mhurhangee/patent-ind-claim-en huggingface dataset:
A working vehicle comprising: a running vehicle body (F); a floor provided on the running vehicle body (F) and serving as a floor surface of an operation part in which a driver is located; a floor bracket configured to support the floor ; a fuel tank provided below the floor ; and a pedal configured to move the running vehicle body (F) forward or backward and comprising pivot shafts provided on the floor bracket between the floor and the fuel tank . a running vehicle body (F); a floor provided on the running vehicle body (F) and serving as a floor surface of an operation part in which a driver is located; a floor bracket configured to support the floor ; a fuel tank provided below the floor ; and a pedal configured to move the running vehicle body (F) forward or backward and comprising pivot shafts provided on the floor bracket between the floor and the fuel tank .
A three-dimensional laser line scan imaging system having a field of view, FOV, comprising: a pulsed laser transmitter to illuminate the FOV; a rotatable optical scanner comprising: a single four-facet pyramidal mirror to reflect laser pulses transmitted by the pulsed laser transmitter to a target in the FOV and to reflect signal return in the form of an incoming optical return ray bundle from the target in the FOV; a rotating housing with four optical ports , one for each facet of the four-facet pyramidal mirror, wherein the single four-facet pyramidal mirror is in the rotating housing, and wherein each facet and each port supports separate and non-overlapping optical paths for both an outgoing transit beam and the incoming optical return ray bundle; and an aperture slit plate , the slit plate having four elongated pinholes , one at each mirror facet local plane; wherein the pyramidal mirror, the rotating housing, and the aperture slit plate all rotate together; and a photo-multiplier-tube, PMT, based detector to detect the signal return and generate a PMT output; and a processor and memory configured to process the PMT output. a pulsed laser transmitter to illuminate the FOV; a rotatable optical scanner comprising: a single four-facet pyramidal mirror to reflect laser pulses transmitted by the pulsed laser transmitter to a target in the FOV and to reflect signal return in the form of an incoming optical return ray bundle from the target in the FOV; a rotating housing with four optical ports , one for each facet of the four-facet pyramidal mirror, wherein the single four-facet pyramidal mirror is in the rotating housing, and wherein each facet and each port supports separate and non-overlapping optical paths for both an outgoing transit beam and the incoming optical return ray bundle; and an aperture slit plate , the slit plate having four elongated pinholes , one at each mirror facet local plane; wherein the pyramidal mirror, the rotating housing, and the aperture slit plate all rotate together; and a photo-multiplier-tube, PMT, based detector to detect the signal return and generate a PMT output; and a processor and memory configured to process the PMT output. a single four-facet pyramidal mirror to reflect laser pulses transmitted by the pulsed laser transmitter to a target in the FOV and to reflect signal return in the form of an incoming optical return ray bundle from the target in the FOV; a rotating housing with four optical ports , one for each facet of the four-facet pyramidal mirror, wherein the single four-facet pyramidal mirror is in the rotating housing, and wherein each facet and each port supports separate and non-overlapping optical paths for both an outgoing transit beam and the incoming optical return ray bundle; and an aperture slit plate , the slit plate having four elongated pinholes , one at each mirror facet local plane; wherein the pyramidal mirror, the rotating housing, and the aperture slit plate all rotate together; and a photo-multiplier-tube, PMT, based detector to detect the signal return and generate a PMT output; and a processor and memory configured to process the PMT output.
A method of manufacturing air swirlers (10;24) for fuel injection devices for gas turbine engines, the method comprising the steps of: a) providing a plurality of swirler blanks ; b) arranging said plurality of swirler blanks in a coaxial manner; c) nesting the plurality of swirler blanks and securing the plurality of nested swirler blanks together; and d) forming a slot pattern in each of said plurality of swirler blanks, wherein the step of nesting a plurality of swirler blanks in a stack includes nesting swirler blanks in a stack so that the slot pattern can be provided in each of said plurality of swirler blanks in the stack simultaneously, and wherein the step of forming a slot pattern through each of the swirler blanks further comprises machining the slot pattern through each of said swirler blanks simultaneously. a) providing a plurality of swirler blanks ; b) arranging said plurality of swirler blanks in a coaxial manner; c) nesting the plurality of swirler blanks and securing the plurality of nested swirler blanks together; and d) forming a slot pattern in each of said plurality of swirler blanks,
Semiconductor chip, comprising a substrate , a stack of insulating layers arranged on the substrate , in a centre area (CA) of the semiconductor chip at least one of - a sensing element , and a circuit in the stack for electrically connecting the sensing element , and - electronic circuitry in the stack , between the centre area (CA) and an edge (ED) of the semiconductor chip: - a seal ring (SR), and - an optical inspection area (OI), wherein both, the seal ring (SR) and the optical inspection area (OI), comprise conductive structures around the centre area (CA), wherein the optical inspection area (OI) is arranged between the seal ring (SR) and the edge (ED) of the semiconductor chip, wherein each of the seal ring (SR) and the optical inspection area (OI) is implemented in the stack , wherein the seal ring (SR) is configured to protect the centre area (CA) from lateral impact, and wherein the optical inspection area (OI) is configured to enable the detection of a crack propagated into the optical inspection area (OI) by optical inspection means, characterized in that the semiconductor chip further comprises a crack stop area (SA) between the optical inspection area (OI) and the edge (ED) of the semiconductor chip, wherein the crack stop area (SA) is implemented in the stack , and wherein the crack stop area (SA) is configured to prevent an expansion of a crack towards the centre area (CA) induced from dicing a semiconductor wafer into multiple semiconductor chips, wherein the crack stop area (SA) comprises a conductive structure for preventing the expansion of cracks, wherein the conductive structure in the crack stop area (SA) is disconnected from the conducting structure in the optical inspection area (OI), wherein the conductive structure of the crack stop area (SA) includes multiple conductive elements on different levels in the stack disconnected from each other per level and across levels, and wherein the conductive elements of at least two adjacent levels are offset from each other in a direction from the centre area (CA) to the edge (ED). - a sensing element , and a circuit in the stack for electrically connecting the sensing element , and - electronic circuitry in the stack , - a seal ring (SR), and - an optical inspection area (OI),
Fluid distribution system for a battery module assembly with a number of battery modules (2.1-2.6), in which the battery modules (2.1-2.6) each have at least one first fluid connector (F1) and each have at least one second fluid connector (F2), which fluid distribution system has: a first main line element from which at least one first branch line portion (7.1) branches off, preferably at right angles; a second main line element from which at least one second branch line portion (7.1') branches off, preferably at right angles; a first connection element (8.1) which is detachably connected or connectable to the branch line portion (7.1) of the first main line element ; a second connection element (8.2) which is detachably connected or connectable to the branch line portion (7.1') of the second main line element ; which first connection element (8.1) has a first curvature to match a routing direction of the first branch line portion (7.1) to a routing direction of the first fluid connector (F1); which second connection element (8.2) has a second curvature to match a routing direction of the second branch line portion (7.1') to a routing direction of the second fluid connector (F2); characterized by at least one flexible line element , preferably a corrugated hose, which is intended and made for the detachable connection of second first or second main line elements . a first main line element from which at least one first branch line portion (7.1) branches off, preferably at right angles; a second main line element from which at least one second branch line portion (7.1') branches off, preferably at right angles; a first connection element (8.1) which is detachably connected or connectable to the branch line portion (7.1) of the first main line element ; a second connection element (8.2) which is detachably connected or connectable to the branch line portion (7.1') of the second main line element ; which first connection element (8.1) has a first curvature to match a routing direction of the first branch line portion (7.1) to a routing direction of the first fluid connector (F1); which second connection element (8.2) has a second curvature to match a routing direction of the second branch line portion (7.1') to a routing direction of the second fluid connector (F2); characterized by at least one flexible line element , preferably a corrugated hose, which is intended and made for the detachable connection of second first or second main line elements .
A rotorcraft comprising: a fuselage ; a main rotor ; a tailboom extending from the fuselage , the tailboom having an aft portion; and an anti-torque system at least partially located at the aft portion of the tailboom , the anti-torque system comprising: a first tail fan assembly including a plurality of first fan blades and including a first motor configured to provide torque to the plurality of first fan blades ; a second tail fan assembly including a plurality of second fan blades ; and including a second motor configured to provide torque to the plurality of second fan blades ; wherein, the first tail fan assembly has a larger rotational inertia than the second tail fan assembly such that the second tail fan assembly is adapted to experience a larger angular acceleration than the first tail fan assembly in response to torque, thereby providing yaw control for the rotorcraft , characterized in that the plurality of first fan blades includes a larger number of fan blades than the plurality of second fan blades ; and in that the first fan blades are formed from a different material than the second fan blades . a fuselage ; a main rotor ; a tailboom extending from the fuselage , the tailboom having an aft portion; and an anti-torque system at least partially located at the aft portion of the tailboom , the anti-torque system comprising: a first tail fan assembly including a plurality of first fan blades and including a first motor configured to provide torque to the plurality of first fan blades ; a second tail fan assembly including a plurality of second fan blades ; and including a second motor configured to provide torque to the plurality of second fan blades ; wherein, the first tail fan assembly has a larger rotational inertia than the second tail fan assembly such that the second tail fan assembly is adapted to experience a larger angular acceleration than the first tail fan assembly in response to torque, thereby providing yaw control for the rotorcraft , characterized in that the plurality of first fan blades includes a larger number of fan blades than the plurality of second fan blades ; and in that the first fan blades are formed from a different material than the second fan blades . a first tail fan assembly including a plurality of first fan blades and including a first motor configured to provide torque to the plurality of first fan blades ; a second tail fan assembly including a plurality of second fan blades ; and including a second motor configured to provide torque to the plurality of second fan blades ; wherein, the first tail fan assembly has a larger rotational inertia than the second tail fan assembly such that the second tail fan assembly is adapted to experience a larger angular acceleration than the first tail fan assembly in response to torque, thereby providing yaw control for the rotorcraft , characterized in that the plurality of first fan blades includes a larger number of fan blades than the plurality of second fan blades ; and in that the first fan blades are formed from a different material than the second fan blades .
A clamp assembly for mounting a solar module to a mounting structure , the clamp assembly comprising: a base configured to couple to the mounting structure , the base having a pivot portion and a fastening portion ; a clamp body coupled to the base , the clamp body having a clamping member and a pivoting member , the pivoting member pivotally engaged with the pivot portion of the base to pivot about a pivot axis; and a connecting portion configured to secure the clamping member of the clamp body to the fastening portion of the base , characterized in that the clamp body comprises a clamping surface that extends outwardly beyond the base in a direction parallel to the pivot axis, the clamping surface configured to clamp a portion of the solar module to the mounting structure . a base configured to couple to the mounting structure , the base having a pivot portion and a fastening portion ; a clamp body coupled to the base , the clamp body having a clamping member and a pivoting member , the pivoting member pivotally engaged with the pivot portion of the base to pivot about a pivot axis; and a connecting portion configured to secure the clamping member of the clamp body to the fastening portion of the base , characterized in that the clamp body comprises a clamping surface that extends outwardly beyond the base in a direction parallel to the pivot axis, the clamping surface configured to clamp a portion of the solar module to the mounting structure .
A bearing arrangement for supporting a rotor shaft of a wind turbine, the bearing arrangement comprising an outer housing and a bearing with a plurality of slide bearing segments , the bearing comprising two annular support bodies , each with a spherical receiving surface , which are arranged on the outer housing , the slide bearing segments resting with a spherical contact surface on the receiving surfaces , characterised in that one of the two support bodies is arranged in such a way that it can be removed in the axial direction in relation to the longitudinal direction of a shaft to be supported in the bearing arrangement without the shaft having to be removed from the bearing arrangement.
A method for printing and selective drying of a substrate , comprising: receiving a print job that includes an image to be printed upon a substrate utilizing printheads; analyzing the print job to determine a set of imaged segments of the print job; a set of image-adjacent segments of the print job; a set of remote segments of the print job; printing the print job upon the substrate utilizing a first set of printheads ; applying a cooling liquid to the set of image-adjacent segments of the printed print job utilizing a second set of printheads downstream from the first set of printheads ; exposing the printed print job to an array of controllable illumination elements ; and controlling the array of illumination elements to apply a drying illumination to the imaged segments and the image-adjacent segments of the printed print job, without providing the drying illumination to the remote segments . receiving a print job that includes an image to be printed upon a substrate utilizing printheads; analyzing the print job to determine a set of imaged segments of the print job; a set of image-adjacent segments of the print job; a set of remote segments of the print job; a set of imaged segments of the print job; a set of image-adjacent segments of the print job; a set of remote segments of the print job; printing the print job upon the substrate utilizing a first set of printheads ; applying a cooling liquid to the set of image-adjacent segments of the printed print job utilizing a second set of printheads downstream from the first set of printheads ; exposing the printed print job to an array of controllable illumination elements ; and controlling the array of illumination elements to apply a drying illumination to the imaged segments and the image-adjacent segments of the printed print job, without providing the drying illumination to the remote segments .
Cleaning apparatus for cleaning with a cleaning fluid (F), in particular for cleaning hollow bodies, comprising a tubular portion , a cleaning head , which is rotatable about a first axis of rotation (Z), at a cleaning-head end region of the tubular portion , at least one spray arm , which is rotatable about a second axis of rotation (X) oriented at least substantially perpendicularly to the first axis of rotation (Z), on the cleaning head , a drive apparatus for driving the cleaning head and the spray arm at a drive end region, opposite the cleaning-head end region, of the tubular portion , and a cleaning fluid line for the cleaning fluid (F), which extends through the tubular portion , wherein the cleaning fluid line additionally extends through the cleaning head and the spray arm and leads out in at least one outlet opening , wherein the cleaning fluid line is fluid-tight with respect to a cleaning apparatus interior, and wherein all the cleaning apparatus components are arranged outside the cleaning fluid line , characterized by two mutually independent drive arrangements for driving the cleaning head and for driving the spray arm , which each comprise a drive unit, in particular each comprise a drive motor , wherein the tubular portion comprises an outer hollow shaft which is coupled to the cleaning head and, via a gear mechanism , to the drive unit, which is in the form in particular of a drive motor , for driving the cleaning head , wherein an inner hollow shaft is arranged in the outer hollow shaft , said inner hollow shaft being coupled, via a gear mechanism on the spray arm side, to the spray arm and, via a gear mechanism on the drive motor side, to the drive unit, which is in the form in particular of a drive motor , for driving the spray arm .
A solid oxide fuel cell comprising: a metallic layer ; a glass layer ; and a barrier layer disposed between the metallic layer and the glass layer , wherein the barrier layer comprises alumina and a phosphate, and wherein the phosphate comprises an aluminum dihydrogen phosphate, an aluminum-containing phosphate, a phosphate of an element of the metallic layer, a phosphate of an element of the glass layer, or combinations thereof. a metallic layer ; a glass layer ; and a barrier layer disposed between the metallic layer and the glass layer , wherein the barrier layer comprises alumina and a phosphate, and wherein the phosphate comprises an aluminum dihydrogen phosphate, an aluminum-containing phosphate, a phosphate of an element of the metallic layer, a phosphate of an element of the glass layer, or combinations thereof.
A composition comprising a mixture of bacteria, which comprises or, alternatively, consists of: - at least a strain of bacterium selected from the group comprising the strain Lactobacillus plantarum LMG P-21021 (LP01) and the strain Lactobacillus plantarum LMG P-21020 (LP02), combined with: - at least a strain of bacterium selected from the group comprising the strain of bacteria Lactobacillus fermentum DSM 26955 (LF15) and the strain of bacteria Lactobacillus fermentum DSM 26956 (LF16), for use in the preventive and/or curative treatment of bacterial vaginosis, vaginitis and vaginal infections related with coliform pathogens and/or Gardnerella. - at least a strain of bacterium selected from the group comprising the strain Lactobacillus plantarum LMG P-21021 (LP01) and the strain Lactobacillus plantarum LMG P-21020 (LP02), combined with: - at least a strain of bacterium selected from the group comprising the strain of bacteria Lactobacillus fermentum DSM 26955 (LF15) and the strain of bacteria Lactobacillus fermentum DSM 26956 (LF16), - at least a strain of bacterium selected from the group comprising the strain of bacteria Lactobacillus fermentum DSM 26955 (LF15) and the strain of bacteria Lactobacillus fermentum DSM 26956 (LF16),
Centrifuge (1; 10) for separating sugar crystals from massecuite, said centrifuge (1; 10) being, according to a first option, continuously operating , or, according to a second option, discontinuously operating, said centrifuge (1; 10) comprising: - a rotary, permeable-wall centrifugation drum (2; 12); - a liquid collection system (4; 14) for collecting liquids having passed through the permeable wall of the centrifugation drum (2; 12); characterised in that the centrifuge (1; 10) comprises an external enclosure (50; 140) which, on one hand, surrounds said centrifugation drum (2; 12) and which, on the other, comprises one or more flexible walls (6; 16) delimiting the centrifuge (1; 10), said enclosure (50; 140) comprising a support frame (7; 17) whereon the flexible wall(s) (6; 16) are attached and stretched. - a rotary, permeable-wall centrifugation drum (2; 12); - a liquid collection system (4; 14) for collecting liquids having passed through the permeable wall of the centrifugation drum (2; 12);