mhurhangee/ep-ind-claims huggingface dataset:
A drain, comprising: - a drain pot having a connection to which a waste water line is connectable, - an odour trap including an odour trap nozzle which includes an upper end having an inlet opening and a lower outlet opening which protrudes into an odour trap pot that is open at the top and is formed for forming an odour trap reservoir, and - a fire protection device for closing the odour trap in case of fire by means of intumescence material, wherein a closing plug is disposed within the odour trap pot, wherein intumescence material is provided between the closing plug and the odour trap pot such that in case of fire the closing plug is pressed against and closes the outlet opening of the odour trap nozzle by expanding intumescence material, characterized in that at the upper end of the odour trap nozzle, an annular arrangement of intumescence material is provided for sealing and/or fixing the odour trap nozzle relative to the drain pot. - a drain pot having a connection to which a waste water line is connectable, - an odour trap including an odour trap nozzle which includes an upper end having an inlet opening and a lower outlet opening which protrudes into an odour trap pot that is open at the top and is formed for forming an odour trap reservoir, and - a fire protection device for closing the odour trap in case of fire by means of intumescence material, wherein a closing plug is disposed within the odour trap pot, wherein intumescence material is provided between the closing plug and the odour trap pot such that in case of fire the closing plug is pressed against and closes the outlet opening of the odour trap nozzle by expanding intumescence material, characterized in that at the upper end of the odour trap nozzle, an annular arrangement of intumescence material is provided for sealing and/or fixing the odour trap nozzle relative to the drain pot.
A surgical instrument assembly, comprising: a shaft; an articulation region; and an end effector attached to the shaft by way of the articulation region, wherein the end effector is configured to be articulated relative to the shaft, wherein the shaft comprises: an outer housing; an inner spine positioned with the outer housing; and a core member positioned within the inner spine, wherein the core member comprises: a distal end attached to a component of the end effector; and a proximal end attached to a proximal housing of the surgical instrument assembly, wherein the core member comprises a material different than a material of the inner spine, and wherein the core member defines a maximum system stretch of the inner spine; characterized in that the core member comprises a proximal core member and a distal core member, wherein the proximal core member is attached to the proximal housing and the distal core member is attached to the component of the end effector. a shaft; an articulation region; and an end effector attached to the shaft by way of the articulation region, wherein the end effector is configured to be articulated relative to the shaft, wherein the shaft comprises: an outer housing; an inner spine positioned with the outer housing; and a core member positioned within the inner spine, wherein the core member comprises: a distal end attached to a component of the end effector; and a proximal end attached to a proximal housing of the surgical instrument assembly, wherein the core member comprises a material different than a material of the inner spine, and wherein the core member defines a maximum system stretch of the inner spine; an outer housing; an inner spine positioned with the outer housing; and a core member positioned within the inner spine, wherein the core member comprises: a distal end attached to a component of the end effector; and a proximal end attached to a proximal housing of the surgical instrument assembly, wherein the core member comprises a material different than a material of the inner spine, and wherein the core member defines a maximum system stretch of the inner spine; a distal end attached to a component of the end effector; and a proximal end attached to a proximal housing of the surgical instrument assembly, wherein the core member comprises a material different than a material of the inner spine, and wherein the core member defines a maximum system stretch of the inner spine; characterized in that the core member comprises a proximal core member and a distal core member, wherein the proximal core member is attached to the proximal housing and the distal core member is attached to the component of the end effector.
A method for making a coated cutting tool insert having an upper face (rake face), an opposite face and at least one clearance face intersecting said upper and opposite faces to define cutting edges characterized in depositing by CVD, onto a cemented carbide, titanium based or ceramic substrate - a hard layer system, having a total thickness of 2-50 μm, comprising at least one layer selected from titanium carbide, titanium nitride, titanium carbonitride, titanium carboxide and aluminum oxide, and an outer, 1-15 μm thick, aluminum oxide layer or (Al 2 O 3 + ZrO 2) *N multilayer, - a penultimate outermost layer of TiO x, where x ranges from 1 to 2, preferably from 1.3 to 1.9, and wherein the deposited TiO x layer thickness is 0.05-3 μm, and - an outermost, 0.3-2 μm thick, TiC x N y O z layer, where x+y+z=1, x≥0, y≥0, and z≥0, preferably a single layer or multilayer of TiN, TiC or TiC x N y, where x+y=1, x≥0 and y≥0, followed by a post-treatment, preferably blasting or brushing, removing at least said outermost layer on the edge-line and on the rake face. - a hard layer system, having a total thickness of 2-50 μm, comprising at least one layer selected from titanium carbide, titanium nitride, titanium carbonitride, titanium carboxide and aluminum oxide, and an outer, 1-15 μm thick, aluminum oxide layer or (Al 2 O 3 + ZrO 2) *N multilayer, - a penultimate outermost layer of TiO x, where x ranges from 1 to 2, preferably from 1.3 to 1.9, and wherein the deposited TiO x layer thickness is 0.05-3 μm, and - an outermost, 0.3-2 μm thick, TiC x N y O z layer, where x+y+z=1, x≥0, y≥0, and z≥0, preferably a single layer or multilayer of TiN, TiC or TiC x N y, where x+y=1, x≥0 and y≥0,
A gas turbine engine comprises: a fan drive turbine driving a gear reduction, said gear reduction, in turn, driving a fan rotor, said fan rotor delivering air into a bypass duct as bypass air and into a compressor section as core flow; a forward bearing positioned between said gear reduction and said fan rotor and supporting said gear reduction, and a second bearing positioned aft of said gear reduction and supporting said gear reduction, said forward bearing being a thrust bearing; a fan drive turbine drive shaft driving said gear reduction; and a catcher provided to resist movement of said gear reduction and said fan rotor in an outer direction in the event of a failure of said forward bearing, wherein said gear reduction is an epicyclic gear reduction, wherein said epicyclic gear reduction includes a sun gear, intermediate gears driven by said sun gear, and a ring gear driven by said intermediate gears, with a static carrier, and said ring gear driving a fan drive shaft to drive said fan rotor, characterized in that: said catcher is bolted to a frame structure associated with said static carrier. a fan drive turbine driving a gear reduction, said gear reduction, in turn, driving a fan rotor, said fan rotor delivering air into a bypass duct as bypass air and into a compressor section as core flow; a forward bearing positioned between said gear reduction and said fan rotor and supporting said gear reduction, and a second bearing positioned aft of said gear reduction and supporting said gear reduction, said forward bearing being a thrust bearing; a fan drive turbine drive shaft driving said gear reduction; and a catcher provided to resist movement of said gear reduction and said fan rotor in an outer direction in the event of a failure of said forward bearing, wherein said gear reduction is an epicyclic gear reduction, wherein said epicyclic gear reduction includes a sun gear, intermediate gears driven by said sun gear, and a ring gear driven by said intermediate gears, with a static carrier, and said ring gear driving a fan drive shaft to drive said fan rotor,
Manipulator for positioning an end effector for charging vehicles, comprising: a support, a stage comprising the end effector, a first link comprising a first end providing a first pivoting connection connected to the support and a second end providing a second pivoting connection connected to the stage, wherein the first link defines a first longitudinal axis between the first end and the second end,and a second link comprising a first end providing a first pivoting connection connected to the support and a second end providing a second pivoting connection connected to the stage at a first position offset from the second pivoting connection of the first link, characterised in that the manipulator further comprises: a first and a second actuating mechanism providing an actuatable connection between the stage and the support through the first link, each of the first and the second actuating mechanisms configured to exert a first actuating force on the first link for moving the second end of the first link through a volume. a support, a stage comprising the end effector, a first link comprising a first end providing a first pivoting connection connected to the support and a second end providing a second pivoting connection connected to the stage, wherein the first link defines a first longitudinal axis between the first end and the second end,and a second link comprising a first end providing a first pivoting connection connected to the support and a second end providing a second pivoting connection connected to the stage at a first position offset from the second pivoting connection of the first link, characterised in that the manipulator further comprises: a first and a second actuating mechanism providing an actuatable connection between the stage and the support through the first link, each of the first and the second actuating mechanisms configured to exert a first actuating force on the first link for moving the second end of the first link through a volume.
A method for modifying a polyolefin film, comprising following steps: cleaning a surface of the polyolefin film to be treated with acetone, and drying the polyolefin film in the air for later use; placing the polyolefin film in step into a low-temperature plasma reaction chamber, and vacuuming the low-temperature plasma reaction chamber to 10-30Pa; after step ends up, introducing polar molecules into the reaction chamber, adjusting temperature and pressure, and performing a gas-phase graft reaction on the surface of the polyolefin by a radio-frequency low-temperature plasma treatment at a power supply of 100-600W and a temperature of 0-75° C to obtain a modified polyolefin film, wherein, the polar molecules in step are one or more than one selected from a group consisting of chlorine gas, hydrogen sulfide, ammonia gas, hydrogen chloride, acrylic acid, 3-aminopropyltriethoxysilane, 3-aminopropyltrimethoxysilane, 3-aminopropyldiethoxysilane, cyclohexylaminopropyltrimethoxysilane, 3-ureidopropyltrimethoxysilane, 3-mercaptopropyltriethoxysilane, 3-mercaptopropyltripropoxysilane, 3-chloropropyltrimethoxysilane, 3-chloropropyltriethoxysilane, 3-chloropropylmethyldimethoxysilane, 3-chloropropylmethyldiethoxysilane. cleaning a surface of the polyolefin film to be treated with acetone, and drying the polyolefin film in the air for later use; placing the polyolefin film in step into a low-temperature plasma reaction chamber, and vacuuming the low-temperature plasma reaction chamber to 10-30Pa; after step ends up, introducing polar molecules into the reaction chamber, adjusting temperature and pressure, and performing a gas-phase graft reaction on the surface of the polyolefin by a radio-frequency low-temperature plasma treatment at a power supply of 100-600W and a temperature of 0-75° C to obtain a modified polyolefin film, wherein,
A method, comprising: determining by a network node positioning assistance data blocks to be requested by the network node to be broadcasted by a base station to a user equipment for use by the user equipment in calculating a position of the user equipment; sending by the network node an assistance data broadcast request message toward the base station with positioning assistance data blocks and corresponding information, the information indicating to the base station that the base station is to admit or not admit for broadcasting one or more of the positioning assistance data blocks in response to insufficient resources at the base station to broadcast all the positioning assistance data blocks in the assistance data broadcast request message; and receiving, at the network node and from the base station, indications of success or failure by the base station of broadcasting the positioning assistance data blocks, the success or failure based on the base station's admitting or not admitting, respectively, the positioning assistance data blocks. determining by a network node positioning assistance data blocks to be requested by the network node to be broadcasted by a base station to a user equipment for use by the user equipment in calculating a position of the user equipment; sending by the network node an assistance data broadcast request message toward the base station with positioning assistance data blocks and corresponding information, the information indicating to the base station that the base station is to admit or not admit for broadcasting one or more of the positioning assistance data blocks in response to insufficient resources at the base station to broadcast all the positioning assistance data blocks in the assistance data broadcast request message; and receiving, at the network node and from the base station, indications of success or failure by the base station of broadcasting the positioning assistance data blocks, the success or failure based on the base station's admitting or not admitting, respectively, the positioning assistance data blocks.
Method to produce a microelectronic device comprising a micro-electro-mechanical system (MEMS) structure in a hermetic cavity comprising: - the provision of a substrate comprising a base layer, a sacrificial intermediate layer and a top layer, - the machining of the MEMS structure in the top layer up to the intermediate layer, - the provision of an encapsulation cover and the creation of a cavity in said cover, - the creation of at least one vent opening into the cavity in the cover, - the bonding of the substrate and the cover, the MEMS structure being located in the cavity, - the release of the MEMS structure by means of HF vapour etching of the sacrificial layer via the vents, - the filling of the vents. - the provision of a substrate comprising a base layer, a sacrificial intermediate layer and a top layer, - the machining of the MEMS structure in the top layer up to the intermediate layer, - the provision of an encapsulation cover and the creation of a cavity in said cover, - the creation of at least one vent opening into the cavity in the cover, - the bonding of the substrate and the cover, the MEMS structure being located in the cavity, - the release of the MEMS structure by means of HF vapour etching of the sacrificial layer via the vents, - the filling of the vents.
A scanning probe for the dimensional acquisition of an object by irradiating the object with light and detecting reflected light comprising: - a detection unit comprising an imaging sensor and a sensor lens assembly for detecting the reflected light, - a light projecting unit comprising a light source for generating light, and source optics for focusing the light, and light plane generating optics for generating a light plane for irradiating the object, and - an adjustment mechanism comprised in the light projecting unit, for adjusting the position and/or orientation of the light plane relative to the detection unit such that it coincides with an object-side imaging plane of the sensor lens assembly and wherein the adjustment to the light plane is fixable for operational stability, wherein - the sensor lens assembly comprises a plurality of lenses, wherein all the lenses in the sensor lens assembly are arranged in fixed non-adjustable alignment with each other, - the detection unit and the light projecting unit are attached to a rigid base plate, - the sensor lens assembly is rigidly and non-adjustably attached to the rigid base plate, and - which rigid base plate is configured for mounting the scanning probe onto a localizer. - a detection unit comprising an imaging sensor and a sensor lens assembly for detecting the reflected light, - a light projecting unit comprising a light source for generating light, and source optics for focusing the light, and light plane generating optics for generating a light plane for irradiating the object, and - an adjustment mechanism comprised in the light projecting unit, for adjusting the position and/or orientation of the light plane relative to the detection unit such that it coincides with an object-side imaging plane of the sensor lens assembly and wherein the adjustment to the light plane is fixable for operational stability, wherein - the sensor lens assembly comprises a plurality of lenses, wherein all the lenses in the sensor lens assembly are arranged in fixed non-adjustable alignment with each other, - the detection unit and the light projecting unit are attached to a rigid base plate, - the sensor lens assembly is rigidly and non-adjustably attached to the rigid base plate, and - which rigid base plate is configured for mounting the scanning probe onto a localizer. - the sensor lens assembly comprises a plurality of lenses, wherein all the lenses in the sensor lens assembly are arranged in fixed non-adjustable alignment with each other, - the detection unit and the light projecting unit are attached to a rigid base plate, - the sensor lens assembly is rigidly and non-adjustably attached to the rigid base plate, and - which rigid base plate is configured for mounting the scanning probe onto a localizer.
Chair of a chairlift with at least one seat comprising a seat surface, with a safety bar, which extends transversely over the seat and can be pivoted from an open position into a closed position, and with at least one footrest, characterised in that the footrest is connected to an automatic positioning mechanism (17, 22) and can be adjusted below the seat, separately time-wise from the safety bar, between a travel position and a boarding/disembarking position.
Agricultural appliance for applying liquid manure, in particular a pump tanker, having a receiving device and a liquid manure pump which is arranged below the receiving device and which is connected releasably thereto and which is installed in an operating position in the direction of travel of a tractor vehicle, in particular a pump tanker, such that shaft journals (4, 5), which are arranged one above the other, of the liquid manure pump lie axially, and the connections for a pressure and suction line (6, 7) lie laterally, with respect to the tractor vehicle, characterized in that, by means of an axis of rotation arranged between the receiving device and liquid manure pump, the pump is pivotable from the operating position into a maintenance position, in which a suction housing and a closure cover of the liquid manure pump are freely accessible, in order to carry out maintenance and servicing work.
A method of preparing a diorganodihalosilane, the method comprising the following separate and consecutive steps: (a) treating a metal catalyst comprising a metal selected from the group consisting of i) gold, ii) gold and copper, iii) gold, copper and magnesium, iv) copper, rhodium and gold, v) copper, rhodium, and rhenium, vi) rhenium and palladium, vii) copper, and viii) copper and magnesium with a mixture comprising hydrogen gas and an organotrihalosilane at a temperature from 500 to 1400 °C to form a silicon-containing metal intermediate; and (b) reacting the silicon-containing metal intermediate with an organohalide according to the formula RX, wherein R is C 1 -C 10 hydrocarbyl and X is halo, at a temperature from 100 to 600 °C to form a diorganodihalosilane and a depleted silicon-containing metal intermediate. (a) treating a metal catalyst comprising a metal selected from the group consisting of i) gold, ii) gold and copper, iii) gold, copper and magnesium, iv) copper, rhodium and gold, v) copper, rhodium, and rhenium, vi) rhenium and palladium, vii) copper, and viii) copper and magnesium with a mixture comprising hydrogen gas and an organotrihalosilane at a temperature from 500 to 1400 °C to form a silicon-containing metal intermediate; and (b) reacting the silicon-containing metal intermediate with an organohalide according to the formula RX, wherein R is C 1 -C 10 hydrocarbyl and X is halo, at a temperature from 100 to 600 °C to form a diorganodihalosilane and a depleted silicon-containing metal intermediate.
Fixed-dose combination pharmaceutical formulation containing a tamoxifen parent substance, the action of which is dependent on the quantity or the activity of expressed protein variants, enzyme variants, receptor variants or transporter variants, and at least endoxifen, one of the metabolites of the tamoxifen parent substance, comprising 15-25 mg of tamoxifen and 0.25-5.0 mg of endoxifen.