mhurhangee/ep-ind-claims huggingface dataset:
A mobile elevating work platform comprising: a chassis; a pair of fixed wheels secured to the chassis; a pair of caster wheels secured to the chassis; a driving and steering wheel secured to the chassis; a control implement coupled with the driving and steering wheel, the control implement being configured to adjust a steering position of the driving and steering wheel; and a drive motor operable to drive the driving and steering wheel, wherein the chassis comprises a pivot link, and wherein the drive motor and the driving and steering wheel are pivotally secured to the chassis via the pivot link, characterized in that the mobile elevating work platform further comprising a driving wheel suspension secured between the driving and steering wheel and the chassis, wherein the driving wheel suspension comprises a spring. a chassis; a pair of fixed wheels secured to the chassis; a pair of caster wheels secured to the chassis; a driving and steering wheel secured to the chassis; a control implement coupled with the driving and steering wheel, the control implement being configured to adjust a steering position of the driving and steering wheel; and a drive motor operable to drive the driving and steering wheel, wherein the chassis comprises a pivot link, and wherein the drive motor and the driving and steering wheel are pivotally secured to the chassis via the pivot link, characterized in that the mobile elevating work platform further comprising a driving wheel suspension secured between the driving and steering wheel and the chassis, wherein the driving wheel suspension comprises a spring.
A propulsion system for a tiltrotor aircraft, having two rotatable proprotors the propulsion system comprising: an engine configured to be disposed within a fuselage; a wing member having a first rib, a second rib, a first spar, a second spar and an upper wing skin, wherein the first rib, the second rib, the first spar and the second spar are coupled together to form a torque box proximate to each end of the wing member; a first gearbox disposed midwing and coupled to the engine; two second gear boxes, each second gear box for one of the rotatable proprotors and disposed either outboard from its respective second rib or inboard from its respective first rib; two drive shafts disposed within the wing member, each drive shaft mechanically coupling the first gearbox to one of the second gear boxes; each of the two rotatable proprotors mechanically coupled to one of the second gear boxes, each rotatable proprotor comprising: a plurality of rotor blades; a rotor mast having a rotor mast axis of rotation; and a proprotor gearbox coupled to the rotor mast and the second gearbox, the proprotor gearbox being rotatable about a conversion axis, the conversion axis and the rotor mast axis of rotation intersecting at an intersection point, the intersection point being located in a central region within its respective torque box and above an airfoil surface profile of the upper wing skin. an engine configured to be disposed within a fuselage; a wing member having a first rib, a second rib, a first spar, a second spar and an upper wing skin, wherein the first rib, the second rib, the first spar and the second spar are coupled together to form a torque box proximate to each end of the wing member; a first gearbox disposed midwing and coupled to the engine; two second gear boxes, each second gear box for one of the rotatable proprotors and disposed either outboard from its respective second rib or inboard from its respective first rib; two drive shafts disposed within the wing member, each drive shaft mechanically coupling the first gearbox to one of the second gear boxes; each of the two rotatable proprotors mechanically coupled to one of the second gear boxes, each rotatable proprotor comprising: a plurality of rotor blades; a rotor mast having a rotor mast axis of rotation; and a proprotor gearbox coupled to the rotor mast and the second gearbox, the proprotor gearbox being rotatable about a conversion axis, the conversion axis and the rotor mast axis of rotation intersecting at an intersection point, the intersection point being located in a central region within its respective torque box and above an airfoil surface profile of the upper wing skin. a plurality of rotor blades; a rotor mast having a rotor mast axis of rotation; and a proprotor gearbox coupled to the rotor mast and the second gearbox, the proprotor gearbox being rotatable about a conversion axis, the conversion axis and the rotor mast axis of rotation intersecting at an intersection point, the intersection point being located in a central region within its respective torque box and above an airfoil surface profile of the upper wing skin.
A bearing element, comprising: a bearing element substrate; and a sliding layer (5a, 5b, 5c) applied to a surface of the bearing element substrate, the sliding layer being formed of a sliding layer material; wherein a surface roughness (Ra) of the surface of the bearing element substrate is less than 1μm; wherein the sliding layer material comprises:- a polymeric material; and iron oxide; and wherein the sliding layer (5a, 5b, 5c) comprises at least three layers (5a, 5b, 5c) of the sliding layer material, wherein a surface roughness (Rz) of the surface of the bearing element substrate is less than 1μm. characterized in that the sliding layer material comprises iron oxide in flaked form. a bearing element substrate; and a sliding layer (5a, 5b, 5c) applied to a surface of the bearing element substrate, the sliding layer being formed of a sliding layer material; wherein a surface roughness (Ra) of the surface of the bearing element substrate is less than 1μm; wherein the sliding layer material comprises:- a polymeric material; and iron oxide; and a polymeric material; and iron oxide; and wherein the sliding layer (5a, 5b, 5c) comprises at least three layers (5a, 5b, 5c) of the sliding layer material, wherein a surface roughness (Rz) of the surface of the bearing element substrate is less than 1μm.
A composition for use in the treatment and prevention of scars comprising a therapeutically effective amount of at least one EP4 agonist having the structure:
A passive matrix or electrophoretic display device comprising: a combined panel circuit operable to perform capacitive sensing responsive to application of a first voltage and updating of an image displayed by the display device responsive to application of a second voltage, the combined panel circuit including a top conductive layer and a bottom conductive layer which are configured to implement a first electrode pattern and a second electrode pattern, respectively, across which the first voltage and the second voltage are applied, the first electrode pattern formed as horizontal control lines and the second electrode pattern formed as vertical control lines, intersections of the horizontal control lines and the vertical control lines corresponding to pixel positions of the display device, wherein display particles are sandwiched between the top conductive layer and bottom conductive layer and the display particles at a pixel position change between states in response to applying the second voltage across a horizontal control line and a vertical control line at the pixel position to update the image; and a controller configured to measure via the combined panel circuit capacitance associated with touch input at the pixel positions of the display device by selectively applying the first voltage across the first electrode pattern and the second electrode pattern; and cause formation of an image for display via the display device by applying the second voltage across the first electrode pattern and the second electrode pattern, wherein the first voltage is insufficient to activate the display particles. a combined panel circuit operable to perform capacitive sensing responsive to application of a first voltage and updating of an image displayed by the display device responsive to application of a second voltage, the combined panel circuit including a top conductive layer and a bottom conductive layer which are configured to implement a first electrode pattern and a second electrode pattern, respectively, across which the first voltage and the second voltage are applied, the first electrode pattern formed as horizontal control lines and the second electrode pattern formed as vertical control lines, intersections of the horizontal control lines and the vertical control lines corresponding to pixel positions of the display device, wherein display particles are sandwiched between the top conductive layer and bottom conductive layer and the display particles at a pixel position change between states in response to applying the second voltage across a horizontal control line and a vertical control line at the pixel position to update the image; and a controller configured to measure via the combined panel circuit capacitance associated with touch input at the pixel positions of the display device by selectively applying the first voltage across the first electrode pattern and the second electrode pattern; and cause formation of an image for display via the display device by applying the second voltage across the first electrode pattern and the second electrode pattern, wherein the first voltage is insufficient to activate the display particles.
A card body comprising: a card part onto which an IC module is to be mounted, the IC module including an IC chip and a contact pattern; and a bracket part to support the card part; wherein the card part includes a bevel, and the bracket part includes a hole formed at a circumference of the card part, a first bridge part connecting the bracket part and the card part, a second bridge part connecting the bracket part and the card part, the second bridge part is provided at a position further away from the bevel than the first bridge part, a first break-off line provided at both surfaces of a connection part between the card part and the first bridge part so that a thickness of the connection part is equal to a first thickness, and a second break-off line provided at both surfaces of a connection part between the card part and the second bridge part so that a thickness of the connection part is equal to a second thickness, characterized by the first thickness being shorter than the second thickness. a card part onto which an IC module is to be mounted, the IC module including an IC chip and a contact pattern; and a bracket part to support the card part; wherein the card part includes a bevel, and the bracket part includes a hole formed at a circumference of the card part, a first bridge part connecting the bracket part and the card part, a second bridge part connecting the bracket part and the card part, the second bridge part is provided at a position further away from the bevel than the first bridge part, a first break-off line provided at both surfaces of a connection part between the card part and the first bridge part so that a thickness of the connection part is equal to a first thickness, and a second break-off line provided at both surfaces of a connection part between the card part and the second bridge part so that a thickness of the connection part is equal to a second thickness, characterized by the first thickness being shorter than the second thickness.
A preemie swaddling wrap (20; 70), comprising: a kite-shaped body (22; 72) defining a head-supporting portion (24; 74), a body-supporting portion(26; 76), a bottom flap (28; 78), and opposing right and left wings(30, 32; 80, 82), the bottom flap (28; 78) configured to be folded upward over the legs and torso of an infant to be swaddled, the right wing (30; 80) configured to be folded over the torso and the bottom flap (28; 78), and the left wing (32; 82) configured to be folded over the torso and right wing (30; 80); and a plurality of hook-and-loop fasteners (34, 35, 36, 37, 38, 40, 42, 44, 46; 84, 86, 88, 90, 92, 94, 96, 98, 102) attached to the body (22; 72) at a plurality of positions for realisably engaging with other plurality of positions on the kite-shaped body; characterized in that the preemie swaddling wrap further comprises the head-supporting portion (24; 74) including a non-circular recess (48; 106) formed therein for positioning a head of a preemie to be swaddled therein, the head-supporting portion being padded and including a greater degree of padding above (50; 108) and below (50; 108) the recess (48; 106) and a lesser degree of padding to the sides (52; 110) of the recess to prevent any blocking of breathing. a kite-shaped body (22; 72) defining a head-supporting portion (24; 74), a body-supporting portion(26; 76), a bottom flap (28; 78), and opposing right and left wings(30, 32; 80, 82), the bottom flap (28; 78) configured to be folded upward over the legs and torso of an infant to be swaddled, the right wing (30; 80) configured to be folded over the torso and the bottom flap (28; 78), and the left wing (32; 82) configured to be folded over the torso and right wing (30; 80); and a plurality of hook-and-loop fasteners (34, 35, 36, 37, 38, 40, 42, 44, 46; 84, 86, 88, 90, 92, 94, 96, 98, 102) attached to the body (22; 72) at a plurality of positions for realisably engaging with other plurality of positions on the kite-shaped body; characterized in that the preemie swaddling wrap further comprises the head-supporting portion (24; 74) including a non-circular recess (48; 106) formed therein for positioning a head of a preemie to be swaddled therein, the head-supporting portion being padded and including a greater degree of padding above (50; 108) and below (50; 108) the recess (48; 106) and a lesser degree of padding to the sides (52; 110) of the recess to prevent any blocking of breathing.
A battery module, comprising: a battery cell assembly, comprising at least two battery cells arranged along a third direction (z), wherein each of the battery cells comprises electrode terminals; and a first busbar, comprising a main portion and two connecting portions, wherein the first busbar is set at an angle with respect to the third direction (z), the two connecting portions are connected to the electrode terminals of the two battery cells in an identical battery cell assembly respectively, the main portion is connected between the two connecting portions, a deformation inducing portion is disposed on the main portion, and the deformation inducing portion is configured to reduce at least a force required for deforming the main portion along a first direction (x), and the first direction (x) is parallel to a lateral surface of the battery cell and perpendicular to the third direction (z), wherein the lateral surface is a surface on which the electrode terminals are disposed; wherein the deformation inducing portion comprises a gap, and the gap runs through along a thickness direction of the main portion, the gap comprises two transverse grooves, and the two transverse grooves extend along a width direction of the first busbar and are spaced apart along a length direction of the first busbar. a battery cell assembly, comprising at least two battery cells arranged along a third direction (z), wherein each of the battery cells comprises electrode terminals; and a first busbar, comprising a main portion and two connecting portions, wherein the first busbar is set at an angle with respect to the third direction (z), the two connecting portions are connected to the electrode terminals of the two battery cells in an identical battery cell assembly respectively, the main portion is connected between the two connecting portions, a deformation inducing portion is disposed on the main portion, and the deformation inducing portion is configured to reduce at least a force required for deforming the main portion along a first direction (x), and the first direction (x) is parallel to a lateral surface of the battery cell and perpendicular to the third direction (z), wherein the lateral surface is a surface on which the electrode terminals are disposed; wherein the deformation inducing portion comprises a gap, and the gap runs through along a thickness direction of the main portion, the gap comprises two transverse grooves, and the two transverse grooves extend along a width direction of the first busbar and are spaced apart along a length direction of the first busbar.
A hinge having a hinge part, which is fixable on a door or flap and is pivotably mounted via a support lever and a guide lever on a side part, having a linear damper having a piston rod movable in relation to the damper housing for damping a closing and/or opening movement of the hinge part, wherein a deflection element is provided, which is mounted so it is rotatable about an axis on the side part and is articulated with the damper or a component coupled to the damper and is arranged between the damper and the guide lever, to move the damper to generate a damping force during a closing movement of the hinge part, whereby, during an opening movement of the hinge part, the deflection element moves the damper to generate a damping force before reaching the maximally open position of the hinge part, characterized in that the deflection element is articulated with or a component connected to the guide lever, whereby the opening damping is active at least in an angle range (β) of at least 10° before the maximally open position of the hinge part and whereby at least one spring is provided, by means of which the hinge part is pre-tensioned into a closed position in a self-retraction range of the hinge.
Method for making a reclosable cap, such as a reclosable cap reclosable by screwing, comprising the steps of: i) providing a metal layer with a plurality of scores at locations defined by an ultimate position in the reclosable caps to be formed out of the metal layer; ii) providing the scored metal layer on at least the scored side with a coating; iii) cutting shells from the scored metal layer, which shells include a score; and iv) forming a reclosable cap from the shell, with the score at the ultimate position, characterized in that the scoring is carried out by low speed scoring, and the coating, cutting and forming of the reclosable cap is carried out at high speed, and that the metal layer comprises a metal sheet cut from a metal strip forming the metal layer and stored on a stack, and the cut and scored metal sheet to be coated in step (ii) originates from the stack of metal sheets. i) providing a metal layer with a plurality of scores at locations defined by an ultimate position in the reclosable caps to be formed out of the metal layer; ii) providing the scored metal layer on at least the scored side with a coating; iii) cutting shells from the scored metal layer, which shells include a score; and iv) forming a reclosable cap from the shell, with the score at the ultimate position,
A method of obtaining liquid biohydrocarbons from oils of natural origin, especially waste vegetable oils, animal fats, algal oils and lipid fractions of ligno-cellulose waste, carried out in two steps in a coupled flow system in the presence of heterophase catalysts, wherein in the first step, the oil and/or waste oil is/are heated at temperatures in a range 100-500°C, at pressures in a range 0.1-5 MPa in the presence of a mixture of hydrogen and carbon monoxide, in the presence of a catalyst in the form of a metal oxide selected from a group comprising CoO, NiO, MoO 3, ZrO 2, or a mixture of such metal oxides, on an oxide support selected from a group comprising SiO 2, Al 2 O 3, TiO 2, and wherein in the second step a product of the first step is contacted with hydrogen gas or with a mixture of hydrogen and carbon monoxide at temperatures in a range 100-500°C, at pressures in a range 0.1-5 MPa, in the presence of a metallic catalyst selected from a group comprising Pd, Pt, Co/Mo, Ni/Mo, Zr on an oxide support selected from a group comprising SiO 2, Al 2 O 3, TiO 2, P 2 O 5, ZrO 2 or on a mixture of such oxides. at temperatures in a range 100-500°C, at pressures in a range 0.1-5 MPa in the presence of a mixture of hydrogen and carbon monoxide, in the presence of a catalyst in the form of a metal oxide selected from a group comprising CoO, NiO, MoO 3, ZrO 2, or a mixture of such metal oxides, on an oxide support selected from a group comprising SiO 2, Al 2 O 3, TiO 2, at temperatures in a range 100-500°C, at pressures in a range 0.1-5 MPa, in the presence of a metallic catalyst selected from a group comprising Pd, Pt, Co/Mo, Ni/Mo, Zr on an oxide support selected from a group comprising SiO 2, Al 2 O 3, TiO 2, P 2 O 5, ZrO 2 or on a mixture of such oxides.
A method of controlling vehicle systems in a motor vehicle, comprising: receiving monitoring information from one or more monitoring systems; determining a plurality of driver states based on the monitoring information from the one or more monitoring systems, the plurality of driver states being at least one of the following types of driver states: physiological driver state, behavioral driver state, and vehicular-sensed driver state; determining a combined driver state index based on the plurality of driver states; and modifying control of one or more vehicle systems based on the combined driver state index. receiving monitoring information from one or more monitoring systems; determining a plurality of driver states based on the monitoring information from the one or more monitoring systems, the plurality of driver states being at least one of the following types of driver states: physiological driver state, behavioral driver state, and vehicular-sensed driver state; determining a combined driver state index based on the plurality of driver states; and modifying control of one or more vehicle systems based on the combined driver state index.
A pressure-compensated magnetic valve, in particular for an air suspension system of a vehicle, comprising: - an electrically energizable coil, and - a magnetic armature movably mounted with reference to a longitudinal axis of the coil, - a plunger connected to the magnetic armature, wherein - both the magnetic armature and the plunger are out-of-tool components, and characterized in that - the plunger is slipped onto the magnetic armature so that it at least partially encloses the magnetic armature, and the magnetic armature in the enclosed region comprises at least one axially extending, outer channel which contributes to pressure compensation. - an electrically energizable coil, and - a magnetic armature movably mounted with reference to a longitudinal axis of the coil, - a plunger connected to the magnetic armature, wherein - both the magnetic armature and the plunger are out-of-tool components, and characterized in that - the plunger is slipped onto the magnetic armature so that it at least partially encloses the magnetic armature, and the magnetic armature in the enclosed region comprises at least one axially extending, outer channel which contributes to pressure compensation.