mhurhangee/patent-ind-claim-en huggingface dataset:
An air-cooled engine unit comprising: an engine main body forming at least one combustion chamber ; a fin portion configured to dissipate heat generated in the engine main body from a surface of the engine main body ; an exhaust passage member connecting an exhaust port provided through the combustion chamber with an atmosphere discharge port through which exhaust gas is discharged to the atmosphere, the exhaust gas flowing inside the exhaust passage member from the exhaust port to the atmosphere discharge port ; a catalyst provided in the exhaust passage member , and a compression ratio of the engine main body including the fin portion that is 10 or higher, the air-cooled engine unit being characterized in that the catalyst is a close-to-combustion-chamber catalyst which is disposed so that a path length of a first portion of the exhaust passage member is shorter than a path length of a second portion of the exhaust passage member , the first portion of the exhaust passage member being from the exhaust port to an upstream end of the close-to-combustion-chamber catalyst , the second portion of the exhaust passage member being from a downstream end of the close-to-combustion-chamber catalyst to the atmosphere discharge port . an engine main body forming at least one combustion chamber ; a fin portion configured to dissipate heat generated in the engine main body from a surface of the engine main body ; an exhaust passage member connecting an exhaust port provided through the combustion chamber with an atmosphere discharge port through which exhaust gas is discharged to the atmosphere, the exhaust gas flowing inside the exhaust passage member from the exhaust port to the atmosphere discharge port ; a catalyst provided in the exhaust passage member , and a compression ratio of the engine main body including the fin portion that is 10 or higher, the air-cooled engine unit being characterized in that the catalyst is a close-to-combustion-chamber catalyst which is disposed so that a path length of a first portion of the exhaust passage member is shorter than a path length of a second portion of the exhaust passage member , the first portion of the exhaust passage member being from the exhaust port to an upstream end of the close-to-combustion-chamber catalyst , the second portion of the exhaust passage member being from a downstream end of the close-to-combustion-chamber catalyst to the atmosphere discharge port .
An electric motor with a rotor and stator, wherein the rotor has a rotor shaft on which a laminated rotor core is placed and is connected in rotation-resistant manner to the rotor shaft , wherein the laminated rotor core has rotor segments which are stacked on one another in the axial direction and a centring disc and also a press connection means, wherein the stack formed from the rotor segments is arranged between the centring disc and the press connection means, wherein to produce a press connection of the rotor shaft with a hollow shaft which is to be driven the press connection means can be actuated by means of one or more of the clamping screws , wherein the clamping screws are passed through cutouts in the rotor segments and in the centring disc , wherein the stack can be clamped between the centring disc and the press connection means by means of the clamping screws , wherein the head of a respective clamping screw presses the centring disc onto the stack, wherein the press connection means has a shrink disc and two pressing rings , wherein the shrink disc has on its radially outer surface two conical portions which run in opposite directions, wherein the clamping screws are screw-connected at least to that pressing ring which is arranged axially further removed from the rotor segments , wherein the shrink disc together with the pressing rings is connected non-detachably to the rotor by means of the clamping screws , wherein by means of the screwing-in of the clamping screws the two pressing rings (8 and 9) which are placed on the shrink disc by axially approaching press the shrink disc onto the hollow shaft , so that the hollow shaft is shrunk onto the rotor shaft , wherein the screwing-in of the clamping screws is carried out from the centring-disc side.
A component arrangement for installation on an aircraft structure , in particular on a fuselage structure of an aircraft , with at least one mounting structure able to be connected with the aircraft structure , and at least one component assigned to the aircraft structure , in particular a measuring device, wherein the mounting structure is Z able to be connected with an inner surface of the aircraft structure , wherein at least one component carrier for the reception of the component to be mounted is provided, wherein the component carrier can be connected with the mounting structure , and an outer surface of the component carrier , facing away from the component , extends in use approximately flush with an outer surface of the aircraft structure , wherein the component carrier is provided as an aerodynamic plate, and the installation of the component takes place directly on the aerodynamic plate, wherein the component carrier is approximately cup-shaped in design, and wherein the component carrier can be inserted into a receptacle of the approximately ring-shaped mounting structure, and wherein the assembly takes place from an inner side, wherein a supporting surface of the component carrier is brought into abutment against a seating face of the mounting structure. wherein the mounting structure is Z able to be connected with an inner surface of the aircraft structure , wherein at least one component carrier for the reception of the component to be mounted is provided, wherein the component carrier can be connected with the mounting structure , and an outer surface of the component carrier , facing away from the component , extends in use approximately flush with an outer surface of the aircraft structure , wherein the component carrier is provided as an aerodynamic plate, and the installation of the component takes place directly on the aerodynamic plate, wherein the component carrier is approximately cup-shaped in design, and wherein the component carrier can be inserted into a receptacle of the approximately ring-shaped mounting structure, and wherein the assembly takes place from an inner side, wherein a supporting surface of the component carrier is brought into abutment against a seating face of the mounting structure.
A method for predicting the break-up possibility of a synthetic resin filament in a melt blowing process, comprising the steps of: applying 200 % strain to a synthetic resin sample at 235 °C, and then measuring a change in residual stress with passage of time; and confirming whether or not the change in residual stress fulfills the following Mathematical Formula 1. RS 1 / RS 0 * 100 ≤ 0.04 In Mathematical Formula 1, RS 0 is residual stress at one time point (t 0 ) of less than 0.05 seconds after applying 200 % strain to the synthetic resin sample at 235 °C, and RS 1 is residual stress at one time point (t 1 ) between 0.05 seconds and 1.50 seconds after applying 200 % strain to the synthetic resin sample at 235 °C. applying 200 % strain to a synthetic resin sample at 235 °C, and then measuring a change in residual stress with passage of time; and confirming whether or not the change in residual stress fulfills the following Mathematical Formula 1. RS 1 / RS 0 * 100 ≤ 0.04 In Mathematical Formula 1, RS 0 is residual stress at one time point (t 0 ) of less than 0.05 seconds after applying 200 % strain to the synthetic resin sample at 235 °C, and RS 1 is residual stress at one time point (t 1 ) between 0.05 seconds and 1.50 seconds after applying 200 % strain to the synthetic resin sample at 235 °C. RS 0 is residual stress at one time point (t 0 ) of less than 0.05 seconds after applying 200 % strain to the synthetic resin sample at 235 °C, and RS 1 is residual stress at one time point (t 1 ) between 0.05 seconds and 1.50 seconds after applying 200 % strain to the synthetic resin sample at 235 °C.
Use of fibrosis inhibitor for the normalization of culture of corneal endothelial cells, wherein said fibrosis inhibitor comprises a transforming growth factor (TGF) β signal inhibiting agent.
A surgical bur comprising: a plurality of flutes , wherein each of the plurality of flutes comprises a cutting edge , a plurality of rake surfaces and a clearance surface , wherein the plurality of rake surfaces of one of the plurality of flutes are decoupled from each other; and a plurality of lands , each of the plurality of lands is disposed between a pair of the plurality of flutes. a plurality of flutes , wherein each of the plurality of flutes comprises a cutting edge , a plurality of rake surfaces and a clearance surface , wherein the plurality of rake surfaces of one of the plurality of flutes are decoupled from each other; and a plurality of lands , each of the plurality of lands is disposed between a pair of the plurality of flutes.
Tyre comprising a rubber composition comprising a substituted diene elastomer, characterized in that the said substituted diene elastomer comprises units bearing an A-B radical, in which: - A represents an aliphatic C 3 -C 35 radical which can be interrupted by one or more heteroatom(s) - B represents a linear, branched or cyclic C 1 -C 6 hydrocarbon radical A and B are such that the melting point of the analogue, H-A-B, is less than 70°C and the substituted diene elastomer comprises from 10% to 40% by weight of the said A-B radical, with respect to the total weight of the elastomer. - A represents an aliphatic C 3 -C 35 radical which can be interrupted by one or more heteroatom(s) - B represents a linear, branched or cyclic C 1 -C 6 hydrocarbon radical
Bitumen which is solid at ambient temperature, in the form of granules comprising a core and a coating layer obtained by applying a composition comprising at least one viscosifying compound and at least one anti-agglomerating compound to all or part of the surface of the core, in which: - the core comprises at least one bitumen base, and - the coating layer comprises at least 10% by weight of viscosifying compounds relative to the total weight of the coating layer, and at least one anti-agglomerating compound. - the core comprises at least one bitumen base, and - the coating layer comprises at least 10% by weight of viscosifying compounds relative to the total weight of the coating layer, and at least one anti-agglomerating compound.
A method for improving mixing of content in a container provided in a filter system , said container being a flexible, disposable bag, being devoid of an impeller and being connected to a filter by a recirculation flow path , said method comprising providing a mixing loop to the container , said mixing loop being provided in parallel with the recirculation flow path of the filter system .
A knotter system for performing a knotter cycle of a baler, said knotter cycle comprising at least a first knot forming cycle and a second knot forming cycle, said knotter system comprising: a needle configured for delivering a needle twine; a tucker arm configured for delivering a tucker twine; a billhook assembly comprising a billhook with a lower lip and an upper lip mounted pivotally with respect to lower lip , said billhook being mounted rotatably around a rotation axis ; a drive means adapted to make the billhook perform at least a first full rotation around its rotation axis during the first knot forming cycle and a second full rotation around its rotation axis during the second knot forming cycle, the billhook assembly is configured to move the upper lip away from the lower lip in a first angular range and to move the upper lip away from the lower lip in a second angular range of at least one of the first and second full rotation, characterized in that the first angular range is located within a range between 0° and 160°, and the second angular range is located within a range between 160° and 360°, and in that the billhook assembly comprises a cam surface , and wherein the billhook is provided with a cam follower in contact with the cam surface , wherein the cam surface is provided with a first and a second cam configured for pushing the upper lip away from the lower lip , in the first angular range and in the second angular range, respectively, during said first full rotation and during said second full rotation. a needle configured for delivering a needle twine; a tucker arm configured for delivering a tucker twine; a billhook assembly comprising a billhook with a lower lip and an upper lip mounted pivotally with respect to lower lip , said billhook being mounted rotatably around a rotation axis ; a drive means adapted to make the billhook perform at least a first full rotation around its rotation axis during the first knot forming cycle and a second full rotation around its rotation axis during the second knot forming cycle, the billhook assembly is configured to move the upper lip away from the lower lip in a first angular range and to move the upper lip away from the lower lip in a second angular range of at least one of the first and second full rotation, characterized in that the first angular range is located within a range between 0° and 160°, and the second angular range is located within a range between 160° and 360°, and in that the billhook assembly comprises a cam surface , and wherein the billhook is provided with a cam follower in contact with the cam surface , wherein the cam surface is provided with a first and a second cam configured for pushing the upper lip away from the lower lip , in the first angular range and in the second angular range, respectively, during said first full rotation and during said second full rotation.
A method for producing phenyl (meth)acrylate through reaction of (meth)acrylic acid and diphenyl carbonate, wherein no solvent is used and the reaction temperature is set in a range of 80 °C to 160 °C, wherein (meth)acrylic acid and diphenyl carbonate are reacted in the presence of a catalyst, wherein the catalyst is at least one type selected from among nitrogen-containing organic compounds, Group 1 metal compounds, Group 2 metal compounds, and metal trifluoromethanesulfonates.
A stabilized formulation of ADAMTS13, comprising less than 100 mM of a pharmaceutically acceptable salt.
A method for setting frame rates of a camera , wherein the camera comprises a plurality of image sensors (116a:116K) arranged to capture images to be stitched into a panorama image of a scene , and wherein each of the plurality of image sensors (116a:116K) has a respective optical axis (210a:210K), the method being performed by a controller , the method comprising: obtaining (S106) information of a respective angle ( α k;k =1... K ) between the optical axis (210a:210K) of each of the plurality of image sensors (116a:116K) and a direction (D) along which a straight path structure , to be monitored by the camera , extends through the scene ; dividing (S108) the plurality of image sensors (116a:116K) into at least two groups (820a:820d) as a function of the angles ( α k;k =1... K ), wherein all the angles ( α k;k =1... K ) of the image sensors (116a:116K) within each of the at least two groups (820a:820d) are part of its own continuous angle interval (810a:810e); and setting (S110) one frame rate per each of the at least two groups (820a:820d), wherein the frame rate is decreasing from the group with highest continuous angle interval towards the group with lowest continuous angle interval . obtaining (S106) information of a respective angle ( α k;k =1... K ) between the optical axis (210a:210K) of each of the plurality of image sensors (116a:116K) and a direction (D) along which a straight path structure , to be monitored by the camera , extends through the scene ; dividing (S108) the plurality of image sensors (116a:116K) into at least two groups (820a:820d) as a function of the angles ( α k;k =1... K ), wherein all the angles ( α k;k =1... K ) of the image sensors (116a:116K) within each of the at least two groups (820a:820d) are part of its own continuous angle interval (810a:810e); and setting (S110) one frame rate per each of the at least two groups (820a:820d), wherein the frame rate is decreasing from the group with highest continuous angle interval towards the group with lowest continuous angle interval .
A vascular access device, the device comprising: a needle section comprising a hollow needle (180; 144) and a proximal fitting portion , the hollow needle having a sharpened distal tip and defining at least one lateral opening (182; 149) proximal to the distal tip; a dilator section comprising a dilator (184; 152) and a hub , the dilator being coaxially mounted on the needle forming a space (194; 170) between the needle and the dilator and arranged so that blood flowing in the needle (180; 144) flows into the space (194; 170) through the at least one lateral opening ( 182; 149); a sheath section comprising a proximal section and a sheath (196; 162) coaxially mounted on the dilator (184; 152) forming a second space between the dilator (184; 152) and the sheath (196; 162), the dilator being provided with an opening or spaces arranged so that blood flowing in the needle (180; 144) and then through the at least one lateral opening (182; 149) flows into the second space ; and one or more small openings, pores or spots of porous material on the dilator, or a porous vent on the dilator hub , to allow air or gas to escape from the space (194; 170) or the second space yet retain blood; wherein the dilator (184; 152) or the sheath (196; 162) is clear, semi-opaque, or translucent, so that when blood flows into needle (180; 144) and then through the lateral opening (182 149) into the space (194; 170) or the second space it may be seen to indicate that the distal tip of the needle (180; 144) has punctured a blood vessel. a needle section comprising a hollow needle (180; 144) and a proximal fitting portion , the hollow needle having a sharpened distal tip and defining at least one lateral opening (182; 149) proximal to the distal tip; a dilator section comprising a dilator (184; 152) and a hub , the dilator being coaxially mounted on the needle forming a space (194; 170) between the needle and the dilator and arranged so that blood flowing in the needle (180; 144) flows into the space (194; 170) through the at least one lateral opening ( 182; 149); a sheath section comprising a proximal section and a sheath (196; 162) coaxially mounted on the dilator (184; 152) forming a second space between the dilator (184; 152) and the sheath (196; 162), the dilator being provided with an opening or spaces arranged so that blood flowing in the needle (180; 144) and then through the at least one lateral opening (182; 149) flows into the second space ; and one or more small openings, pores or spots of porous material on the dilator, or a porous vent on the dilator hub , to allow air or gas to escape from the space (194; 170) or the second space yet retain blood; wherein the dilator (184; 152) or the sheath (196; 162) is clear, semi-opaque, or translucent, so that when blood flows into needle (180; 144) and then through the lateral opening (182 149) into the space (194; 170) or the second space it may be seen to indicate that the distal tip of the needle (180; 144) has punctured a blood vessel.
A method performed by an access point, AP, for downlink transmission in a beamforming radio communication network, the method comprising: grouping a plurality of terminal devices to be scheduled for the downlink transmission into one or more groups; characterized by : determining a priority for each of the plurality of terminal devices at least based on a type of payload to be transmitted to each of the plurality of terminal devices, wherein the grouping comprises grouping the plurality of terminal devices in a descending order of the priority; and associating each of the one or more groups with a different one of digital chains in the AP, each digital chain comprising a digital-to-analogue converter, wherein payloads, to be transmitted to terminal devices in a same group, are processed by a digital chain associated with the same group. determining a priority for each of the plurality of terminal devices at least based on a type of payload to be transmitted to each of the plurality of terminal devices, wherein the grouping comprises grouping the plurality of terminal devices in a descending order of the priority; and associating each of the one or more groups with a different one of digital chains in the AP, each digital chain comprising a digital-to-analogue converter, wherein payloads, to be transmitted to terminal devices in a same group, are processed by a digital chain associated with the same group.
A nickel-based superalloy with high γ' phase content, intended for the manufacture of components by additive manufacturing followed by heat treatment, characterized in that its composition comprises, advantageously consists essentially of, in percentages by weight of the total composition: chromium: 15.5 - 16.5; cobalt: 7.7 - 11, advantageously 7.7 - 9; molybdenum and tungsten such that the molybdenum + tungsten content = 5.5 - 7.5, advantageously 6.2 - 7.5; aluminum: 2.9 - 4.3, advantageously 3 - 4; titanium: 2.6 - 3.2, advantageously 2.6 - 3.1; tantalum: 1.5 - 2.2; niobium: 0.3 - 1.1, advantageously 0.3 - 0.5; carbon: 0.01 - 0.13, advantageously 0.01 - 0.07; boron: 0.0005 - 0.015; zirconium: ≤ 0.01, advantageously ≤ 0.009; hafnium: 0.0001 - 0.5, advantageously 0.0001 - 0.2; silicon: ≤ 0.06, advantageously ≤ 0.03; nickel: balance and also the unavoidable impurities. chromium: 15.5 - 16.5; cobalt: 7.7 - 11, advantageously 7.7 - 9; molybdenum and tungsten such that the molybdenum + tungsten content = 5.5 - 7.5, advantageously 6.2 - 7.5; aluminum: 2.9 - 4.3, advantageously 3 - 4; titanium: 2.6 - 3.2, advantageously 2.6 - 3.1; tantalum: 1.5 - 2.2; niobium: 0.3 - 1.1, advantageously 0.3 - 0.5; carbon: 0.01 - 0.13, advantageously 0.01 - 0.07; boron: 0.0005 - 0.015; zirconium: ≤ 0.01, advantageously ≤ 0.009; hafnium: 0.0001 - 0.5, advantageously 0.0001 - 0.2; silicon: ≤ 0.06, advantageously ≤ 0.03; nickel: balance and also the unavoidable impurities.
A method for molding a fiber-reinforced composite structure, the method comprising: dropping chopped fiber composite pieces into a mold ; detecting characteristics of individual chopped fiber composite pieces as they drop; directing individual ones of the chopped fiber composite pieces into a predetermined region of the mold based on one or more detected characteristics of respective individual ones of the chopped fiber composite pieces as they drop and/or altering orientations of individual ones of the chopped fiber composite pieces based on one or more detected characteristics of respective individual ones of the chopped fiber composite pieces as they drop; compressing the chopped fiber composite pieces within the mold; and curing the compressed chopped fiber composite pieces to define the fiber-reinforced composite structure. dropping chopped fiber composite pieces into a mold ; detecting characteristics of individual chopped fiber composite pieces as they drop; directing individual ones of the chopped fiber composite pieces into a predetermined region of the mold based on one or more detected characteristics of respective individual ones of the chopped fiber composite pieces as they drop and/or altering orientations of individual ones of the chopped fiber composite pieces based on one or more detected characteristics of respective individual ones of the chopped fiber composite pieces as they drop; compressing the chopped fiber composite pieces within the mold; and curing the compressed chopped fiber composite pieces to define the fiber-reinforced composite structure.