mhurhangee/ep-ind-claims huggingface dataset:
A dental filler system comprising: a polytetrafluoroethylene dental filament (700, 800, 900, 1000, 1100) having a first length and a first diameter; and a dental prosthetic (212, 312, 412) having an access channel (214, 314, 414) formed therein, the access channel (214, 314, 414) having a second diameter that is larger than the first diameter, having a fill length that is smaller than the first length, and being shaped to receive a fastener (206, 306, 406), characterized in that the polytetrafluoroethylene dental filament (700, 800, 900, 1000, 1100) includes porous polytetrafluoroethylene. a polytetrafluoroethylene dental filament (700, 800, 900, 1000, 1100) having a first length and a first diameter; and a dental prosthetic (212, 312, 412) having an access channel (214, 314, 414) formed therein, the access channel (214, 314, 414) having a second diameter that is larger than the first diameter, having a fill length that is smaller than the first length, and being shaped to receive a fastener (206, 306, 406), characterized in that the polytetrafluoroethylene dental filament (700, 800, 900, 1000, 1100) includes porous polytetrafluoroethylene.
An auxiliary apparatus for MIS to maneuver a surgery target comprising: a) an in vivo device, with an in vivo magnet comprised in the in vivo device, the in vivo device further comprises a clip to anchor the in vivo device to the surgery target and a connector to join the clip with the in vivo magnet; b) an external device, comprised of an external magnetic field generating element; wherein the in vivo magnet can move and/or rotate in accordance with a direction change of an external magnetic field which is generated by the external magnetic field generating element, and thereby the surgery target can move in a controlled speed and/or rotate in a controlled angle in accordance with the direction change of the said external magnetic field, wherein the in vivo device comprises a supporting set to integrate the in vivo magnet into an assembly; characterized in that, the supporting set comprises a base and a top cover, the base comprises a bed to attach with the top cover and limit the in vivo magnet to move along the length direction of the supporting set, and a supporting column which runs from the bed to the top cover to limit the in vivo magnet to move along the radial direction of the supporting set; the top cover comprises a cavity to receive and fasten a distal end of the supporting column, which is distant from the bed; and a hole is disposed between the base and the top cover for the connector to pass along the length direction of the supporting set. a) an in vivo device, with an in vivo magnet comprised in the in vivo device, the in vivo device further comprises a clip to anchor the in vivo device to the surgery target and a connector to join the clip with the in vivo magnet; b) an external device, comprised of an external magnetic field generating element; wherein the in vivo magnet can move and/or rotate in accordance with a direction change of an external magnetic field which is generated by the external magnetic field generating element, and thereby the surgery target can move in a controlled speed and/or rotate in a controlled angle in accordance with the direction change of the said external magnetic field, wherein the in vivo device comprises a supporting set to integrate the in vivo magnet into an assembly; characterized in that, the supporting set comprises a base and a top cover, the base comprises a bed to attach with the top cover and limit the in vivo magnet to move along the length direction of the supporting set, and a supporting column which runs from the bed to the top cover to limit the in vivo magnet to move along the radial direction of the supporting set; the top cover comprises a cavity to receive and fasten a distal end of the supporting column, which is distant from the bed; and a hole is disposed between the base and the top cover for the connector to pass along the length direction of the supporting set.
A method, for handover of activities between a vehicle and a wearable device comprising: inputting a destination into a wearable device; providing, by a wearable device, walking guidance to a vehicle; determining, by a wireless phone that is paired with the wearable device, that the wearable device has reached the vehicle; establishing a connection between the wireless phone and a device in the vehicle; transferring the destination from the wireless phone to the device in the vehicle over the established connection; and providing driving navigation guidance to the destination by the device in the vehicle. inputting a destination into a wearable device; providing, by a wearable device, walking guidance to a vehicle; determining, by a wireless phone that is paired with the wearable device, that the wearable device has reached the vehicle; establishing a connection between the wireless phone and a device in the vehicle; transferring the destination from the wireless phone to the device in the vehicle over the established connection; and providing driving navigation guidance to the destination by the device in the vehicle.
A pulse wave analyzing apparatus comprising: an acquiring section which is configured to acquire a pulse wave that is non-invasively measured; and an analyzer which is configured to calculate data on a frequency axis by using the pulse wave, and obtain an index value of a respiratory-induced variation based on the data on the frequency axis, wherein the analyzer is configured to produce data on a time axis indicating a variation rate of an amplitude of the pulse wave, by using the pulse wave, characterized in that the analyzer is further configured to frequency-analyze the variation rate on the time axis, and calculate the index value of the respiratory-induced variation based on a power value of the variation rate at a frequency corresponding to a respiratory cycle of a subject. an acquiring section which is configured to acquire a pulse wave that is non-invasively measured; and an analyzer which is configured to calculate data on a frequency axis by using the pulse wave, and obtain an index value of a respiratory-induced variation based on the data on the frequency axis, wherein the analyzer is configured to produce data on a time axis indicating a variation rate of an amplitude of the pulse wave, by using the pulse wave, characterized in that the analyzer is further configured to frequency-analyze the variation rate on the time axis, and calculate the index value of the respiratory-induced variation based on a power value of the variation rate at a frequency corresponding to a respiratory cycle of a subject.
A method for additional cladding of pipe form parts, in which the pipe form part is cladded by means of a shrink-on sleeve that shrinks when heat is applied, characterized in that a plastic pipe material, which is widened under pressure and heat, is initially cut up into axial segmental elements (12a, 12b, 12c, 12d), the segmental elements are pushed on a core pipe of the pipe form part and these segmental elements are reassembled into a segmental shrink-on sleeve at angles corresponding to the pipe form part to be produced, wherein the segmental elements are butt-welded to one another so as to form a segmental shrink-on sleeve by means of an apertured heat reflector and the segmental shrink-on sleeve is then shrunk under the input of heat.
A sorbent material comprising silanized silica at least partially coated with poly(benzyl methacrylate), obtainable by the method comprising: suspending silica in a solution of dimethylvinylchlorosilane in trifluorotoluene; removing the liquid and resuspending the silica in a fresh solution of dimethylvinylchlorosilane in trifluorotoluene; optionally removing the liquid and resuspending the silica again in a fresh 5% solution of dimethylvinylchlorosilane in trifluorotoluene; collecting and drying the resulting silanized silica; adding the silanized silica, benzylmethacrylate and potassium peroxodisulfate to a stirred solution of sodium stearate in water; and collecting and drying the resultant sorbent material comprising silanized silica coated with poly(benzyl methacrylate). suspending silica in a solution of dimethylvinylchlorosilane in trifluorotoluene; removing the liquid and resuspending the silica in a fresh solution of dimethylvinylchlorosilane in trifluorotoluene; optionally removing the liquid and resuspending the silica again in a fresh 5% solution of dimethylvinylchlorosilane in trifluorotoluene; collecting and drying the resulting silanized silica; adding the silanized silica, benzylmethacrylate and potassium peroxodisulfate to a stirred solution of sodium stearate in water; and collecting and drying the resultant sorbent material comprising silanized silica coated with poly(benzyl methacrylate).
A method comprising: causing one or more sensors arranged on an aircraft to acquire, over a window of time, first data associated with a first object that is within an environment of the aircraft, wherein the one or more sensors include one or more of a light detection and ranging sensor, a radar sensor, or a camera; causing an array of microphones arranged on the aircraft to acquire, over approximately the same window of time as the first data is acquired, first acoustic data associated with the first object; and training, by a processor, a machine learning model by using the first acoustic data as an input value to the machine learning model and by using an azimuth of the first object, a range of the first object, an elevation of the first object, and a type of the first object identified from the first data as ground truth output labels for the machine learning model, wherein the machine learning model is configured to predict, based on target acoustic data subsequently acquired by the array of microphones and associated with a target object within the environment of the aircraft, an azimuth of the target object, a range of the target object, an elevation of the target object, and a type of the target object. causing one or more sensors arranged on an aircraft to acquire, over a window of time, first data associated with a first object that is within an environment of the aircraft, wherein the one or more sensors include one or more of a light detection and ranging sensor, a radar sensor, or a camera; causing an array of microphones arranged on the aircraft to acquire, over approximately the same window of time as the first data is acquired, first acoustic data associated with the first object; and training, by a processor, a machine learning model by using the first acoustic data as an input value to the machine learning model and by using an azimuth of the first object, a range of the first object, an elevation of the first object, and a type of the first object identified from the first data as ground truth output labels for the machine learning model, wherein the machine learning model is configured to predict, based on target acoustic data subsequently acquired by the array of microphones and associated with a target object within the environment of the aircraft, an azimuth of the target object, a range of the target object, an elevation of the target object, and a type of the target object.
An underfloor distributor for electrical and/or electronic devices, particularly for telecommunications, with a duct which is installable in the ground under the floor, which has at least one cover and an airtight cap, in which the electrical and/or electronic devices are arranged and which is arranged to be pivotable upwardly out of a horizontal position in the duct, in which the bottom of the cap is open, into a vertical position, wherein secured in the cap there is a housing, which includes a cold air chamber and at least one further separate chamber, wherein formed in the at least one cover on an edge region there is at least one opening for the entry of cold air into the duct, wherein the region below this at least one opening is shielded by plates of the remaining duct and wherein the upper end of a cold air pipe projects into this region, wherein in the base region the cold air chamber has an opening, with which the cold air pipe communicates, wherein the cold air chamber is in flow communication with the at least one separate further chamber, wherein the electrical and/or electronic devices are arranged in the at least one separate chamber, wherein the at least one further chamber is designed so that the cold air under pressure flows through it and thus cools the electrical and/or electronic devices and wherein the arrangement consisting of cap and chamber is so designed that the thus heated air discharges out of the at least one further separate chamber and then downwardly out of the cap and leaves the duct through openings in the at least one cover.
A pump with variable suction/discharge amount, which includes a vane chamber body and a vane rotor, the vane chamber body having a vane chamber, characterized in that the vane chamber is defined between a fixed wall member, a movable wall member and a movable vane chamber sleeve in the vane chamber body and having a capacity space, the vane chamber being partitioned by an impeller of the vane rotor in the vane chamber to form at least one eccentric vane chamber sections (2301,2303), at least one vane being disposed on the impeller, the number of the eccentric vane chamber sections (2301, 2302) being more than or equal to the number of the vanes, one side of the vanes in the eccentric vane chamber sections (2301, 2302) being a suction side, while one side of the vanes in the eccentric vane chamber sections (2301, 2302) being a discharge side, the suction side and the discharge side respectively having suction/discharge passages in communication with outer side of the pump, the fixed wall member being positioned in a fixed position in the vane chamber body, the movable wall member and the movable vane chamber sleeve being displaceable in an axial direction of the vane rotor relative to the fixed wall member to increase/decrease and change the capacity space of the vane chamber, so as to form a pump with variable suction/discharge amount.
Motorized strength training machine comprising an electric motor unit, an axle and a first user force input element, said electric motor unit comprising an electric motor, said electric motor being connected to said axle such that rotation of the electric motor drives said axle and rotation of the axle drives the electric motor, and said first user force input element being connected to said axle such that rotation of said axle displaces the first user force input element and displacement of said first user force input element rotates the axle, said machine further comprising a mechanical range limiting mechanism (24, 57) comprising displaceable first and second rotation limiting stop elements (94, 96) which can be mechanically locked at different angular locations around the axle to mechanically limit the range of rotational motion of the axle, characterized in that the mechanical range limiting mechanism comprises a motorized displacement mechanism which is arranged to displace the first and/or second rotation limiting end stops angularly around the axle based on inputs from a controller.
A tubular damper unit to be disposed between a propeller shaft of a vessel propulsion apparatus and a propeller member including a plurality of blades provided on an outer surface of the propeller member, the damper unit comprising: a bushing to be spline-coupled to the propeller shaft, including a first cylindrical portion and a plurality of first protrusions, the first cylindrical portion being made of metal, the first cylindrical portion surrounding the propeller shaft, the first cylindrical portion including a spline hole provided on an inner circumferential surface of the first cylindrical portion, the first protrusions being integral with the first cylindrical portion; and a propeller damper made of an elastic material and disposed around the first cylindrical portion of the bushing; characterized in that the first protrusions protrude outward from a front portion of the first cylindrical portion; and the propeller damper is disposed at a position more rearward than the first protrusions. a bushing to be spline-coupled to the propeller shaft, including a first cylindrical portion and a plurality of first protrusions, the first cylindrical portion being made of metal, the first cylindrical portion surrounding the propeller shaft, the first cylindrical portion including a spline hole provided on an inner circumferential surface of the first cylindrical portion, the first protrusions being integral with the first cylindrical portion; and a propeller damper made of an elastic material and disposed around the first cylindrical portion of the bushing; characterized in that the first protrusions protrude outward from a front portion of the first cylindrical portion; and the propeller damper is disposed at a position more rearward than the first protrusions.
Method for determining geometric properties of a structure of an object displayed in a 3D image, comprising a computer performing the steps of: (a) loading a predetermined extended deformable 3D surface model of a training object corresponding to the displayed object, wherein the deformable surface model describes a surface of the object and comprises integrated additional geometrical information identifying surface elements of the deformable 3D surface model which belong to a sub-part of the object, identifying a geometric primitive in accordance with the form of the sub-part, and identifying a transformation rule which maps the geometric primitive onto the surface elements of the deformable surface model; (b) adapting (102, 103) the loaded extended deformable 3D surface model to the surface of the displayed object; (c) adapting (104, 105) the additional geometric information of the extended deformable 3D surface model to the object, by using the rule to map the geometric primitive onto a sub-part of the displayed object; and then (d) extracting the geometric properties of the structure of the displayed object from the adapted extended deformable 3D surface model to which additional geometrical information has been applied. (a) loading a predetermined extended deformable 3D surface model of a training object corresponding to the displayed object, wherein the deformable surface model describes a surface of the object and comprises integrated additional geometrical information identifying surface elements of the deformable 3D surface model which belong to a sub-part of the object, identifying a geometric primitive in accordance with the form of the sub-part, and identifying a transformation rule which maps the geometric primitive onto the surface elements of the deformable surface model; (b) adapting (102, 103) the loaded extended deformable 3D surface model to the surface of the displayed object; (c) adapting (104, 105) the additional geometric information of the extended deformable 3D surface model to the object, by using the rule to map the geometric primitive onto a sub-part of the displayed object; and then (d) extracting the geometric properties of the structure of the displayed object from the adapted extended deformable 3D surface model to which additional geometrical information has been applied.
A method for detecting an antigen in a sample, the method comprising: printing a plurality of capture antibody features in a well of a testing substrate, printing a calibration compound of known concentration on one of the capture antibody features in the well of the testing substrate, wherein the calibration compound of known concentration is capable of binding to the capture antibody feature, wherein at least one capture antibody feature in the well of the testing substrate does not have a calibration compound of known concentration printed onto the at least one capture antibody feature and is capable of binding to the antigen in the sample, and adding the sample to the well of the testing substrate, wherein the calibration compound and the antigen are each capable of binding to a same enzyme linked detect antibody. printing a plurality of capture antibody features in a well of a testing substrate, printing a calibration compound of known concentration on one of the capture antibody features in the well of the testing substrate, wherein the calibration compound of known concentration is capable of binding to the capture antibody feature, wherein at least one capture antibody feature in the well of the testing substrate does not have a calibration compound of known concentration printed onto the at least one capture antibody feature and is capable of binding to the antigen in the sample, and adding the sample to the well of the testing substrate, wherein the calibration compound and the antigen are each capable of binding to a same enzyme linked detect antibody.
A tire mold having one or more moveable elements to bring the tire mold from an open into a closed position, the tire mold comprising: an actuating ring, a top plate and a bottom plate, upper and lower side members (7, 9), a plurality of mold segments and slide blocks; wherein the upper and lower side members (7, 9) and the plurality of mold segments define a mold cavity; and wherein the tire mold further comprises a vacuum device for removing gas from the mold cavity upon its activation; characterized in that the tire mold has sealing means comprising one or more closing seal members (39, 41, 43, 45, 47) configured to cooperate with associated cooperating surfaces for sealing the mold cavity by contact with each other, the one or more closing seal members and the associated cooperating surfaces being moveable relative to one another upon the displacement of the one or more moveable elements, and wherein said one or more closing seal members are in a position in which they are facing their associated cooperating surfaces without contacting them, both in a partial closure position of the tire mold and in the closed position of the tire mold when the vacuum device is not activated. an actuating ring, a top plate and a bottom plate, upper and lower side members (7, 9), a plurality of mold segments and slide blocks; wherein the upper and lower side members (7, 9) and the plurality of mold segments define a mold cavity; and wherein the tire mold further comprises a vacuum device for removing gas from the mold cavity upon its activation; characterized in that the tire mold has sealing means comprising one or more closing seal members (39, 41, 43, 45, 47) configured to cooperate with associated cooperating surfaces for sealing the mold cavity by contact with each other, the one or more closing seal members and the associated cooperating surfaces being moveable relative to one another upon the displacement of the one or more moveable elements, and wherein said one or more closing seal members are in a position in which they are facing their associated cooperating surfaces without contacting them, both in a partial closure position of the tire mold and in the closed position of the tire mold when the vacuum device is not activated.
Detoxifying composition for use thereof via oral administration route as detoxifier with a view to promoting elimination of body waste via hepatic route, characterized in that it comprises dried pepper plant inflorescence stems, optionally ground, and optionally screened and/or an aqueous or dry extract of pepper plant inflorescence stems.