mhurhangee/ep-ind-claims huggingface dataset:
A cooling system, comprising: a housing (70; 160), including a top section (80; 168) and a bottom section (82; 170); a connector (74; 164) within the housing (70; 160) capable of communicating with an exterior power source; a first membrane (72; 162) within the housing (70, 160), wherein the first membrane (72; 162) is connected to driver electronics; and a second membrane (72; 162) connected to the driver electronics; wherein a first synthetic jet is formed between the first membrane (72;162) and the top section (80; 168) of the housing (70, 160), a second synthetic jet is formed between the first and second membranes (72; 162) and a third synthetic jet 96) is formed between the second membrane (72; 162) and the bottom section (82; 170) of the housing (70, 160); characterized in that the driver electronics are located within the housing (70, 160). a housing (70; 160), including a top section (80; 168) and a bottom section (82; 170); a connector (74; 164) within the housing (70; 160) capable of communicating with an exterior power source; a first membrane (72; 162) within the housing (70, 160), wherein the first membrane (72; 162) is connected to driver electronics; and a second membrane (72; 162) connected to the driver electronics; wherein a first synthetic jet is formed between the first membrane (72;162) and the top section (80; 168) of the housing (70, 160), a second synthetic jet is formed between the first and second membranes (72; 162) and a third synthetic jet 96) is formed between the second membrane (72; 162) and the bottom section (82; 170) of the housing (70, 160);
Needling machine for the reinforcement of a textile fabric, in particular a fibrous fleece or a fibrous pile web, which can be conveyed through the needling machine in a conveying direction, with: a first main shaft and a second main shaft; at least one first connecting rod, which is eccentrically mounted on the first main shaft, and at least one second connecting rod, which is eccentrically mounted on the second main shaft, wherein the at least one first connecting rod and the at least one second connecting rod are connected to each other in an articulated manner; and at least one needle bar (24, 26), wherein each of the at least one needle bars (24, 26) is rigidly connected to the at least one first connecting rod, or to the at least one second connecting rod; characterised in that, the first main shaft and the second main shaft can be driven in opposite directions. a first main shaft and a second main shaft; at least one first connecting rod, which is eccentrically mounted on the first main shaft, and at least one second connecting rod, which is eccentrically mounted on the second main shaft, wherein the at least one first connecting rod and the at least one second connecting rod are connected to each other in an articulated manner; and at least one needle bar (24, 26), wherein each of the at least one needle bars (24, 26) is rigidly connected to the at least one first connecting rod, or to the at least one second connecting rod; characterised in that, the first main shaft and the second main shaft can be driven in opposite directions.
A telescoping ladder, comprising: a first stile, a second stile, the first and second stiles (14, 16) each having a plurality of columns disposed in a nested arrangement for relative axial movement in a telescopic fashion along an axis of the plurality of columns between an fully-extended position and a collapsed position, wherein, each column having a hollow body, such that when the ladder is collapsed from the fully-extended position, each column substantially nests within another column; a plurality of rungs extending between the first stile and the second stile, each rung connected to a column of the first stile and a column of the second stile; and a plurality of column retaining mechanisms, each column retaining mechanism being provided on one of the columns, each column retaining mechanism adapted to retain a further column which is nested immediately within the one of the columns in the collapsed position, each column retaining mechanism preventing the column immediately within the one of the columns from being extended from its nested position until the one of the columns is fully extended from its nested position with respect to the column which is immediately outside the one of the columns, the telescoping ladder being characterized in that each column retaining mechanism is provided on an outer surface of the one of the columns. a first stile, a second stile, the first and second stiles (14, 16) each having a plurality of columns disposed in a nested arrangement for relative axial movement in a telescopic fashion along an axis of the plurality of columns between an fully-extended position and a collapsed position, wherein, each column having a hollow body, such that when the ladder is collapsed from the fully-extended position, each column substantially nests within another column; a plurality of rungs extending between the first stile and the second stile, each rung connected to a column of the first stile and a column of the second stile; and a plurality of column retaining mechanisms, each column retaining mechanism being provided on one of the columns, each column retaining mechanism adapted to retain a further column which is nested immediately within the one of the columns in the collapsed position, each column retaining mechanism preventing the column immediately within the one of the columns from being extended from its nested position until the one of the columns is fully extended from its nested position with respect to the column which is immediately outside the one of the columns, the telescoping ladder being characterized in that each column retaining mechanism is provided on an outer surface of the one of the columns.
Filter element for filtering a liquid, in particular an urea solution, wherein the filter element annularly encloses an interior space and can be flowed through from a raw side to a clean side in parallel through at least a first and a second filter medium which are each disposed between the raw side and the clean side (41, 42) of the filter element, wherein the first filter medium is liquid-permeable and gas-impermeable and the second filter medium is liquid-impermeable and gas-permeable, and wherein the first filter medium features an end disc on one or both front faces and the second filter medium is disposed in an opening in an end disc.
A MEMS device comprising: a body of semiconductor material defining a support structure; a pass-through cavity in the body, surrounded by the support structure; a movable structure suspended in the pass-through cavity; an elastic structure extending in the pass-through cavity between the support structure and the movable structure, the elastic structure comprising a first portion and a second portion and being subject, in use, to mechanical stress; a metal region extending on the first portion of the elastic structure; and a buried cavity in the elastic structure; the buried cavity extending between the first and the second portions of the elastic structure. a body of semiconductor material defining a support structure; a pass-through cavity in the body, surrounded by the support structure; a movable structure suspended in the pass-through cavity; an elastic structure extending in the pass-through cavity between the support structure and the movable structure, the elastic structure comprising a first portion and a second portion and being subject, in use, to mechanical stress; a metal region extending on the first portion of the elastic structure; and a buried cavity in the elastic structure; the buried cavity extending between the first and the second portions of the elastic structure.
(Currently amended) A power source equipment, PSE, controller exhibiting low standby levels for power over Ethernet, PoE, characterized by comprising: a micro-controller; a detection and classification circuitry coupled to the micro-controller and arranged to detect if a powered device, PD, is connected for a first period of time and determines power needed to operate the connected PD; and a power control and monitor circuitry coupled to the micro-controller and arranged to power the connected PD and to monitor the power consumption of the PD, wherein the micro-controtier is arranged to: in the event the detection and classification circuitry does not detect a PD, deactivate the detection and classification circuitry, the power control and monitor circuitry to minimize standby power, put the micro-controller itself into deep sleep after a second period of time waking the micro-controller (301 itself up; and in the event the detection and classification circuitry detects a PD, check whether the PD is coupled, if the PD is coupled deactivate the detection and classification circuitry, and power the PD by activating the power control and monitor circuitry 303) a micro-controller; a detection and classification circuitry coupled to the micro-controller and arranged to detect if a powered device, PD, is connected for a first period of time and determines power needed to operate the connected PD; and a power control and monitor circuitry coupled to the micro-controller and arranged to power the connected PD and to monitor the power consumption of the PD, wherein the micro-controtier is arranged to: in the event the detection and classification circuitry does not detect a PD, deactivate the detection and classification circuitry, the power control and monitor circuitry to minimize standby power, put the micro-controller itself into deep sleep after a second period of time waking the micro-controller (301 itself up; and in the event the detection and classification circuitry detects a PD, check whether the PD is coupled, if the PD is coupled deactivate the detection and classification circuitry, and power the PD by activating the power control and monitor circuitry 303) in the event the detection and classification circuitry does not detect a PD, deactivate the detection and classification circuitry, the power control and monitor circuitry to minimize standby power, put the micro-controller itself into deep sleep after a second period of time waking the micro-controller (301 itself up; and in the event the detection and classification circuitry detects a PD, check whether the PD is coupled, if the PD is coupled deactivate the detection and classification circuitry, and power the PD by activating the power control and monitor circuitry 303)
Grinding wheel with a support body (2, 3), which has a central coupling region for attaching the grinding wheel to a rotary drive for rotating the grinding wheel about a rotational axis running through the coupling region and a circumferential surface, and with a grinding layer, which is applied, in particular sintered, onto the circumferential surface of the support body (2, 3), wherein the support body (2, 3) comprises a first part and a second part connected thereto, wherein the first part has the circumferential surface, and the second part exclusively has the coupling region and consists of a vibration-damping material, characterized in that the vibration-damping material of the second part is cast iron, preferably with lamellar graphite, spheroidal graphite, vermicular graphite, or cast steel, and/or aluminium bronze.
Modified homoserine dehydrogenase, wherein in the amino acid sequence of SEQ ID NO: 1, the amino acid at position 285 is substituted with isoleucine; the amino acid at position 398 is substituted with glutamine; or the amino acids at both positions are substituted with isoleucine and glutamine, respectively.
A secondary molded article using a laminate comprising a layer comprising a saponified ethylene/vinyl ester copolymer and a layer which comprises a thermoplastic resin that is not a saponified ethylene/vinyl ester copolymer and which has been laminated to at least one surface of the layer comprising a saponified ethylene/vinyl ester copolymer via a layer comprising an adhesive resin, wherein shear viscosity ratio of the saponified ethylene/vinyl ester copolymer and the adhesive resin is 0.70-1.50 at a shear rate of 0.1 [1/s] and 0.90-1.10 at a shear rate of 1.0 [1/s]; wherein the respective value of the shear viscosity is measured with a rotary rheometer under the following conditions: atmosphere: nitrogen atmosphere; temperature: 210 °C; strain: 5 %; measuring jig: parallel-parallel plates with a diameter of 25 mm; preheating time: 10 min; and wherein the secondary molded article has a draw ratio of 0.1-3; wherein the draw ratio is the depth of the molded article in mm divided by a maximum diameter of the molded article in mm. wherein the respective value of the shear viscosity is measured with a rotary rheometer under the following conditions: atmosphere: nitrogen atmosphere; temperature: 210 °C; strain: 5 %; measuring jig: parallel-parallel plates with a diameter of 25 mm; preheating time: 10 min; and wherein the secondary molded article has a draw ratio of 0.1-3; wherein the draw ratio is the depth of the molded article in mm divided by a maximum diameter of the molded article in mm.
An exhaust system for reducing infrared emissions of a rotary wing aircraft having an engine, an aft turbine section, a tail fairing, and an aft propeller, the exhaust system comprising: an exhaust duct having a fore end connected with the aft turbine section of the engine of the rotary wing aircraft, in a fluidly sealed manner, the exhaust duct having an aft end having an exhaust opening to expel engine exhaust proximate to the tail fairing of the rotary wing aircraft; characterized in that the exhaust system further comprises a drive shaft collocated with the exhaust duct as a single transfer duct, wherein, the single transfer duct is a single component configured to transfer exhaust from the engine and to transfer force from the engine to the propeller, the drive shaft being concentric with the exhaust duct and configured to provide rotational force to the aft propeller of the rotary wing aircraft, wherein the exhaust opening is configured to emit exhaust about the propeller proximate to the tail fairing. an exhaust duct having a fore end connected with the aft turbine section of the engine of the rotary wing aircraft, in a fluidly sealed manner, the exhaust duct having an aft end having an exhaust opening to expel engine exhaust proximate to the tail fairing of the rotary wing aircraft; characterized in that the exhaust system further comprises a drive shaft collocated with the exhaust duct as a single transfer duct, wherein, the single transfer duct is a single component configured to transfer exhaust from the engine and to transfer force from the engine to the propeller, the drive shaft being concentric with the exhaust duct and configured to provide rotational force to the aft propeller of the rotary wing aircraft, wherein the exhaust opening is configured to emit exhaust about the propeller proximate to the tail fairing.
An ear shape analysis device comprising: a sample ear analyzer configured to generate a plurality of ear shape data sets (V -V) for a plurality of sample ears, each set representing a difference between a point group (P R) representative of a three-dimensional shape of a reference ear and a point group (P S (n)) representative of a three-dimensional shape of a corresponding one of the plurality of sample ears; an averaging calculator configured to generate averaged shape data (V A) by averaging the plurality of ear shape data sets (V -V) generated by the sample ear analyzer for the plurality of sample ears; and an ear shape identifier configured to generate three-dimensional shape data representing an average ear shape (Z A) comprehensively reflecting the shapes of the plurality of sample ears by translating coordinates of respective points of the point group (P R) representing the three-dimensional shape of the reference ear, by using the averaged shape data (V A). a sample ear analyzer configured to generate a plurality of ear shape data sets (V -V) for a plurality of sample ears, each set representing a difference between a point group (P R) representative of a three-dimensional shape of a reference ear and a point group (P S (n)) representative of a three-dimensional shape of a corresponding one of the plurality of sample ears; an averaging calculator configured to generate averaged shape data (V A) by averaging the plurality of ear shape data sets (V -V) generated by the sample ear analyzer for the plurality of sample ears; and an ear shape identifier configured to generate three-dimensional shape data representing an average ear shape (Z A) comprehensively reflecting the shapes of the plurality of sample ears by translating coordinates of respective points of the point group (P R) representing the three-dimensional shape of the reference ear, by using the averaged shape data (V A).
A thread remaining amount detecting device comprising: a pedestal on which a cone of a thread cone can be placed; and a detector that includes a light emitter and a light receiver, wherein the thread remaining amount detecting device is configured to detect a remaining amount of yarn of said thread cone supplied to a knitting machine, and is characterized in that the detector is disposed on the pedestal, the light emitter irradiates with light a bottom surface of a thread-wound part of the thread cone, and the light receiver receives reflected light from the bottom surface. a pedestal on which a cone of a thread cone can be placed; and a detector that includes a light emitter and a light receiver, wherein the thread remaining amount detecting device is configured to detect a remaining amount of yarn of said thread cone supplied to a knitting machine, and is characterized in that the detector is disposed on the pedestal, the light emitter irradiates with light a bottom surface of a thread-wound part of the thread cone, and the light receiver receives reflected light from the bottom surface.
System for manoeuvring an aircraft landing gear which is articulated in a gear bay closed by a set of 5 doors, comprising: - a general control unit for the gear bay to initiate the various manoeuvres, - a control chain for the doors, comprising at least one device for locking the door, at least one member for actuating the door and a member for controlling the actuating member, - a control chain for the landing gear, comprising at least one device for holding the gear, at least one member for actuating the gear and a member for controlling the actuating member, characterized in that the general control unit, the door control chain and the control chain for the gear are controlled by a source of electrical energy during normal operation of the aircraft, during emergency operation and during maintenance, said door locking device(s), said member(s) for controlling the door actuating member, said device(s) for holding the gear and said member(s) for controlling the gear actuating member being controlled electrically, said door locking device consisting of a locking hook that is controlled electrically from an electric actuator, said device for holding the gear consists of a hook for holding the gear, controlled electrically from an electric actuator, the control chain for the doors and the control chain for the landing gear each being connected to the general control unit only by an electric connection and being able to receive control commands sent by the general control unit according to a predetermined sequence. - a general control unit for the gear bay to initiate the various manoeuvres, - a control chain for the doors, comprising at least one device for locking the door, at least one member for actuating the door and a member for controlling the actuating member, - a control chain for the landing gear, comprising at least one device for holding the gear, at least one member for actuating the gear and a member for controlling the actuating member,
A method of controlling a wind turbine comprising one or more component cooling devices, the method comprising: receiving one or more inputs indicative of noise generated by the one or more component cooling devices; determining the contribution of noise from the one or more component cooling devices to overall turbine noise based upon the one or more inputs; and modifying turbine operation based upon the contribution of cooling device noise to overall turbine noise and based upon turbine noise requirements, characterized in that modifying turbine operation comprises: one or more of increasing power output, increasing rotor speed, varying the pitch angle of the blades, or any combination thereof, when the contribution of noise from the one or more component cooling devices decreases; and one or more of decreasing power output, reducing rotor speed, varying the pitch angle of the blades, or any combination thereof, when the contribution of noise from the one or more component cooling devices increases. receiving one or more inputs indicative of noise generated by the one or more component cooling devices; determining the contribution of noise from the one or more component cooling devices to overall turbine noise based upon the one or more inputs; and modifying turbine operation based upon the contribution of cooling device noise to overall turbine noise and based upon turbine noise requirements, characterized in that modifying turbine operation comprises: one or more of increasing power output, increasing rotor speed, varying the pitch angle of the blades, or any combination thereof, when the contribution of noise from the one or more component cooling devices decreases; and one or more of decreasing power output, reducing rotor speed, varying the pitch angle of the blades, or any combination thereof, when the contribution of noise from the one or more component cooling devices increases. one or more of increasing power output, increasing rotor speed, varying the pitch angle of the blades, or any combination thereof, when the contribution of noise from the one or more component cooling devices decreases; and one or more of decreasing power output, reducing rotor speed, varying the pitch angle of the blades, or any combination thereof, when the contribution of noise from the one or more component cooling devices increases.
A hydrogen-absorbing alloy for hybrid electric vehicles which is an AB 5 -type alloy having a CaCu 5 -type crystal structure, characterized by having the general formula R Ni a Co b Al c Mn d (R: mixture of rare earth metals), wherein 4.15≦a≦4.4, 0.15≦b≦0.35, 1.2≦c/d≦1.7, 5.25≦a + b + c + d≦5.45.