mhurhangee/patent-ind-claim-en huggingface dataset:
A process for separating solid olefin catalyst component particles from a medium in which they are present which process comprises: (i) providing in a first vessel a slurry of a liquid medium and solid olefin catalyst component particles; (ii) transferring the slurry into a hydrocyclone; (iii) removing a first by-product stream depleted in solid olefin polymerization catalyst component particles and a first product stream enriched in solid olefin polymerization catalyst component particles from the hydrocyclone; (iv) transferring the first product stream to a second vessel and in the presence of a washing medium to form a slurry and washing the solid olefin polymerization catalyst component particles with said washing medium e.g. by agitation thereof; (v) transferring the slurry back to the hydrocyclone; (vi) removing a second by-product stream depleted in solid olefin polymerization catalyst component particles and a second product stream enriched in solid olefin polymerization catalyst component particles from the hydrocyclone. (i) providing in a first vessel a slurry of a liquid medium and solid olefin catalyst component particles; (ii) transferring the slurry into a hydrocyclone; (iii) removing a first by-product stream depleted in solid olefin polymerization catalyst component particles and a first product stream enriched in solid olefin polymerization catalyst component particles from the hydrocyclone; (iv) transferring the first product stream to a second vessel and in the presence of a washing medium to form a slurry and washing the solid olefin polymerization catalyst component particles with said washing medium e.g. by agitation thereof; (v) transferring the slurry back to the hydrocyclone; (vi) removing a second by-product stream depleted in solid olefin polymerization catalyst component particles and a second product stream enriched in solid olefin polymerization catalyst component particles from the hydrocyclone.
A system for protecting the structural integrity of an engine strut , comprising: a first monitor mounted proximate an engine strut coupling a turbine engine to an airframe of an aircraft ; a second monitor mounted proximate the first monitor , the first monitor and the second monitor each configured to fail upon reaching a triggering temperature indicative of a burn-through in an engine case during operation of the turbine engine ; and a controller communicatively coupled to the first monitor and the second monitor , the controller configured to automatically reduce an operating parameter of the turbine engine upon a failure of both the first monitor and the second monitor , characterized in that at least one of the first monitor and the second monitor comprises an electrical continuity circuit having opposing ends coupled to the controller ; the controller configured to continuously pass an electrical current through the electrical continuity circuit ; and the controller correlating a cessation of electrical current flow through the electrical continuity circuit to a break in the electrical continuity circuit corresponding to failure of at least one of the first monitor and the second monitor . a first monitor mounted proximate an engine strut coupling a turbine engine to an airframe of an aircraft ; a second monitor mounted proximate the first monitor , the first monitor and the second monitor each configured to fail upon reaching a triggering temperature indicative of a burn-through in an engine case during operation of the turbine engine ; and a controller communicatively coupled to the first monitor and the second monitor , the controller configured to automatically reduce an operating parameter of the turbine engine upon a failure of both the first monitor and the second monitor , characterized in that at least one of the first monitor and the second monitor comprises an electrical continuity circuit having opposing ends coupled to the controller ; the controller configured to continuously pass an electrical current through the electrical continuity circuit ; and the controller correlating a cessation of electrical current flow through the electrical continuity circuit to a break in the electrical continuity circuit corresponding to failure of at least one of the first monitor and the second monitor .
A computer-implemented method for automatically generating a thumbnail image representing a video associated with a listing for an item in an electronic marketplace, the method comprising: retrieving the video associated with the item, wherein the video comprises a plurality of frame images; retrieving a set of item images published in positions on the listing for the item in the electronic marketplace, wherein the set of item images include an item image associated with the item; extracting a set of video frames from the video based on a sampling rule; determining a score for each of the set of video frames, wherein the score represents a degree of similarity between each of the set of video frames and each item image of the set of item images ; determining , based on the score, a weighted score for each of the set of video frames, wherein the weighted score includes a weight associated with a position of an item image of the set of item images relative to the positions of other item images published on the listing for the item in the electronic marketplace; selecting , based on the weighted score, a video frame from the set of video frames as the thumbnail image for the video ; and publishing the thumbnail image for representing the video . retrieving the video associated with the item, wherein the video comprises a plurality of frame images; retrieving a set of item images published in positions on the listing for the item in the electronic marketplace, wherein the set of item images include an item image associated with the item; extracting a set of video frames from the video based on a sampling rule; determining a score for each of the set of video frames, wherein the score represents a degree of similarity between each of the set of video frames and each item image of the set of item images ; determining , based on the score, a weighted score for each of the set of video frames, wherein the weighted score includes a weight associated with a position of an item image of the set of item images relative to the positions of other item images published on the listing for the item in the electronic marketplace; selecting , based on the weighted score, a video frame from the set of video frames as the thumbnail image for the video ; and publishing the thumbnail image for representing the video .
A translation axis assembly , comprising: a supporting arm ; a connecting plate ; and a center-of-gravity adjusting device connected between the supporting arm and the connecting plate , wherein: a position of the supporting arm on the connecting plate is adjusted by the center-of-gravity adjusting device to adjust the center of gravity of the translation axis assembly ; the center-of-gravity adjusting device comprises a locking and attachment assembly that causes the supporting arm and the connecting plate to be in a loose fit during an adjustment of the center of gravity, and that causes the connecting plate and the supporting arm to hold tightly after the adjustment of the center of gravity, wherein: the supporting arm is provided with a penetration hole connecting the connecting plate , and a locking hole in communication with the penetration hole ; characterized in that , after the adjustment of the center of gravity, the locking and attachment assembly reduces the size of the locking hole to hold the supporting arm tightly in the penetration hole . a supporting arm ; a connecting plate ; and a center-of-gravity adjusting device connected between the supporting arm and the connecting plate , wherein: a position of the supporting arm on the connecting plate is adjusted by the center-of-gravity adjusting device to adjust the center of gravity of the translation axis assembly ; the center-of-gravity adjusting device comprises a locking and attachment assembly that causes the supporting arm and the connecting plate to be in a loose fit during an adjustment of the center of gravity, and that causes the connecting plate and the supporting arm to hold tightly after the adjustment of the center of gravity, wherein: the supporting arm is provided with a penetration hole connecting the connecting plate , and a locking hole in communication with the penetration hole ; characterized in that , after the adjustment of the center of gravity, the locking and attachment assembly reduces the size of the locking hole to hold the supporting arm tightly in the penetration hole . a position of the supporting arm on the connecting plate is adjusted by the center-of-gravity adjusting device to adjust the center of gravity of the translation axis assembly ; the center-of-gravity adjusting device comprises a locking and attachment assembly that causes the supporting arm and the connecting plate to be in a loose fit during an adjustment of the center of gravity, and that causes the connecting plate and the supporting arm to hold tightly after the adjustment of the center of gravity,
A roof window with a blind frame and a sash frame that is displaceable with regard to the blind frame and bears a glazing, wherein the glazing is supported against a sash frame beam of the sash frame vertically to a glazing plane of the glazing, wherein a positioning projection for positioning the sash frame with regard to the blind frame in a lateral direction when the roof window is being closed by cooperating with a positioning device present at the sash frame is formed on the blind frame , wherein the positioning device is mounted to a sash frame beam of the sash frame and a securing device engages a side surface of the glazing, overlapping the same at least in part, to secure the glazing, characterised in that the positioning device is integrally formed with the securing device , with the result that the positioning device and the securing device are present at a structural part that is formed in one piece and/or is made of a uniform material, so that they can be commonly mounted to the sash frame beam .
An indoor unit of an air-conditioning apparatus, comprising a main body and a mounting plate , the indoor unit being configured to be installed on a wall surface by fixing the indoor unit to the wall surface by hooking a back face of the main body of the indoor unit to the mounting plate mounted on the wall surface, such that a lower part of the indoor unit may be raised in a direction away from the wall surface and the mounting plate, the main body including a back case shaped like a box and provided with an open front face , and a front case joined to the front face of the back case , characterised in that a bottom face of the front case has a step formed thereon, configured for hooking fingers and/or configured for mounting a tool for installation when the indoor unit is raised, the step being formed at a location away from a joining portion between a bottom face of the back case and the bottom face of the front case , the step protruding downward, wherein a height of the step is between 4 mm and 10 mm, both inclusive, and wherein the step is formed at a location 10 mm or more away from the joining portion . a back case shaped like a box and provided with an open front face , and a front case joined to the front face of the back case , characterised in that a bottom face of the front case has a step formed thereon, configured for hooking fingers and/or configured for mounting a tool for installation when the indoor unit is raised, the step being formed at a location away from a joining portion between a bottom face of the back case and the bottom face of the front case , the step protruding downward, wherein a height of the step is between 4 mm and 10 mm, both inclusive, and wherein the step is formed at a location 10 mm or more away from the joining portion .
In vitro use of a composition for identifying exposure to particulate matter in a lung, wherein the composition comprises an agent for measuring an expression level of Testican-1 gene or an expression level of Testican-1 protein or a fragment thereof; and wherein identifying exposure to particulate matter in a lung is by identifying an increase in expression level of Testican-1 gene or an increase in expression level of Testican-1 protein or a fragment thereof. wherein the composition comprises an agent for measuring an expression level of Testican-1 gene or an expression level of Testican-1 protein or a fragment thereof; and wherein identifying exposure to particulate matter in a lung is by identifying an increase in expression level of Testican-1 gene or an increase in expression level of Testican-1 protein or a fragment thereof.
A training device for training abdominal muscles of a user, the training device comprising an arm , a handle for holding with two hands, the handle being attached to or forming an integral part of the arm , a platform attached to or forming an integral part of the arm and configured to carry a mass , wheels or gliding or rolling means attached to the platform for enabling movement of the training device on the surface by the user when the user is holding the handle and the body of the user from hip downwards remains stationary, wherein the training device is configured to be moveable to any direction on a surface, characterized in that the training device further comprises height adjustment means for adjusting the length of the arm and thus the height of the handle , and in that the arm is a straight piece at an angle relative to the platform of approximately 45 to 75 degrees, wherein an adjustment of the length of the arm by the height adjustment means results in that the height of the handle and the radius of the mass movement are adjusted simultaneously.
A printing system , comprising: a printhead that is relatively moveable with respect to a print platform ; and an airflow generator assembly to: generate a first cooling airflow towards the printhead responsive to the printhead being in a first inactive region (118; 204-1) on a first side of the print platform , generate a second cooling airflow towards the printhead responsive to the printhead being in a second inactive region (120; 204-2) on a second side of the print platform different from the first side of the print platform , and generate a third cooling airflow towards the printhead responsive to the printhead being in a third inactive region (120; 204-2) on a third side of the print platform different from the first and second sides of the print platform . a printhead that is relatively moveable with respect to a print platform ; and an airflow generator assembly to: generate a first cooling airflow towards the printhead responsive to the printhead being in a first inactive region (118; 204-1) on a first side of the print platform , generate a second cooling airflow towards the printhead responsive to the printhead being in a second inactive region (120; 204-2) on a second side of the print platform different from the first side of the print platform , and generate a third cooling airflow towards the printhead responsive to the printhead being in a third inactive region (120; 204-2) on a third side of the print platform different from the first and second sides of the print platform . generate a first cooling airflow towards the printhead responsive to the printhead being in a first inactive region (118; 204-1) on a first side of the print platform , generate a second cooling airflow towards the printhead responsive to the printhead being in a second inactive region (120; 204-2) on a second side of the print platform different from the first side of the print platform , and generate a third cooling airflow towards the printhead responsive to the printhead being in a third inactive region (120; 204-2) on a third side of the print platform different from the first and second sides of the print platform .
A high-lift device for a flight vehicle, the high-lift device comprising: a flap main body adapted to be provided at a trailing portion of a main wing of the flight vehicle so as to be extracted from and be retracted in the trailing portion and extending in a wing span direction of the main wing ; and a vortex suppressing portion provided at a tip end portion of the flap main body in an extending direction of the flap main body and configured to suppress a vortex rolling up from a lower surface of the tip end portion of the flap main body to an upper surface of the tip end portion of the flap main body , characterized in that : the vortex suppressing portion is a flow suppressing portion formed at an upper surface side of a leading edge portion of the tip end portion of the flap main body and configured to cause a flow along the upper surface of the tip end portion of the flap main body to be separated from the upper surface; and the flow suppressing portion is a projection provided only at the tip end portion of the flap main body along the wing span direction and projecting upward from the upper surface of the flap main body . a flap main body adapted to be provided at a trailing portion of a main wing of the flight vehicle so as to be extracted from and be retracted in the trailing portion and extending in a wing span direction of the main wing ; and a vortex suppressing portion provided at a tip end portion of the flap main body in an extending direction of the flap main body and configured to suppress a vortex rolling up from a lower surface of the tip end portion of the flap main body to an upper surface of the tip end portion of the flap main body , characterized in that : the vortex suppressing portion is a flow suppressing portion formed at an upper surface side of a leading edge portion of the tip end portion of the flap main body and configured to cause a flow along the upper surface of the tip end portion of the flap main body to be separated from the upper surface; and the flow suppressing portion is a projection provided only at the tip end portion of the flap main body along the wing span direction and projecting upward from the upper surface of the flap main body . the vortex suppressing portion is a flow suppressing portion formed at an upper surface side of a leading edge portion of the tip end portion of the flap main body and configured to cause a flow along the upper surface of the tip end portion of the flap main body to be separated from the upper surface; and the flow suppressing portion is a projection provided only at the tip end portion of the flap main body along the wing span direction and projecting upward from the upper surface of the flap main body .
A device, comprising a unit of detectors that are sensitive to electromagnetic radiation, in particular an image sensor, in particular for endoscopic applications, or miniaturized monitoring cameras, wherein said sensor comprises a matrix of pixels arranged to provide an image of the explored area, the shape of which substantially corresponds to the geometry of the matrix, wherein the detectors are addressed via an addressing scheme along the lines and columns of the matrix, for permitting each line of the cell matrix to be connected to at least one reading circuit arranged at the periphery of the matrix, wherein the device is composed of a matrix of photodetection cells structured along the mutually orthogonal lines and columns, which has a polygonal shape, the contour of which comprises at least five sides inscribed in a closed line with orthogonal edges, and at least one oblique edge connecting two orthogonal edges, in particular a square or rectangular surface with at least one cut corner, in particular cut at 45°, which defines the photodetection cells cut along the oblique edge, wherein each of the photodetection cells is connected directly in terms of tension or current via an addressing system along the lines and columns to a reading circuit, characterized in that the addressing circuits of the lines or the columns are located along at least one same side of the matrix such that the addressing circuits are arranged mutually parallel and perpendicular to the at least one oblique edge.
A wear indicator operable to be secured to a surface of a gas turbine engine, the wear indicator comprising: a first side which delaminates when impacted by a blade of the gas turbine engine; a second side parallel to the first side , the second side operable to be secured to the surface of the gas turbine engine; a mid-section interposed between the first side and the second side , wherein the midsection includes one outer surface between the first side and the second side ; characterized in that the wear indicator further comprises: an orifice initiating at the first side and extending through the midsection to the second side ; and at least three reference dimensions (ID1, OD3, α) that remain constant when the first side delaminates, wherein the at least three reference dimensions include a diameter (ID1) of the orifice , an outer diameter (OD3) of the second side , and an angle (α) between the second side and the outer surface of the midsection . a first side which delaminates when impacted by a blade of the gas turbine engine; a second side parallel to the first side , the second side operable to be secured to the surface of the gas turbine engine; a mid-section interposed between the first side and the second side , wherein the midsection includes one outer surface between the first side and the second side ; characterized in that the wear indicator further comprises: an orifice initiating at the first side and extending through the midsection to the second side ; and at least three reference dimensions (ID1, OD3, α) that remain constant when the first side delaminates, wherein the at least three reference dimensions include a diameter (ID1) of the orifice , an outer diameter (OD3) of the second side , and an angle (α) between the second side and the outer surface of the midsection . an orifice initiating at the first side and extending through the midsection to the second side ; and at least three reference dimensions (ID1, OD3, α) that remain constant when the first side delaminates, wherein the at least three reference dimensions include a diameter (ID1) of the orifice , an outer diameter (OD3) of the second side , and an angle (α) between the second side and the outer surface of the midsection .
A vacuum cleaning utensil having a brush (B) arranged for rotating about a substantially vertical axis (A), wherein the vacuum cleaning utensil is provided with a guide (G) for pushing the brush (B) towards a surface (S) to be cleaned during only a part of the rotation of the brush (B), characterized in that the brush (B) is arranged for being released from the surface (S) during another part of the rotation.
Side gate nozzle comprising a supply block , a distribution block and a nozzle block interconnected to each other in an axial direction (z), a. wherein the nozzle block comprises at least one nozzle recess , in which a nozzle insert is arranged which in the axial direction (z) is held by a set screw interconnected to the nozzle block , characterized in that b. the set screw expands at least partially across the nozzle recess ; c. the diameter of the set screw is bigger than the width of the nozzle recess in a lateral direction , d. the set screw interacts with an inside thread arranged at two opposite side walls of the nozzle recess . a. wherein the nozzle block comprises at least one nozzle recess , in which a nozzle insert is arranged which in the axial direction (z) is held by a set screw interconnected to the nozzle block , characterized in that b. the set screw expands at least partially across the nozzle recess ; c. the diameter of the set screw is bigger than the width of the nozzle recess in a lateral direction , d. the set screw interacts with an inside thread arranged at two opposite side walls of the nozzle recess .