mhurhangee/ep-ind-claims huggingface dataset:
An aircraft component comprising: a first electrically conductive metallic component (114; 502); a second electrically conductive metallic component (114; 504); an elastomeric ellectrically insulative component (116; 506) disposed directly between the first electrically conductive metallic component (114; 502) and the second electrically conductive metallic component (114; 504); and an electrically conductive nanocoating disposed on the elastomeric electrically insulative component (116; 506) and electrically connecting the first electrically conductive metallic component (114; 502) to the second electrically conductive metallic component (114; 504), wherein the nanocoating is a coating comprising at least one of: a thickness comprising a dimension between 0.1 nanometers to 200 nanometers; and constituent particles comprising a dimension between 0.1 nanometers to 200 nanometers; and wherein the aircraft component is generally flexible insofar as the elastomeric electrically insulative component (116; 506) may elastically deform, shear, expand, and/or compress in response to applied forces. a first electrically conductive metallic component (114; 502); a second electrically conductive metallic component (114; 504); an elastomeric ellectrically insulative component (116; 506) disposed directly between the first electrically conductive metallic component (114; 502) and the second electrically conductive metallic component (114; 504); and an electrically conductive nanocoating disposed on the elastomeric electrically insulative component (116; 506) and electrically connecting the first electrically conductive metallic component (114; 502) to the second electrically conductive metallic component (114; 504), wherein the nanocoating is a coating comprising at least one of: a thickness comprising a dimension between 0.1 nanometers to 200 nanometers; and constituent particles comprising a dimension between 0.1 nanometers to 200 nanometers; and a thickness comprising a dimension between 0.1 nanometers to 200 nanometers; and constituent particles comprising a dimension between 0.1 nanometers to 200 nanometers; and
A turbomachine combustor comprising: a combustion chamber; a plurality of micro-mixer nozzles mounted to an end cover of the combustion chamber, each micro-mixer nozzle including a fuel supply pipe affixed to a nozzle body located within the combustion chamber, each nozzle body comprising a substantially hollow body formed with an upstream end face, a downstream end face and a peripheral wall extending therebetween, wherein each substantially hollow body is provided with a plurality of pre-mix tubes or passages extending axially through said substantially hollow body, thereby permitting fuel from the supply pipe to mix with air in said nozzle body prior to discharge into said combustion chamber; characterized in that at least some nozzle bodies of said plurality of micro-mixer nozzles have axial length dimensions that differ from axial length dimensions of other of said nozzle bodies along an inlet end of the nozzle bodies; and wherein said nozzle body of one or more of said plurality of micro-mixer nozzles is formed to include a radially outer portion of a first diameter, and at least one radially inner portion of a second diameter less than said first diameter, connected by a radially-oriented shoulder, and wherein said radially outer and radially inner portions (46,48) have differential axial lengths. a combustion chamber; a plurality of micro-mixer nozzles mounted to an end cover of the combustion chamber, each micro-mixer nozzle including a fuel supply pipe affixed to a nozzle body located within the combustion chamber, each nozzle body comprising a substantially hollow body formed with an upstream end face, a downstream end face and a peripheral wall extending therebetween, wherein each substantially hollow body is provided with a plurality of pre-mix tubes or passages extending axially through said substantially hollow body, thereby permitting fuel from the supply pipe to mix with air in said nozzle body prior to discharge into said combustion chamber; characterized in that at least some nozzle bodies of said plurality of micro-mixer nozzles have axial length dimensions that differ from axial length dimensions of other of said nozzle bodies along an inlet end of the nozzle bodies; and wherein said nozzle body of one or more of said plurality of micro-mixer nozzles is formed to include a radially outer portion of a first diameter, and at least one radially inner portion of a second diameter less than said first diameter, connected by a radially-oriented shoulder, and wherein said radially outer and radially inner portions (46,48) have differential axial lengths.
A compound of Formula A wherein each R 1, R 2, R 3, and R 4 are each independently H, a substituted or unsubstituted linear or branched C 1 -C 12 alkyl, a substituted or unsubstituted cyclic C 3 -C 12 alkyl, a substituted or unsubstituted C 3 -C 12 alkenyl, or a substituted or unsubstituted aryl or heteroaryl group; W is an oxygen atom or an NH group W' is a nitrogen atom; the dashed line is present and denotes the presence of one bond of a double bond; R is absent; R', taken together with R 5 and the atoms to which they are attached, forms a substituted or unsubstituted pyridyl; n and m are each independently an integer 1 or 2; and the substituent, if present, is selected from the group consisting of: alkyl, alkenyl, alkynyl, aryl, aryl-halide, heteroaryl, cycloalkyl, Si(alkyl) 3, Si(alkoxy) 3, halo, alkoxyl, amino, alkylamino, alkenylamino, amide, amidine, hydroxyl, thioether, alkyl carbonyl, alkylcarbonyloxy, arylcarbonyloxy, alkoxycarbonyloxy, aryloxycarbonyloxy, carbonate, alkoxycarbonyl, aminocarbonyl, alkylthiocarbonyl, phosphate, phosphate ester, phosphonato, phosphinato, cyano, acylamino, imino, sulfhydryl, alkylthio, arylthio, thiocarboxylate, dithiocarboxylate, sulfate, sulfato, sulfonate, sulfamoyl, sulfonamide, nitro, nitrile, azido, heterocyclyl, ether, ester, silicon-containing moieties, thioester, or a combination thereof. each R 1, R 2, R 3, and R 4 are each independently H, a substituted or unsubstituted linear or branched C 1 -C 12 alkyl, a substituted or unsubstituted cyclic C 3 -C 12 alkyl, a substituted or unsubstituted C 3 -C 12 alkenyl, or a substituted or unsubstituted aryl or heteroaryl group; W is an oxygen atom or an NH group W' is a nitrogen atom; the dashed line is present and denotes the presence of one bond of a double bond; R is absent; R', taken together with R 5 and the atoms to which they are attached, forms a substituted or unsubstituted pyridyl; n and m are each independently an integer 1 or 2; and the substituent, if present, is selected from the group consisting of: alkyl, alkenyl, alkynyl, aryl, aryl-halide, heteroaryl, cycloalkyl, Si(alkyl) 3, Si(alkoxy) 3, halo, alkoxyl, amino, alkylamino, alkenylamino, amide, amidine, hydroxyl, thioether, alkyl carbonyl, alkylcarbonyloxy, arylcarbonyloxy, alkoxycarbonyloxy, aryloxycarbonyloxy, carbonate, alkoxycarbonyl, aminocarbonyl, alkylthiocarbonyl, phosphate, phosphate ester, phosphonato, phosphinato, cyano, acylamino, imino, sulfhydryl, alkylthio, arylthio, thiocarboxylate, dithiocarboxylate, sulfate, sulfato, sulfonate, sulfamoyl, sulfonamide, nitro, nitrile, azido, heterocyclyl, ether, ester, silicon-containing moieties, thioester, or a combination thereof.
A two-stroke or four-stroke marine engine lubricating oil composition comprising 50 mass % or more of an oil of lubricating viscosity and less than 50 mass % of additives; and a viscosity modifier in the form of a polymer comprising a core and a plurality of polymeric arms extending therefrom, in an amount in the range of 0.05 to 6 mass %; wherein the composition includes less than 0.5 mass%, preferably less than 0.1 mass%, of brightstock; preferably brightstock is completely absent from the composition; and wherein the two-stroke marine engine lubricating oil composition has a TBN of 40 to 100 using ASTM D2896, or the four-stroke marine engine lubricating oil composition has a TBN of 25 to 60 using ASTM D2896. less than 50 mass % of additives; and a viscosity modifier in the form of a polymer comprising a core and a plurality of polymeric arms extending therefrom, in an amount in the range of 0.05 to 6 mass %;
A reinforcing tape for reinforcing a tensile strength of a cloth comprising: weft threads which constitute a weave structure of the reinforcing tape, and warp threads (12, 121) which constitute a weave structure of the reinforcing tape, characterized in that the warp threads (12, 121) consist of certain warp yarn consisting of fibers, and other warp yarn consisting of high-strength fiber, the fiber are made of polyamide fibers, polyester fibers, rayon fibers or polyacrylonitrile fibers; and the high-strength fiber are made of a single fiber or a combination of multiple fibers selected from the group consisting of polyethylene fibers, aramid fibers, polyacrylate fibers and PBO fibers; wherein the weave structure is constituted by a plain weave structure comprising coarse lattices having an aperture of 0.1 mm or more and 2 mm or less, and the warp threads (12, 121) made of high-strength fiber is placed at a center section in the width direction of the reinforcing tape.
The ventilation device with heat recovery, with a housing, in which a heat exchanger is arranged via which air is conveyed by means of at least one blower (58, 60) arranged in the housing, wherein the housing has a front wall, a back wall and a side wall, as well as air connections for different types of air, i.e. ingoing air, discharge air, outgoing air and outside air, the air connection for ingoing air being an ingoing air connection (17, 18), the air connection for discharge air being a discharge air connection, the air connection for outgoing air being an outgoing air connection and the air connection for outside air being an outside air connection, at least some of the air connections on the side wall being arranged such that an air connection of a first type of air is situated between at least two air connections of a second type of air, wherein the air connection of the first type of air is the discharge air connection and the air connections of the second type of air are the ingoing air connections (17, 18), the air connection of the first type of air has a straight air connection piece and the two air connections of the second type of air respectively have an arcuate or angled air connection piece that can be rotated or mounted in a desired angular position, wherein a first air pathway that leads through the heat exchanger and connects the discharge air connection with the outgoing air connection is formed in the housing, and wherein a second air pathway that leads through the heat exchanger and connects the outside air connection with one of the ingoing air connections (17, 18) is formed in the housing, wherein an air junction of the second air pathway that is situated in the housing leads to the other one of the ingoing air connections (18, 17), and the air junction has an air channel that crosses the first air pathway.
A gun heel, comprising at least two distinct bearing parts (4, 5) intended to rest against the user's body, at least one of the bearing parts being movable relative to the other for the adjustment of its position, the at least two bearing parts (4, 5) being mounted to move independently on the same base, characterized in that a first bearing part of the at least two bearing parts (4, 5) is indirectly mounted on said base through a first connector, said first connector comprising at least one through groove extending along a transverse axis, a screw inserted into a bore of the first bearing part crossing said through groove, which can be tightened into a nut positioned behind said through groove, the first bearing part being free to move along said through groove, granting the first bearing part freedom of movement along a transverse axis T relative to the base when the screw is not tightened.
A gas turbine engine comprising: a core nacelle; a core engine disposed in the core nacelle, the core engine including at least a compressor section, a combustor section, and a turbine section, which define a core flow path; a bypass duct radially outwards of the core nacelle; a component disposed in the core engine; a cooling cavity disposed outside of the bypass duct; a heat pipe containing a working medium sealed therein, the heat pipe including a first section configured to accept thermal energy from the component and/or transferred from the hot combustion gases in the core gas path and a second section configured to dissipate the thermal energy in the cooling cavity, characterized by: a tap from the compressor section, the tap configured to provide bleed air to the cooling cavity and dissipate the thermal energy from the second section, wherein the core nacelle defines an outer boundary of the cooling cavity. a core nacelle; a core engine disposed in the core nacelle, the core engine including at least a compressor section, a combustor section, and a turbine section, which define a core flow path; a bypass duct radially outwards of the core nacelle; a component disposed in the core engine; a cooling cavity disposed outside of the bypass duct; a heat pipe containing a working medium sealed therein, the heat pipe including a first section configured to accept thermal energy from the component and/or transferred from the hot combustion gases in the core gas path and a second section configured to dissipate the thermal energy in the cooling cavity, characterized by: a tap from the compressor section, the tap configured to provide bleed air to the cooling cavity and dissipate the thermal energy from the second section, wherein the core nacelle defines an outer boundary of the cooling cavity.
A portable information terminal (200; 200-1∼200-3) having a tethering function for operating as a host terminal which is connected to a base station using a first wireless communication and connects other portable information terminals (200; 200-1 ∼ 200-3) to the base station using a second wireless communication, characterized by comprising: a group terminal connection status management section which manages connection statuses of a plurality of portable information terminals (200; 200-1 ∼ 200-3) belonging to the same group connected by the tethering function; a host terminal order determination section which determines selection order of a portable information terminal (200; 200-1 ∼ 200-3) to serve as the host terminal from among the portable information terminals (200; 200-1 ∼ 200-3) belonging to the same group including its own terminal and managed by the group terminal connection status management section, based at least on reception quality from the base station, remaining battery capacity, and either a contracted allowable data transmission speed or a maximum data transmission speed notified from a network; and a control section which controls whether to operate as the host terminal or to communicate with the base station via the host terminal, based on the selection order determined by the host terminal order determination section. a group terminal connection status management section which manages connection statuses of a plurality of portable information terminals (200; 200-1 ∼ 200-3) belonging to the same group connected by the tethering function; a host terminal order determination section which determines selection order of a portable information terminal (200; 200-1 ∼ 200-3) to serve as the host terminal from among the portable information terminals (200; 200-1 ∼ 200-3) belonging to the same group including its own terminal and managed by the group terminal connection status management section, based at least on reception quality from the base station, remaining battery capacity, and either a contracted allowable data transmission speed or a maximum data transmission speed notified from a network; and a control section which controls whether to operate as the host terminal or to communicate with the base station via the host terminal, based on the selection order determined by the host terminal order determination section.
Control device with keys comprising at least two control keys associated with functions and arranged contiguously to one another, said at least two control keys respectively comprising: - a mobile element intended to move between an idle position and a control position which comprises an outer part on which a user presses, - a function indicator situated on the outer part of the mobile element, - first backlighting means configured to backlight the function indicator when the function associated with the control key is activated, the control device also comprising second backlighting means having a different colour from the first backlighting means and intended to be activated independently of the activation status of the function associated with the control key, characterized in that said second backlighting means are arranged at the interface between two contiguous control keys so as to light the function indicators of two contiguous keys. - a mobile element intended to move between an idle position and a control position which comprises an outer part on which a user presses, - a function indicator situated on the outer part of the mobile element, - first backlighting means configured to backlight the function indicator when the function associated with the control key is activated,
Device for releasably fixing a workpiece to be measured and/or to be processed, wherein: - the device has at least one supporting strut, at the end of which that faces the workpiece, an adapter is arranged, - the supporting strut is mounted with its end opposite the workpiece in a housing so as to be pivotable, rotatable and variable in its axial length, and - the adapter receives a bearing unit, characterized in that the bearing unit is in the form of a hexapod. - the device has at least one supporting strut, at the end of which that faces the workpiece, an adapter is arranged, - the supporting strut is mounted with its end opposite the workpiece in a housing so as to be pivotable, rotatable and variable in its axial length, and - the adapter receives a bearing unit, characterized in that the bearing unit is in the form of a hexapod.
Actuating arrangement for a unit of an internal combustion engine with a drive element a housing and an intermediate element which is arranged in a prestressed manner between the drive element and the housing, wherein the housing, in which the drive element is arranged, comprises a fixed receiving part and a cover which is attached thereto and bears axially against a stop on the fixed receiving part, characterized in that the intermediate element is arranged radially between the cover and the drive element and is arranged elastically deformed axially between the drive element and the cover, wherein the intermediate element comprises an axially extending annular elastic collar against which the drive element abuts radially inwardly and against which the cover abuts radially outwardly, wherein the intermediate element is manufactured in unitary manner from an elastomer or from another elastic non-metallic material. a drive element a housing and an intermediate element which is arranged in a prestressed manner between the drive element and the housing, wherein the housing, in which the drive element is arranged, comprises a fixed receiving part and a cover which is attached thereto and bears axially against a stop on the fixed receiving part, characterized in that the intermediate element is arranged radially between the cover and the drive element and is arranged elastically deformed axially between the drive element and the cover, wherein the intermediate element comprises an axially extending annular elastic collar against which the drive element abuts radially inwardly and against which the cover abuts radially outwardly, wherein the intermediate element is manufactured in unitary manner from an elastomer or from another elastic non-metallic material.
A computer readable medium programmed with instructions to cause an apparatus comprising: - a controller comprising a processor; - at least one electrode couplable to at least one vagus nerve of a patient, - an implantable device operatively coupled to the at least one electrode and comprising an electrical signal generator configured to apply an electrical signal to the at least one vagus nerve, - a sensor configured to sense a body parameter that corresponds to a symptom of a medical condition, and - a respiration cycle sensing element; to apply an electrical signal to the at least one vagus nerve in response to sensing the symptom of the medical condition of the patient in the apparatus, wherein the instructions, when executed by the processor, perform a method comprising: - generating a first electrical signal with the electrical signal generator, - sensing the symptom of the medical condition, - detecting at least a portion of a physiological cycle of the patient selected from the cardiac cycle and the respiratory cycle of the patient, and - applying the first electrical signal to the at least one vagus nerve of the patient to treat the medical condition; characterized in that the applying of the first electrical signal to the at least one vagus nerve is performed during inspiration by the patient. - a controller comprising a processor; - at least one electrode couplable to at least one vagus nerve of a patient, - an implantable device operatively coupled to the at least one electrode and comprising an electrical signal generator configured to apply an electrical signal to the at least one vagus nerve, - a sensor configured to sense a body parameter that corresponds to a symptom of a medical condition, and - a respiration cycle sensing element; - generating a first electrical signal with the electrical signal generator, - sensing the symptom of the medical condition, - detecting at least a portion of a physiological cycle of the patient selected from the cardiac cycle and the respiratory cycle of the patient, and - applying the first electrical signal to the at least one vagus nerve of the patient to treat the medical condition;