mhurhangee/ep-ind-claims huggingface dataset:
A method for lightening keratin fibers, in particular human hair, which method is characterized in that the components of a multicomponent packaging unit (kit of parts) for lightening keratin fibers are applied to the keratin-containing fibers and left on the fibers for from 5 to 60 minutes, and the fibers are then rinsed with water or washed with a surfactant-containing cleansing agent, the multicomponent packaging unit containing at least the following three components that are packaged separately from one another: i) a first component which contains, in a cosmetically acceptable carrier, at least one organic thiol compound, ii) a second component which contains at least one persulfate salt, and iii) a third component which contains, in a cosmetically acceptable carrier, hydrogen peroxide, the method being characterized in that, a) in a first step, the first component of the kit, containing, in a cosmetically acceptable carrier, at least one organic thiol compound, is applied to the dry or damp fibers and is left on the fibers for a reaction time of from 5 to 45 minutes, b) in a second step, the keratin fibers are rinsed with water or a surfactant-containing cleansing agent, c) in a further step, a mixture of components and of the kit is applied to the fibers and left on the fibers for a reaction time of from 10 to 45 minutes, d) and the fibers are then rinsed with water or washed with a surfactant-containing cleansing agent. i) a first component which contains, in a cosmetically acceptable carrier, at least one organic thiol compound, ii) a second component which contains at least one persulfate salt, and iii) a third component which contains, in a cosmetically acceptable carrier, hydrogen peroxide, a) in a first step, the first component of the kit, containing, in a cosmetically acceptable carrier, at least one organic thiol compound, is applied to the dry or damp fibers and is left on the fibers for a reaction time of from 5 to 45 minutes, b) in a second step, the keratin fibers are rinsed with water or a surfactant-containing cleansing agent, c) in a further step, a mixture of components and of the kit is applied to the fibers and left on the fibers for a reaction time of from 10 to 45 minutes, d) and the fibers are then rinsed with water or washed with a surfactant-containing cleansing agent.
An article of footwear, comprising: a sole structure (10, 10A, 10B), comprising: a midsole body (14, 32) having a proximal surface and a distal surface; wherein the midsole body (14, 32) has a first set of holes extending through the midsole body (14, 32) from the proximal surface to the distal surface, a second set of holes extending through the midsole body (14, 32) from the proximal surface to the distal surface, and a cleft extending partway through the midsole body (14, 32) between the first set of holes and the second set of holes; wherein center axes of holes of the first set are parallel with center axes of holes of the second set with the cleft open, and are nonparallel with the center axes of the holes of the second set with the cleft closed; a plurality of proprioceptive elements, each proprioceptive element disposed in a different hole of the first set or of the second set, and translatable relative to the midsole body (14, 32) along a central axis of the respective hole in a direction toward the proximal surface under a force along the central axis at a distal end of the proprioceptive element; a connecting web integral with the plurality of proprioceptive elements at either proximal ends or distal ends of the plurality of proprioceptive elements such that the connecting web and the plurality of proprioceptive elements are a single, unitary component; and in combination with a sock overlying the connecting web such that the proximal ends of the plurality of proprioceptive elements translate into a foot-receiving cavity of the sock. a midsole body (14, 32) having a proximal surface and a distal surface; wherein the midsole body (14, 32) has a first set of holes extending through the midsole body (14, 32) from the proximal surface to the distal surface, a second set of holes extending through the midsole body (14, 32) from the proximal surface to the distal surface, and a cleft extending partway through the midsole body (14, 32) between the first set of holes and the second set of holes; wherein center axes of holes of the first set are parallel with center axes of holes of the second set with the cleft open, and are nonparallel with the center axes of the holes of the second set with the cleft closed; a plurality of proprioceptive elements, each proprioceptive element disposed in a different hole of the first set or of the second set, and translatable relative to the midsole body (14, 32) along a central axis of the respective hole in a direction toward the proximal surface under a force along the central axis at a distal end of the proprioceptive element; a connecting web integral with the plurality of proprioceptive elements at either proximal ends or distal ends of the plurality of proprioceptive elements such that the connecting web and the plurality of proprioceptive elements are a single, unitary component; and in combination with a sock overlying the connecting web such that the proximal ends of the plurality of proprioceptive elements translate into a foot-receiving cavity of the sock.
A method of producing a recombinantly produced antibody or fragment thereof comprising the step of culturing a cell comprising a nucleic acid encoding the antibody or fragment thereof in a cell culture medium, wherein the antibody or fragment thereof is secreted into the cell culture medium, wherein the cell culture medium comprises hypotaurine; and wherein the cell culture medium comprising hypotaurine reduces the color intensity of a composition comprising the antibody or fragment thereof produced by the cell as compared to a composition comprising the antibody or fragment thereof produced by the cell cultured in a cell culture medium that does not comprise hypotaurine.
An assembly comprising a metal piece, a piece made of ceramic material and at least one intermediate connection element (10', 10") assembled to each of said pieces (16, 18) by brazing, this assembly being characterized in that said intermediate connection element is constituted by a deformable sheet presenting at least two flat zones (11, 12) brazed respectively to said pieces (16, 18), these two flat zones (11, 12) being interconnected by a deformable zone presenting at least two free, that is non-brazed, undulations (19, 20) oriented in alternation towards said metal piece and towards said piece made of ceramic material.
A method of operating an electronic device having a display panel, the method comprising: receiving, by a display driving circuit configured to drive the display panel of the electronic device, main image data over a first channel from a first processor of the electronic device; receiving, by the display driving circuit, a control signal over a second channel from a second processor of the electronic device, wherein the control signal comprises a coordinate value on a screen; generating, by the display driving circuit, an additional image different from the main image and performing anti-aliasing processing on the additional image based on the coordinate value; merging, by the display driving circuit, the main image with the additional image to form a merged image; and outputting, by the display driving circuit, the merged image on the display panel. receiving, by a display driving circuit configured to drive the display panel of the electronic device, main image data over a first channel from a first processor of the electronic device; receiving, by the display driving circuit, a control signal over a second channel from a second processor of the electronic device, wherein the control signal comprises a coordinate value on a screen; generating, by the display driving circuit, an additional image different from the main image and performing anti-aliasing processing on the additional image based on the coordinate value; merging, by the display driving circuit, the main image with the additional image to form a merged image; and outputting, by the display driving circuit, the merged image on the display panel.
An automatic darkening filter for welding protection, comprising a first liquid crystal cell having two flat ultrathin glass substrates, characterized in that the ultrathin glass substrates have a thickness of between 30 μm and 200 μm.
End fitting for a wiper blade of a pane of glass of a motor vehicle comprising at least one flexible support and also a squeegee blade designed to be applied against the pane of glass, the end fitting comprising a housing capable of receiving a terminal part of the flexible support, the end fitting comprising two distinct elements (5, 6) including an external shell and an internal liner that is provided with the housing, the external shell accommodating the internal liner in a position of use of the wiper blade, the end fitting being provided with at least one first locking means (10, 11, 14, 15) of the internal liner inside the external shell, the end fitting being characterised in that the first locking means (10, 11, 14, 15) comprises at least two antagonistic stops (14, 15) of which at least one first stop equipping a second internal face of the external shell and at least one second stop equipping a second internal face of the internal liner.
An apparatus for a gas turbine engine comprising: a rotating part of a gas turbine engine, having a cooling channel and being attached to a disk for rotation about an axis, said disk having a conduit for feeding a cooling fluid to said cooling channel; and a first impeller (90, 150) rotating with said disk and in register with said conduit and an outer periphery of said disk, said first impeller directing said cooling fluid to said conduit, characterized in that: said first impeller (90, 150) is on said disk and wherein said first impeller has a radial portion and an extension whereby said radial portion and said extension form a J-shape, wherein said radial portion has a saddle disposed therein that extends in a direction parallel to the axis; wherein the apparatus further comprises a cover enclosing said first impeller (90, 150) such that cooling fluid does not flow axially around said first impeller (90, 150). a rotating part of a gas turbine engine, having a cooling channel and being attached to a disk for rotation about an axis, said disk having a conduit for feeding a cooling fluid to said cooling channel; and a first impeller (90, 150) rotating with said disk and in register with said conduit and an outer periphery of said disk, said first impeller directing said cooling fluid to said conduit, characterized in that: said first impeller (90, 150) is on said disk and wherein said first impeller has a radial portion and an extension whereby said radial portion and said extension form a J-shape, wherein said radial portion has a saddle disposed therein that extends in a direction parallel to the axis; wherein the apparatus further comprises a cover enclosing said first impeller (90, 150) such that cooling fluid does not flow axially around said first impeller (90, 150). said first impeller (90, 150) is on said disk and wherein said first impeller has a radial portion and an extension whereby said radial portion and said extension form a J-shape, wherein said radial portion has a saddle disposed therein that extends in a direction parallel to the axis; wherein the apparatus further comprises a cover enclosing said first impeller (90, 150) such that cooling fluid does not flow axially around said first impeller (90, 150).
A process for preparing sugammadex of formula I, comprising, a) reacting γ-cyclodextrin of formula II, with a halogenating agent, selected from a group consisting of oxalyl chloride, oxalyl bromide, thionyl chloride and thionyl bromide, in an organic solvent, b) mixing the reaction mixture of step a) with an aqueous solution of base and alcoholic solvent, c) isolating 6-per-deoxy-6-per-halo-γ-cyclodextrin of compound of formula III, wherein x is bromide or chloride, from the reaction mixture, d) optionally, drying the 6-per-deoxy-6-per-halo-γ-cyclodextrin, e) optionally, purifying the compound of step c) or d), f) reacting the 6-per-deoxy-6-per-halo-γ-cyclodextrin with 3-mercaptopropionic acid in presence of alkali metal alkoxide base in an organic solvent to obtain sugammadex. a) reacting γ-cyclodextrin of formula II, with a halogenating agent, selected from a group consisting of oxalyl chloride, oxalyl bromide, thionyl chloride and thionyl bromide, in an organic solvent, b) mixing the reaction mixture of step a) with an aqueous solution of base and alcoholic solvent, c) isolating 6-per-deoxy-6-per-halo-γ-cyclodextrin of compound of formula III, wherein x is bromide or chloride, from the reaction mixture, d) optionally, drying the 6-per-deoxy-6-per-halo-γ-cyclodextrin, e) optionally, purifying the compound of step c) or d), f) reacting the 6-per-deoxy-6-per-halo-γ-cyclodextrin with 3-mercaptopropionic acid in presence of alkali metal alkoxide base in an organic solvent to obtain sugammadex.
Clamping device for fixing a clamping rail between a first wall surface or a ceiling surface and a rod arranged parallel to the first wall surface or the ceiling surface, having a connecting part which is configured to fasten the clamping device with the clamping rail, and having at least one first receiving device for receiving the rod, wherein the connecting part has a connecting sleeve arrangeable between the clamping rail and the rod, within which a tensioning element is arranged axially, wherein by means of the tensioning element a tension is applicable to the first receiving device with respect to the connecting part, wherein the connecting part has a support device, by means of which the clamping device can be supported in a direction perpendicular to a longitudinal axis of the connecting sleeve on the first wall surface or ceiling surface, wherein for fastening the clamping device with the clamping rail, the connecting part has at least one protrusion which is configured to engage in a profile of the clamping rail, characterized in that the connecting part is made in one piece, comprising the connecting sleeve, the support device and the at least one protrusion.
A turbine blade comprising: a blade main body that is provided with a plurality of film cooling holes and inside which at least two cavities (C1,C2) are formed by at least one plate-like rib provided substantially orthogonal to a center line connecting a leading edge and a trailing edge, in a cross-sectional plane substantially orthogonal to an upright-direction axis; and at least one hollow insert (12a,12b,12c) that is disposed in each of the cavities (C1,C2) so as to form a cooling space between outer circumferential surfaces of the inserts (12a,12b,12c) and an inner circumferential surface of the blade main body, wherein the inserts (12a,12b,12c) are provided with a plurality of impingement cooling holes, characterized in that two inserts (12a,12b) are disposed, one each, on a ventral side and a dorsal side in one of the cavities such that part of a cooling medium blown out toward the ventral side of the inner circumferential surface of the blade main body through the impingement cooling holes in the insert that is disposed on the ventral side passes through the cooling space, is initially introduced to the inside of the insert that is disposed on the dorsal side, and is then blown out toward the dorsal side of the inner circumferential surface of the blade main body through the impingement cooling holes in the insert that is disposed on the dorsal side. a blade main body that is provided with a plurality of film cooling holes and inside which at least two cavities (C1,C2) are formed by at least one plate-like rib provided substantially orthogonal to a center line connecting a leading edge and a trailing edge, in a cross-sectional plane substantially orthogonal to an upright-direction axis; and at least one hollow insert (12a,12b,12c) that is disposed in each of the cavities (C1,C2) so as to form a cooling space between outer circumferential surfaces of the inserts (12a,12b,12c) and an inner circumferential surface of the blade main body, wherein the inserts (12a,12b,12c) are provided with a plurality of impingement cooling holes, characterized in that two inserts (12a,12b) are disposed, one each, on a ventral side and a dorsal side in one of the cavities such that part of a cooling medium blown out toward the ventral side of the inner circumferential surface of the blade main body through the impingement cooling holes in the insert that is disposed on the ventral side passes through the cooling space, is initially introduced to the inside of the insert that is disposed on the dorsal side, and is then blown out toward the dorsal side of the inner circumferential surface of the blade main body through the impingement cooling holes in the insert that is disposed on the dorsal side.
A nitrogen generation and oxygen distribution system, comprising: a nitrogen generation system operative to create nitrogen enriched air as a primary product and oxygen enriched air as a secondary product, and route the nitrogen enriched air to a fuel tank of an aircraft; and the nitrogen generation and oxygen distribution system being characterized by an oxygen distribution processor communicatively coupled to the nitrogen generation system and operative to determine a plurality of flight parameters; determine from the plurality of flight parameters, a selection of an oxygen distribution configuration associated with the nitrogen generation system, the oxygen distribution configuration comprising a first oxygen distribution configuration and a second oxygen distribution configuration; in response to selecting the first oxygen distribution configuration, route the oxygen enriched air from the nitrogen generation system to an ambient environment surrounding the aircraft; and in response to selecting the second oxygen distribution configuration, route the oxygen enriched air from the nitrogen generation system to an engine of the aircraft. a nitrogen generation system operative to create nitrogen enriched air as a primary product and oxygen enriched air as a secondary product, and route the nitrogen enriched air to a fuel tank of an aircraft; and the nitrogen generation and oxygen distribution system being characterized by create nitrogen enriched air as a primary product and oxygen enriched air as a secondary product, and route the nitrogen enriched air to a fuel tank of an aircraft; and the nitrogen generation and oxygen distribution system being characterized by an oxygen distribution processor communicatively coupled to the nitrogen generation system and operative to determine a plurality of flight parameters; determine from the plurality of flight parameters, a selection of an oxygen distribution configuration associated with the nitrogen generation system, the oxygen distribution configuration comprising a first oxygen distribution configuration and a second oxygen distribution configuration; in response to selecting the first oxygen distribution configuration, route the oxygen enriched air from the nitrogen generation system to an ambient environment surrounding the aircraft; and in response to selecting the second oxygen distribution configuration, route the oxygen enriched air from the nitrogen generation system to an engine of the aircraft. determine a plurality of flight parameters; determine from the plurality of flight parameters, a selection of an oxygen distribution configuration associated with the nitrogen generation system, the oxygen distribution configuration comprising a first oxygen distribution configuration and a second oxygen distribution configuration; in response to selecting the first oxygen distribution configuration, route the oxygen enriched air from the nitrogen generation system to an ambient environment surrounding the aircraft; and in response to selecting the second oxygen distribution configuration, route the oxygen enriched air from the nitrogen generation system to an engine of the aircraft.
A non-aqueous lubricant composition comprising: a base stock; and at least 0.02wt% of a friction reducing additive which consists essentially of a block co-polymer of at least one block A which is an oligo- or polyester residue of a hydroxycarboxylic acid and at least one block B which is a residue of a polyalkylene glycol, and wherein the block co-polymer has an HLB value of at least 6.5. a base stock; and at least 0.02wt% of a friction reducing additive which consists essentially of a block co-polymer of at least one block A which is an oligo- or polyester residue of a hydroxycarboxylic acid and at least one block B which is a residue of a polyalkylene glycol,
A combustion chamber module comprising an annular combustion chamber and an outer casing, the combustion chamber being attached to the outer casing, the downstream end of an outer wall of said combustion chamber being secured to an annular connection part, characterized in that the annular connection part includes a plurality of fastener tabs directed radially outwards and upstream, each tab end being engaged in a hook-forming groove that is laterally open in a downstream direction and that is secured to the inside wall of the casing.
Plug system comprising a plug connector designed to transmit currents of 50 A or more and a mating plug connector for coupling to the plug connector, comprising a closure device which, in a closed position, prevents the plug connector from being pulled off the mating plug connector, the closure device having a lever part pivotably fastened to the plug connector and a securing clip hingedly attached thereto for engaging in an engagement portion of the mating plug connector in the closed position, and comprising a pretensioning part which acts in the closed position between the plug connector and the mating plug connector, is yielding in the axial direction, and can be compressed in the axial direction when the closure device moves into the closed position, characterized by a securing device which can be moved from a release position, in which it allows a pivoting movement of the lever part, into a securing position, in which it blocks a pivoting movement of the lever part starting from the closed position, and vice versa, the securing device having a locking bolt which is arranged so as to be movable in the axial direction and which engages in a pivot path of the lever part in the closed position.
A machine room of a refrigerator comprising: a defrost water tray to collect defrost water; a condenser installed at an upper side of the defrost water tray; an air blowing fan installed at one side of the condenser to generate air flow; and a guide part to guide air supplied from the air blowing fan, wherein the air blowing fan is disposed at an upper side of the defrost water tray, and the guide part is disposed between the condenser and the air blowing fan to prevent a portion of the air flow supplied by the air blowing fan from moving to the defrost water tray, characterized in that a through surface having a path guiding air to the defrost water tray is arranged between the condenser and the air blowing fan and wherein the guide part closes a portion of the through surface. a defrost water tray to collect defrost water; a condenser installed at an upper side of the defrost water tray; an air blowing fan installed at one side of the condenser to generate air flow; and a guide part to guide air supplied from the air blowing fan,