mhurhangee/patent-ind-claim-en huggingface dataset:
Window , in particular door window, having a. a window frame and at least one sash rotatably attached thereto, b. which has at least one sash frame , wherein the sash frame accommodates a panel element and the sash frame is composed of a plurality of sash frame spars (103-106, 103'-106'), and c. having fittings for rotatably moving the sash relative to the window frame into an open state and into a closed state, d. wherein a movable rebate drive bolt is preferably provided for locking the sash in the closed state, which is movable into the window frame - in particular into a striking plate which is fastened to/in the window frame - and then engages there, e. and at least one sash stop and support device , which is designed to stop a rotary movement of the wing , f. the sash stop and support device has a support block and stop movable by a magnetic pivot drive means with a support cam on the sash or window frame and an abutment on the window frame or sash , in which the support cam engages at least in the closed state of the sash, characterized in that g. the sash stop and support device is further designed to lift the sash so that a lower corner of the sash facing away from the pivot fitting is firmly supported in the closed state. a. a window frame and at least one sash rotatably attached thereto, b. which has at least one sash frame , wherein the sash frame accommodates a panel element and the sash frame is composed of a plurality of sash frame spars (103-106, 103'-106'), and c. having fittings for rotatably moving the sash relative to the window frame into an open state and into a closed state, d. wherein a movable rebate drive bolt is preferably provided for locking the sash in the closed state, which is movable into the window frame - in particular into a striking plate which is fastened to/in the window frame - and then engages there, e. and at least one sash stop and support device , which is designed to stop a rotary movement of the wing , f. the sash stop and support device has a support block and stop movable by a magnetic pivot drive means with a support cam on the sash or window frame and an abutment on the window frame or sash , in which the support cam engages at least in the closed state of the sash, characterized in that g. the sash stop and support device is further designed to lift the sash so that a lower corner of the sash facing away from the pivot fitting is firmly supported in the closed state.
A scheduling timing determination method, applied to a terminal, comprising: receiving scheduling information from a network side device carried in a control channel on a scheduling carrier, and obtaining a slot offset between the control channel and a data channel according to the scheduling information; determining a relative slot where the data channel is transmitted on a scheduled carrier according to a subcarrier spacing of the scheduling carrier, a subcarrier spacing of the scheduled carrier, the slot offset between the control channel and the data channel, and a starting symbol of the control channel transmitted in a slot on the scheduling carrier, wherein the relative slot uses a starting time of the slot where the control channel is transmitted on the scheduling carrier as a reference point; determining a transmission slot of the data channel on the scheduled carrier according to the relative slot; characterized in that the relative slot is: K slot = ⌊ 2 μ scheduled / 2 μ scheduling × S / m ⌋ + K indicated , wherein, μ scheduled is a index of the subcarrier spacing of the scheduled carrier, μ scheduling is a index of the subcarrier spacing of the scheduling carrier, S is a index of the starting symbol of the control channel transmitted in the slot on the scheduling carrier, K indicated is the slot offset value between the control channel and the data channel, and m is the quantity of symbols within one slot. receiving scheduling information from a network side device carried in a control channel on a scheduling carrier, and obtaining a slot offset between the control channel and a data channel according to the scheduling information; determining a relative slot where the data channel is transmitted on a scheduled carrier according to a subcarrier spacing of the scheduling carrier, a subcarrier spacing of the scheduled carrier, the slot offset between the control channel and the data channel, and a starting symbol of the control channel transmitted in a slot on the scheduling carrier, wherein the relative slot uses a starting time of the slot where the control channel is transmitted on the scheduling carrier as a reference point; determining a transmission slot of the data channel on the scheduled carrier according to the relative slot; characterized in that the relative slot is: K slot = ⌊ 2 μ scheduled / 2 μ scheduling × S / m ⌋ + K indicated , wherein, μ scheduled is a index of the subcarrier spacing of the scheduled carrier, μ scheduling is a index of the subcarrier spacing of the scheduling carrier, S is a index of the starting symbol of the control channel transmitted in the slot on the scheduling carrier, K indicated is the slot offset value between the control channel and the data channel, and m is the quantity of symbols within one slot.
A glass panel unit comprising: a first panel (T10) including at least a first glass plate ; a second panel (T20) facing the first panel (T10) and including at least a second glass plate ; a sealing member formed in a frame shape and bonded hermetically to respective facing peripheral portions of the first panel (T10) and the second panel (T20); and at least one spacer provided in an inner space between the first panel (T10) and the second panel (T20), the inner space being a reduced pressure space, the at least one spacer including a resin body , characterised in that said at least one spacer further includes at least one ultraviolet protective layer provided on a surface of the resin body , a thickness of the ultraviolet protective layer being in a range of 0.01 to 10 μm. a first panel (T10) including at least a first glass plate ; a second panel (T20) facing the first panel (T10) and including at least a second glass plate ; a sealing member formed in a frame shape and bonded hermetically to respective facing peripheral portions of the first panel (T10) and the second panel (T20); and at least one spacer provided in an inner space between the first panel (T10) and the second panel (T20), the inner space being a reduced pressure space, the at least one spacer including a resin body , characterised in that said at least one spacer further includes at least one ultraviolet protective layer provided on a surface of the resin body , a thickness of the ultraviolet protective layer being in a range of 0.01 to 10 μm.
An aerodynamic blade , comprising: a blade body comprising an inboard end and a tip outboard of the inboard end, the blade body being connectable with a hub at the inboard end such that rotations of the hub drive rotations of the tip about a rotational axis (A); and a light module disposed in the tip and configured to activate in response to the rotations of the tip about the rotational axis to emit light visible at an exterior of the blade body; wherein the blade body has an airfoil shape configured for operation with one or more of a rotor, a propeller and a fan; the aerodynamic blade characterized in that the tip of the blade body comprises: inboard and outboard blade structures, the inboard blade structure having an outboard side adjacent to the light module ; a securing feature interposed between the light module and the outboard blade structure; and sheaths partially covering upper and lower surfaces of the inboard and outboard blade structures, the light module and the securing feature, the sheaths defining slots and the light module comprising lenses protruding through the slots. a blade body comprising an inboard end and a tip outboard of the inboard end, the blade body being connectable with a hub at the inboard end such that rotations of the hub drive rotations of the tip about a rotational axis (A); and a light module disposed in the tip and configured to activate in response to the rotations of the tip about the rotational axis to emit light visible at an exterior of the blade body; wherein the blade body has an airfoil shape configured for operation with one or more of a rotor, a propeller and a fan; the aerodynamic blade characterized in that the tip of the blade body comprises: inboard and outboard blade structures, the inboard blade structure having an outboard side adjacent to the light module ; a securing feature interposed between the light module and the outboard blade structure; and sheaths partially covering upper and lower surfaces of the inboard and outboard blade structures, the light module and the securing feature, the sheaths defining slots and the light module comprising lenses protruding through the slots. inboard and outboard blade structures, the inboard blade structure having an outboard side adjacent to the light module ; a securing feature interposed between the light module and the outboard blade structure; and sheaths partially covering upper and lower surfaces of the inboard and outboard blade structures, the light module and the securing feature, the sheaths defining slots and the light module comprising lenses protruding through the slots.
Electrical distribution device for an ignition system of an engine of an aircraft comprising a main electrical power supply and a secondary electrical power supply , a main ignitor and a secondary ignitor comprising an electrical power supply system suitable for powering at least one of said ignitors alternately by one or other of said electrical power supplies, said electrical power supply system comprising a switch linked to at least one of said main and secondary ignitors and suitable for alternately powering it by one or other of the two electrical power supplies, characterized in that it comprises a means for breaking at least one of the main and secondary power supplies to simulate an electrical power supply failure and a power supply control means configured to detect whether the ignitor linked to the switch is powered or not.
Rotor of an axial compressor stage of a turbomachine, featuring: - a rotor body including a rotary axis , a circumference and a blade ring arranged on the circumference with a radially outer ring surface , and - a plurality of rotor blades arranged on the blade ring , wherein the ring surface has at least one area between two adjacent rotor blades of the plurality of rotor blades, which shows a changing radius (r) relative to the rotary axis of the rotor body both in the axial direction (x) and in the circumferential direction (Φ), wherein in an area between two adjacent rotor blades the ring surface is shaped such that it has a resulting surface line which shows in the direction of an axially rear face of the blade ring first a concave depression and at a certain axial distance to said depression a convex elevation , with the concave depression being situated at the start of the blade duct formed by two rotor blades in each case, and the convex elevation being situated behind the concave depression in the axial direction, wherein the convex elevation includes a mountain, which in the area between two adjacent rotor blades extends at a certain distance to both, the suction side of the one rotor blade and the pressure side of the other rotor blade , while being arranged closer to the suction side of the one rotor blade , wherein in the area between two adjacent rotor blades , on which the ring surface is formed with a concave depression and with a convex elevation , a second surface line of an area through the rotor body in a plane perpendicular to the rotary axis of the rotor body obeys a mathematical function in the form of a single sine function or a single cosine function, and wherein in the area between two adjacent rotor blades each section through the blade ring in a plane perpendicular to the rotary axis of the rotor body has a surface line, which obeys a mathematical function in the form of a single sine function or a single cosine function. - a rotor body including a rotary axis , a circumference and a blade ring arranged on the circumference with a radially outer ring surface , and - a plurality of rotor blades arranged on the blade ring ,
An electrical installation housing comprising at least one support pillar at whose upper side fastening means for cover plates or for frame elements are provided, wherein at least one partition wall dividing the installation housing can be inserted into the support pillar or the support pillar is provided with at least one such partition wall , characterized in that the support pillar can be fastened without tools in the installation housing in that the support pillar can be clipped into the installation housing from above or laterally.
A dispense volume monitor comprising: a capacitor that comprises: at least one upper electrode ; at least one lower electrode ; and a test plate comprising at least one well adapted to contain a dispensed liquid volume ; wherein said at least one upper electrode is cylindrical, having an upper end and a lower end and an outer diameter that is smaller than the inner diameter of said at least one well; and said at least one upper electrode is capable of being positioned in said at least one well of said test plate and said at least one lower electrode is adjacent to an exterior bottom surface of said test plate , below said at least one well , wherein said at least one upper electrode does not come into contact with the dispensed liquid volume; characterized in that said lower end of said at least one upper electrode is positioned at 50% or less of the total height of said at least one well . a capacitor that comprises: at least one upper electrode ; at least one lower electrode ; and a test plate comprising at least one well adapted to contain a dispensed liquid volume ; at least one upper electrode ; at least one lower electrode ; and a test plate comprising at least one well adapted to contain a dispensed liquid volume ; wherein said at least one upper electrode is cylindrical, having an upper end and a lower end and an outer diameter that is smaller than the inner diameter of said at least one well; and said at least one upper electrode is capable of being positioned in said at least one well of said test plate and said at least one lower electrode is adjacent to an exterior bottom surface of said test plate , below said at least one well , wherein said at least one upper electrode does not come into contact with the dispensed liquid volume; characterized in that said lower end of said at least one upper electrode is positioned at 50% or less of the total height of said at least one well .
An inspection device for parisons comprising at least a first conveying means having, on one side of it, a plurality of seats for receiving an array of respective parisons , wherein the first conveying means is movable between a first station (S1) for receiving the parisons and a second station (S2) for releasing the parisons and wherein the first conveying means is movable between the first and second stations (S1, S2) along a trajectory having at least one stretch which is transverse to the longitudinal axis of the parisons on the first conveying means , wherein the device comprises a first optical detection unit located at a fixed position and facing the first conveying means on the side of the latter which receives the parisons at least at the transverse stretch of the trajectory to inspect at least one portion of the parisons which faces the first optical detection unit , characterized in that it further comprises a second conveying means having, on one side of it, a plurality of respective seats for receiving an array of respective parisons and movable between the second station (S2), where it receives a plurality of parisons from the first conveying means and a third station (S3) for unloading the parisons , where the second conveying means is configured to hold the parisons at the ends of the parisons opposite the portions of the parisons gripped by the first conveying means , the second conveying means being movable between the second and third stations (S2, S3) along a trajectory having at least one stretch which is transverse to the longitudinal axis of the parisons on the second conveying means , the device further comprising a second optical detection unit facing the second conveying means on the side of the latter which receives the parisons at least at the transverse stretch of the trajectory of the second conveying means to inspect at least one portion of the parisons which faces the second optical detection unit .
Piezoelectric composite comprising a polymeric matrix and piezoelectric inorganic fillers in the form of particles which are not bound to the polymeric matrix, which are dispersed in said polymeric matrix, said polymeric matrix comprising a thermoplastic elastomer which is a linear or star-branched diblock or triblock copolymer, in that the glass transition temperature, Tg, of each thermoplastic block of the thermoplastic elastomer is lower than the lowest Curie temperature, Tc, of the piezoelectric inorganic fillers, moreover when the thermoplastic blocks have a melting point, Tm, said melting point of each thermoplastic block is also lower than the lowest Curie temperature of the piezoelectric inorganic fillers, and in that the filler content of the piezoelectric inorganic fillers is at least 5% by volume relative to the total volume of polymeric matrix, characterized in that the thermoplastic elastomer is selected from styrene/butadiene, styrene/isoprene, styrene/butadiene/isoprene, styrene/butadiene/styrene, styrene/isoprene/styrene, styrene/butadiene/isoprene/styrene and mixtures of these copolymers.
Apparatus for cutting products, comprising: - a base (100; 110; 130); - a cutting head (200; 400; 600) with at least one cutting element (208; 258, 259; 402) along the circumference of the cutting head for cutting products fed into the cutting head, the cutting head being rotatably fitted to the base with the at least one cutting element oriented to impart cutting action in a first rotational direction; - an impeller (300; 410; 420; 500) adapted for rotating concentrically within the cutting head to urge products fed into the cutting head towards the circumference of the cutting head by means of centrifugal force; - an impeller drive mechanism (301-303) adapted for driving the impeller to make it rotate in said first rotational direction at an impeller rotational speed which sets the centrifugal force; and - a cutting head drive mechanism (201-203) adapted for driving the cutting head to make it rotate in said first rotational direction at a cutting head rotational speed, such that the product is cut by the at least one cutting element at a predetermined cutting velocity; characterised in that the impeller drive mechanism and the cutting head drive mechanism are provided with controls for controlling the impeller rotational speed and the cutting head rotational speed within respectively a first range and a second range with the cutting head rotational speed a predetermined difference greater than the impeller rotational speed. - a base (100; 110; 130); - a cutting head (200; 400; 600) with at least one cutting element (208; 258, 259; 402) along the circumference of the cutting head for cutting products fed into the cutting head, the cutting head being rotatably fitted to the base with the at least one cutting element oriented to impart cutting action in a first rotational direction; - an impeller (300; 410; 420; 500) adapted for rotating concentrically within the cutting head to urge products fed into the cutting head towards the circumference of the cutting head by means of centrifugal force; - an impeller drive mechanism (301-303) adapted for driving the impeller to make it rotate in said first rotational direction at an impeller rotational speed which sets the centrifugal force; and - a cutting head drive mechanism (201-203) adapted for driving the cutting head to make it rotate in said first rotational direction at a cutting head rotational speed, such that the product is cut by the at least one cutting element at a predetermined cutting velocity;
A method for generating a blurred image, comprising: determining (S101), according to preview image data acquired via two rear cameras of a dual-camera device, first depth-of-field information for a foreground region and second depth-of-field information for a background region in a current preview image, wherein the two rear cameras face the same direction and are arranged along a horizontal direction or along a vertical direction; acquiring (S102) a basic value of a blurring degree according to the first depth-of-field information and the second depth-of-field information; and performing (S103; S307) Gaussian blur process on the background region according to the basic value of the blurring degree to generate (S308) the blurred image; wherein acquiring (S102) the basic value of the blurring degree according to the first depth-of-field information and the second depth-of-field information comprises: acquiring a first average value for the first depth-of-field information and a second average value for the second depth-of-field information; and calculating (S305) a ratio of the first average value and the second average value to acquire the basic value of the blurring degree. determining (S101), according to preview image data acquired via two rear cameras of a dual-camera device, first depth-of-field information for a foreground region and second depth-of-field information for a background region in a current preview image, wherein the two rear cameras face the same direction and are arranged along a horizontal direction or along a vertical direction; acquiring (S102) a basic value of a blurring degree according to the first depth-of-field information and the second depth-of-field information; and performing (S103; S307) Gaussian blur process on the background region according to the basic value of the blurring degree to generate (S308) the blurred image; wherein acquiring (S102) the basic value of the blurring degree according to the first depth-of-field information and the second depth-of-field information comprises: acquiring a first average value for the first depth-of-field information and a second average value for the second depth-of-field information; and calculating (S305) a ratio of the first average value and the second average value to acquire the basic value of the blurring degree. acquiring a first average value for the first depth-of-field information and a second average value for the second depth-of-field information; and calculating (S305) a ratio of the first average value and the second average value to acquire the basic value of the blurring degree.