mhurhangee/ep-ind-claims huggingface dataset:
A carbon black for batteries having: a BET specific surface area of 50 to 220 m 2 /g, measured by BET one point method at a relative pressure p/p 0 = 0.30 ± 0.04 and using nitrogen as adsorption gas; a crystallite diameter La of 30 to 42 Å, measured in accordance with JIS R 7651; and a number of CO 2 desorption molecules per unit surface area of 8.0×10 16 to 15.0×10 16 molecules/m 2, measured by a temperature-rising desorption gas analysis method set forth in the description comprising raising the temperature from 50 °C to 1200 °C. a BET specific surface area of 50 to 220 m 2 /g, measured by BET one point method at a relative pressure p/p 0 = 0.30 ± 0.04 and using nitrogen as adsorption gas; a crystallite diameter La of 30 to 42 Å, measured in accordance with JIS R 7651; and a number of CO 2 desorption molecules per unit surface area of 8.0×10 16 to 15.0×10 16 molecules/m 2, measured by a temperature-rising desorption gas analysis method set forth in the description comprising raising the temperature from 50 °C to 1200 °C.
A sectional rail system for constructing a base for plate covering, where the sectional rail system includes at least two outer rails (3, 7) extending in a longitudinal direction and between which are provided at least two intermediate rails (6-6b, 8), where the outer rails (3, 7) have U-shaped cross-section, including a sectional back and two screw webs, and where the intermediate rails (6-6b, 8) have C-shaped cross-section, including a sectional back and two screw webs and two inwardly projecting reinforcement webs, where each outer rail (3, 7) has a retention means, where each of the intermediate rails (6-6b, 8) are with two end parts, where each of the two end parts are fastened to a retention means of an outer rail (3, 7), characterised in that each of the retention means of the outer rail includes at least one stop pin and at least one resilient lock pin, where the lock pins are with resilient means for passage of an end part of an intermediate rail (6-6b, 8) and for retention of the same end part on the same intermediate rail (6-6b, 8) against the stop pin in the retention means, respectively, where the stop pin is disposed close to the inner side of the screw web of the outer rail (3, 7) and extends linearly inwards from an inner side of the screw webs in a direction orthogonal to said longitudinal direction such as to form a stop for said one reinforcement web, where the stop pin is provided with arresting means for the end part of an intermediate rail (6-6b, 8), the stop pin further extending into a support flange, which extends in said longitudinal direction, for supporting an end part of the reinforcement web of the intermediate rail (6-6b, 8), such as to form a support of said one reinforcement web.
A forage harvester with a frame assembly and a chopping drum assembly rotatably mounted on the frame assembly, wherein the frame assembly comprises two frame elements extending in the longitudinal direction of the forage harvester and two clamp bearings for mounting the chopping drum assembly, wherein a respective clamp bearing is associated with a respective frame element, wherein each clamp bearing comprises a first clamp bearing element and a second clamp bearing element which is pivotably fixed to the first clamp bearing element, characterized in that each clamp bearing comprises a locking device, which is configured to releasably lock the second clamp bearing element in an open position in which the clamp bearing is open for insertion or removal of the chopping drum assembly.
A vaccine comprising one or more mRNA or DNA molecule(s) encoding all of the functional immunostimulatory proteins CD40L, CD70 and caTLR4 (constitutively active TLR4) for use in eliciting an immune response towards a tumor in a subject, characterized in that said vaccine is administered via intratumoral injection.
A catheter assembly comprising a catheter; and a wetting agent storage chamber in which the catheter is located, wherein the wetting agent storage chamber comprises at least one projection configured to guide the catheter within the wetting agent storage chamber, wherein the at least one projection retains a seal element in the wetting agent storage chamber during withdrawal of the catheter, wherein the at least one projection comprises a plurality of ribs, wherein the plurality of ribs extend axially and radially. a catheter; and a wetting agent storage chamber in which the catheter is located, wherein the wetting agent storage chamber comprises at least one projection configured to guide the catheter within the wetting agent storage chamber, wherein the at least one projection retains a seal element in the wetting agent storage chamber during withdrawal of the catheter, wherein the at least one projection comprises a plurality of ribs, wherein the plurality of ribs extend axially and radially.
Mixtures containing • fungicidal reactive active compounds selected from the group consisting of benzisothiazolinone, octylisothiazolinone, dichlorooctylisothiazolinone (DCOIT) and • two phenolic active compounds selected from the series consisting of 3-methyl-4-chlorophenol, 3,5-dimethyl-4-chlorophenol, o-phenylphenol, 2-benzyl-4-chlorophenol (chlorophene), and their ammonium, alkali metal and alkaline earth metal salts, in a weight ratio between 1:1 and 1:10. • fungicidal reactive active compounds selected from the group consisting of benzisothiazolinone, octylisothiazolinone, dichlorooctylisothiazolinone (DCOIT) and • two phenolic active compounds selected from the series consisting of 3-methyl-4-chlorophenol, 3,5-dimethyl-4-chlorophenol, o-phenylphenol, 2-benzyl-4-chlorophenol (chlorophene), and their ammonium, alkali metal and alkaline earth metal salts, in a weight ratio between 1:1 and 1:10.
An assembly for transporting fluid comprising: a. a barge or ship comprising a cargo hold including a lower support and a side support on each side of the lower support, said cargo hold being upon or within the barge or ship; b. a plurality of pipes for fluid containment, each pipe of the plurality of pipes having at least one end that is open, wherein the plurality of pipes are stacked in a hexagonal manner and are oriented lengthwise and along almost the entire length of the barge or ship, in continuous lengths, the plurality of pipes being supported on the lower support between each side support; c. a forcing member that is configured to forcefully bear down on the plurality of pipes via a forcing mechanism to apply sufficient compressive force to the plurality of pipes stacked in the cargo hold so that friction between the pipes will prevent any significant relative movement of the pipes caused by motions of the barge or ship, or by flexing of the barge or ship, or by strains caused by differential temperature or pressure; d. a fluid line system connected to the open ends of the plurality of pipes for filling and unloading fluid to the pipes; and e. a stress-spreading structure between said forcing member and said plurality of pipes for spreading concentrated stresses generated by compressive forces exerted by said forcing mechanism, wherein said stress spreading structure is a layer of empty pipe surrounding the plurality of pipes for fluid containment. a. a barge or ship comprising a cargo hold including a lower support and a side support on each side of the lower support, said cargo hold being upon or within the barge or ship; b. a plurality of pipes for fluid containment, each pipe of the plurality of pipes having at least one end that is open, wherein the plurality of pipes are stacked in a hexagonal manner and are oriented lengthwise and along almost the entire length of the barge or ship, in continuous lengths, the plurality of pipes being supported on the lower support between each side support; c. a forcing member that is configured to forcefully bear down on the plurality of pipes via a forcing mechanism to apply sufficient compressive force to the plurality of pipes stacked in the cargo hold so that friction between the pipes will prevent any significant relative movement of the pipes caused by motions of the barge or ship, or by flexing of the barge or ship, or by strains caused by differential temperature or pressure; d. a fluid line system connected to the open ends of the plurality of pipes for filling and unloading fluid to the pipes; and e. a stress-spreading structure between said forcing member and said plurality of pipes for spreading concentrated stresses generated by compressive forces exerted by said forcing mechanism, wherein said stress spreading structure is a layer of empty pipe surrounding the plurality of pipes for fluid containment.
A thermosetting composition comprising 30 to 70 % by mass of a compound represented by Formula below and 70 to 30 % by mass of a compound represented by Formula below: wherein in Formulae and, R 1, R 2, R 3 and R 4 may be the same or different from one another and are each selected independently with respect to each molecule of the compounds from the group consisting of -H, -CH 3, -C(CH 3) 3 and a group represented by Formula (i) below: wherein in Formula (i), Y is selected from the group consisting of -O-, -CH 2 - and -C(CH 3) 2 --
A method of forming an optical fiber, comprising the following steps: forming a silica-based soot blank with at least one silica-based soot core cane at least partially embedded in the soot blank; consolidating the soot blank with the at least one soot core cane positioned therein to form a preform; and drawing the preform to form an optical fiber, wherein the expression silica-based soot core cane refers to a core cane having an unconsolidated or partially consolidated inner portion and an unconsolidated or partially consolidated outer portion, and wherein the density of the at least one soot core cane is within 10% of the density of the soot blank prior to consolidating the soot blank and the soot core cane to form the preform. forming a silica-based soot blank with at least one silica-based soot core cane at least partially embedded in the soot blank; consolidating the soot blank with the at least one soot core cane positioned therein to form a preform; and drawing the preform to form an optical fiber, wherein the expression silica-based soot core cane refers to a core cane having an unconsolidated or partially consolidated inner portion and an unconsolidated or partially consolidated outer portion, and wherein the density of the at least one soot core cane is within 10% of the density of the soot blank prior to consolidating the soot blank and the soot core cane to form the preform.
A method of disengaging an axle disconnect system, which comprises: providing an actuator comprising: a coil having a plurality of copper windings, a housing at least partially surrounding said coil, an armature slidably disposed within said housing and said coil, wherein said actuator includes a first axial position of said armature and a second axial position of said armature, a magnetic circuit comprising at least one of said housing and said armature, and applying a current to said coil, whereby said armature is actuated from said first axial position to said second axial position; developing an uninterrupted magnetic flux through said magnetic circuit, ceasing flow of said current to said coil; maintaining said armature in said second axial position via said uninterrupted magnetic flux; and applying an alternating current having decreasing amplitude over time to said coil such that said magnetic flux through said magnetic circuit is decreased. providing an actuator comprising: a coil having a plurality of copper windings, a housing at least partially surrounding said coil, an armature slidably disposed within said housing and said coil, wherein said actuator includes a first axial position of said armature and a second axial position of said armature, a magnetic circuit comprising at least one of said housing and said armature, and a coil having a plurality of copper windings, a housing at least partially surrounding said coil, an armature slidably disposed within said housing and said coil, wherein said actuator includes a first axial position of said armature and a second axial position of said armature, a magnetic circuit comprising at least one of said housing and said armature, and applying a current to said coil, whereby said armature is actuated from said first axial position to said second axial position; developing an uninterrupted magnetic flux through said magnetic circuit, ceasing flow of said current to said coil; maintaining said armature in said second axial position via said uninterrupted magnetic flux; and applying an alternating current having decreasing amplitude over time to said coil such that said magnetic flux through said magnetic circuit is decreased.
A vector comprising: (a) an origin of replication for propagation and stable maintenance in Escherichia coli; (b) an origin of replication for propagation and stable maintenance in Agrobacterium spp.; (c) a selectable marker gene; and (d) Agrobacterium spp. virulence genes: (i) virB1-B11 having SEQ ID NOS: 4-14, respectively, or r-virB1-B11 having SEQ ID NOS: 80-90, respectively, (ii) virC1-C2 having SEQ ID NOS: 16-17, respectively, or r-virC1-C2 having SEQ ID NOS: 92-93, respectively, (iii) virD1-D2 having SEQ ID NOS: 18-19, respectively, or r-virD1- D2 having SEQ ID NOS: 94-95, respectively, and (iv) virG having SEQ ID NO: 15 or r-virG having SEQ ID NO: 91, wherein the vector comprising r-virB1-B11 having SEQ ID NOS: 80-90, respectively, r-virC1-C2 having SEQ ID NOS: 92-93, respectively, r- virD1-D2 having SEQ ID NOS: 94-95, respectively, and r-virG having SEQ ID NO: 91 further comprises r-galls having SEQ ID NO: 101. (a) an origin of replication for propagation and stable maintenance in Escherichia coli; (b) an origin of replication for propagation and stable maintenance in Agrobacterium spp.; (c) a selectable marker gene; and (d) Agrobacterium spp. virulence genes: (i) virB1-B11 having SEQ ID NOS: 4-14, respectively, or r-virB1-B11 having SEQ ID NOS: 80-90, respectively, (ii) virC1-C2 having SEQ ID NOS: 16-17, respectively, or r-virC1-C2 having SEQ ID NOS: 92-93, respectively, (iii) virD1-D2 having SEQ ID NOS: 18-19, respectively, or r-virD1- D2 having SEQ ID NOS: 94-95, respectively, and (iv) virG having SEQ ID NO: 15 or r-virG having SEQ ID NO: 91, wherein the vector comprising r-virB1-B11 having SEQ ID NOS: 80-90, respectively, r-virC1-C2 having SEQ ID NOS: 92-93, respectively, r- virD1-D2 having SEQ ID NOS: 94-95, respectively, and r-virG having SEQ ID NO: 91 further comprises r-galls having SEQ ID NO: 101. (i) virB1-B11 having SEQ ID NOS: 4-14, respectively, or r-virB1-B11 having SEQ ID NOS: 80-90, respectively, (ii) virC1-C2 having SEQ ID NOS: 16-17, respectively, or r-virC1-C2 having SEQ ID NOS: 92-93, respectively, (iii) virD1-D2 having SEQ ID NOS: 18-19, respectively, or r-virD1- D2 having SEQ ID NOS: 94-95, respectively, and (iv) virG having SEQ ID NO: 15 or r-virG having SEQ ID NO: 91, wherein the vector comprising r-virB1-B11 having SEQ ID NOS: 80-90, respectively, r-virC1-C2 having SEQ ID NOS: 92-93, respectively, r- virD1-D2 having SEQ ID NOS: 94-95, respectively, and r-virG having SEQ ID NO: 91 further comprises r-galls having SEQ ID NO: 101.
An air temperature sensor suitable for use on an aircraft, the temperature sensor comprising: a housing having at least a portion with an airfoil cross section to define an airfoil portion with an upper surface and a lower surface; a temperature sensor located within the airfoil portion; an air flow path having an inlet in the lower surface and extending through the housing to the temperature sensor to provide for diverted air from air flowing along the lower surface to contact the temperature sensor; characterized in that the air temperature sensor further comprises: a drip guard located on the lower surface upstream of the inlet such that liquid travelling along the lower surface will be kicked out away from the inlet and kicked out away from the upper surface. a housing having at least a portion with an airfoil cross section to define an airfoil portion with an upper surface and a lower surface; a temperature sensor located within the airfoil portion; an air flow path having an inlet in the lower surface and extending through the housing to the temperature sensor to provide for diverted air from air flowing along the lower surface to contact the temperature sensor; a drip guard located on the lower surface upstream of the inlet such that liquid travelling along the lower surface will be kicked out away from the inlet and kicked out away from the upper surface.
A cartridge (20, 40), comprising: a body having an exterior and a plurality of bins, each bin having an opening; a plurality of lids movably attached to the body, each lid configured to cover the opening of a bin, each lid having a fastening element; a release mechanism movably attached to the body, the release mechanism movable along an axis; and a plurality of latches (40, 62) movably attached to the body, each of the plurality of latches configured to engage the respective fastening element of the plurality of lids when in a first position and to release the respective fastening element when in a second position; wherein when the release mechanism is moving along the axis in a first direction the release mechanism will cause a latch or an arm of a latch to rotate such that the release mechanism will not cause the latch to move to the second position, and wherein the release mechanism will cause a single latch to move to the second position while leaving the remaining latches in the first position when the release mechanism is moving along the axis in a second direction that is opposite to the first direction. a body having an exterior and a plurality of bins, each bin having an opening; a plurality of lids movably attached to the body, each lid configured to cover the opening of a bin, each lid having a fastening element; a release mechanism movably attached to the body, the release mechanism movable along an axis; and a plurality of latches (40, 62) movably attached to the body, each of the plurality of latches configured to engage the respective fastening element of the plurality of lids when in a first position and to release the respective fastening element when in a second position; wherein when the release mechanism is moving along the axis in a first direction the release mechanism will cause a latch or an arm of a latch to rotate such that the release mechanism will not cause the latch to move to the second position, and wherein the release mechanism will cause a single latch to move to the second position while leaving the remaining latches in the first position when the release mechanism is moving along the axis in a second direction that is opposite to the first direction.
Motor vehicle comprising an understructure provided with a rear floor, the vehicle also comprising a fuel tank situated at the front of the rear floor, characterized in that catching means are provided on a low point of the rear floor, these catching means being situated substantially at the same height as a rear axle assembly crossmember of the vehicle that is situated in front of the catching means, these catching means being shaped so as to catch a longitudinal edge of the rear axle assembly crossmember when these catching means are moved towards the front by a deformation of the rear floor under the influence of a rear impact.
A de-icing assembly for a surface of an aircraft, the de-icing assembly comprising: a carcass with a first layer, a second layer, and a carcass centerline (CL C); a plurality of seams sewn into the carcass, wherein the plurality of seams join the first and second layers of the carcass together; a plurality of inflation passages formed by the plurality of seams and disposed between the first and second layers of the carcass; a manifold fluidly connected to and disposed beneath the carcass, the manifold comprising a width and a manifold centerline (CL M) oriented approximately perpendicular or parallel to the carcass centerline; and characterized in that the seams are sown by a stitchline formed of carbon nanotube yarn, wherein each seam of the plurality of seams comprises includes a single stitchline; the assembly further comprising a control unit that provides an electrical current to the single stitchline. a carcass with a first layer, a second layer, and a carcass centerline (CL C); a plurality of seams sewn into the carcass, wherein the plurality of seams join the first and second layers of the carcass together; a plurality of inflation passages formed by the plurality of seams and disposed between the first and second layers of the carcass; a manifold fluidly connected to and disposed beneath the carcass, the manifold comprising a width and a manifold centerline (CL M) oriented approximately perpendicular or parallel to the carcass centerline; and characterized in that the seams are sown by a stitchline formed of carbon nanotube yarn, wherein each seam of the plurality of seams comprises includes a single stitchline; the assembly further comprising a control unit that provides an electrical current to the single stitchline.
Wind turbine comprising a cooling system - whereby a wind turbine comprises a nacelle and a tower, and the nacelle is rotatable arranged on top of the tower, - whereby a component is arranged in the nacelle and the component emits excess heat and a first cooling system is coupled with the component in a way to cool the component in the nacelle, - whereby the tower comprises a chamber that is arranged in the upper part of the tower, directly below and in contact with the nacelle, - whereby the roof of the chamber is the bottom part of the nacelle and the roof of the chamber is rotatable together with the nacelle in respect to the tower, characterized in that the first cooling system is connected to the chamber through the roof of the chamber, so that the heat from the first cooling system is transferred to the air in the chamber, - whereby the chamber is cooled by a second cooling system, - whereby the chamber comprises a floor and the second cooling system comprises a connection (9, 10) between the chamber and the tower through the floor, whereby a first opening to allow air from the chamber to flow into the tower and a second opening to allow cool air from the tower to flow into the chamber are arranged in the floor of the chamber, to guide the warm air from the chamber into the tower, so that the warm air flows along the wall of the tower and is cooled by the tower wall, so that the tower is used as a heat sink, - so that transportation of heat from the first cooling system to the tower is independent from the rotation or orientation of the nacelle in respect to the tower. - whereby a wind turbine comprises a nacelle and a tower, and the nacelle is rotatable arranged on top of the tower, - whereby a component is arranged in the nacelle and the component emits excess heat and a first cooling system is coupled with the component in a way to cool the component in the nacelle, - whereby the tower comprises a chamber that is arranged in the upper part of the tower, directly below and in contact with the nacelle, - whereby the roof of the chamber is the bottom part of the nacelle and the roof of the chamber is rotatable together with the nacelle in respect to the tower, - whereby the chamber is cooled by a second cooling system, - whereby the chamber comprises a floor and the second cooling system comprises a connection (9, 10) between the chamber and the tower through the floor, whereby a first opening to allow air from the chamber to flow into the tower and a second opening to allow cool air from the tower to flow into the chamber are arranged in the floor of the chamber, to guide the warm air from the chamber into the tower, so that the warm air flows along the wall of the tower and is cooled by the tower wall, so that the tower is used as a heat sink, - so that transportation of heat from the first cooling system to the tower is independent from the rotation or orientation of the nacelle in respect to the tower.