mhurhangee/patent-ind-claim-en huggingface dataset:
Capillary pumped heat pipe with reentering grooves extending at least along a first longitudinal direction (X), comprising a first longitudinal end intended to be heated and a second longitudinal end intended to be cooled, a sealed enclosure extending between the first end and the second end , the enclosure comprising a stack of plates along a second direction (Z), said stack comprising two closure plates , at least one module with at least two intermediate plates between the closure plates , the heat pipe being characterised in that said intermediate plates include at least one first intermediate plate including at least one central window the edges of which partially define a vapour channel extending along the first direction (X), in which the vapour is intended to circulate, and on each side of the at least one central window in a third direction (Y) orthogonal to the first (X) and the second (Z) directions, a structure, the edges of which partially define a liquid channel, at least one other intermediate plate having at least one window, the edges of which partially define the vapour channel , and wherein the heat pipe includes at least two exchange zones (10.1, 110.1, 310.1) defined between the at least one intermediate plate and the at least one other intermediate plate, linking the vapour channel and the liquid channel.
An apparatus implementing an access node, comprising at least one processor and at least one memory , said at least one memory stored with computer program code thereon, the at least one memory and the computer program code configured to, with the at least one processor, cause the apparatus at least to perform: receive requests from a plurality of master nodes to be added as a secondary node as part of a conditional handover process for a user equipment; obtain , from each of said requests, an identification of the user equipment involved in the conditional handover process characterized in that the identification of the user equipment is unique among said master nodes, and that said at least one memory stored with computer program code thereon, the at least one memory and the computer program code configured to, with the at least one processor, cause the apparatus to determine , based on said identifications of the user equipment, that a plurality of said requests concern the same user equipment. receive requests from a plurality of master nodes to be added as a secondary node as part of a conditional handover process for a user equipment; obtain , from each of said requests, an identification of the user equipment involved in the conditional handover process characterized in that the identification of the user equipment is unique among said master nodes, and that said at least one memory stored with computer program code thereon, the at least one memory and the computer program code configured to, with the at least one processor, cause the apparatus to determine , based on said identifications of the user equipment, that a plurality of said requests concern the same user equipment.
Method for obtaining and storing the optimal operating points of a generator set comprising a heat engine coupled to an electric generator , wherein the generator set has a plurality of possible operating points, each operating point comprising an angular speed of the heat engine , a torque of the electric generator and an output power of the generator set , comprising the following steps: - obtaining all the possible combinations of angular speed of the heat engine and torque of the electric generator for each output power of the generator set , - calculating the efficiency of the generator set in each of said combinations of angular speed of the heat engine and torque of the electric generator taking into account the efficiency of the heat engine and the efficiency of the electric generator at each of said possible operating points of the generator set and characterized by the following steps: - selecting the optimum combination of angular speed of the heat engine and torque of the electric generator for each output power of the generator set such that the efficiency of the generator set at each of the selected operating points is maximum, calculating said efficiency as the sum of the efficiency of the generator set calculated in the preceding step for each possible operating point of the generator set , and the efficiency of the transition to the angular speed of the heat engine at said operating point from the angular speed of the heat engine at the operating point previously selected for the immediately preceding power of said generator set , and - storing said optimum combination of angular speed of the heat engine and torque of the electric generator for each output power of the generator set in data storage means. - obtaining all the possible combinations of angular speed of the heat engine and torque of the electric generator for each output power of the generator set , - calculating the efficiency of the generator set in each of said combinations of angular speed of the heat engine and torque of the electric generator taking into account the efficiency of the heat engine and the efficiency of the electric generator at each of said possible operating points of the generator set - selecting the optimum combination of angular speed of the heat engine and torque of the electric generator for each output power of the generator set such that the efficiency of the generator set at each of the selected operating points is maximum, calculating said efficiency as the sum of the efficiency of the generator set calculated in the preceding step for each possible operating point of the generator set , and the efficiency of the transition to the angular speed of the heat engine at said operating point from the angular speed of the heat engine at the operating point previously selected for the immediately preceding power of said generator set , and - storing said optimum combination of angular speed of the heat engine and torque of the electric generator for each output power of the generator set in data storage means.
A non-aqueous electrolyte for lithium ion battery, comprising a non-aqueous organic solvent, a lithium salt; characterized in that : the non-aqueous electrolyte for lithium ion battery further comprises a compound A represented by formula I and a compound B represented by formula II, in formula I, R 0 is C2-C4 alkylene or alkenylene, or C2-C4 fluoroalkylene or fluoroalkenylene; in formula II, R 1 , R 2 , R 3 , R 4 , R 5 and R 6 are each independently selected from one of hydrogen atom, fluorine atom and C1-C5 hydrocarbon group; wherein the percentage mass content of the compound A is 0.1-3% based on the total mass of the non-aqueous electrolyte for lithium ion battery being 100%; wherein the percentage mass content of the compound B is 0.1-5% based on the total mass of the non-aqueous electrolyte for lithium ion battery being 100%. the non-aqueous electrolyte for lithium ion battery further comprises a compound A represented by formula I and a compound B represented by formula II, in formula I, R 0 is C2-C4 alkylene or alkenylene, or C2-C4 fluoroalkylene or fluoroalkenylene; in formula II, R 1 , R 2 , R 3 , R 4 , R 5 and R 6 are each independently selected from one of hydrogen atom, fluorine atom and C1-C5 hydrocarbon group; wherein the percentage mass content of the compound A is 0.1-3% based on the total mass of the non-aqueous electrolyte for lithium ion battery being 100%; wherein the percentage mass content of the compound B is 0.1-5% based on the total mass of the non-aqueous electrolyte for lithium ion battery being 100%.
Method for determining a degree to which a bag has peeled away from the inner face of the wall of a container , a volume by which the bag can be collapsed and/or a corresponding parameter, the container comprising an extraction opening and a ventilation opening , an interior space of the container comprising an extraction side associated with the extraction opening and a ventilation side associated with the ventilation opening , which sides are separated from one another by the bag , characterized in that a pressure storage volume is brought to a target pressure and is subsequently connected to the ventilation side such that the pressure between the pressure storage volume and the ventilation side is equalized, and wherein the resultant pressure after the pressure equalization being measured as a parameter or to determine either the degree of peeling or the volume.
A method for applying a non-stick coating onto an article, wherein the non-stick coating comprises at least one adhesion-promoting layer (V) arranged on a surface of the article and a covering layer (D) arranged above the adhesion-promoting layer, wherein the adhesion-promoting layer has a dry film thickness of 5 to 25 μm, and wherein the covering layer has a dry film thickness of 10 to 65 μm, wherein the covering layer contains, related to the total solid material content of the covering layer, 95 to 100 wt.-% PTFE and optionally up to 5 wt.-% pigments, and is free of melt-processable fluoropolymers, and that the PTFE contained therein contains between 1 and 100 wt.-% of a high molecular weight modified PTFE, which contains < 1 wt.-% of perfluoropropylvinyl ether (PPVE) as a modifying comonomer and was obtained by emulsion polymerization, wherein the adhesion-promoting layer to be formed is applied on the surface of the article in liquid form as a first aqueous dispersion and then dried for 5 to 15 minutes at 60 to 110°C, and wherein subsequently the covering layer is applied on the pre-dried adhesion-promoting layer as a second aqueous dispersion and the layers are bonded to each other and with the surface of the article by subsequent drying and sintering or melting at 410 to 430°C, characterized in that the second aqueous dispersion is free of melt-processable fluoropolymers and free of low molecular weight PTFE.
A ram air turbine comprising: a turbine comprising a blade ; a strut removably coupled to the turbine and comprising a drive section , a gearbox section , and a generator adapter section , wherein the gearbox section comprises a turbine shaft and a bevel gear ; a generator positioned within the generator adapter section of the strut and comprising a turbine side , wherein an exciter is positioned at the turbine side of the generator , and wherein a permanent magnet generator is located at least partially within a stator of the exciter , and a driveshaft having a pinion gear that engages the bevel gear , wherein the driveshaft is removably coupled to the generator ; wherein the strut comprises a cone positioned between the drive section and the generator adapter section , and wherein the permanent magnet generator and the exciter are positioned within the cone of the strut . a turbine comprising a blade ; a strut removably coupled to the turbine and comprising a drive section , a gearbox section , and a generator adapter section , wherein the gearbox section comprises a turbine shaft and a bevel gear ; a generator positioned within the generator adapter section of the strut and comprising a turbine side , wherein an exciter is positioned at the turbine side of the generator , and wherein a permanent magnet generator is located at least partially within a stator of the exciter , and a driveshaft having a pinion gear that engages the bevel gear , wherein the driveshaft is removably coupled to the generator ; wherein the strut comprises a cone positioned between the drive section and the generator adapter section , and wherein the permanent magnet generator and the exciter are positioned within the cone of the strut .
A reciprocating mower unit configured to be driven by a drive unit via a transmission shaft arranged within a transmission tube , the reciprocating mower unit comprising: a housing ; a reduction gear arranged within the housing , the reduction gear being configured to receive an input rotary motion from the transmission shaft at a first, relatively higher, rotation speed, and deliver an output rotary motion to a gear output shaft at a second, relatively lower, rotation speed; and a crank mechanism arranged within the housing, the crank mechanism being configured to convert the output rotary motion of the gear output shaft to an oscillating motion of a pair of mowing blades oscillating in mutual anti-phase about a common oscillation axis (A1), wherein the reciprocating mower unit is characterized in comprising an input shaft for receiving said input rotary motion from the transmission shaft , wherein the input shaft is provided with a coupling interface for releasably coupling the input shaft to the transmission shaft . a housing ; a reduction gear arranged within the housing , the reduction gear being configured to receive an input rotary motion from the transmission shaft at a first, relatively higher, rotation speed, and deliver an output rotary motion to a gear output shaft at a second, relatively lower, rotation speed; and a crank mechanism arranged within the housing, the crank mechanism being configured to convert the output rotary motion of the gear output shaft to an oscillating motion of a pair of mowing blades oscillating in mutual anti-phase about a common oscillation axis (A1), wherein the reciprocating mower unit is characterized in comprising an input shaft for receiving said input rotary motion from the transmission shaft , wherein the input shaft is provided with a coupling interface for releasably coupling the input shaft to the transmission shaft .
Process for the manufacture of food flakes comprising: - cooking a nonfermented food mixture until an intermediate moisture content of between 7% and 24% is achieved, in order to obtain a cooked composition, then - cooling the cooked composition so that the texture of the cooked composition is suitable for granulation, the cooling being carried out at a temperature of between 0°C and 35°C for a period of time of between 1 h and 48 h, then - granulating the cooked composition by virtue of a granulator in order to obtain food flakes, characterized in that the process subsequently comprises: - drying the food flakes, the drying being carried out at a temperature of between 70°C and 175°C for a period of time of between 5 min and 5 h, and that the granulator comprises a rotor and a sieve , the rotor being provided with fins or vanes or slats to press the cooked composition against the sieve, and in which the rotor carries out an oscillating or rotating movement. - cooking a nonfermented food mixture until an intermediate moisture content of between 7% and 24% is achieved, in order to obtain a cooked composition, then - cooling the cooked composition so that the texture of the cooked composition is suitable for granulation, the cooling being carried out at a temperature of between 0°C and 35°C for a period of time of between 1 h and 48 h, then - granulating the cooked composition by virtue of a granulator in order to obtain food flakes, characterized in that the process subsequently comprises: - drying the food flakes, the drying being carried out at a temperature of between 70°C and 175°C for a period of time of between 5 min and 5 h, and that the granulator comprises a rotor and a sieve , the rotor being provided with fins or vanes or slats to press the cooked composition against the sieve, and in which the rotor carries out an oscillating or rotating movement. - drying the food flakes, the drying being carried out at a temperature of between 70°C and 175°C for a period of time of between 5 min and 5 h, and that the granulator comprises a rotor and a sieve , the rotor being provided with fins or vanes or slats to press the cooked composition against the sieve, and in which the rotor carries out an oscillating or rotating movement.
A nacelle configured to be mounted on top of a wind turbine tower and comprising a nacelle hatch for covering a nacelle opening at a side of the nacelle facing a wind turbine hub , wherein the nacelle hatch is completely supported by the nacelle when the hatch is closed, and the nacelle hatch is configured to be deployed from a closed position in which it covers the nacelle opening to an open position in which it forms a passageway to an opening in the wind turbine hub at a side of the wind turbine hub facing the nacelle , the passageway comprising a first side structure at least partially obstructing a downwards view on a first side of the hub and a second side structure at least partially obstructing a downwards view on a second side of the hub , the second side being opposite to the first side. the nacelle hatch is completely supported by the nacelle when the hatch is closed, and the nacelle hatch is configured to be deployed from a closed position in which it covers the nacelle opening to an open position in which it forms a passageway to an opening in the wind turbine hub at a side of the wind turbine hub facing the nacelle , the passageway comprising a first side structure at least partially obstructing a downwards view on a first side of the hub and a second side structure at least partially obstructing a downwards view on a second side of the hub , the second side being opposite to the first side.
A combination therapy for use in a method of treating cancer in a subject in need thereof comprising: (i) administering to the subject an adoptive cell therapeutic (ACT) comprising a population of CD8+ T cells wherein at least 50%, preferably at least 60% or at least 70%, of the CD8+ T cells display a central memory phenotype and are specific for a tumor antigen expressed by the cancer and (ii) subsequently administering to the subject a replicative oncolytic virus (OV) vaccine expressing the tumor antigen. (i) administering to the subject an adoptive cell therapeutic (ACT) comprising a population of CD8+ T cells wherein at least 50%, preferably at least 60% or at least 70%, of the CD8+ T cells display a central memory phenotype and are specific for a tumor antigen expressed by the cancer and (ii) subsequently administering to the subject a replicative oncolytic virus (OV) vaccine expressing the tumor antigen.
A foldable terminal, comprising a housing and an elastic sheet , the elastic sheet being disposed at an inner side of the housing and in the middle of the housing , the housing includes two shells and a bending portion which is bendable and deformable, and the bending portion is connected between the two shells ; two ends of the elastic sheet are disposed in correspondence to the two shells , and a middle portion of the elastic sheet is disposed in correspondence to the bending portion , wherein the foldable terminal further comprises two bodies , and the two bodies are fixed to the two shells correspondingly; two ends of the elastic sheet are fixedly connected to the two bodies correspondingly, wherein the foldable terminal further comprises a flexible screen , the flexible screen comprises two fixed areas and a bending area , the two fixed areas are fixed to the two bodies correspondingly, and the bending area is connected between the two fixed areas ; the elastic sheet is sandwiched between the bending portion and the bending area , wherein the elastic sheet has a bow shape in a nature state, wherein the middle portion of the elastic sheet is configured to protrude towards the housing when the foldable terminal is in a folded state, characterized in that the middle portion of the elastic sheet is further configured to deform and protrude reversely, and to support an inner side of the bending area , when the foldable terminal is in an unfolded state, and in that the elastic sheet has a bow shape, and comprises two end portions and an arc portion connected therebetween, the two ends of the elastic sheet are fixedly connected to the two bodies , respectively, and the arc portion is fixedly connected with a middle portion of the bending area and configured to have an equal protrusion height when the foldable terminal is in the folded state or the unfolded state, wherein the end of the elastic sheet is fixedly connected to a middle portion of the body in a thickness direction of the body .
A spacecraft having a satellite bus comprising: a first arm having a first end pivotably coupled to the anti-nadir face of said satellite bus at a first pivot point and a second end ; a first motor coupled to the first end of the first arm at the first pivot point; a first gimbaled platform coupled to the second end of the first arm; a first thruster rotatably coupled via the first gimballed platform to the second end of the first arm , the first arm to selectively pivot about the spacecraft to position the first thruster to generate a change in velocity of the spacecraft to maintain the spacecraft within an orbit station; a second arm having a first end pivotably coupled to said anti-nadir face of said satellite bus at a second pivot point and a second end ; a second motor coupled to the first end of the second arm at the second pivot point; a second gimbaled platform coupled to the second end of the second arm; a second thruster coupled via the second gimballed platform to said second end of said second arm ; said first pivot point is disposed proximate to a first corner of said satellite bus and said second pivot point is disposed proximate to a second corner of said satellite bus , wherein said second corner is diagonal to said first corner ; and said first and second arm has a length substantially equal to a length of the anti-nadir face of the satellite bus . a first arm having a first end pivotably coupled to the anti-nadir face of said satellite bus at a first pivot point and a second end ; a first motor coupled to the first end of the first arm at the first pivot point; a first gimbaled platform coupled to the second end of the first arm; a first thruster rotatably coupled via the first gimballed platform to the second end of the first arm , the first arm to selectively pivot about the spacecraft to position the first thruster to generate a change in velocity of the spacecraft to maintain the spacecraft within an orbit station; a second arm having a first end pivotably coupled to said anti-nadir face of said satellite bus at a second pivot point and a second end ; a second motor coupled to the first end of the second arm at the second pivot point; a second gimbaled platform coupled to the second end of the second arm; a second thruster coupled via the second gimballed platform to said second end of said second arm ; said first pivot point is disposed proximate to a first corner of said satellite bus and said second pivot point is disposed proximate to a second corner of said satellite bus , wherein said second corner is diagonal to said first corner ; and said first and second arm has a length substantially equal to a length of the anti-nadir face of the satellite bus .