mhurhangee/ep-ind-claims huggingface dataset:
A redox-complementary electrochromic device exhibiting black-to-transmissive switching, wherein the device comprises an electrochromic layer and a redox-active material layer sandwiched between a transparent first electrode formed on a transparent first substrate and a transparent secondary electrode formed on a transparent secondary substrate, said electrochromic layer comprising an electrochromic Co-based metallo-supramolecular polymer represented by the formula, and said redox-active material being capable of reacting with the electrochromic material to change the electrochromic material from black state into colorless transmissive state: wherein, in the formula, X represents a counter anion, R represents a single bond or a spacer comprising a carbon atom and a hydrogen atom, each of R 1 to R 4 independently represents a hydrogen atom or a substituent group, and n represents an integer of from 2 to 5000, which indicates a degree of polymerization; wherein the redox-active material is at least one compound selected from the group consisting of ferricyanide salts, ferrocene, and (2,2,6,6-Tetramethylpiperidin-1-yl)oxyl; and wherein the redox-active material layer comprises an electrolyte and a solvent capable of dissolving both the redox-active material and the electrolyte therein. wherein, in the formula, X represents a counter anion, R represents a single bond or a spacer comprising a carbon atom and a hydrogen atom, each of R 1 to R 4 independently represents a hydrogen atom or a substituent group, and n represents an integer of from 2 to 5000, which indicates a degree of polymerization; wherein the redox-active material is at least one compound selected from the group consisting of ferricyanide salts, ferrocene, and (2,2,6,6-Tetramethylpiperidin-1-yl)oxyl; and wherein the redox-active material layer comprises an electrolyte and a solvent capable of dissolving both the redox-active material and the electrolyte therein.
Valve for controlling a fluid flow, comprising: - a valve housing with a fluid channel (2.1), the housing comprising an inlet (2.2), an outlet (2.3) and a valve seat (2.4); - a valve body that can be moved in the valve housing to open and close the valve; - a permanent magnet provided at the valve housing; - an electric coil arranged at the valve housing for generating a magnetic field acting on the valve body; wherein the valve body is slidable along the longitudinal axis of the fluid channel (2.1) in the valve housing, wherein the valve body comprises a first free end (3.1) facing the inlet (2.2) and a second free end (3.2) facing the outlet (2.3), wherein the valve body interacts with the valve seat (2.4) by means of its second free end (3.2) in order to open or close the valve, wherein the valve body is made at least partially from a ferrite material and forms an armature which interacts with the permanent magnet and the electric coil, wherein the permanent magnet is configured to apply a force acting in the direction of the valve seat (2.4) to the valve body so as to close the valve, wherein the valve body can be lifted off the valve seat (2.4) when an electric current is applied to the coil in order to open the valve, wherein the valve body tapers towards the first free end, and wherein the fluid flowing through the fluid channel (2.1) flows around the outside of the valve body. - a valve housing with a fluid channel (2.1), the housing comprising an inlet (2.2), an outlet (2.3) and a valve seat (2.4); - a valve body that can be moved in the valve housing to open and close the valve; - a permanent magnet provided at the valve housing; - an electric coil arranged at the valve housing for generating a magnetic field acting on the valve body;
An aircraft with a door system that is adapted to control an opening of a door module that separates compartments (102a, 102b) of the aircraft, the door module comprising a door panel and a door frame, wherein the door panel performs a rotational movement above a floor structure of the aircraft during an opening of the door module, the door system comprising a deceleration mechanism that is operable in a normal operation mode and a deceleration mode, wherein the deceleration mechanism comprises: a hinge, and a wedge-shaped component that is rotatably attached to the hinge, characterised in that during the rotational movement of the door panel from a closed position to any open position (394, 396): the wedge-shaped component is embedded in the floor structure of the aircraft to prevent an interaction with the door panel in the normal operation mode, and the wedge-shaped component protrudes from the floor structure of the aircraft and interacts with the door panel such that the rotational movement of the door panel is decelerated at least between a first open position and a second open position in the deceleration mode; and characterised in that the deceleration mechanism further comprises an activation device that is coupled to the wedge-shaped component and that switches the deceleration mechanism from operating in the normal operation mode to operating in the deceleration mode when a difference in pressure between the compartments (102a, 102b) exceeds a predetermined threshold. a hinge, and a wedge-shaped component that is rotatably attached to the hinge, characterised in that during the rotational movement of the door panel from a closed position to any open position (394, 396): the wedge-shaped component is embedded in the floor structure of the aircraft to prevent an interaction with the door panel in the normal operation mode, and the wedge-shaped component protrudes from the floor structure of the aircraft and interacts with the door panel such that the rotational movement of the door panel is decelerated at least between a first open position and a second open position in the deceleration mode; and characterised in that the deceleration mechanism further comprises the wedge-shaped component is embedded in the floor structure of the aircraft to prevent an interaction with the door panel in the normal operation mode, and the wedge-shaped component protrudes from the floor structure of the aircraft and interacts with the door panel such that the rotational movement of the door panel is decelerated at least between a first open position and a second open position in the deceleration mode; and characterised in that the deceleration mechanism further comprises an activation device that is coupled to the wedge-shaped component and that switches the deceleration mechanism from operating in the normal operation mode to operating in the deceleration mode when a difference in pressure between the compartments (102a, 102b) exceeds a predetermined threshold.
A landing gear assembly comprising: a pivotally mounted first part including a first engagement surface which defines a swept volume as the first part moves; a pivotally mounted second part including a second engagement surface, the second part being movable between: a locked condition, in which the second engagement surface is within a locking region of the swept volume for engagement with the first engagement surface to inhibit movement of the first part; and an unlocked condition, in which the second engagement surface is outside of the locking region of the swept volume; and a member comprising a pair of lugs disposed in a parallel relationship with a space between them, each lug defining a hole, the holes being coaxially aligned, wherein the second part including first and second bearing portions (16e, 16f) with a locking portion between them, the locking portion defining the second engagement surface, the second part being configured to be inserted into and mounted within the lug holes with the locking portion being disposed in the space between the lugs, characterised in that: the lug holes are through holes and the locking portion has a radius not greater than a radius of at least one of the bearing portions. a pivotally mounted first part including a first engagement surface which defines a swept volume as the first part moves; a pivotally mounted second part including a second engagement surface, the second part being movable between: a locked condition, in which the second engagement surface is within a locking region of the swept volume for engagement with the first engagement surface to inhibit movement of the first part; and an unlocked condition, in which the second engagement surface is outside of the locking region of the swept volume; and a locked condition, in which the second engagement surface is within a locking region of the swept volume for engagement with the first engagement surface to inhibit movement of the first part; and an unlocked condition, in which the second engagement surface is outside of the locking region of the swept volume; and a member comprising a pair of lugs disposed in a parallel relationship with a space between them, each lug defining a hole, the holes being coaxially aligned, wherein the second part including first and second bearing portions (16e, 16f) with a locking portion between them, the locking portion defining the second engagement surface, the second part being configured to be inserted into and mounted within the lug holes with the locking portion being disposed in the space between the lugs, characterised in that: the lug holes are through holes and the locking portion has a radius not greater than a radius of at least one of the bearing portions.
A method of replicating nucleic acids, said method comprising: replicating nucleic acid in a replication reaction medium, said replication reaction medium comprising at least one NTP and a reaction buffer, wherein said at least one NTP added to said reaction buffer comprises a thermally labile 3'-substitution group, and wherein said replicating is preceded by heat induction by incubating said replication reaction medium at 50°C-100°C. replicating nucleic acid in a replication reaction medium, said replication reaction medium comprising at least one NTP and a reaction buffer, wherein said at least one NTP added to said reaction buffer comprises a thermally labile 3'-substitution group, and wherein said replicating is preceded by heat induction by incubating said replication reaction medium at 50°C-100°C.
A visible plane determining method, comprising: obtaining plane information of planes to be determined in a target space; detecting, for a first plane to be determined, whether there is a second plane to be determined that makes each line segment formed by connecting each plane convex point in the first plane to be determined with a signal transmission point pass through the second plane to be determined, wherein the first plane to be determined and the second plane to be determined are any two planes in the planes to be determined; determining whether the first plane to be determined is a visible plane according to the detecting result; and performing the detecting step and the determining step for a next plane to be determined until all the planes to be determined are traversed so as to obtain a set of visible planes in the target space, wherein the next plane to be determined is one of the planes which have not been determined among the planes to be determined, and wherein the planes to be determined comprise planes where surfaces of objects in the target space are located, and wherein three of the planes to be determined intersect at one plane convex point. obtaining plane information of planes to be determined in a target space; detecting, for a first plane to be determined, whether there is a second plane to be determined that makes each line segment formed by connecting each plane convex point in the first plane to be determined with a signal transmission point pass through the second plane to be determined, wherein the first plane to be determined and the second plane to be determined are any two planes in the planes to be determined; determining whether the first plane to be determined is a visible plane according to the detecting result; and performing the detecting step and the determining step for a next plane to be determined until all the planes to be determined are traversed so as to obtain a set of visible planes in the target space, wherein the next plane to be determined is one of the planes which have not been determined among the planes to be determined, and wherein the planes to be determined comprise planes where surfaces of objects in the target space are located, and wherein three of the planes to be determined intersect at one plane convex point.
A minimally invasive skin treatment device, comprising: a handpiece having a perimeter elevation and a top which cooperatively define a recessed area, an inner side of the perimeter elevation and the top defining an apposition surface facing into the recessed area, wherein the recessed area is dimensioned to receive a target tissue comprising epidermis, dermis, and subcutaneous layers such that, in use, the epidermis of the target tissue contacts the apposition surface and a least a portion of the subcutaneous layer of the target tissue is in the recessed area; a conduit extending through a side of the perimeter elevation to the recessed area, wherein the conduit is positioned at a distance from the apposition surface, the distance defining a treatment depth; and a tool for treating the target tissue, the tool comprising a proximal end and a distal end, and the tool being configured to allow at least the distal end of the tool to extend through the conduit, into the recessed area, and into the subcutaneous layer of the target tissue disposed within the recessed area in use; characterized in that the conduit is configured to constrain the movement of the tool to forward, reverse and side to side movements within the recessed area, said movements occurring in a plane at the treatment depth. a handpiece having a perimeter elevation and a top which cooperatively define a recessed area, an inner side of the perimeter elevation and the top defining an apposition surface facing into the recessed area, wherein the recessed area is dimensioned to receive a target tissue comprising epidermis, dermis, and subcutaneous layers such that, in use, the epidermis of the target tissue contacts the apposition surface and a least a portion of the subcutaneous layer of the target tissue is in the recessed area; a conduit extending through a side of the perimeter elevation to the recessed area, wherein the conduit is positioned at a distance from the apposition surface, the distance defining a treatment depth; and a tool for treating the target tissue, the tool comprising a proximal end and a distal end, and the tool being configured to allow at least the distal end of the tool to extend through the conduit, into the recessed area, and into the subcutaneous layer of the target tissue disposed within the recessed area in use; characterized in that the conduit is configured to constrain the movement of the tool to forward, reverse and side to side movements within the recessed area, said movements occurring in a plane at the treatment depth.
A pharmaceutical composition, comprising: at least one hydrophobic camptothecin derivative or a pharmaceutically acceptable salt of said derivative; and at least one polyethylene glycol conjugated phospholipid; wherein the molar ratio of said PEG conjugated phospholipid to said hydrophobic camptothecin derivative or said pharmaceutically acceptable salt of said hydrophobic camptothecin derivative is greater than 0.45:1; said PEG conjugated phospholipid comprises a PEG moiety having a molecular weight from 1,000 to 20,000 daltons conjugated to a phospholipid moiety and the phospholipid moiety is selected from the group consisting of: distearoylphosphatidylethanolamine (DSPE), dipalmitoylphosphatidylethanolamine (DPPE), dioleoylphosphatidylethanolamine (DOPE), 1-palmitoyl-2-oleyl, phosphatidylethanolamine (POPE), and dimyristoylphosphatidylethanolamine (DMPE); and said hydrophobic camptothecin derivative is a compound selected from the group consisting of: TLC388 HCl ( -10-[(dimethylamino)methyl]-4-ethyl-9-hydroxy-4-O-[(±)-2-(2",4",5",7"-tetranitro-9"-fluorenylideneaminooxy) propionyl]-1H-pyrano [3',4':6,7]indolizino [1,2-b]quinoline- 3,14-(4H, 12H)-dione, monohydrochloride); TLC1988 HCl ( -10-[(dimethylamino)methyl]-4-ethyl-9-hydroxy-4-O-[2-methyl-2-(2",4",5",7"-tetranitro-9"-fluorenylideneaminooxy)propionyl]-1H-pyrano[3',4':6,7]indolizino [1,2-b]quinoline-3,14-(4H,12H)-dione, monohydrochloride); and mixtures thereof. at least one hydrophobic camptothecin derivative or a pharmaceutically acceptable salt of said derivative; and at least one polyethylene glycol conjugated phospholipid; wherein the molar ratio of said PEG conjugated phospholipid to said hydrophobic camptothecin derivative or said pharmaceutically acceptable salt of said hydrophobic camptothecin derivative is greater than 0.45:1; said PEG conjugated phospholipid comprises a PEG moiety having a molecular weight from 1,000 to 20,000 daltons conjugated to a phospholipid moiety and the phospholipid moiety is selected from the group consisting of: distearoylphosphatidylethanolamine (DSPE), dipalmitoylphosphatidylethanolamine (DPPE), dioleoylphosphatidylethanolamine (DOPE), 1-palmitoyl-2-oleyl, phosphatidylethanolamine (POPE), and dimyristoylphosphatidylethanolamine (DMPE); and said hydrophobic camptothecin derivative is a compound selected from the group consisting of: TLC388 HCl ( -10-[(dimethylamino)methyl]-4-ethyl-9-hydroxy-4-O-[(±)-2-(2",4",5",7"-tetranitro-9"-fluorenylideneaminooxy) propionyl]-1H-pyrano [3',4':6,7]indolizino [1,2-b]quinoline- 3,14-(4H, 12H)-dione, monohydrochloride); TLC1988 HCl ( -10-[(dimethylamino)methyl]-4-ethyl-9-hydroxy-4-O-[2-methyl-2-(2",4",5",7"-tetranitro-9"-fluorenylideneaminooxy)propionyl]-1H-pyrano[3',4':6,7]indolizino [1,2-b]quinoline-3,14-(4H,12H)-dione, monohydrochloride); and mixtures thereof.
A method of preparing an electrode for an electrode assembly having a structure in which electrodes are laminated, comprising: (i) a process of coating an electrode mixture on at least one surface of a metal sheet so that n (n ≧ 2) electrode mixture coated layer lines (211, 212, 213, 214) are formed between non-coated portions (201, 305, 306) parallel to a first direction; (ii) a process of rolling the metal sheet sequentially from a first electrode mixture coated layer line (211, 212, 213, 214) to an n th electrode mixture coated layer line (211, 212, 213, 214) using a rolling roller rotated in a second direction perpendicular to the first direction; (iii) a process of slitting the rolled metal sheet at least twice in the second direction to prepare electrode plate base materials having n electrode mixture coated layers (301, 302, 303, 304) formed thereon; and (iv) a process of cutting each of the electrode plate base materials in the first direction to obtain n single sheet electrodes. (i) a process of coating an electrode mixture on at least one surface of a metal sheet so that n (n ≧ 2) electrode mixture coated layer lines (211, 212, 213, 214) are formed between non-coated portions (201, 305, 306) parallel to a first direction; (ii) a process of rolling the metal sheet sequentially from a first electrode mixture coated layer line (211, 212, 213, 214) to an n th electrode mixture coated layer line (211, 212, 213, 214) using a rolling roller rotated in a second direction perpendicular to the first direction; (iii) a process of slitting the rolled metal sheet at least twice in the second direction to prepare electrode plate base materials having n electrode mixture coated layers (301, 302, 303, 304) formed thereon; and (iv) a process of cutting each of the electrode plate base materials in the first direction to obtain n single sheet electrodes.
Segmented rolling bearing ring for a large rolling bearing with an inner side facing at least one raceway system for rolling elements, on which at least one rolling bearing raceway is provided, the rolling bearing ring being divided into ring segments (7, 8, 9), which adjoin one another in the circumferential direction, forming butt joints on abutting sides (11, 12), and which are sealed off from one another in the region of the butt joints by means of strip-shaped seals (13, 14), characterized in that the butt joint between a first and a second of the ring segments (7, 8, 9) on an outer side of the rolling bearing ring facing away from the inner side is covered by one of the strip-shaped seals (13, 14), this strip-shaped seal resting with its longitudinal edge regions on both sides of the butt joint on the ring segments (7, 8) on both sides of the butt joint and covering the butt joint with a central region and the seal being clamped against the butt joint by means of at least one clamping plate (16, 17, 18, 19) screwed to the first and/or the second ring segment.
A nanostructure having a physical structure which in at least one dimension has a size ranging from 10 to 300 nm and which has a largest dimension that is less than 1000 nm in size comprising molecules of the following compound non-covalently bound to each other, wherein the compound is selected from: where Y = OH or NH 2, where Z = O; X represents a linking group, wherein X is selected from the group consisting of - NH-(C=Z)-, -(C=Z)-NH-, where heteroatom Z can be either O or S; and R c represents a substituted or unsubstituted alkyl group selected from the group consisting of with the proviso that the nanostructure does not comprise these compounds associated non-covalently with a benzimidazolone pigment. where Y = OH or NH 2, where Z = O; X represents a linking group, wherein X is selected from the group consisting of - NH-(C=Z)-, -(C=Z)-NH-, where heteroatom Z can be either O or S; and R c represents a substituted or unsubstituted alkyl group selected from the group consisting of with the proviso that the nanostructure does not comprise these compounds associated non-covalently with a benzimidazolone pigment.
An exhaust gas heater for an exhaust gas system of an internal combustion engine, comprising: - a disc-like carrier having an outer circumferential region, which is arranged radially on the outside with respect to a heater longitudinal axis and a central region, which is arranged radially on the inside, - a heating conductor with a heating region arranged on a first axial side of the carrier, - at least one holding member for holding the heating conductor on the carrier, wherein the holding member comprises a plurality of alternatingly successive holding portions which engage around the heating conductor in its heating region and fastening portions which engage into fastening openings in the carrier and fixed to the carrier, wherein the at least one holding member is of wave-like form with successive alternating first wave loop regions and second wave loop regions, wherein the first wave loop regions form the holding portions and the second wave loop regions form the fastening portions, characterized in that at least one holding member is fixed to the carrier with at least one fastening portion on a second axial side of the carrier by material bonding, that at least one second wave loop region engaging into a fastening opening of the carrier is fixed to the carrier by material bonding in its length portion protruding from the second axial side of the carrier. - a disc-like carrier having an outer circumferential region, which is arranged radially on the outside with respect to a heater longitudinal axis and a central region, which is arranged radially on the inside, - a heating conductor with a heating region arranged on a first axial side of the carrier, - at least one holding member for holding the heating conductor on the carrier,