mhurhangee/patent-ind-claim-en huggingface dataset:
Method for producing a sandwich structure comprising a honeycomb core and at least one outer layer , with the following steps: - applying a powdered thermoplastic material to one side of the honeycomb core , - placing the outer layer onto the side of the honeycomb core that has been provided with the powdered thermoplastic material , - heating the honeycomb core provided with the outer layer until the thermoplastic material plastifies, and - pressing the honeycomb core and the outer layer in the or in a heated state to produce the sandwich structure , characterized in that - in a first method step, before applying the powdered thermoplastic material , a bonding agent is applied to the honeycomb core , - wherein water is used as the bonding agent, - wherein the bonding agent serves the purpose of temporarily fixing the powdered thermoplastic material on the honeycomb core until the outer layer is placed on, and the pressing of the honeycomb core is performed while heating, wherein - after the first method step, no heating and melting of the powdered thermoplastic material fixed on the honeycomb core takes place, and the outer layer is placed directly onto the side of the honeycomb core and then the heating of this arrangement is performed to a temperature at which the thermoplastic material plastifies. - applying a powdered thermoplastic material to one side of the honeycomb core , - placing the outer layer onto the side of the honeycomb core that has been provided with the powdered thermoplastic material , - heating the honeycomb core provided with the outer layer until the thermoplastic material plastifies, and - pressing the honeycomb core and the outer layer in the or in a heated state to produce the sandwich structure , characterized in that - in a first method step, before applying the powdered thermoplastic material , a bonding agent is applied to the honeycomb core , - wherein water is used as the bonding agent, - wherein the bonding agent serves the purpose of temporarily fixing the powdered thermoplastic material on the honeycomb core until the outer layer is placed on, and the pressing of the honeycomb core is performed while heating, wherein - after the first method step, no heating and melting of the powdered thermoplastic material fixed on the honeycomb core takes place, and the outer layer is placed directly onto the side of the honeycomb core and then the heating of this arrangement is performed to a temperature at which the thermoplastic material plastifies.
A method of evaluating a composite material containing a polymer and fibrous carbon nanostructures, comprising: a step (A) of heating the composite material in an inert gas atmosphere to remove a polymer component from the composite material and obtain a polymer-removed product; a step (B) of performing thermogravimetric analysis of the polymer-removed product in an oxygen-containing atmosphere to measure change over time of mass of the polymer-removed product; and a step (C) of evaluating a disentanglement state of the fibrous carbon nanostructures in the composite material from a relationship between mass change of the polymer-removed product and elapsed time obtained in the step (B). a step (A) of heating the composite material in an inert gas atmosphere to remove a polymer component from the composite material and obtain a polymer-removed product; a step (B) of performing thermogravimetric analysis of the polymer-removed product in an oxygen-containing atmosphere to measure change over time of mass of the polymer-removed product; and a step (C) of evaluating a disentanglement state of the fibrous carbon nanostructures in the composite material from a relationship between mass change of the polymer-removed product and elapsed time obtained in the step (B).
An engine inlet for efficient operation in both subsonic and supersonic flight, wherein the inlet has a caret inlet aperture and is rotatable about an off-body axis of rotation and thereby compression ramp angle and capture area are variable, further comprising a diffuser engaged to the inlet and wherein the inlet incorporates an inlet interface portion having an arc shape and the diffuser incorporates a diffuser interface portion having an arc shape, wherein either as a first alternative the inlet interface portion engages the diffuser interface portion during rotation of the inlet about the off-body axis whereby opposing surfaces of the inlet interface portion and the diffuser interface portion engage one another in a scrubbing relationship to maintain a seal, or wherein, as a second alternative, the engine inlet further comprises a plurality of scales (40a, b, c) having arc shapes relative to the off-body axis of rotation , the scales telescopically engaging one another in a scrubbing relationship to maintain a seal, a forward scale engaging the inlet interface portion and an aft scale engaging the diffuser interface portion in a scrubbing relationship to maintain a seal during rotation of the inlet.
An artificial satellite (100; 502; 1201) comprising: a satellite structure (804; 907; 1002; 1104; 1404); an onboard control system (504; 904; 1004; 1101) for controlling a plurality of satellite components; and a memory system (536; 700; 902; 1001; 1105; 1401), the memory system physically coupled to the satellite structure and independently powerable with respect to the onboard control system and thereby operable to at least receive and store information even when the onboard control system is in an OFF state, the memory system arranged (i) to communicatively couple with the onboard control system, and (ii) to store data which specifies one or more launch-specific parameters for configuring at least one of the satellite components, the onboard control system being adapted to operate in a transfer phase in response to the satellite separating from a payload dispenser, the onboard control system further adapted to autonomously control, while operating in the transfer phase, one or more aspects of the at least one satellite component at least partly based on the data. a satellite structure (804; 907; 1002; 1104; 1404); an onboard control system (504; 904; 1004; 1101) for controlling a plurality of satellite components; and a memory system (536; 700; 902; 1001; 1105; 1401), the memory system physically coupled to the satellite structure and independently powerable with respect to the onboard control system and thereby operable to at least receive and store information even when the onboard control system is in an OFF state, the memory system arranged (i) to communicatively couple with the onboard control system, and (ii) to store data which specifies one or more launch-specific parameters for configuring at least one of the satellite components, the onboard control system being adapted to operate in a transfer phase in response to the satellite separating from a payload dispenser, the onboard control system further adapted to autonomously control, while operating in the transfer phase, one or more aspects of the at least one satellite component at least partly based on the data.
A combine harvester comprising: - an axial flow crop processor with a rotor mounted for rotation inside a rotor housing arranged substantially longitudinally with respect to the harvester; - a feed beater mounted for rotation on a substantially transverse axis and serving to tangentially impel crop material into the crop processor; characterised in further comprising a multi-speed beater drive system comprising: - a beater shaft upon which the beater is mounted via bearings to permit relative rotational movement; - a secondary shaft arranged parallel to the beater shaft; - a first selectable drive path between the beater shaft and the beater; and, - a second, alternate, selectable drive path between the secondary shaft and the beater; - a grain cleaning shoe driven via a driveline which includes the secondary shaft ; - wherein both the beater shaft and the secondary shaft are driven simultaneously during operation. - an axial flow crop processor with a rotor mounted for rotation inside a rotor housing arranged substantially longitudinally with respect to the harvester; - a feed beater mounted for rotation on a substantially transverse axis and serving to tangentially impel crop material into the crop processor; characterised in further comprising a multi-speed beater drive system comprising: - a beater shaft upon which the beater is mounted via bearings to permit relative rotational movement; - a secondary shaft arranged parallel to the beater shaft; - a first selectable drive path between the beater shaft and the beater; and, - a second, alternate, selectable drive path between the secondary shaft and the beater; - a beater shaft upon which the beater is mounted via bearings to permit relative rotational movement; - a secondary shaft arranged parallel to the beater shaft; - a first selectable drive path between the beater shaft and the beater; and, - a second, alternate, selectable drive path between the secondary shaft and the beater; - a grain cleaning shoe driven via a driveline which includes the secondary shaft ; - wherein both the beater shaft and the secondary shaft are driven simultaneously during operation.
A fastener comprising: a connecting member having a first axis and an accommodating space extended along the first axis ; and a handling member having a second axis and movably disposed in the accommodating space of the connecting member , the handling member being movable between a first position and a second position, when located at the first position, the handling member being disposed in the accommodating space in a way that the second axis is approximately coaxial with the first axis of the connecting member , when located at the second position, the handling member being positioned on the connecting member in a way that an included angle is provided between the second axis and the first axis of the connecting member so that the handling member is capable of being rotated by an external force to drive the connecting member to rotate at a to-be fastened position; wherein the handling member has a limiting portion ; characterized in that the connecting member is integrally formed with a stopping portion located in the accommodating space ; the limiting portion is larger in size than an opening on a cross section of the accommodating space at the stopping portion so that the handling member is prevented from being separated from the connecting member . a connecting member having a first axis and an accommodating space extended along the first axis ; and a handling member having a second axis and movably disposed in the accommodating space of the connecting member , the handling member being movable between a first position and a second position, when located at the first position, the handling member being disposed in the accommodating space in a way that the second axis is approximately coaxial with the first axis of the connecting member , when located at the second position, the handling member being positioned on the connecting member in a way that an included angle is provided between the second axis and the first axis of the connecting member so that the handling member is capable of being rotated by an external force to drive the connecting member to rotate at a to-be fastened position; wherein the handling member has a limiting portion ; characterized in that the connecting member is integrally formed with a stopping portion located in the accommodating space ; the limiting portion is larger in size than an opening on a cross section of the accommodating space at the stopping portion so that the handling member is prevented from being separated from the connecting member .
Fastening arrangement having a metal sheet and having a cage nut , wherein the cage nut has a cage and a nut which is accommodated in a rotationally fixed manner in the cage , wherein the cage is fastened to the metal sheet in such a way that a screw can be screwed into the nut through an opening in the metal sheet , wherein the fastening arrangement has a fixing element which serves for fixing the position of the nut in the cage and by way of which the nut is subjected to a force directed in the direction of the metal sheet that pushes the nut against the metal sheet and/or against a reinforcement plate of the cage nut , characterized in that the fixing element has a sealing region for sealing off the internal thread of the nut . the fastening arrangement has a fixing element which serves for fixing the position of the nut in the cage and by way of which the nut is subjected to a force directed in the direction of the metal sheet that pushes the nut against the metal sheet and/or against a reinforcement plate of the cage nut , characterized in that the fixing element has a sealing region for sealing off the internal thread of the nut .
An in situ process for producing fructooligosaccharides in a food product, the process comprising, a) obtaining a food product containing sucrose and b) contacting the food product with the Aspergillus japonicus fructosyltransferase to enzymatically convert sucrose in the food product to fructooligosaccharides (FOSs); wherein (i) the sucrose content of the food product is reduced by at least 75% after 1 hour exposure to the fructosyltransferase as compared to a corresponding food product that has not been contacted with the fructosyltransferase but has otherwise been exposed to essentially the same conditions; or (ii) the sucrose content of the food product is reduced by at least 90% after 24 hrs exposure to the fructosyltransferase as compared to a corresponding food product that has not been contacted with the fructosyltransferase but has otherwise been exposed to essentially the same conditions. a) obtaining a food product containing sucrose and b) contacting the food product with the Aspergillus japonicus fructosyltransferase to enzymatically convert sucrose in the food product to fructooligosaccharides (FOSs); (i) the sucrose content of the food product is reduced by at least 75% after 1 hour exposure to the fructosyltransferase as compared to a corresponding food product that has not been contacted with the fructosyltransferase but has otherwise been exposed to essentially the same conditions; or (ii) the sucrose content of the food product is reduced by at least 90% after 24 hrs exposure to the fructosyltransferase as compared to a corresponding food product that has not been contacted with the fructosyltransferase but has otherwise been exposed to essentially the same conditions.
Method for preparing activated carbon , the method comprising the steps of - providing the starting material in the form of pure natural wood, wherein the composition of the starting material comprises 35-45% by weight of coniferous wood and 55-65% by weight of hardwood, - comminution of the starting material into pieces of maximum edge length of 45 mm, - drying of the starting material to a water content of maximum 20% by weight, - pyrolysis of the dried pieces of the starting material in a reactor under exclusion of oxygen to produce biochar, - quenching of the biochar after the pyrolysis by addition of water, wherein the pyrolysis is carried out in the temperature range of 720°C to 800°C and wherein the residence time in the reactor is at least 60 minutes, in particular wherein the residence time in the reactor is between 60 and 80 minutes, wherein, as last step , the biochar is grinded to a particle size of at most 3 mm, in particular less than 1 mm, wherein, in a further step , the ground biochar is oxidically activated in a fluidized bed reactor. - providing the starting material in the form of pure natural wood, wherein the composition of the starting material comprises 35-45% by weight of coniferous wood and 55-65% by weight of hardwood, - comminution of the starting material into pieces of maximum edge length of 45 mm, - drying of the starting material to a water content of maximum 20% by weight, - pyrolysis of the dried pieces of the starting material in a reactor under exclusion of oxygen to produce biochar, - quenching of the biochar after the pyrolysis by addition of water,
A method for preparing a positive electrode material having a general formula Li i+a' M i-a' O 2 , with M= (Ni z (Ni 1⁄2 Mn 1⁄2 ) y Co x ) 1-k A k , wherein x+y+z=1, 0.1≤x≤0.4, 0.30≤z≤0.55, A is a dopant, 0≤k≤0.1, and 0.01≤a'≤0.10, comprising the steps of: - providing a M-based precursor prepared from the co-precipitation of metal sulphates with a base; - mixing the M-based precursor with Li 2 CO 3 , thereby obtaining a first mixture, whereby the Li to transition metal ratio in the first mixture is between 0.50 and 0.90, - sintering the first mixture in an oxidizing atmosphere at a temperature between 860 and 930°C, for a time between 8 and 36 hrs, thereby obtaining a lithium deficient precursor powder, - mixing the lithium deficient precursor powder with either one of LiOH and LiOH.H 2 O, thereby obtaining a second mixture, - sintering the second mixture in an oxidizing atmosphere at a temperature between 800 and 1000°C, for a time between 6 and 36 hrs. - providing a M-based precursor prepared from the co-precipitation of metal sulphates with a base; - mixing the M-based precursor with Li 2 CO 3 , thereby obtaining a first mixture, whereby the Li to transition metal ratio in the first mixture is between 0.50 and 0.90, - sintering the first mixture in an oxidizing atmosphere at a temperature between 860 and 930°C, for a time between 8 and 36 hrs, thereby obtaining a lithium deficient precursor powder, - mixing the lithium deficient precursor powder with either one of LiOH and LiOH.H 2 O, thereby obtaining a second mixture, - sintering the second mixture in an oxidizing atmosphere at a temperature between 800 and 1000°C, for a time between 6 and 36 hrs.
A method for manufacturing a laminated film comprising: a step of forming an uncured hard coat layer by applying an active energy-ray curable composition for forming a hard coat layer to one side of a first support substrate having a thickness of 50 μm or more and 600 μm or less, and then drying the composition; a step of forming an uncured optical interference layer by applying an active energy-ray curable composition for forming a optical interference layer on one surface of a second support substrate so that the thickness of the uncured optical interference layer is between 15 nm or more and 200 nm or less, and then drying the composition; and a lamination step of laminating a surface of the uncured hard coat layer opposite the first support substrate and a surface of the uncured optical interference layer opposite the second support substrate to obtain a laminated film, wherein a stretch ratio of the laminated film at 160°C is 50% or more, characterised in that a surface tension γ2 of the one surface of the second support substrate, a surface tension γL 1 of the uncured optical interference layer, and a surface tension γH 1 of the uncured hard coat layer satisfy relationships of the following formulas 1 and 2: y 2 ≤ yL 1 y 2 − yL 1 > yH 1 − yL 1 . a step of forming an uncured hard coat layer by applying an active energy-ray curable composition for forming a hard coat layer to one side of a first support substrate having a thickness of 50 μm or more and 600 μm or less, and then drying the composition; a step of forming an uncured optical interference layer by applying an active energy-ray curable composition for forming a optical interference layer on one surface of a second support substrate so that the thickness of the uncured optical interference layer is between 15 nm or more and 200 nm or less, and then drying the composition; and a lamination step of laminating a surface of the uncured hard coat layer opposite the first support substrate and a surface of the uncured optical interference layer opposite the second support substrate to obtain a laminated film, wherein a stretch ratio of the laminated film at 160°C is 50% or more, characterised in that a surface tension γ2 of the one surface of the second support substrate, a surface tension γL 1 of the uncured optical interference layer, and a surface tension γH 1 of the uncured hard coat layer satisfy relationships of the following formulas 1 and 2: y 2 ≤ yL 1 y 2 − yL 1 > yH 1 − yL 1 .
A system on a chip integrated circuit, SoC, including: an active base die including a first cache memory (412A-F); a first die mounted on and coupled with the active base die, the first die including an interconnect fabric, an input/output interface, and an atomic operation handler; and a second die mounted on the active base die and coupled with the active base die and the first die , the second die including an array of graphics processing elements and an interface to the first cache memory of the active base die, wherein at least one of the graphics processing elements are configured to perform, via the atomic operation handler, an atomic operation to a memory device ; wherein the first die includes media engine configured to perform an atomic operation to the memory device ; the memory device is coupled with the second die via the first die ; the memory device is coupled with a host processor and accessible via the input/output interface; the SoC further comprising a second cache memory to cache data associated with the atomic operation performed to the memory device, the second cache memory is associated with a burst buffer cache that is configured to be enabled when a rate of incoming atomic requests exceeds a burst rate threshold. an active base die including a first cache memory (412A-F); a first die mounted on and coupled with the active base die, the first die including an interconnect fabric, an input/output interface, and an atomic operation handler; and a second die mounted on the active base die and coupled with the active base die and the first die , the second die including an array of graphics processing elements and an interface to the first cache memory of the active base die, wherein at least one of the graphics processing elements are configured to perform, via the atomic operation handler, an atomic operation to a memory device ; the first die includes media engine configured to perform an atomic operation to the memory device ; the memory device is coupled with the second die via the first die ; the memory device is coupled with a host processor and accessible via the input/output interface; the SoC further comprising a second cache memory to cache data associated with the atomic operation performed to the memory device, the second cache memory is associated with a burst buffer cache that is configured to be enabled when a rate of incoming atomic requests exceeds a burst rate threshold.
An assembly comprising at least two devices and a floating device having a work deck for connecting a hollow tubular structure in erected state to the work deck , which hollow tubular structure extends in a longitudinal direction and defines a radial direction running perpendicularly of a peripheral wall of the hollow tubular structure , each device comprising two clamping parts , a guide configured to run in the installed state in the radial direction of the hollow tubular structure when the hollow tubular structure is connected to the work deck , and the guide is further configured to connect the clamping parts to the work deck , and each device further comprising clamping means for shifting the clamping parts toward each other over the guide in the radial direction from an open position into a clamping position, in which a wall part of the structure is clamped between the clamping parts , wherein in the clamping position the clamping parts can collectively be moved freely over the guide in the radial direction , wherein the at least two devices of the assembly are connected on the work deck of the floating device along the periphery of a cross-section of the hollow tubular structure when the hollow tubular structure is connected to the work deck , which allows clamping wall parts of the same hollow tubular structure in erected state in the radial direction , and the assembly further comprises support elements supported by the work deck for supporting a lower edge of the tubular structure .