mhurhangee/ep-ind-claims huggingface dataset:
A method of compensating a non-linear optical effect that is caused when an optical signal is propagated through an optical fiber, the method comprising: obtaining a phase conjugate signal pair which comprises an upper sideband and a lower sideband of an optical carrier wave by means of an optical modulator which is an electro-optical effect phase conjugate signal pair generator; simultaneously inputting the upper sideband and the lower sideband to the optical fiber; multiplexing the optical signal having a same frequency as the optical carrier wave with the upper sideband and the lower sideband in a state where there is no phase difference among the optical signal, the upper sideband, and the lower sideband; causing a photodetector to detect the multiplexed optical signal; transmitting an electric signal based on the optical signal detected by the photodetector to a transmitting antenna; and causing the transmitting antenna to emit a radio signal based on the electric signal. obtaining a phase conjugate signal pair which comprises an upper sideband and a lower sideband of an optical carrier wave by means of an optical modulator which is an electro-optical effect phase conjugate signal pair generator; simultaneously inputting the upper sideband and the lower sideband to the optical fiber; multiplexing the optical signal having a same frequency as the optical carrier wave with the upper sideband and the lower sideband in a state where there is no phase difference among the optical signal, the upper sideband, and the lower sideband; causing a photodetector to detect the multiplexed optical signal; transmitting an electric signal based on the optical signal detected by the photodetector to a transmitting antenna; and causing the transmitting antenna to emit a radio signal based on the electric signal.
An aircraft comprising: a gas turbine engine comprising a control unit to command the gas turbine engine to perform one of a rolling takeoff procedure and an unrestricted takeoff procedure, characterised in that: the control unit is configured to command the gas turbine engine to perform the rolling takeoff procedure when information required to determine whether the unrestricted takeoff procedure can be performed is unavailable to the control unit, wherein the information includes a ground wind speed, wherein, following initiation of the rolling takeoff procedure, the control unit is configured to power the gas turbine engine to full power after running at intermediate power for a period of time to allow the ground speed of an aircraft to reach a predetermined ground speed.
A container comprising smoking articles, comprising container walls, wherein the container is formed from a blank, wherein the container is a hinge-lid container, comprising a box and a lid, wherein a front wall of the lid is formed from a panel of the blank, wherein the lid front wall is fixed by means of an adhesive to a further component of the container, wherein the further component is an inner liner, which encloses a bundle of smoking articles and is arranged in between the smoking articles and the container walls, wherein the inner liner comprises a cover flap, covering a designated opening of the inner liner, and the cover flap is fixed to the inside of the lid front wall, wherein the cover flap of the inner liner is attached by the adhesive to the inside of the lid front wall, and wherein the adhesive is applied in the form of several glue dots, characterized in that the lid front wall comprises a fluid guide element (16, 17, 18), wherein the fluid guide element (16, 17, 18) is provided on the inside of the lid front wall, and the adhesive is provided in the fluid guide element (16, 17, 18), wherein the fluid guide element (16, 17, 18) is adapted to promote the adhesive into advancing into a predetermined direction.
A mold configuration (220, 320, 420) for forming a pocket in a film of a pressurized product containment pouch (200, 300, 400) having a base film (202, 402) and a lid film (204, 304, 404) adhered about a perimeter seal seam, the mold configuration (220, 320, 420) comprising: a film support surface (222, 322, 422); a perimeter edge (226, 326, 426) at said film support surface (222, 322, 422); wall surfaces inward of said perimeter edge (226, 326, 426) defining a mold cavity, said wall surfaces including a bottom wall surface, transition wall surfaces (225, 325, 425) extending to said bottom wall surface (228, 328, 428); and a plateau surface (230, 330, 430) inward of said perimeter edge (226, 326, 426), the mold configuration (220, 320, 420) being characterized in that, said plateau surface (230, 330, 430) is spaced inward of said film support surface (222, 322, 422) a distance sufficient to prevent adherence of the lid film (204, 304, 404) to the base film (202, 402) overlying said plateau surfaces (230, 330, 430) while limiting deformation or stretch of the film into the mold configuration (220, 320, 420) from the film support surface (222, 322, 422). a film support surface (222, 322, 422); a perimeter edge (226, 326, 426) at said film support surface (222, 322, 422); wall surfaces inward of said perimeter edge (226, 326, 426) defining a mold cavity, said wall surfaces including a bottom wall surface, transition wall surfaces (225, 325, 425) extending to said bottom wall surface (228, 328, 428); and a plateau surface (230, 330, 430) inward of said perimeter edge (226, 326, 426), the mold configuration (220, 320, 420) being characterized in that,
A remotely operable inspection device for inspecting an underbody of a vehicle, the inspection device comprising: a device controller configured to control operation of the inspection device; a shuttle having first and second parts (18, 20), the first part arranged to move substantially along a horizontally-extending first axis on a surface under a frame of a vehicle, the second part engaged or engageable with the first part and at least part of the second part being arranged to move relative to the first part substantially along a horizontally-extending second axis, the first axis being transverse to the second axis, the shuttle having at least a narrow configuration when moving the shuttle under a frame of a vehicle, and an extended configuration when inspecting an underbody of a vehicle, and the first and second parts (18, 20) being arranged so that, in the extended configuration: a first end (28, 30) of the second part is further away, in a direction along the second axis, from a middle of the first part than the first end (28, 30) of the second part is in the narrow configuration, and the first end (28, 30) of the second part is located beyond an end (22, 24) of the first part in the direction along the second axis; and a camera module having a camera and being configured to generate image data representing at least a part of an underbody of a vehicle, the camera being movable with the second part relative to the first part. a device controller configured to control operation of the inspection device; a shuttle having first and second parts (18, 20), the first part arranged to move substantially along a horizontally-extending first axis on a surface under a frame of a vehicle, the second part engaged or engageable with the first part and at least part of the second part being arranged to move relative to the first part substantially along a horizontally-extending second axis, the first axis being transverse to the second axis, the shuttle having at least a narrow configuration when moving the shuttle under a frame of a vehicle, and an extended configuration when inspecting an underbody of a vehicle, and the first and second parts (18, 20) being arranged so that, in the extended configuration: a first end (28, 30) of the second part is further away, in a direction along the second axis, from a middle of the first part than the first end (28, 30) of the second part is in the narrow configuration, and the first end (28, 30) of the second part is located beyond an end (22, 24) of the first part in the direction along the second axis; and a camera module having a camera and being configured to generate image data representing at least a part of an underbody of a vehicle, the camera being movable with the second part relative to the first part. a first end (28, 30) of the second part is further away, in a direction along the second axis, from a middle of the first part than the first end (28, 30) of the second part is in the narrow configuration, and the first end (28, 30) of the second part is located beyond an end (22, 24) of the first part in the direction along the second axis; and
A coupling device for transferring a driving motion from a vibration transferring handpiece to a medical, in particular dental, tool, comprising: a first coupling element which is provided on the handpiece, and a second coupling element which is provided on the tool, wherein one of the two coupling elements is designed as a coupling protrusion, which can be inserted into a coupling recess on the other coupling element, wherein the coupling protrusion and the coupling recess each have a first section (8, 9) for releasable connection of the two coupling elements (4, 5) and a second section (10, 11) for positioning the two coupling elements (4, 5) along their joint longitudinal axis, wherein the second section (10, 11) on the coupling protrusion and on the coupling recess is formed such that the two coupling elements (4, 5) can be positioned relative to one another, are guided along one another and can be displaced along the joint longitudinal axis before the two coupling elements (4, 5) can be releasably connected to one another through the first section (8, 9), wherein the first sections (8, 9) for releasable connection of the two coupling elements (4, 5) each have a thread (13, 14) with at least one thread flight each, characterized in that a guide ring which runs around the coupling protrusion is provided on one end of that thread which is arranged on the coupling element designed as a coupling protrusion, wherein the at least one thread flight of the thread ends at the guide ring so that a lateral surface of the guide ring is not interrupted by the at least one thread flight of the thread and is preferably designed as a continuous cylindrical lateral surface.
A method of operating a tillage implement, the method characterized by: selecting a variation of an operating parameter of a tillage implement with respect to a position within a field based on information collected by a harvester relating to an amount of grain harvested or an amount of material other than grain processed and returned to the field by the harvester; propelling the tillage implement through the field; and adjusting the operating parameter of the tillage implement based on the selected variation. selecting a variation of an operating parameter of a tillage implement with respect to a position within a field based on information collected by a harvester relating to an amount of grain harvested or an amount of material other than grain processed and returned to the field by the harvester; propelling the tillage implement through the field; and adjusting the operating parameter of the tillage implement based on the selected variation.
A method of forming a bias-ply (158, 640) with an automated material preparation device, the method comprising: laying out a length of bias-ply backing material (146, 622), the bias-ply backing material (146, 622) having a select width; laying out a length of feedstock having feedstock backing material and a layer of fiber reinforced pre-preg material, the feedstock crossing a select portion of the width of the bias-ply backing material (146, 622) along a first section of the bias-ply backing material (146, 622) at a select angle; transferring the pre-preg (300, 660) from the feedstock backing material directly onto the first section of the bias-ply backing material (146, 622); and cutting the pre-preg (300, 660) of the transferred pre-preg (300, 660) on the first section of bias-ply backing material (146, 622) without cutting the feedstock backing material with an automated cutter to form a bias-ply (158, 640) having pre-preg (300, 660) with reinforcing fibers at a select orientation relative to an edge of the formed bias-ply (158, 640). laying out a length of bias-ply backing material (146, 622), the bias-ply backing material (146, 622) having a select width; laying out a length of feedstock having feedstock backing material and a layer of fiber reinforced pre-preg material, the feedstock crossing a select portion of the width of the bias-ply backing material (146, 622) along a first section of the bias-ply backing material (146, 622) at a select angle; transferring the pre-preg (300, 660) from the feedstock backing material directly onto the first section of the bias-ply backing material (146, 622); and cutting the pre-preg (300, 660) of the transferred pre-preg (300, 660) on the first section of bias-ply backing material (146, 622) without cutting the feedstock backing material with an automated cutter to form a bias-ply (158, 640) having pre-preg (300, 660) with reinforcing fibers at a select orientation relative to an edge of the formed bias-ply (158, 640).
A tie comprising a strip of fabric or other flexible sheet material, having two opposite longitudinal ends (11, 12), the tie comprising one or more binding means provided on the tie at a position spaced from at least a first one of the two ends, whereby the binding means are adapted to define a closed loop passage through which the first end can be introduced and run; characterised in that said binding means are located in proximity of the second end of the tie opposite to said first end.
An antenna including a plurality of antenna elements (B1-B10) and a feed network configured to feed signals to and/or receive signals from the antenna elements, wherein the feed network includes a multi-bladed wiper-type phase shifter characterized in: i. two or more conductive strips (55, 56, 57, 58) positioned about a pivot point wherein at least one of the conductive strips (55, 56, 57, 58) provides a series of notches or open-circuit stubs that increase an electrical length of the conductive strip; ii. a wiper configured to pivot about the pivot point and having a first blade extending in a first direction for coupling with one or more of the conductive strips (55, 56, 57, 58) and a second blade extending in a second direction for coupling with one or more of the conductive strips (55, 56, 57, 58); and iii. an input line configured to couple with the wiper near the pivot point; wherein the wiper is configured to pivot about the pivot point so as to vary lengths of paths from the input line to the antenna elements connected to the conductive strips (55, 56, 57, 58); characterised in that the plurality of antenna elements (B1 -B10) includes pairs of adjacent antenna elements, and wherein the adjacent antenna elements of each pair are connected to different conductive strips (55, 56, 57, 58); and wherein an antenna element having a first maximum phase shift is connected to a first conductive strip and another antenna element having a second maximum phase shift opposite to the first maximum phase shift is connected to a second conductive strip. i. two or more conductive strips (55, 56, 57, 58) positioned about a pivot point wherein at least one of the conductive strips (55, 56, 57, 58) provides a series of notches or open-circuit stubs that increase an electrical length of the conductive strip; ii. a wiper configured to pivot about the pivot point and having a first blade extending in a first direction for coupling with one or more of the conductive strips (55, 56, 57, 58) and a second blade extending in a second direction for coupling with one or more of the conductive strips (55, 56, 57, 58); and iii. an input line configured to couple with the wiper near the pivot point;
Trephine drill bit for making an incision on an external part of an implant-bone connection, comprising a cylindrical body and a cylindrical cutting tip protruding longitudinally from a distal end of the cylindrical body, the cylindrical cutting tip is made of a different material than the cylindrical body and has a smaller diameter than a diameter of the cylindrical body, the cylindrical body ends in a stop extending outwardly radially from said cylindrical cutting tip for rubbing against bone upon contact to indicate a surgeon that the trephine drill bit has been inserted to a required limit.
A multi-purpose self-propelled railway vehicle designed for the construction, repair and maintenance of railway lines, comprising a main frame equipped with at least two axles and forming at the top a work platform, a driver's cab positioned at a first end of the main frame, a plurality of operating units (W1-W3) mounted or mountable on the work platform for performing respective operations linked to the construction, repair and maintenance of the railway lines, and a plurality of functional units (F1-F4) mounted or mountable below the main frame and intended for supplying the power necessary for moving the railway vehicle and for powering the operating units (W1-W3), wherein said operating units (W1-W3) are applicable to the main frame, and can be removed from it, independently from each other and preferably modular for modifying the configuration of the vehicle as a function of the operations to be performed characterized in that each of said functional units (F1-F4) is housed in a respective containment frame individually applicable below the main frame, and removable or extractable from it, in order to perform maintenance operations on the functional unit (F1-F4).
Heat absorbing device comprising a structure (S1, S2, S3, S3') having a plurality of individual cells (2, 102, 202, 302), each cell (2, 102, 202, 302) being delimited by an envelope made of a material that has good thermal conductivity and contains at least one phase-change material, said structure comprising a first end surface intended to be in contact with a surface emitting a thermal flux to be absorbed, said thermal flux being made up of at least two thermal events of different amplitudes and different frequencies, said structure (S1, S2, S3, S3') comprising at least one first size of cell and one second size of cell, said device being characterized in that said cells (2, 102, 202, 302) are stacked on top of one another from said end surface so that the structure (S1, S2, S3, S3') extends at least in the direction of the thermal flux, the cells (2, 102, 202, 302) being in contact with each other by their envelope, and in that the quantity of phase-change material in each cell (102, 202, 302) is proportional to its size, wherein the first size of cell is determined as a function of the frequency of the first event and the second size of cell is determined as a function of the frequency of the second event and wherein the distribution between the number of cells of first size and the number of cells of second size is determined as a function of the amplitudes of the first and second events, and wherein the first size of cell and the second size of cell increase when the frequency of the first event and the frequency of the second event respectively reduce and wherein the number of cells of first size and the number of cells of second size increase when the amplitude of the first event and the amplitude of the second event respectively increase.
A bayonet connection structure between a mouth portion 21 of a container 20 where a pump dispenser is mounted via a cap 11, and the cap 11, wherein the cap 11 includes a plurality of slip prevention claws 12,13 spaced apart from each other in a circumferential direction on an inner circumferential surface, one of the plurality of slip prevention claws 12,13 is a slip prevention claw 12 elastically displaceable in a radial direction, and a rotation prevention projection 14 extending in an axial direction is provided between the elastically-displaceable slip prevention claw 12 and each of the other slip prevention claws 13, and the mouth portion 21 of the container 20 has a hollow cylindrical portion 22 with an outer circumferential surface provided with a plurality of slip prevention claw engagement portions 23 with which the plurality of slip prevention claws 12,13 of the cap 11 engage, the slip prevention claw engagement portions 23 being as many as the plurality of slip prevention claws, each of the slip prevention claw engagement portions 23 engaging with the other slip prevention claws 13 has an end in a clockwise direction provided with a rotation prevention stopper 24 adjacently extending in the axial direction, characterized in that the mouth portion 21 further includes a rotation prevention rib 25 extending in the axial direction, the rotation prevention rib 25 to be got over by the rotation prevention projection 14 of the cap 11 when the cap 11 is rotated.
Equipment for a wheel of a bicycle, which equipment comprises at least one profiled wing-shaped projection (25A, 25B, 25C, 25D; 25A*, 25B*, 25C*) and a rim, the profiled wing-shaped projection (25A, 25B, 25C, 25D; 25A*, 25B*, 25C*) being designed to be secured to the inner surface of the rim of the wheel itself, which equipment is characterised in that the inner profile of the profiled wing-shaped projection (25A, 25B, 25C, 25D; 25A*, 25B*, 25C*) has the following geometrical characteristics with reference to the inner radius of the rim: R 2 = 0.6 ÷ 0.8 R 1; where is the radius of an arc defining the profiled wing-shaped projection (25A, 25B, 25C, 25D; 25A*, 25B*, 25C*) and where is the inner radius of the rim; = 0.1 ÷ 0.2; where is the distance between a centre point of the rim and a centre point of the arc; and taking a quadrant of the rim delimited by points,, and, by removing from the point an angle (α) = 20° ÷ 45°, a point is drawn on the arc; and, by removing from the point an angle (β) = 20° ÷ 45°, a point is drawn on the arc; the points,,, delimiting the profiled wing-shaped projection (25A, 25B, 25C, 25D; 25A*, 25B*, 25C*). where is the radius of an arc defining the profiled wing-shaped projection (25A, 25B, 25C, 25D; 25A*, 25B*, 25C*) and where is the inner radius of the rim; = 0.1 ÷ 0.2; where is the distance between a centre point of the rim and a centre point of the arc; and taking a quadrant of the rim delimited by points,, and, by removing from the point an angle (α) = 20° ÷ 45°, a point is drawn on the arc; and, by removing from the point an angle (β) = 20° ÷ 45°, a point is drawn on the arc; the points,,, delimiting the profiled wing-shaped projection (25A, 25B, 25C, 25D; 25A*, 25B*, 25C*).