortex from the leader aircraft; - compare (503, 603; 706, 806) the obtained value with a predetermined threshold representative of excessive vibrations with regard to the location of said at least one accelerometer on the follower aircraft; - generate (504, 604; 707, 807) a notification when the comparison shows that the obtained value is greater than the predetermined threshold, the notification being a message sent to the flight command management system,
An apparatus for thermotherapy of a predefined treatment lesion covering at least a portion of a tumour, said apparatus comprises: a heating probe (10, 110) comprising an optical fiber and a cooling catheter, said optical fiber is inserted in said cooling catheter, said heating probe has a light emitting area, and said heating probe is interstitially insertable into said predefined treatment lesion, and is internally coolable by a fluid circulating in said catheter; and wherein said heating probe is connectable to a pump unit (52, 152) by two tubes configured for circulating said fluid; a light source connectable to said optical fiber for heating said predefined treatment lesion the apparatus being characterised by further comprising: at least a first thermal sensor member having at least one sensor area, said first thermal sensor member is positionable in tissue at a distance outside of a boundary of said predefined treatment lesion to monitor or estimate a first temperature. a control unit for controlling a power output of said light source based on said measured first temperature for maintaining said first temperature at a predetermined temperature, thereby obtaining and maintaining said predefined treatment lesion. a heating probe (10, 110) comprising an optical fiber and a cooling catheter, said optical fiber is inserted in said cooling catheter, said heating probe has a light emitting area, and said heating probe is interstitially insertable into said predefined treatment lesion, and is internally coolable by a fluid circulating in said catheter; and wherein said heating probe is connectable to a pump unit (52, 152) by two tubes configured for circulating said fluid; a light source connectable to said optical fiber for heating said predefined treatment lesion the apparatus being characterised by further comprising: at least a first thermal sensor member having at least one sensor area, said first thermal sensor member is positionable in tissue at a distance outside of a boundary of said predefined treatment lesion to monitor or estimate a first temperature. a control unit for controlling a power output of said light source based on said measured first temperature for maintaining said first temperature at a predetermined temperature, thereby obtaining and maintaining said predefined treatment lesion. at least a first thermal sensor member having at least one sensor area, said first thermal sensor member is positionable in tissue at a distance outside of a boundary of said predefined treatment lesion to monitor or estimate a first temperature. a control unit for controlling a power output of said light source based on said measured first temperature for maintaining said first temperature at a predetermined temperature, thereby obtaining and maintaining said predefined treatment lesion.
A method for controlling power flow in a regulated group of energy producing/consuming devices (FG, NFG, RNFG) in an electricity network, the method comprising: applying one or more fixed or variable power flow sequential trigger levels to disconnect individual regulated energy producing/consuming devices (FG, NFG, RNFG) in the event that the trigger point is exceeded, wherein the regulated energy producing/consuming devices (FG, NFG, RNFG) are individually and sequentially disconnected from the network; applying one or more reset power flow trigger levels which when breached reset the regulated energy producing/consuming devices (FG, NFG, RNFG) to re-start producing/consuming power, the reset level being lower than the sequential trigger level; applying one or more trim power flow trigger levels, which when breached causes the regulated energy producing/consuming devices (FG, NFG, RNFG) to reduce their producing/consuming power, applying a trip power flow trigger level which when breached causes all of the regulated energy producing/consuming devices (FG, NFG, RNFG) to stop producing/consuming power, and monitoring one or more power flow parameters to determine whether the one or more power flow trigger levels are breached. applying one or more fixed or variable power flow sequential trigger levels to disconnect individual regulated energy producing/consuming devices (FG, NFG, RNFG) in the event that the trigger point is exceeded, wherein the regulated energy producing/consuming devices (FG, NFG, RNFG) are individually and sequentially disconnected from the network; applying one or more reset power flow trigger levels which when breached reset the regulated energy producing/consuming devices (FG, NFG, RNFG) to re-start producing/consuming power, the reset level being lower than the sequential trigger level; applying one or more trim power flow trigger levels, which when breached causes the regulated energy producing/consuming devices (FG, NFG, RNFG) to reduce their producing/consuming power, applying a trip power flow trigger level which when breached causes all of the regulated energy producing/consuming devices (FG, NFG, RNFG) to stop producing/consuming power, and monitoring one or more power flow parameters to determine whether the one or more power flow trigger levels are breached.
A cosmetic container having an airtight refill case, comprising: a container main body; and a container lid hinged to a side of the container main body and vertically opening and closing, wherein a refill case having an upper lid connected to a side of a lower main body for keeping a cosmetic by a butterfly hinge and vertically opening and closing is inserted in a seat inside the container main body, and the refill case is doubly hermetically sealed by forming an assembly groove part having a ring-shaped assembly protrusion around an edge of a top of the lower main body, forming an assembly protrusion part having a ring-shaped assembly groove where the assembly protrusion is inserted around an edge of a bottom of the upper lid, and inserting the assembly protrusion part into the assembly groove part, characterised in that the ring-shaped assembly groove of the upper lid has inner and outer inclined portions to be fitted in a wedge type fashion onto the assembly protrusion of the lower main body. a container main body; and a container lid hinged to a side of the container main body and vertically opening and closing, wherein a refill case having an upper lid connected to a side of a lower main body for keeping a cosmetic by a butterfly hinge and vertically opening and closing is inserted in a seat inside the container main body, and the refill case is doubly hermetically sealed by forming an assembly groove part having a ring-shaped assembly protrusion around an edge of a top of the lower main body, forming an assembly protrusion part having a ring-shaped assembly groove where the assembly protrusion is inserted around an edge of a bottom of the upper lid, and inserting the assembly protrusion part into the assembly groove part, characterised in that the ring-shaped assembly groove of the upper lid has inner and outer inclined portions to be fitted in a wedge type fashion onto the assembly protrusion of the lower main body.