mhurhangee/ep-ind-claims huggingface dataset:
A storage and distribution unit for a container filling plant (20, 30), comprising: - a store comprising storage areas for individual containers, the storage areas being especially distributed in a grid pattern, a container feed for connection to a discharge line section of a filling line, and a container outlet for connection to inspection units (9.1, 9.2, 9.3, 9.4); - a robot for putting filled containers into storage by transferring them from the container feed to the storage areas as well as for taking the containers out of storage by transferring them from the storage areas to the container outlet; and - a programmable control unit used for the robot and configured for selectively taking the containers out of storage independently of the moment in time at which and/or the sequence in which they have been put into storage, characterized in that the robot is configured to handle individual containers by taking hold of their neck and/or closure area, when putting them into a respective storage area and when taking them out of a respective storage area, and the control unit is configured for taking the containers out of storage on the basis of an electronically stored inspection plan. - a store comprising storage areas for individual containers, the storage areas being especially distributed in a grid pattern, a container feed for connection to a discharge line section of a filling line, and a container outlet for connection to inspection units (9.1, 9.2, 9.3, 9.4); - a robot for putting filled containers into storage by transferring them from the container feed to the storage areas as well as for taking the containers out of storage by transferring them from the storage areas to the container outlet; and - a programmable control unit used for the robot and configured for selectively taking the containers out of storage independently of the moment in time at which and/or the sequence in which they have been put into storage,
Landing gear of a light aircraft, i.e. weighing less than 5.7 tonnes, the landing gear consisting of at least one wheel attached to a chassis or to a fuselage of the aircraft by means of a connecting element, the wheel being connected to the connecting element via a system of two damping cylinders arranged between the wheel and the connecting element, said system of two damping cylinders being composed of two rods extending from a support part and of two struts mounted with the ability for damped sliding around the rods and secured to the connecting element, characterized in that the support part is attached to an axle of the wheel, and in that the two struts of the system of two damping cylinders are secured to the connecting element via a connecting part attached to the connecting element and connecting the two struts to one another.
A driving control system for a spinning machine having a plurality of spinning units, an individual driving device, which is provided for each spinning unit for a first group of driving members (4a, 4b, 5, 10, 38, 5a, 5b, 14c) acting directly on a bundle of fibers or a yarn, a shared driving device provided for all of said plurality of spinning units for a second group of driving members (4d, 4e, 6, 13, 44) in each spinning unit also acting directly on a bundle of fibers or a yarn, electric power failure detecting means for detecting an electric power failure in a system electric power source for said individual driving devices, the driving control system comprising intra-frame member driving device that drives member not acting directly on said bundle of fibers or yarn, and deceleration control means for controllably decelerating said intra-frame member driving device activated when the electric power failure detecting means detects an electric power failure in the system electric power source, and supply means for supplying said individual driving devices for the respective spinning units with regenerative electric power, resulting from said deceleration control, characterized by further comprising free-run control means for operating said shared driving device with a light-load when an electric power failure is detected.
A gas turbine engine comprising: a blade outer air seal (BOAS) comprising: a seal body having a radially inner face and a radially outer face that axially extend between a leading edge portion and a trailing edge portion; a retention flange that extends from said seal body at said trailing edge portion; and a seal that contacts said retention flange; and a casing that surrounds said BOAS; characterised in that: said retention flange is biased against a flange of said casing, said retention flange includes a fishmouth body and an outer lip that extends radially outward from said fishmouth body, a groove is formed in said casing, and said seal is positioned within said groove to bias the outer lip against the flange. a blade outer air seal (BOAS) comprising: a seal body having a radially inner face and a radially outer face that axially extend between a leading edge portion and a trailing edge portion; a retention flange that extends from said seal body at said trailing edge portion; and a seal that contacts said retention flange; and a seal body having a radially inner face and a radially outer face that axially extend between a leading edge portion and a trailing edge portion; a retention flange that extends from said seal body at said trailing edge portion; and a seal that contacts said retention flange; and a casing that surrounds said BOAS; characterised in that: said retention flange is biased against a flange of said casing, said retention flange includes a fishmouth body and an outer lip that extends radially outward from said fishmouth body, a groove is formed in said casing, and said seal is positioned within said groove to bias the outer lip against the flange.
A method for targeted alteration of a duplex acceptor DNA sequence comprising a first DNA sequence and a second DNA sequence which is the complement of the first DNA sequence, the method comprising combining the duplex acceptor DNA sequence with at least a first oligonucleotide and a second oligonucleotide, wherein the first oligonucleotide comprises at least one domain that is capable of hybridizing to the first DNA sequence and wherein the first oligonucleotide further comprises at least one mismatch with respect to the first DNA sequence and wherein the at least one mismatch is positioned at most 2 nucleotides from the 3 'end of said first oligonucleotide; and wherein the second oligonucleotide comprises at least one domain that is capable of hybridizing to the second DNA sequence and wherein the second oligonucleotide further comprises at least one mismatch with respect to the second DNA sequence and wherein the at least one mismatch is positioned at most 2 nucleotides from the 3'end of said second oligonucleotide; and wherein the at least one mismatch in the first oligonucleotide is relative to a nucleotide in the first DNA sequence of the duplex acceptor DNA sequence and wherein the at least one mismatch in the second oligonucleotide is relative to a nucleotide in the second DNA sequence of the duplex acceptor DNA, and wherein said nucleotides occupy complementary positions in the duplex acceptor DNA, wherein the method is not for treatment of a human or animal body by therapy or for modifying the germ line genetic identity of human beings.
A combustor of a gas turbine engine comprising: a support shell (60,62); a heat shield panel (68,70) mounted to said support shell (60,62); and an insert (80;80A;80B;80C) adjacent to said support shell (60,62) and said heat shield panel (68,70) said insert exposed to a combustion chamber, wherein said heat shield panel (68,70) includes a heat shield dilution hole and said support shell (60,62) includes a support shell dilution hole along a common dilution axis, said insert is located offset from said dilution axis and located adjacent to said dilution hole. a support shell (60,62); a heat shield panel (68,70) mounted to said support shell (60,62); and an insert (80;80A;80B;80C) adjacent to said support shell (60,62) and said heat shield panel (68,70) said insert exposed to a combustion chamber, wherein said heat shield panel (68,70) includes a heat shield dilution hole and said support shell (60,62) includes a support shell dilution hole along a common dilution axis, said insert is located offset from said dilution axis and located adjacent to said dilution hole.
A method of driving a liquid crystal display having output pixels, each comprising a plurality of subpixels each of which is capable of providing a light output of at least a first and a second color different from the first color, the first and second colors being selected from the group of three colors: red, green, and blue, and a backlight arrangement for generating light in the colors of red, green and blue illuminating the subpixels, the method comprising: performing first and second illumination cycles of the display in sequence to implement a sequential drive scheme, wherein each illumination cycle comprises illuminating the subpixels of the display with a first set of subpixels being illuminated with a first color only and a second set of subpixels, different to the first set, illuminated with a second color only, the second color different to the first color, the same first and second set of subpixels being illuminated in each cycle, wherein the first and second colors of the two cycles together include all three colors of the group for forming an image, wherein there are exactly two illumination cycles corresponding to an image forming period of the display, and the first and second colors of the first cycle comprise two of red, green and blue, and the first and second colors of the second cycle comprise two of red, green and blue, and wherein each output pixel consists of three subpixels having no color filters, and wherein in the first illumination cycle, first, second and third sub-pixels of each output pixel are illuminated respectively with the colors red, green and blue only, and wherein in the second illumination cycle, said first, second and third sub-pixels of each output pixel are illuminated respectively with the colors blue, green and red only. performing first and second illumination cycles of the display in sequence to implement a sequential drive scheme, wherein each illumination cycle comprises illuminating the subpixels of the display with a first set of subpixels being illuminated with a first color only and a second set of subpixels, different to the first set, illuminated with a second color only, the second color different to the first color, the same first and second set of subpixels being illuminated in each cycle, wherein the first and second colors of the two cycles together include all three colors of the group for forming an image, wherein there are exactly two illumination cycles corresponding to an image forming period of the display, and the first and second colors of the first cycle comprise two of red, green and blue, and the first and second colors of the second cycle comprise two of red, green and blue, and wherein each output pixel consists of three subpixels having no color filters, and wherein in the first illumination cycle, first, second and third sub-pixels of each output pixel are illuminated respectively with the colors red, green and blue only, and wherein in the second illumination cycle, said first, second and third sub-pixels of each output pixel are illuminated respectively with the colors blue, green and red only.
A device for making ablations on a lens of an eye, wherein the lens includes an inner central nucleus, a cortex and a capsule, the device including: a laser for controllably ablating ocular tissue at selected depths within the lens of the eye; and a controller for controlling the laser, wherein the controller is adapted to cause the laser to execute the following ablation steps: (i) create within the lens a posterior bounding ablation, (ii) create central phaco block chopping cuts and (iii) create an anterior bounding ablation; wherein the bounding ablations describe the extent of a central lens core to be extracted and the chopping cuts section the central lens core into fragments; characterised in that the controller is adapted to cause the laser to create peripheral portions of the anterior bounding ablation before central portions of the anterior bounding ablation. a laser for controllably ablating ocular tissue at selected depths within the lens of the eye; and a controller for controlling the laser, wherein the controller is adapted to cause the laser to execute the following ablation steps: (i) create within the lens a posterior bounding ablation, (ii) create central phaco block chopping cuts and (iii) create an anterior bounding ablation; wherein the bounding ablations describe the extent of a central lens core to be extracted and the chopping cuts section the central lens core into fragments; characterised in that the controller is adapted to cause the laser to create peripheral portions of the anterior bounding ablation before central portions of the anterior bounding ablation.
A dishwasher comprising - a tub wherein the items to be washed are placed, - a body having two side walls that surround the tub, - a fan receptacle located between the tub and the side wall, - an air channel located in the fan receptacle, having an inlet that provides the humid air in the tub to be received therein and an outlet that provides the dehumidified air to be sent back to the tub, - a fan located in the fan receptacle, providing the humid air in the tub to be sucked during the drying step and - a hole arranged on the fan receptacle, that allows the air received from the outer environment to enter into the air channel. characterized by - a guiding member that is located in the air channel, between the inlet and the hole and that forms a wall between the humid air entering the air channel through the inlet and the outer environment air entering into the air channel through the hole, thus enabling them to flow a portion of the distance they cover in the air channel without mixing with each other. - a tub wherein the items to be washed are placed, - a body having two side walls that surround the tub, - a fan receptacle located between the tub and the side wall, - an air channel located in the fan receptacle, having an inlet that provides the humid air in the tub to be received therein and an outlet that provides the dehumidified air to be sent back to the tub, - a fan located in the fan receptacle, providing the humid air in the tub to be sucked during the drying step and - a hole arranged on the fan receptacle, that allows the air received from the outer environment to enter into the air channel. - a guiding member that is located in the air channel, between the inlet and the hole and that forms a wall between the humid air entering the air channel through the inlet and the outer environment air entering into the air channel through the hole, thus enabling them to flow a portion of the distance they cover in the air channel without mixing with each other.
Ice axe, comprising a head portion that has a pick, a tip, a shaft portion that extends between the head portion and the tip, and a hand rest which is displaceable along the shaft portion and can be fixed at different positions, the hand rest having a projection which protrudes from the shaft portion in a radial direction, the hand rest having a first blocking portion (50, 52), the first blocking portion (50, 52) coming into blocking engagement with a second blocking portion (40, 44) of the shaft portion when a force is exerted on the projection in the direction of the tip of the ice pick, such that movement of the hand rest in the direction of the tip is blocked, the first blocking portion (50, 52) being released from the blocking engagement with the second blocking portion (40, 44) when a force is exerted on the projection in the direction of the head portion of the ice axe, such that movement of the hand rest in the direction of the head portion is permitted, and the hand rest canting on the outer circumference (40, 44) of the shaft portion when a force is exerted on the projection in the direction of the tip of the ice axe, such that movement along the shaft portion is blocked, characterised in that the shaft portion has a cylindrical outer circumference and in that the hand rest has a through-opening in which the shaft portion is fittingly received, the through-opening having a first contact portion for contacting a surface portion of the shaft portion that faces the projection and having a second contact portion for contacting a surface portion of the shaft portion that faces away from the projection, the first contact portion being offset, in relation to the second contact portion, towards the head portion of the ice axe in the axial direction of the shaft portion and the first and the second contact portion (42, 38) overlapping one another in the axial direction.
A shape-forming shutter apparatus, comprising: a plurality of shutter pieces, each of the shutter pieces having a shaping surface and a sliding surface, the plurality of shutter pieces being arranged in a circle in a manner such that the shaping surface of each shutter piece is slidably in sliding contact with the sliding surface of the neighboring separate shutter piece; and an opening part being surrounded by the shaping surfaces of the plurality of shutter pieces, the opening part being capable of dilating and contracting, wherein the shape-forming shutter apparatus comprises a pressure contact biasing module configured to always keep the shaping surface of each shutter piece and the sliding surface of the neighboring shutter piece slidably in pressure contact with each other, and to bias the shutter pieces in the direction in which the opening part is closed, the apparatus being characterized in that the pressure contact biasing module is a ring-shaped elastic member for biasing the shutter pieces equally, and the pressure contact biasing module is stretchingly wound around the shutter pieces. a plurality of shutter pieces, each of the shutter pieces having a shaping surface and a sliding surface, the plurality of shutter pieces being arranged in a circle in a manner such that the shaping surface of each shutter piece is slidably in sliding contact with the sliding surface of the neighboring separate shutter piece; and an opening part being surrounded by the shaping surfaces of the plurality of shutter pieces, the opening part being capable of dilating and contracting, wherein the shape-forming shutter apparatus comprises a pressure contact biasing module configured to always keep the shaping surface of each shutter piece and the sliding surface of the neighboring shutter piece slidably in pressure contact with each other, and to bias the shutter pieces in the direction in which the opening part is closed, the apparatus being characterized in that the pressure contact biasing module is a ring-shaped elastic member for biasing the shutter pieces equally, and the pressure contact biasing module is stretchingly wound around the shutter pieces.
An organopolysiloxane represented by formula shown below: wherein each R 1 independently represents a methyl group or a butyl group, each R 2 independently represents a group selected from the group consisting of groups represented by formula shown below: and groups represented by formula shown below: wherein within formulas and, R 4 represents a 1,3-propanediol-2-yl group or 1,2-propanediol-3-yl group, R 5 and R 6 are both hydrogen atoms, and g represents an integer of 2 to 20, A is a group represented by formula shown below: wherein R 1 is as defined above, k represents an integer of 1 to 5, and h represents an integer of 0 to 500, a and b each represents an integer of 0 to 3, c represents an integer of 0 to 100, provided that 1 ≤ a+b+c, d represents an integer of 0 to 2,000, e represents an integer of 0 to 500, and f represents an integer of 0 to 500.
A joined body, comprising: a first member; a second member; and a sintered metal layer that joins the first member and the second member, wherein the sintered metal layer includes a plurality of flake-shaped structures derived from flake-shaped copper particles having a maximum particle size of 1 μm to 20 μm and an aspect ratio of 4 or greater, major axes of the plurality of flake-shaped particles being oriented in approximately parallel to an interface between the first member or the second member, and the sintered metal layer, the amount of copper contained in the sintered metal layer is 65% by volume or greater on the basis of a volume of the sintered metal layer, and the degree of orientation order S of the plurality of flake-shaped structures, as expressed by the following formula, is 0.88 to 1.00: S = 1 / 2 × 3 < cos 2 θ > − 1 wherein θ represents the angle made by the interface and a flake-shaped structure and <cos 2 θ> represents the average value of a plurality of values of cos 2 θ. a first member; a second member; and a sintered metal layer that joins the first member and the second member, wherein the sintered metal layer includes a plurality of flake-shaped structures derived from flake-shaped copper particles having a maximum particle size of 1 μm to 20 μm and an aspect ratio of 4 or greater, major axes of the plurality of flake-shaped particles being oriented in approximately parallel to an interface between the first member or the second member, and the sintered metal layer, the amount of copper contained in the sintered metal layer is 65% by volume or greater on the basis of a volume of the sintered metal layer, and the degree of orientation order S of the plurality of flake-shaped structures, as expressed by the following formula, is 0.88 to 1.00: S = 1 / 2 × 3 < cos 2 θ > − 1 wherein θ represents the angle made by the interface and a flake-shaped structure and <cos 2 θ> represents the average value of a plurality of values of cos 2 θ.
A wind turbine control method comprising: - a rotor that in turn comprises a plurality of blades, - an electricity generator connected to the grid, - a power train, - a nacelle, - at least one control unit, and - a blade pitch system configured to control the pitch angle of each blade, wherein the method comprises capturing at least one signal indicative of the state of the grid wherein said signal may be indicative of a voltage dip, said method being characterised in that it comprises: - calculating a minimum dip pitch rate limit (Δβ/Δt)min lower than a maximum design pitch rate limit (Δβ/Δt)max, and in that it comprises, in the event that the signal indicative of the state of the grid indicates the presence of a voltage dip: - calculating at least one signal indicative of a forward/backward oscillation of the nacelle, - calculating a tower damping pitch rate signal in accordance with the signal indicative of the forward/backward acceleration of the nacelle, and - calculating a pitch rate command based on the tower damping pitch rate command and on the minimum dip pitch rate limit (Δβ/Δt)min. - a rotor that in turn comprises a plurality of blades, - an electricity generator connected to the grid, - a power train, - a nacelle, - at least one control unit, and - a blade pitch system configured to control the pitch angle of each blade, - calculating a minimum dip pitch rate limit (Δβ/Δt)min lower than a maximum design pitch rate limit (Δβ/Δt)max, - calculating at least one signal indicative of a forward/backward oscillation of the nacelle, - calculating a tower damping pitch rate signal in accordance with the signal indicative of the forward/backward acceleration of the nacelle, and - calculating a pitch rate command based on the tower damping pitch rate command and on the minimum dip pitch rate limit (Δβ/Δt)min.