mhurhangee/patent-ind-claim-en huggingface dataset:
Aerostatic bearing having a sliding piece (G) which is guided on a guiding face (S), having an inner, conical sliding face (G1) of an inner pneumatic bearing with a central compressed air supply (N1), which sliding face faces the guiding face (S), wherein the conical sliding face (G1) is secured by means of first joints (P1) to the central compressed air supply (N1) and by means of second joints (P2) to a base (B) of the sliding piece (G) which is arranged at a side of the sliding piece (G) facing away from the guiding face (S) so that a cone angle of the conical sliding face (G1) can be changed, characterised in that the conical sliding face (G2) is surrounded by an annular sliding face (G2) of an outer pneumatic bearing which has an annular compressed air supply (N2).
A bonded tungsten carbide-based super hard alloy assembly comprising a first metal member having a first bonding surface and comprised of a steel material containing a martensite structure and a second metal member having a second bonding surface , the second bonding surface having been directly bonded to the first bonding surface of the first metal member , and comprised of a tungsten carbide-based super hard alloy, wherein: the martensite structure-containing steel material constituting the first metal member either: is a stainless steel having an average carbon concentration of from 0.10 to 0.40 mass%; or further contains at least one element selected from the group consisting of Ti, Nb, Mo, Ta, V, W, and Zr, characterised in that : the first metal member has, at a depth thereof ranging from 0.70 to 3.00 mm from the first bonding surface , a high carbon concentration region , the high carbon concentration region having the maximum carbon concentration of from 0.3 to 1.2 mass% when the martensite structure-containing steel material is the stainless steel having the average carbon concentration of from 0.10 to 0.40 mass%, and the maximum carbon concentration of from 0.55 to 1.7 mass% when the martensite structure-containing steel material further contains the at least one element selected from the group consisting of Ti, Nb, Mo, Ta, V, W, and Zr. the martensite structure-containing steel material constituting the first metal member either: is a stainless steel having an average carbon concentration of from 0.10 to 0.40 mass%; or further contains at least one element selected from the group consisting of Ti, Nb, Mo, Ta, V, W, and Zr, is a stainless steel having an average carbon concentration of from 0.10 to 0.40 mass%; or further contains at least one element selected from the group consisting of Ti, Nb, Mo, Ta, V, W, and Zr, characterised in that : the first metal member has, at a depth thereof ranging from 0.70 to 3.00 mm from the first bonding surface , a high carbon concentration region , the high carbon concentration region having the maximum carbon concentration of from 0.3 to 1.2 mass% when the martensite structure-containing steel material is the stainless steel having the average carbon concentration of from 0.10 to 0.40 mass%, and the maximum carbon concentration of from 0.55 to 1.7 mass% when the martensite structure-containing steel material further contains the at least one element selected from the group consisting of Ti, Nb, Mo, Ta, V, W, and Zr. the maximum carbon concentration of from 0.3 to 1.2 mass% when the martensite structure-containing steel material is the stainless steel having the average carbon concentration of from 0.10 to 0.40 mass%, and the maximum carbon concentration of from 0.55 to 1.7 mass% when the martensite structure-containing steel material further contains the at least one element selected from the group consisting of Ti, Nb, Mo, Ta, V, W, and Zr.
A method for replacing an immersion nozzle, wherein a new immersion nozzle is supported by pressing members arranged in parallel in both sides of a lower plane of a flange portion and is caused to slide while being pressed to a lower plane of an upper refractory so as to push out a used immersion nozzle in a lateral direction thereby pressure-joining to the upper refractory , wherein a concave portion is formed on an upper plane of the new immersion nozzle so as to include a nozzle hole therein, and a shaped joint sealer that is a flexible refractory in a plate-like shape with a cutout-portion, the shape of which is equal to or larger than the nozzle hole of the immersion nozzle , is mounted in the said concave portion , wherein the shaped joint sealer can fill a space with being deformed when the immersion nozzle is joined to the upper refractory .
Turbojet engine comprising: a. an upstream ducted fan driven by a gas generator, b. the gas generator comprising a first and a second coaxial compressors, c. an inlet case forming a support for the rotors of the ducted fan and the first compressor , d. an inter-compressor case located downstream from the inlet case , and forming a support of the rotor of the second compressor , e. attachment means for the thrust take-up rods arranged on the inter-compressor case, characterised by the fact that it comprises a stress structural shroud connecting an annular part of the inlet case to an annular part of the inter-compressor case , the annular parts of the inlet and inter-compressor cases being inserted between a primary flowpath and a secondary flowpath, the first compressor comprising a floating case , the floating case forming an outer wall of the primary flowpath, the floating case being connected to one of the two inlet and inter-compressor cases with an axial backlash floating connection (31a; 31'a). a. an upstream ducted fan driven by a gas generator, b. the gas generator comprising a first and a second coaxial compressors, c. an inlet case forming a support for the rotors of the ducted fan and the first compressor , d. an inter-compressor case located downstream from the inlet case , and forming a support of the rotor of the second compressor , e. attachment means for the thrust take-up rods arranged on the inter-compressor case,
Use of a basic substance selected from a basic oxide, a basic carbonate or a basic hydroxide, preferably calcium carbonate or magnesium oxide, and more preferably calcium carbonate, for suppressing bitterness of 4-(3-chloro-4-(cyclopropylaminocarbonyl)aminophenoxy)-7-methoxy-6-quinolinecarboxyamide, or a pharmaceutically acceptable salt thereof, preferably a mesylate thereof, wherein preferably 0.01 to 50 parts by weight of the basic substance is mixed per 1 part by weight of 4-(3-chloro-4-(cyclopropylaminocarbonyl)aminophenoxy)-7-methoxy-6-quinolinecarboxyamide or the pharmaceutically acceptable salt thereof or 0.16 to 80 mol of the basic substance is mixed per 1 mol of 4-(3-chloro-4-(cyclopropylaminocarbonyl)aminophenoxy)-7-methoxy-6-quinolinecarboxyamide or the pharmaceutically acceptable salt thereof.
A system for determining a relative position and/or orientation between a primary winding structure and a secondary winding structure of a system for inductive power transfer, wherein the system comprises at least one secondary-sided transmitting unit, wherein a positioning signal (PS) with a positioning frequency is transmittable by the secondary-sided transmitting unit, wherein the system comprises at least one primary-sided receiving unit, wherein a signal portion of the received signal with the positioning frequency is determinable, wherein the relative position and/or orientation is determinable depending on a signal characteristic of the determined signal portion and using at least one data base containing a relationship between the at least one signal characteristic and the relative position and/or orientation, characterized in that information on the relative position and/or orientation determined by a primary-sided control unit depending on signal portions of signals received by at least two primary-sided direction-sensitive receiving units with differently oriented main reception directions are communicated to the secondary side, or in that information on the relative position and/or orientation is determined by a secondary-sided control unit depending on signal portions of signals received by at least two primary-sided direction-sensitive receiving units with differently oriented main reception directions which are communicated to the secondary side.
Cooling system for a galley for installation in a transportation means, in particular an aircraft, comprising: - a cooling device which comprises a coolant circuit adapted to be flowed through with a coolant, - a fluid line which is adapted to be flowed through with a fluid to be cooled and which is thermally coupled with the coolant circuit of the cooling device in order to transfer heat from the fluid to be cooled flowing through the fluid line to the coolant circulating in the coolant circuit , - an air line which is adapted to be flowed through with air and which is thermally coupled with the coolant circuit of the cooling device in order to transfer heat from the coolant circulating in the coolant circuit to the air flowing through the air line , - wherein the air line , downstream of the thermal coupling of the air line with the coolant circuit of the cooling device , is connectable to a cabin region of the transportation means accommodating the galley in order to supply the cabin region with air warmed by heat transfer from the coolant circulating in the coolant circuit of the cooling device , and - wherein the air line , upstream of the thermal coupling of the air line with the coolant circuit of the cooling device , is connectable to an interior of the galley in order to supply the air line with air to be discharged from the interior of the galley . - a cooling device which comprises a coolant circuit adapted to be flowed through with a coolant, - a fluid line which is adapted to be flowed through with a fluid to be cooled and which is thermally coupled with the coolant circuit of the cooling device in order to transfer heat from the fluid to be cooled flowing through the fluid line to the coolant circulating in the coolant circuit , - an air line which is adapted to be flowed through with air and which is thermally coupled with the coolant circuit of the cooling device in order to transfer heat from the coolant circulating in the coolant circuit to the air flowing through the air line , - wherein the air line , downstream of the thermal coupling of the air line with the coolant circuit of the cooling device , is connectable to a cabin region of the transportation means accommodating the galley in order to supply the cabin region with air warmed by heat transfer from the coolant circulating in the coolant circuit of the cooling device , and - wherein the air line , upstream of the thermal coupling of the air line with the coolant circuit of the cooling device , is connectable to an interior of the galley in order to supply the air line with air to be discharged from the interior of the galley .
A pharmaceutical composition of isolated microvesicles for use in the therapy of skin, wherein the isolated microvesicles are prepared with a method comprising the steps of: (a) obtaining a biological fluid containing microvesicles; (b) clarifying the biological fluid to remove cellular debris; (c) precipitating the microvesicles by adding a precipitating agent which is polyethylene glycol to the clarified biological fluid; (d) collecting the precipitated microvesicles; (e) washing the precipitated microvesicles to remove the precipitating agent; and (f) optionally suspending the microvesicles in a solution for storage or subsequent use to produce an isolated preparation of microvesicles, wherein the microvesicles are isolated without damaging the structural or functional integrity of the microvesicles, and wherein the therapy of skin comprises regenerating at least one tissue in a patient with diseased, damaged, or missing skin selected from a group consisting of epithelial tissue, stromal tissue, nerve tissue, vascular tissue and adnexal structures. (a) obtaining a biological fluid containing microvesicles; (b) clarifying the biological fluid to remove cellular debris; (c) precipitating the microvesicles by adding a precipitating agent which is polyethylene glycol to the clarified biological fluid; (d) collecting the precipitated microvesicles; (e) washing the precipitated microvesicles to remove the precipitating agent; and (f) optionally suspending the microvesicles in a solution for storage or subsequent use to produce an isolated preparation of microvesicles, wherein the microvesicles are isolated without damaging the structural or functional integrity of the microvesicles, and wherein the therapy of skin comprises regenerating at least one tissue in a patient with diseased, damaged, or missing skin selected from a group consisting of epithelial tissue, stromal tissue, nerve tissue, vascular tissue and adnexal structures.
An unmanned aerial vehicle, UAV, comprising: a housing; a line-deployment mechanism couplable to the housing and a line , wherein the line-deployment mechanism is controllable to vary a deployment rate of the line; a payload-release mechanism operable to couple the line to a payload , wherein the payload-release mechanism is configured to release the payload from the line; and a control system configured to determine that the UAV is located at or near a delivery location and responsively: operate the line-deployment mechanism according to a pre-determined variable deployment-rate profile to lower the payload to or near to the ground, wherein the variable deployment-rate profile specifies for the payload to initially descend at a pre-determined first rate and subsequently, during the descent, to decrease in speed from the first rate to a pre-determined second rate; and subsequently determine that the payload is touching or is within a threshold distance from the ground, and responsively operate the payload-release mechanism to release the payload from the line. a housing; a line-deployment mechanism couplable to the housing and a line , wherein the line-deployment mechanism is controllable to vary a deployment rate of the line; a payload-release mechanism operable to couple the line to a payload , wherein the payload-release mechanism is configured to release the payload from the line; and a control system configured to determine that the UAV is located at or near a delivery location and responsively: operate the line-deployment mechanism according to a pre-determined variable deployment-rate profile to lower the payload to or near to the ground, wherein the variable deployment-rate profile specifies for the payload to initially descend at a pre-determined first rate and subsequently, during the descent, to decrease in speed from the first rate to a pre-determined second rate; and subsequently determine that the payload is touching or is within a threshold distance from the ground, and responsively operate the payload-release mechanism to release the payload from the line. operate the line-deployment mechanism according to a pre-determined variable deployment-rate profile to lower the payload to or near to the ground, wherein the variable deployment-rate profile specifies for the payload to initially descend at a pre-determined first rate and subsequently, during the descent, to decrease in speed from the first rate to a pre-determined second rate; and subsequently determine that the payload is touching or is within a threshold distance from the ground, and responsively operate the payload-release mechanism to release the payload from the line.
A positive electrode active material for a secondary battery, the positive electrode active material comprising a lithium composite transition metal oxide including nickel (Ni), cobalt (Co), and manganese (Mn), wherein the lithium composite transition metal oxide comprises 60 mol% or more of the nickel (Ni) among metals excluding lithium, and a coating layer is formed on surfaces of particles of the lithium composite transition metal oxide, wherein the coating layer comprises a lithium-polymer compound which is formed by a reaction of a lithium by-product with a polymer, characterized in that the polymer comprises at least one selected from the group consisting of polyacrylamide (PAA) and polyimide (PI). a coating layer is formed on surfaces of particles of the lithium composite transition metal oxide, wherein the coating layer comprises a lithium-polymer compound which is formed by a reaction of a lithium by-product with a polymer, characterized in that the polymer comprises at least one selected from the group consisting of polyacrylamide (PAA) and polyimide (PI).
Hydrogen tank for aircrafts, comprising: - an inner vessel adapted to contain hydrogen; - first and second outer jacket domes having a semi-sphere shape, - a first cylindrical outer jacket established on top of the first and second outer jacket domes , - a second cylindrical outer jacket established in the bottom of the first and second outer jacket domes ; characterized in that the first and second outer jacket domes have first L-shaped ends and in that the first and second cylindrical outer jackets comprise second L-shaped ends ; and in that the first and second L-shaped ends form L-shaped junctions to attach the first and second outer jacket domes to the first and second cylindrical outer jackets . - an inner vessel adapted to contain hydrogen; - first and second outer jacket domes having a semi-sphere shape, - a first cylindrical outer jacket established on top of the first and second outer jacket domes , - a second cylindrical outer jacket established in the bottom of the first and second outer jacket domes ; characterized in that the first and second outer jacket domes have first L-shaped ends and in that the first and second cylindrical outer jackets comprise second L-shaped ends ; and in that the first and second L-shaped ends form L-shaped junctions to attach the first and second outer jacket domes to the first and second cylindrical outer jackets .
A foam booster comprising a saccharide blend having: (a) 30 wt. % to 50 wt. % of an aldohexose or mixture of aldohexoses; (b) 20 wt. % to 55 wt. % of a ketohexose or mixture of ketohexoses; (c) 10 wt. % to 25 wt. % of a disaccharide or mixture of disaccharides; and (d) 5 wt. % to 20 wt. % of a high level saccharide or mixture of high level saccharides wherein the higher level polysaccharides comprise at least 4 monosaccharide units. (a) 30 wt. % to 50 wt. % of an aldohexose or mixture of aldohexoses; (b) 20 wt. % to 55 wt. % of a ketohexose or mixture of ketohexoses; (c) 10 wt. % to 25 wt. % of a disaccharide or mixture of disaccharides; and (d) 5 wt. % to 20 wt. % of a high level saccharide or mixture of high level saccharides wherein the higher level polysaccharides comprise at least 4 monosaccharide units.
An antibody that selectively binds to a complex comprising (i) trimeric TNFα and (ii) a compound selected from the group consisting of compounds - , or salts or solvates thereof: or wherein the antibody binds selectively to the trimer-compound complex compared with binding to the compound in the absence of the TNFα trimer and compared with binding to the TNFα trimer in the absence of the compound.
A method by a machine-type communication, MTC, terminal device for reporting channel state information corresponding to a communication link between the MTC terminal device and a base station operable in a wireless communications system, the method comprising receiving signals at the MTC terminal device, the signals having been transmitted from a base station of the wireless communication system via a wireless access interface, the wireless access interface providing a plurality of communications resource elements within a system bandwidth wherein the receiving includes receiving the signals from within a virtual carrier, the virtual carrier providing a subset of the plurality of communications resource elements within a narrowband bandwidth, which forms part of and is within the system bandwidth, measuring at the MTC terminal device one or more channel state parameters corresponding to the channel state in one or more of the communications resource elements of the virtual carrier; generating aggregate channel state information from at least one measured channel state parameter corresponding to the channel state of the communications resource elements of the virtual carrier, generating sub-band channel state information from at least one measured channel state parameter corresponding to the channel state of the communications resource elements within respective sub-band parts of the virtual carrier, each of the respective sub-band parts of the virtual carrier comprising a selection the communications resource elements of the virtual carrier, selecting a size of each of the respective sub-band parts of the virtual carrier, wherein the size of each of the respective sub-band parts of the virtual carrier is dependent upon radio propagation conditions, and transmitting to the base station an indication of the aggregate channel state information for the communications resource elements of the virtual carrier and the sub-band channel state information for each of the respective sub-band parts of the virtual carrier to the base station.
An adjusting device for furniture, in particular for adjusting table legs or backrests or slatted frames, comprising a first profile which is guided such that it can be displaced in the longitudinal direction on or in a second profile , wherein the first profile can be latched in different positions along the second profile via a latching means in order to be blocked in a loading direction, and is movable in an adjusting direction counter to the loading direction, wherein, when an end position in the adjusting direction has been reached, the latching means is rendered inactive and, for a restoring operation, the first profile can be moved in the loading direction as far as a starting position , at which the latching means is rendered active, wherein a spring is provided, said spring counteracting a movement of the first profile into the end position , and the latching means is rendered inactive only once the spring force has been overcome, characterized in that the first profile comprises a switching element on which a protruding pin is fixed and which is displaceable along a guide track on the second profile , wherein a linear guide is provided on one side of the guide track in a direction parallel to the longitudinal direction of the profiles and a multitude of curved latching recesses are provided on the opposite side, into which the pin of the switching element can be latched, whereby the switching element is pretensioned towards the opposite side during an adjusting operation, so that a latching occurs when the first profile is retracted into the second profile .