mhurhangee/ep-ind-claims huggingface dataset:
A compound of formula IA: or a pharmaceutically acceptable salt thereof, wherein: X a is CR 2a; Y a is CR 4a; R 1a, R 2a, R 3a, R 4a and R 5a each independently represent H, F or Cl; wherein: two of R 1a, R 2a, R 3a, R 4a and R 5a represent Cl, one of R 1a, R 2a, R 3a, R 4a and R 5a represents F, and two of R 1a, R 2a, R 3a, R 4a and R 5a represent H; two of R 1a, R 2a, R 3a, R 4a and R 5a represent F, one of R 1a, R 2a, R 3a, R 4a and R 5a represents Cl, and two of R 1a, R 2a, R 3a, R 4a and R 5a represent H; or the compound is selected from: 2-(3,4,5-trichlorobenzylidene)hydrazine-1-carboximidamide; 2-(2,4,5-trichlorobenzylidene)hydrazine-1-carboximidamide; 2-(2,3,4-trichlorobenzylidene)hydrazine-1-carboximidamide, or a pharmaceutically acceptable salt of any one thereof. X a is CR 2a; Y a is CR 4a; R 1a, R 2a, R 3a, R 4a and R 5a each independently represent H, F or Cl; two of R 1a, R 2a, R 3a, R 4a and R 5a represent Cl, one of R 1a, R 2a, R 3a, R 4a and R 5a represents F, and two of R 1a, R 2a, R 3a, R 4a and R 5a represent H; two of R 1a, R 2a, R 3a, R 4a and R 5a represent F, one of R 1a, R 2a, R 3a, R 4a and R 5a represents Cl, and two of R 1a, R 2a, R 3a, R 4a and R 5a represent H; or the compound is selected from: 2-(3,4,5-trichlorobenzylidene)hydrazine-1-carboximidamide; 2-(2,4,5-trichlorobenzylidene)hydrazine-1-carboximidamide; 2-(2,3,4-trichlorobenzylidene)hydrazine-1-carboximidamide, 2-(3,4,5-trichlorobenzylidene)hydrazine-1-carboximidamide; 2-(2,4,5-trichlorobenzylidene)hydrazine-1-carboximidamide; 2-(2,3,4-trichlorobenzylidene)hydrazine-1-carboximidamide,
A process for treating an off-gas from the thermal processing of a precious-metal-containing feedstock, the process comprising: cooling the off-gas to a temperature of from 300 to 500°C, passing the cooled off-gas through a first particulate filter to recover particulate material; and dosing the off-gas from the first particulate filter with a sorbent material and passing the dosed off-gas through a second particulate filter; wherein at least a portion of the particulate material recovered from the first particulate filter is recycled into the thermal processing of the precious-metal-containing feedstock. cooling the off-gas to a temperature of from 300 to 500°C, passing the cooled off-gas through a first particulate filter to recover particulate material; and dosing the off-gas from the first particulate filter with a sorbent material and passing the dosed off-gas through a second particulate filter; wherein at least a portion of the particulate material recovered from the first particulate filter is recycled into the thermal processing of the precious-metal-containing feedstock.
A gas turbine engine comprising: a core gas path extending along an engine axis; a bypass gas path surrounding the core gaspath; a turbine exhaust case inner body having a radially outer surface defining a portion of a radially inner flow boundary wall of the core gaspath; and a lobed exhaust mixer surrounding at least a portion of the turbine exhaust case inner body and defining an intermediate wall between the core gaspath and the bypass gas path, the lobed exhaust mixer including: lobes (44, 42); a stiffener ring; and a plurality of circumferentially spaced-apart struts extending from the stiffener ring to at least some of the lobes (44, 42); characterized in that: the lobed exhaust mixer further includes at least one spring extending from a radially inner surface of the stiffener ring to the radially outer surface of the turbine exhaust case inner body. a core gas path extending along an engine axis; a bypass gas path surrounding the core gaspath; a turbine exhaust case inner body having a radially outer surface defining a portion of a radially inner flow boundary wall of the core gaspath; and a lobed exhaust mixer surrounding at least a portion of the turbine exhaust case inner body and defining an intermediate wall between the core gaspath and the bypass gas path, the lobed exhaust mixer including: lobes (44, 42); a stiffener ring; and a plurality of circumferentially spaced-apart struts extending from the stiffener ring to at least some of the lobes (44, 42); characterized in that: the lobed exhaust mixer further includes at least one spring extending from a radially inner surface of the stiffener ring to the radially outer surface of the turbine exhaust case inner body. lobes (44, 42); a stiffener ring; and a plurality of circumferentially spaced-apart struts extending from the stiffener ring to at least some of the lobes (44, 42); characterized in that: the lobed exhaust mixer further includes at least one spring extending from a radially inner surface of the stiffener ring to the radially outer surface of the turbine exhaust case inner body.
A foldable vehicle comprising a frame, a handlebar support portion for receiving a handlebar at a front end of the frame, a front wheel support portion for receiving a front wheet, a rear wheel support portion for receiving a rear wheel, at a distal end of the frame, a leg support portion for receiving leg supports in a middle part of the frame, and a saddle support portion for receiving a saddle, a support element between the saddle support portion and a lower frame pipe, the support element being pivotally connected to the lower frame pipe, a lower part of the support element having the leg support portion, characterized in that an upper part of the support element has a sliding carriage that is moveable along an upper frame pipe and can be locked and unlocked to the upper frame pipe, and a connecting plate is located at a handlebar side of the lower frame pipe and configured to lock an upright element connecting the front wheel support portion and the handlebar support portion into the riding and/or transporting position.
A mounting system for securing a gas turbine engine to an aircraft support structure comprising: an aircraft support structure; a gas turbine engine including an outer case; an outer link assembly attachable to the aircraft support structure and the gas turbine engine, the outer link assembly including first and second links (52,54) disposed in a first plane transverse to the centerline of the gas turbine engine and an upper thrust link disposed along the centerline; and at least one lower thrust link (38A,38B) attachable to the aircraft support structure and the gas turbine engine, the at least one lower thrust link (38A,38B) attached to the gas turbine engine at a mount location within the first plane transverse to the centerline of the gas turbine engine; a fixed link secured to the support structure; wherein the first and second links (52,54) of the outer link assembly are attached on one end to an outer surface of the outer case of the gas turbine engine, and at a second end to the fixed link; and wherein the upper thrust link is attached to the outer case parallel to the centerline of the gas turbine engine; characterised in that the outer case includes a mounting slot arranged within the first plane within which the upper thrust link is secured by a first fastener such that a portion of the upper thrust link extends from the mounting slot into a pocket defined by the aircraft support structure, and is secured at an end within the pocket by a second fastener, wherein one of the first and second links (52,54) is secured to the fixed link to constrain movement within the first plane transverse to the centerline of the gas turbine engine. an aircraft support structure; a gas turbine engine including an outer case; an outer link assembly attachable to the aircraft support structure and the gas turbine engine, the outer link assembly including first and second links (52,54) disposed in a first plane transverse to the centerline of the gas turbine engine and an upper thrust link disposed along the centerline; and at least one lower thrust link (38A,38B) attachable to the aircraft support structure and the gas turbine engine, the at least one lower thrust link (38A,38B) attached to the gas turbine engine at a mount location within the first plane transverse to the centerline of the gas turbine engine; a fixed link secured to the support structure; wherein the first and second links (52,54) of the outer link assembly are attached on one end to an outer surface of the outer case of the gas turbine engine, and at a second end to the fixed link; and wherein the upper thrust link is attached to the outer case parallel to the centerline of the gas turbine engine;
A medical kit of instruments for transplanting a section of a first bone to a second bone in an arthroscopic procedure, comprising: a double cannula having two tubes (t) extending parallel to each other and having axes at a precise distance from each other; said tubes being similar in length and comprising openings that are leveled with respect to each other on a distal end of said double cannula; said double cannula having a proximal end carrying a handle (h), and a distal end formed with a window (w) in each of said tubes to enable observing the interior of the respective tubes; and two elongated cannulated holding devices, each device sized to fit within one of said two tubes of said double cannula and configured to engage said section of said first bone to firmly attach said bone section to said double cannula. a double cannula having two tubes (t) extending parallel to each other and having axes at a precise distance from each other; said tubes being similar in length and comprising openings that are leveled with respect to each other on a distal end of said double cannula; said double cannula having a proximal end carrying a handle (h), and a distal end formed with a window (w) in each of said tubes to enable observing the interior of the respective tubes; and two elongated cannulated holding devices, each device sized to fit within one of said two tubes of said double cannula and configured to engage said section of said first bone to firmly attach said bone section to said double cannula.
A combination display instrument in a vehicle, in which a plurality of display elements and/or display scales are inserted or applied in or on a common supporting plate, wherein a polarizing film shaped to correspond to the supporting plate is disposed in front of the supporting plate in the viewing direction of an observer, wherein the display elements and/or display scales are inserted as transparent or semi-transparent segments in the otherwise opaque supporting plate, wherein the polarizing film lies flat on the supporting plate over its entire area and is held adhesive-free in its position on the supporting plate by material bonding and/or by force fit by means of suitable moldings in or on a housing of the combination display instrument in an assembled state of the same.
Method for heating at least one building with a geothermal heating system with a first ground loop with a first ground storage tank surrounding it and a second ground loop with a second ground storage tank surrounding it, in that, in a first operating mode, the first ground loop and the second ground loop are coupled to one another via a heat pump and, in a second operating mode, the second ground loop is coupled to a building loop via the heat pump and current is drawn from a power supply system and a value of a current characteristic of the extracted current is determined and, if the extracted current falls below a predetermined value, the geothermal heating system is operated in the first or second operating mode and in the first operating mode heat is fed from the first ground storage tank via the heat pump into the second ground storage tank and in the second operating mode heat is fed from the second ground storage tank via the heat pump into the building loop, characterised in that a room temperature of the building is measured and the geothermal heating system is switched to the second operating mode when the temperature falls below a setpoint temperature. a value of a current characteristic of the extracted current is determined and, if the extracted current falls below a predetermined value, the geothermal heating system is operated in the first or second operating mode and in the first operating mode heat is fed from the first ground storage tank via the heat pump into the second ground storage tank and in the second operating mode heat is fed from the second ground storage tank via the heat pump into the building loop, characterised in that a room temperature of the building is measured and the geothermal heating system is switched to the second operating mode when the temperature falls below a setpoint temperature.
A lancing device for propelling a lancet through a lancing stroke, the lancing device comprising: a housing including an axial bore; a drive mechanism including a lancet carrier and a drive spring, the lancet carrier holding the lancet and translatable axially within the housing bore through the lancing stroke, and the drive spring adapted to propel the lancet carrier through a forward phase of the lancing stroke; characterised by a depth-adjustment mechanism including an adjustably positioned stop surface, a movable adjustment control member operably coupled thereto, and a resiliently deflectable leg operably interposed between the lancet carrier and the stop surface, wherein the lancet carrier engages and deflects the leg in the forward phase of the lancing stroke, and the deflecting leg then engages the stop surface to stop the leg deflection and thus stop the forward motion of the lancet carrier at an extended position for lancing, and wherein the control member is adjustably positionable to move different portions of the stop surface into an engagement position where they are contacted by the leg to adjust the extended position and thereby adjust a penetration depth of the lancet. a housing including an axial bore; a drive mechanism including a lancet carrier and a drive spring, the lancet carrier holding the lancet and translatable axially within the housing bore through the lancing stroke, and the drive spring adapted to propel the lancet carrier through a forward phase of the lancing stroke; characterised by a depth-adjustment mechanism including an adjustably positioned stop surface, a movable adjustment control member operably coupled thereto, and a resiliently deflectable leg operably interposed between the lancet carrier and the stop surface, wherein the lancet carrier engages and deflects the leg in the forward phase of the lancing stroke, and the deflecting leg then engages the stop surface to stop the leg deflection and thus stop the forward motion of the lancet carrier at an extended position for lancing, and wherein the control member is adjustably positionable to move different portions of the stop surface into an engagement position where they are contacted by the leg to adjust the extended position and thereby adjust a penetration depth of the lancet.
A cigarette making method, with recovery of tobacco from defective cigarettes, whereby filter-tipped cigarettes are transported in succession by conveyor means (4, 9, 12, 15, 25, 27) on a machine which assembles filter plugs to respective cigarette sticks to make the filter-tipped cigarettes; the filter-tipped cigarettes are quality-checked by checking means; and defective cigarettes are directed by the selfsame conveyor means (4, 9, 12, 15, 25, 27) towards an expulsion station; characterized in that, at an extraction station located upstream of the expulsion station relative to the feed direction of the cigarettes, the tobacco is removed from each defective cigarette by an extraction device.
Method for authorizing or refusing to measure an insulation fault in an electric energy storage battery for a vehicle, said method being characterized in that it comprises the steps of: - unload a capacity of a powertrain for the first time, - when said capacity is discharged for the first time: o measuring a first battery voltage between a first terminal and a second terminal of a battery, o measure a first leakage voltage between the first terminal and a ground of the vehicle, - discharge a second time said capacity, - when said capacity is discharged a second time: o measure a second battery voltage between the first terminal and the second terminal, o measure a second leakage voltage between the second terminal and the ground of the vehicle, - determining a battery voltage difference between said first measured battery voltage and said second measured battery voltage, - depending on said first measured leakage voltage, said second measured leakage voltage, and said determined battery voltage difference, authorize or refuse an insulation fault detection. - unload a capacity of a powertrain for the first time, - when said capacity is discharged for the first time: o measuring a first battery voltage between a first terminal and a second terminal of a battery, o measure a first leakage voltage between the first terminal and a ground of the vehicle, o measuring a first battery voltage between a first terminal and a second terminal of a battery, o measure a first leakage voltage between the first terminal and a ground of the vehicle, - discharge a second time said capacity, - when said capacity is discharged a second time: o measure a second battery voltage between the first terminal and the second terminal, o measure a second leakage voltage between the second terminal and the ground of the vehicle, o measure a second battery voltage between the first terminal and the second terminal, o measure a second leakage voltage between the second terminal and the ground of the vehicle, - determining a battery voltage difference between said first measured battery voltage and said second measured battery voltage, - depending on said first measured leakage voltage, said second measured leakage voltage, and said determined battery voltage difference, authorize or refuse an insulation fault detection.
A measurement arrangement for determining the rotational position, rotational speed and/or rotational direction of a shaft, in particular of an electric motor of an electromotively adjustable device of a vehicle, comprising: - at least one first electrode and at least one second electrode constituting in each case capacitor elements, wherein an electrical voltage may be applied to the electrodes (20, 30) such that the electrodes (20, 30) generate an electrical field; - a rotatable shaft with a measurement portion having an eccentricity, wherein the measurement portion is arranged relative to the electrodes (20, 30) such that a rotation of the shaft causes the electrical field to change; wherein the shaft axis is arranged perpendicular to an electrode plane, in which the electrodes (20, 30) are arranged; - an evaluation unit conductively connected to an electrode (20, 30) and designed to detect a change of the electrical field capacitively. - at least one first electrode and at least one second electrode constituting in each case capacitor elements, wherein an electrical voltage may be applied to the electrodes (20, 30) such that the electrodes (20, 30) generate an electrical field; - a rotatable shaft with a measurement portion having an eccentricity, wherein the measurement portion is arranged relative to the electrodes (20, 30) such that a rotation of the shaft causes the electrical field to change; wherein the shaft axis is arranged perpendicular to an electrode plane, in which the electrodes (20, 30) are arranged; wherein the measurement portion is arranged relative to the electrodes (20, 30) such that a rotation of the shaft causes the electrical field to change; wherein the shaft axis is arranged perpendicular to an electrode plane, in which the electrodes (20, 30) are arranged; - an evaluation unit conductively connected to an electrode (20, 30) and designed to detect a change of the electrical field capacitively.
A seed distribution element for precision pneumatic seed drills, of the type including: - a sowing disc which is rotated by a motor-driven transmission shaft at controlled speed, - a housing with a fixed portion and a portion which is movable relative to the fixed portion and can be closed against it, - a seed collection chamber being defined in the fixed portion, - a pneumatic suction chamber being defined in the movable portion, - the sowing disc being interposed between the portions (11, 12) and having opposed surfaces delimiting the chambers (15, 17), - the sowing disc having at least one ring of selector holes extending between the opposed surfaces, and - a seal which is arranged on the movable portion and is capable of sliding contact with the facing surface of the disc when the portions (11, 12) are closed against one another, wherein the seed distribution element further comprises a suction device for producing a pressure differential between the opposed surfaces in the region of a circumferential segment of the ring of holes, characterized in that the seed distribution element further comprises a thrust-bearing element of the sowing disc, which thrust-bearing element is supported rotatably in the movable portion in order to withstand at least some of the axial load produced by the disc on the seal. - a sowing disc which is rotated by a motor-driven transmission shaft at controlled speed, - a housing with a fixed portion and a portion which is movable relative to the fixed portion and can be closed against it, - a seed collection chamber being defined in the fixed portion, - a pneumatic suction chamber being defined in the movable portion, - the sowing disc being interposed between the portions (11, 12) and having opposed surfaces delimiting the chambers (15, 17), - the sowing disc having at least one ring of selector holes extending between the opposed surfaces, and - a seal which is arranged on the movable portion and is capable of sliding contact with the facing surface of the disc when the portions (11, 12) are closed against one another,
A composition for a refrigerator comprising a refrigerant and a lubricant composition, wherein the refrigerant comprises at least one kind of unsaturated fluorinated hydrocarbon compound selected from compounds represented by the following molecular formula or comprises a combination of the unsaturated fluorinated hydrocarbon compound and a saturated fluorinated hydrocarbon compound, C p O q F r R s ···, wherein R represents H; "p" represents an integer of 2 to 6, "q" represents 0, "r" represents an integer of 1 to 12, and "s" represents an integer of 0 to 11; and one or more carbon-carbon unsaturated bonds are included in a molecule, and wherein the blending amount of the saturated fluorinated hydrocarbon compound is 30% by mass or less based on the total amount of the refrigerant, and the lubricant composition comprises a base oil comprising, as a main component, a polyoxyalkylene glycol derivative represented by the following formula and having a hydroxyl number measured according to JIS K0070 of 5 mgKOH/g or less, R 1 -[(OR 2) m -OR 3] n wherein R 1 represents a hydrogen atom, a hydrocarbon group having 1 to 10 carbon atoms, an acyl group having 2 to 10 carbon atoms, a hydrocarbon group having 2 to 6 binding sites and 1 to 10 carbon atoms, or an oxygen-containing hydrocarbon group having 1 to 10 carbon atoms; R 2 represents an alkylene group having 2 to 4 carbon atoms; R 3 represents a hydrogen atom, a hydrocarbon group having 1 to 10 carbon atoms, an acyl group having 2 to 10 carbon atoms, or an oxygen-containing hydrocarbon group having 1 to 10 carbon atoms; "n" represents an integer of 1 to 6; and "m" represents a number with which an average value of "mxn" becomes 6 to 80, provided that at least one of R 1 and R 3 represents an alkyl group.