mhurhangee/ep-ind-claims huggingface dataset:
An aircraft having a blended-wing-body configuration, comprising: a centerbody having an airfoil-shaped cross section, an aircraft centerline, an aft portion, an upper mold line, a lower mold line, and a pair of centerbody leading edge portions respectively on opposite sides of the aircraft centerline; a pair of wings integral with the centerbody; at least one pair of engines located on opposite sides of the aircraft centerline and mounted within the centerbody between the upper mold line and the lower mold line; a pair of air inlets located respectively along the pair of centerbody leading edge portions and respectively fluidly coupled to the pair of engines; and a pair of exhaust outlets located in the aft portion of the centerbody and respectively fluidly coupled to the pair of engines; a pair of exhaust ducts respectively fluidly coupling the pair of exhaust outlets to the pair of engines, each exhaust duct having a slight S-shaped configuration when the aircraft is viewed from a top-down direction, wherein: each engine has an engine centerline generally aligned with the aircraft centerline, when the aircraft is viewed from the top-down direction; and each exhaust outlet has an outlet geometric center located inboard of the engine centerline. a centerbody having an airfoil-shaped cross section, an aircraft centerline, an aft portion, an upper mold line, a lower mold line, and a pair of centerbody leading edge portions respectively on opposite sides of the aircraft centerline; a pair of wings integral with the centerbody; at least one pair of engines located on opposite sides of the aircraft centerline and mounted within the centerbody between the upper mold line and the lower mold line; a pair of air inlets located respectively along the pair of centerbody leading edge portions and respectively fluidly coupled to the pair of engines; and a pair of exhaust outlets located in the aft portion of the centerbody and respectively fluidly coupled to the pair of engines; a pair of exhaust ducts respectively fluidly coupling the pair of exhaust outlets to the pair of engines, each exhaust duct having a slight S-shaped configuration when the aircraft is viewed from a top-down direction, wherein: each engine has an engine centerline generally aligned with the aircraft centerline, when the aircraft is viewed from the top-down direction; and each exhaust outlet has an outlet geometric center located inboard of the engine centerline. each engine has an engine centerline generally aligned with the aircraft centerline, when the aircraft is viewed from the top-down direction; and each exhaust outlet has an outlet geometric center located inboard of the engine centerline.
A slitting machine, comprising: at least two knife holders, each of which has a respective knife rotatably mounted thereon; individually activatable electromagnetic sensors disposed on said knife holders; a single magnetostrictive rod, wherein said electromagnetic sensors are also disposed along a length of said rod; and means for processing an interrogation by said magnetostrictive rod of activated ones of said electromagnetic sensors, and for indicating the position of at least one of said knife holders relative to said rod. at least two knife holders, each of which has a respective knife rotatably mounted thereon; individually activatable electromagnetic sensors disposed on said knife holders; a single magnetostrictive rod, wherein said electromagnetic sensors are also disposed along a length of said rod; and means for processing an interrogation by said magnetostrictive rod of activated ones of said electromagnetic sensors, and for indicating the position of at least one of said knife holders relative to said rod.
Heat treatment module for an internal combustion engine, the heat treatment model comprising a primary casing delimiting the primary volume, intended for circulation of a cooling fluid, and a secondary casing extending at least in part in the primary volume and including a plurality of compartments (61, 62, 63), such that: - the secondary casing comprises a first compartment intended to implement a heat exchange between a first stream, in particular an intake gas stream, and the cooling fluid; - the secondary casing comprises a second compartment intended to implement a heat exchange between a second, EGR gas stream and the cooling fluid; - the secondary casing comprises a third compartment intended for the circulation of the second, EGR gas stream and able to ensure thermal insulation the first compartment with respect to the second compartment so as to reach a predetermined temperature threshold; - the heat treatment module comprises a device for controlling the circulation of the second, EGR gas stream that is configured to selectively direct the second stream into the third compartment or into the second compartment. - the secondary casing comprises a first compartment intended to implement a heat exchange between a first stream, in particular an intake gas stream, and the cooling fluid; - the secondary casing comprises a second compartment intended to implement a heat exchange between a second, EGR gas stream and the cooling fluid; - the secondary casing comprises a third compartment intended for the circulation of the second, EGR gas stream and able to ensure thermal insulation the first compartment with respect to the second compartment so as to reach a predetermined temperature threshold; - the heat treatment module comprises a device for controlling the circulation of the second, EGR gas stream that is configured to selectively direct the second stream into the third compartment or into the second compartment.
Rotary feedthrough for a transport device comprising a rotary object carrier which comprises object carrier elements (6.1, 6.2, 6.3, 6.4) arranged so as to be distributed around the circumference, of which at least one object carrier element is arranged on the object carrier so as to be displaceable relative to the object carrier on a circular path or can be locked in place on the object carrier, the rotary feedthrough comprising a stationary component having one or more media inputs (20.1, 20.2, 20.3) for providing one or more media to supply one or more actuator units (12.1, 12.2; 18.1, 18.2) of an object carrier element (6.1, 6.2), characterised in that the rotary feedthrough comprises a plurality of components (24.1, 24.2, 24.3, 24.4) which are rotatable independently of one another about a common central axis relative to the stationary component and each have one or more media outputs (25.1, 25.2), the stationary component and the rotary components (24.1, 24.2, 24.3, 24.4) being designed such that a media connection is formed between a media input of the stationary component and a media output of the rotary component, or a plurality of media inputs (20.1, 20.2, 20.3) of the stationary component and a plurality of media outputs (25.1, 25.2) of the rotary components (24.1, 24.2, 24.3, 24.4).
Flanged bearing shell, in particular for bearings of a crankshaft in a motor vehicle power train, having a semi-cylindrical radial bearing portion and at least one disc-like axial bearing portion, and preferably having one disc-like axial bearing portion on each of its two sides, which bearing shell is produced by a bending and rolling process from a single piece of flat material, the radial bearing portion thus merging integrally into the or each disc-like axial bearing portion, with an axial direction, a radial direction and a circumferential direction being distinguishable, characterised in that, after its production by the bending and rolling process, the disc-like axial bearing portion is cut free from the radial bearing portion over part of its extent in the circumferential direction by a parting process, i.e. a separating slot is provided which forms a freeing cut, and, over the part of its extent in the circumferential direction which is not cut free, the axial bearing portion remains integrally linked to the radial bearing portion, and either in that the axial bearing portion remains linked to the radial bearing portion only in a crest region and forms a uniting bridge there, or in that the axial bearing portion remains linked to the radial bearing portion at two points provided on two sides of the crest region and a uniting bridge is formed at each of these two points provided on two sides of the crest region.
A film cutter for an agricultural bale wrapper, the film cutter including a support element, a collector element, a cushion element and a knife element, wherein the film cutter is reconfigurable between a collecting configuration in which wrapping film dispensed by the bale wrapper is collected by the film cutter and a clamping configuration in which the wrapping film is clamped between the collector element and the cushion element and is severed by the knife element; characterised in that the support element is configured to engage the wrapping film when the film cutter is in the collecting configuration and to disengage the wrapping film when the film cutter is in the clamping configuration, and wherein the support element is configured to move from the engaged condition to the disengaged condition without significant sliding contact between the support element and the film.
Headrest retraction member for transferring a headrest of a vehicle seat from a position for use into a non-use position, the headrest retraction member having a movably supported locking member, which can be moved into and out of engagement with at least one notch of at least one headrest rod of the headrest, and a movably supported actuation component which has a wedge face, wherein, in the event of a movement of the actuation component, the wedge face acts on the locking member in such a manner that the locking member and the at least one notch move out of engagement, wherein the actuation component is coupled to a cable pull and the actuation component is a sliding member (140, 240) which is displaceably guided in a guiding profile (150, 250), characterised in that the headrest retraction member has a bridge for connecting to an end region of the at least one headrest rod, and when the sliding member is displaced, a wedge face of the sliding member initially brings the locking member and the at least one notch out of engagement and subsequently the sliding member also carries the bridge in the direction of the non-use position of the headrest.
A heating control method, applied to a heating element of an electronic atomization device, comprising: controlling (S11, S22) a temperature of the heating element to increase to a first preset temperature in a first time period; controlling (S12, S23) the heating element to keep working under the first preset temperature in a second time period; and controlling (S13, S24) the temperature of the heating element to decrease from the first preset temperature to a second preset temperature in a third time period; wherein the heating element is controlled to operate at least two different power levels in the first time period and/or the second time period; wherein the second time period, comprises the at least two different power levels being operated in the first time period; characterized in that the heating element is controlled to operate a constant power level in the third time period, and the constant power level ranges from 4.5 W to 5.5 W. controlling (S11, S22) a temperature of the heating element to increase to a first preset temperature in a first time period; controlling (S12, S23) the heating element to keep working under the first preset temperature in a second time period; and controlling (S13, S24) the temperature of the heating element to decrease from the first preset temperature to a second preset temperature in a third time period; wherein the heating element is controlled to operate at least two different power levels in the first time period and/or the second time period; wherein the second time period, comprises the at least two different power levels being operated in the first time period; characterized in that the heating element is controlled to operate a constant power level in the third time period, and the constant power level ranges from 4.5 W to 5.5 W.
A door handle arrangement for a vehicle, comprising a housing (18, 18') which is fastenable to a body part (10, 10') of a vehicle body, and a handle lever which is mounted in a handle cutout of the housing (18, 18') so as to be movable between an inoperative position and an actuating position in order to unlock and/or open a vehicle door, wherein the handle lever is mounted with play in the housing (18, 18'), wherein at least one compensating element is provided which is designed to be fastened to at least one fastening portion of the body part (10, 10'), wherein the compensating element forms at least one contact portion (34, 46) for the handle lever, and wherein pretensioning means are provided which pretension the handle lever in its inoperative position against the at least one contact portion (34, 46) in a mounted state of the door handle arrangement.
A system for determining the position of a medical implant, wherein the medical implant is axially symmetrical, comprising: - a database; - a navigation system; and - a processor which is connected to the database and the navigation system and is configured to perform a method for measuring or verifying a position of the medical implant, using an impactor which has an at least partially known or previously determined geometry or at least partially known dimensions and is connected to the medical implant by a connection mechanism fixed and reliably determining the axis of symmetry of the implant relative to the impactor, the medical implant being located in an anatomical body part(s) and/or structure(s), relative to the body part(s) and/or structure(s) or specific points, landmarks or planes of the same, wherein: - positional or landmark information regarding the anatomical body part(s) and/or structure(s) is acquired by detecting or tracking a pointer to which at least one reference element and/or an inertial sensor is connected; - the position of the medical implant is calculated using the navigation system and a reference structure which is connected to the impactor; and - the calculated position of the medical implant is related to or compared with the acquired positional or landmark information regarding the anatomical body part(s) and/or structure(s) in order to measure or verify the position of the medical implant within or relative to the anatomical body part(s) and/or structure(s). - a database; - a navigation system; and - a processor which is connected to the database and the navigation system and is configured to perform a method for measuring or verifying a position of the medical implant, using an impactor which has an at least partially known or previously determined geometry or at least partially known dimensions and is connected to the medical implant by a connection mechanism fixed and reliably determining the axis of symmetry of the implant relative to the impactor, the medical implant being located in an anatomical body part(s) and/or structure(s), relative to the body part(s) and/or structure(s) or specific points, landmarks or planes of the same, wherein: - positional or landmark information regarding the anatomical body part(s) and/or structure(s) is acquired by detecting or tracking a pointer to which at least one reference element and/or an inertial sensor is connected; - the position of the medical implant is calculated using the navigation system and a reference structure which is connected to the impactor; and - the calculated position of the medical implant is related to or compared with the acquired positional or landmark information regarding the anatomical body part(s) and/or structure(s) in order to measure or verify the position of the medical implant within or relative to the anatomical body part(s) and/or structure(s).
An engine-driven system comprising: - an engine having an air intake passage; - a fuel tank operatively coupled to the engine; - a valve coupled between the fuel tank and the air intake passage, the valve being configured to transition between a first position and a second position, wherein the first position allows fuel vapor to flow between the fuel tank and the air intake passage and the second position inhibits the fuel vapor from flowing between the fuel tank and the air intake passage; and - a pressure regulator positioned in line between the fuel tank and the engine, wherein the pressure regulator comprises a pressure relief valve configured to release fuel vapor between the fuel tank and the air intake passage when a pressure of the fuel vapor between the fuel tank and the air intake passage reaches a predetermined first threshold pressure, wherein a check valve is positioned in line between the fuel tank and the air intake passage and in parallel with the pressure regulator, wherein the check valve is configured to allow air into fuel tank when the pressure within the fuel tank is negative, characterized in that the engine is configured to drive a generator, and that a control device is configured to transition the valve between a first position and a second position based on a measured oil pressure within the engine; wherein the valve comprises an inlet, a first outlet, and a second outlet, the inlet being configured to receive fuel vapor from the fuel tank, the first outlet being configured to provide the fuel vapor to the air intake passage, and the second outlet being configured to provide the fuel vapor to the atmosphere or to a storage container; and that the control device is configured to cause the valve to enable release of fuel vapor from the fuel tank when the pressure of the fuel vapor in the fuel tank reaches a second threshold pressure, the second threshold pressure being higher than the first threshold pressure. - an engine having an air intake passage; - a fuel tank operatively coupled to the engine; - a valve coupled between the fuel tank and the air intake passage, the valve being configured to transition between a first position and a second position, wherein the first position allows fuel vapor to flow between the fuel tank and the air intake passage and the second position inhibits the fuel vapor from flowing between the fuel tank and the air intake passage; and - a pressure regulator positioned in line between the fuel tank and the engine, wherein the pressure regulator comprises a pressure relief valve configured to release fuel vapor between the fuel tank and the air intake passage when a pressure of the fuel vapor between the fuel tank and the air intake passage reaches a predetermined first threshold pressure,
A kit for diagnosing thyroid disease, comprising a cell expressing a thyroid stimulating hormone receptor (TSHR), a cAMP dependent calcium channel and a calcium sensitive protein, wherein the calcium sensitive protein is a protein that emits luminescence in response to calcium.
A plasmid DNA molecule that comprises a polynucleotide encoding at least one adeno-associated virus inverted terminal repeat and also encoding an IL-10 molecule operably linked to expression control elements that control expression of said IL-10 molecule in vivo, for use in treating neuropathic pain in a mammalian subject, wherein said plasmid DNA molecule is administered intrathecally to the central nervous system of said subject.
A dental abutment (2, 102, 402, 502), comprising a fixture engagement portion (46, 46', 146, 446, 510, 550) for engaging the dental abutment with a dental fixture (4, 104, 204, 304) adapted to be inserted into a jawbone or for engaging the dental abutment with a fixture replica, the fixture engagement portion having a geometrical central axis and being provided with at least one radially projecting first indexing element (60a-60d, 60'a, 60'd, 80, 80a-80e, 160a-160d, 460a, 520, 560) having an apical end (62d, 162d, 462a), and at least one radially projecting second indexing element (60e-60g, 60'e-60'g, 81a-81c, 160e, 460b, 530, 561) having an apical end (62e-62g, 162e, 462b) located apically of the apical end of said first indexing element, wherein the radially most distant area of the apical end of the second indexing element is located at a shorter radial distance from said central axis than the radially most distant area of the apical end of the first indexing element, and/or wherein the apical end of the second indexing element has, compared to the apical end of the first indexing element, a smaller dimension in the circumferential direction of the fixture engagement portion, wherein said at least one first indexing element is circumferentially separated from any one of said at least one second indexing element, and wherein said at least one second indexing element is a single second indexing element or at least two second indexing elements asymmetrically distributed along the circumference of the fixture engagement portion.
Chip card comprising: - an electronic chip module; - a chip card housing; and - an adhesive layer, partially or fully surrounding the chip module, for bonding the chip module with the chip card housing, wherein the adhesive layer can comprise a isocyanate-based reactive adhesive, wherein the reactive adhesive further comprises a hot adhesive component, characterised in that its activation temperature lies above the melting temperature of the hot adhesive component. - an electronic chip module; - a chip card housing; and - an adhesive layer, partially or fully surrounding the chip module, for bonding the chip module with the chip card housing, wherein the adhesive layer can comprise a isocyanate-based reactive adhesive, wherein the reactive adhesive further comprises a hot adhesive component, characterised in that its activation temperature lies above the melting temperature of the hot adhesive component.
A material having a CHA structure and a pore opening ranging from 3 to 5 Angstroms synthesized by a process free of organic structure directing agent (OSDA), where said material has molar silica to alumina ratio from 3 to 10 and comprises a first metal chosen from alkali-earth group, rare-earth group or mixtures thereof, and a second metal chosen from copper, iron or mixtures thereof, wherein first metal to aluminum atomic ratio is between 0.05 and 0.80.