mhurhangee/ep-ind-claims huggingface dataset:
A power control module comprising: a transistor having a first side and a second side opposite from the first; a heat sink plate; a printed wiring board "PWB" spaced apart from the first side of the transistor, wherein the PWB is electrically connected to the transistor and includes an access hole arranged and configured to allow for pushing the transistor towards the sink plate; and the power control module characterized in that the heat sink plate is soldered to a second side of the transistor for heat dissipation from the transistor, and in that the heat sink plate includes a respective access hole (112, 114) arranged and configured to allow for a soldering tip to access through the heat sink plate and solder the transistor during assembly. a transistor having a first side and a second side opposite from the first; a heat sink plate; a printed wiring board "PWB" spaced apart from the first side of the transistor, wherein the PWB is electrically connected to the transistor and includes an access hole arranged and configured to allow for pushing the transistor towards the sink plate; and the power control module characterized in that the heat sink plate is soldered to a second side of the transistor for heat dissipation from the transistor, and in that the heat sink plate includes a respective access hole (112, 114) arranged and configured to allow for a soldering tip to access through the heat sink plate and solder the transistor during assembly.
An aqueous cleaning solution for removing rouging deposits on media-contacted surfaces of stainless steels, comprising a first component and a second component, characterized in that the first component is an alkali sulfite and the second component is an alkali formate, wherein the concentrations thereof are adjusted in such manner that formate is present in a molar ratio of 1.5 to 4.2 relative to sulfite, and that the pH value of the cleaning solution is 4.0 to 4.8.
An air-conditioned clothing (1,1a) for use with a helmet which can be used in both circumstances when the helmet is worn and when the helmet is not worn, and comprising: a clothing main body which at least covers an upper body of a body; one or more fans which are attached to the clothing main body and which form an air flow path between the clothing main body and the body or an underwear by taking in air from outside and forcefully generate an air flow in the air flow path; an air blow-out unit which is formed between back of a neck of a user and a back collar part of the clothing main body and which blows out the air which flows through the air flow path; a guide sheet which is continuously attached to the back collar part of the clothing main body and which guides the air which blows out from the air blow-out unit to the helmet along back of the neck and back of a head of the user; and an attachment unit (80,80a,800) which is attached to an edge part of the guide sheet and which is used to attach the guide sheet to the helmet, wherein the air is made to flow through the air flow path by the fans and the flowing air evaporates sweat coming out from the body to cool the body with a heat of evaporation and in a case where the helmet is worn, the air which blows out from the air blow-out unit is guided to the helmet by the guide sheet and taken into the helmet from an air intake which is formed between an inner edge of the helmet and the head of the user in order to circulate the air inside the helmet. a clothing main body which at least covers an upper body of a body; one or more fans which are attached to the clothing main body and which form an air flow path between the clothing main body and the body or an underwear by taking in air from outside and forcefully generate an air flow in the air flow path; an air blow-out unit which is formed between back of a neck of a user and a back collar part of the clothing main body and which blows out the air which flows through the air flow path; a guide sheet which is continuously attached to the back collar part of the clothing main body and which guides the air which blows out from the air blow-out unit to the helmet along back of the neck and back of a head of the user; and an attachment unit (80,80a,800) which is attached to an edge part of the guide sheet and which is used to attach the guide sheet to the helmet, wherein the air is made to flow through the air flow path by the fans and the flowing air evaporates sweat coming out from the body to cool the body with a heat of evaporation and in a case where the helmet is worn, the air which blows out from the air blow-out unit is guided to the helmet by the guide sheet and taken into the helmet from an air intake which is formed between an inner edge of the helmet and the head of the user in order to circulate the air inside the helmet.
An allyl compound represented by general formula (α): wherein ring Z 1 is a naphthalene ring, ring Z 2 is a benzene ring or a naphthalene ring, X is a hydrogen atom or a monovalent substituent having 1 to 18 carbon atoms, R is each independently an alkyl group having 1 to 4 carbon atoms or a halogen atom, m is 1 or 2, n is each independently an integer of 0 to 5, and when m is 1, the ring Z 1 and the ring Z 2 are bonded to each other via an oxygen atom.
A method for determining the leakage rate on a non-rigid specimen, comprising the steps of: introducing the specimen into a film chamber which can be evacuated and has at least one wall region made of a flexible material, lowering the pressure in the film chamber outside of the specimen, and measuring the pressure gradient within the film chamber outside of the specimen, characterized in that an outer overpressure is repeatedly exerted periodically at least on the flexible wall region during said pressure measurement until a predetermined threshold is reached, with the overpressure being subsequently released, wherein said overpressure exceeds the pressure in the film chamber and outside of the specimen and the pressure inside the specimen. introducing the specimen into a film chamber which can be evacuated and has at least one wall region made of a flexible material, lowering the pressure in the film chamber outside of the specimen, and measuring the pressure gradient within the film chamber outside of the specimen,
A steering wheel for a motor vehicle steering system, comprising a steering wheel hub which has a longitudinal axis and can be attached coaxially on a rotatably mounted steering spindle, and a steering wheel rim which is attached on the steering wheel hub, is at a radial spacing from the longitudinal axis, and extends in a planar manner transversely with respect to the longitudinal axis, wherein the steering wheel rim is mounted on the steering wheel hub in a bearing (34, 35) such that it can be inclined with respect to the longitudinal axis between an operating position and a stowed position about an inclination axis which lies transversely with respect to the longitudinal axis, the steering wheel rim being inclined at a flatter angle with respect to the longitudinal axis in the stowed position than in the operating position, wherein a torque generating device is arranged between the steering wheel hub and the steering wheel rim, by which torque generating device a torque can be exerted on the steering wheel rim about the inclination axis, and wherein the steering wheel hub has a releasable fixing device which can be moved selectively into at least one fixing position or one release position, the steering wheel rim being fixed relative to the steering wheel hub in a fixing position, and it being possible for the steering wheel rim to be inclined relative to the steering wheel hub in the release position, characterized in that the fixing device has a motorized actuator for setting the fixing position or the release position in a motorized manner.
A compound represented by the following general formula: General Formula m-L- n wherein L represents phenyl; A represents a cyano group; D represents a group having a negative Hammett's σ p value (but excluding a phenyl group); m represents an integer of 1 or more; n represents an integer of 2 or more; two of plural D's each contain an aromatic ring common to them but have a different structure; and the two of plural D's have a diarylamine structure in which two aryl groups constituting the diarylamine structure bond to each other and nitrogen atom of the diarylamine structure bonds to L via a single bond, and wherein the two of the plural D's satisfy the following requirement (a): Requirement (a) Two D's each have a carbazole ring that contains a nitrogen atom bonding to L, and the carbazole ring is common between the two D's, but the two differ from each other in point of at least one condition of the number of the substituents on the carbazole ring, the substitution site of the carbazole ring substituted with the substituent, and the structure of the substituent on the carbazole ring. wherein L represents phenyl; A represents a cyano group; D represents a group having a negative Hammett's σ p value (but excluding a phenyl group); m represents an integer of 1 or more; n represents an integer of 2 or more; two of plural D's each contain an aromatic ring common to them but have a different structure; and the two of plural D's have a diarylamine structure in which two aryl groups constituting the diarylamine structure bond to each other and nitrogen atom of the diarylamine structure bonds to L via a single bond, and wherein the two of the plural D's satisfy the following requirement (a): Requirement (a) Two D's each have a carbazole ring that contains a nitrogen atom bonding to L, and the carbazole ring is common between the two D's, but the two differ from each other in point of at least one condition of the number of the substituents on the carbazole ring, the substitution site of the carbazole ring substituted with the substituent, and the structure of the substituent on the carbazole ring. Requirement (a) Two D's each have a carbazole ring that contains a nitrogen atom bonding to L, and the carbazole ring is common between the two D's, but the two differ from each other in point of at least one condition of the number of the substituents on the carbazole ring, the substitution site of the carbazole ring substituted with the substituent, and the structure of the substituent on the carbazole ring.
A compound of formula, including any stereochemically isomeric form thereof, wherein A is wherein R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is pentafluorosulfanyl, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethyl, R 5 is hydrogen, Z is carbon, and R 6 is methyl; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethyl, R 5 is fluoro, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethoxy, R 5 is hydrogen, Z is carbon, and R 6 is methyl; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethoxy, R 5 is fluoro, Z is carbon, and R 6 is hydrogen; or R 1 is fluoro, R 2 is methoxy, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethoxy, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is hydrogen, R 3 is deuterium, A is (a-1), R 4 is trifluoromethoxy, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is -OCH 2 CH 2 OH, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethoxy, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethyl, R 5 is methoxy, Z is nitrogen, and R 6 is absent; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-2), and R 4 is trifluoromethyl; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethylthio, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or a pharmaceutically acceptable salt, solvate or polymorph thereof. A is wherein R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is pentafluorosulfanyl, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethyl, R 5 is hydrogen, Z is carbon, and R 6 is methyl; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethyl, R 5 is fluoro, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethoxy, R 5 is hydrogen, Z is carbon, and R 6 is methyl; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethoxy, R 5 is fluoro, Z is carbon, and R 6 is hydrogen; or R 1 is fluoro, R 2 is methoxy, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethoxy, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is hydrogen, R 3 is deuterium, A is (a-1), R 4 is trifluoromethoxy, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is -OCH 2 CH 2 OH, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethoxy, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethyl, R 5 is methoxy, Z is nitrogen, and R 6 is absent; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-2), and R 4 is trifluoromethyl; or R 1 is chloro, R 2 is hydrogen, R 3 is hydrogen, A is (a-1), R 4 is trifluoromethylthio, R 5 is hydrogen, Z is carbon, and R 6 is hydrogen;
A tiltrotor aircraft comprising: a fuselage; a wing supported by the fuselage and having first and second outboard ends (20a, 20b); a first pylon assembly coupled to the outboard end of the wing, the pylon assembly having an outboard end; a second pylon assembly coupled to the outboard end of the wing, the pylon assembly having an outboard end; a first wing extension rotatably coupled to the outboard end of the first pylon assembly; and a second wing extension rotatably coupled to the outboard end of the second pylon assembly; wherein the wing extensions (30a, 30b) are rotatable between a flight position in a flight mode and a stow position in a storage mode; wherein, the wing extensions (30a, 30b) fold inboard toward the fuselage in the stow position, thereby reducing a wingspan of the tiltrotor aircraft in the storage mode; and characterized in that the wing extensions (30a, 30b) have an angular range of motion of at least 180 degrees such that the wing extensions (30a, 30b) are substantially parallel with the wing when the wing extensions (30a, 30b) are in the stow position. a fuselage; a wing supported by the fuselage and having first and second outboard ends (20a, 20b); a first pylon assembly coupled to the outboard end of the wing, the pylon assembly having an outboard end; a second pylon assembly coupled to the outboard end of the wing, the pylon assembly having an outboard end; a first wing extension rotatably coupled to the outboard end of the first pylon assembly; and a second wing extension rotatably coupled to the outboard end of the second pylon assembly; wherein the wing extensions (30a, 30b) are rotatable between a flight position in a flight mode and a stow position in a storage mode; wherein, the wing extensions (30a, 30b) fold inboard toward the fuselage in the stow position, thereby reducing a wingspan of the tiltrotor aircraft in the storage mode; and characterized in that the wing extensions (30a, 30b) have an angular range of motion of at least 180 degrees such that the wing extensions (30a, 30b) are substantially parallel with the wing when the wing extensions (30a, 30b) are in the stow position.
A system for autonomously onboarding a vehicle on a ramp comprising one or more ramp paths (51, 52), wherein the system comprises: - a first sensor arranged to be positioned in front of a first front wheel of the vehicle, - a second sensor arranged to be positioned in front of the second front wheel of the vehicle, - the first and second sensors (21, 22) are configured to obtain a three dimensional view of at least an area in front of the first and the second front wheel (11, 12), wherein the area at least comprises an area under the vehicle in front of the first and the second front wheels (11, 12), - a control unit configured to: - receive the three dimensional view from the first and second sensors (21, 22), - identify the one or more ramp paths (51, 52) of the ramp in the three dimensional view, - calculate a three dimensional path for onboarding the vehicle on the one or more ramp paths (51, 52) of the ramp and, - control the vehicle to autonomously onboard the vehicle on to the one or more ramp paths (51, 52) of the ramp along the three dimensional path. - a first sensor arranged to be positioned in front of a first front wheel of the vehicle, - a second sensor arranged to be positioned in front of the second front wheel of the vehicle, - the first and second sensors (21, 22) are configured to obtain a three dimensional view of at least an area in front of the first and the second front wheel (11, 12), wherein the area at least comprises an area under the vehicle in front of the first and the second front wheels (11, 12), - a control unit configured to: - receive the three dimensional view from the first and second sensors (21, 22), - identify the one or more ramp paths (51, 52) of the ramp in the three dimensional view, - calculate a three dimensional path for onboarding the vehicle on the one or more ramp paths (51, 52) of the ramp and, - control the vehicle to autonomously onboard the vehicle on to the one or more ramp paths (51, 52) of the ramp along the three dimensional path. - receive the three dimensional view from the first and second sensors (21, 22), - identify the one or more ramp paths (51, 52) of the ramp in the three dimensional view, - calculate a three dimensional path for onboarding the vehicle on the one or more ramp paths (51, 52) of the ramp and, - control the vehicle to autonomously onboard the vehicle on to the one or more ramp paths (51, 52) of the ramp along the three dimensional path.
A meander-type, azimuth frequency-scanned antenna with reduced elevation beam squint suitable for use on an automated vehicle radar system, said antenna comprising: a plurality of linear parallel sub-arrays formed by a serpentine-arrangement of a continuous-strip of material, wherein a first sub-array, configured to support signal propagation in a first-direction, is adjacent to a second sub-array, wherein the second sub-array is configured to support signal propagation in a second-direction, opposite to the first-direction, wherein the first sub-array and the second sub-array each further comprise a plurality of radiators configured such that a radar-beam emitted by the antenna in response to the signal has an elevation-angle that is substantially unchanged when a frequency of the signal is varied, wherein the radiators are slot-radiators, wherein the slot-radiators have a respective slot-angle measured with respect to an axis of the serpentine-arrangement, characterized in that each instance of a slot-radiator in the first sub-array corresponds to an instance of a slot-radiator in the second sub-array that is adjacent to an instance of a slot-radiator in the first sub-array, and the slot-angles of corresponding instances of slot-radiators vary monotonically across the plurality of sub-arrays. a plurality of linear parallel sub-arrays formed by a serpentine-arrangement of a continuous-strip of material, wherein a first sub-array, configured to support signal propagation in a first-direction, is adjacent to a second sub-array, wherein the second sub-array is configured to support signal propagation in a second-direction, opposite to the first-direction, wherein the first sub-array and the second sub-array each further comprise a plurality of radiators configured such that a radar-beam emitted by the antenna in response to the signal has an elevation-angle that is substantially unchanged when a frequency of the signal is varied, wherein the radiators are slot-radiators, wherein the slot-radiators have a respective slot-angle measured with respect to an axis of the serpentine-arrangement, characterized in that each instance of a slot-radiator in the first sub-array corresponds to an instance of a slot-radiator in the second sub-array that is adjacent to an instance of a slot-radiator in the first sub-array, and the slot-angles of corresponding instances of slot-radiators vary monotonically across the plurality of sub-arrays.
A lens system (200, 300, 400, 600) for use as either an intra-ocular lens or as an insert into the corneal tissue of a natural eye to replace one or more optical functions of the natural eye, the lens system comprising: a base lens element (252, 352, 452, 652) having a base refractive power and formed of a soft acrylic; an electro-active lens element (218, 326, 430, 618, 930), encapsulated within the base lens element, having an electrically controllable focus; and an annular charge storage capacitor arranged around a perimeter of the electro-active lens element (218, 326, 430, 618, 930) or a rechargeable battery ring (324, 424, 624), said annular charge storage capacitor or rechargeable battery ring (324, 424, 624) being configured to power the electro-active lens element and to be charged inductively via an external induction coil. a base lens element (252, 352, 452, 652) having a base refractive power and formed of a soft acrylic; an electro-active lens element (218, 326, 430, 618, 930), encapsulated within the base lens element, having an electrically controllable focus; and an annular charge storage capacitor arranged around a perimeter of the electro-active lens element (218, 326, 430, 618, 930) or a rechargeable battery ring (324, 424, 624), said annular charge storage capacitor or rechargeable battery ring (324, 424, 624) being configured to power the electro-active lens element and to be charged inductively via an external induction coil.
Testing device for testing a tightness of containers, comprising - a receptacle unit for receiving at least one container, having a first receptacle part and a second receptacle part; - wherein a pivot axle for pivoting at least one receptacle part is disposed on the first and/or the second receptacle part (31, 32), characterized in that - the receptacle unit in the direction of a longitudinal axis of the receptacle unit is divided into the first and the second receptacle part (31, 32), wherein the receptacle unit in a partition plane is portioned into the first and the second receptacle parts (31, 32), and wherein the partition plane in relation to a vertical axis (X-X) is disposed so as to be inclined at a first angle (α). - a receptacle unit for receiving at least one container, having a first receptacle part and a second receptacle part; - wherein a pivot axle for pivoting at least one receptacle part is disposed on the first and/or the second receptacle part (31, 32), - the receptacle unit in the direction of a longitudinal axis of the receptacle unit is divided into the first and the second receptacle part (31, 32),