mhurhangee/patent-ind-claim-en huggingface dataset:
A surgical probe for treating rhinitis of a patient, comprising: an elongated probe shaft with a proximal end and a distal end; a handle coupled to the proximal end; an ultrasound transducer coupled to the probe shaft ; and a cryo-ablation element coupled to the probe shaft ; wherein the ultrasound transducer includes an ultrasound emitter configured to emit an ultrasound signal and an ultrasound receiver configured to receive a reflected ultrasound signal for determining a location of a target treatment site within a nasal cavity of the patient, and wherein the cryo-ablation element is configured to be positioned at the target treatment site location to cryogenically ablate the target treatment site in order to ablate at least one nasal nerve to reduce at least one symptom of rhinitis, characterized in that the probe shaft includes a cryo-ablation element portion along the probe shaft , and the ultrasound transducer is coupled to the probe shaft towards the distal end of the probe shaft and distal of the cryo-ablation element , and the probe shaft comprises an articulation joint configured to facilitate articulation of the ultrasound transducer relative to the cryo-ablation element . an elongated probe shaft with a proximal end and a distal end; a handle coupled to the proximal end; an ultrasound transducer coupled to the probe shaft ; and a cryo-ablation element coupled to the probe shaft ; wherein the ultrasound transducer includes an ultrasound emitter configured to emit an ultrasound signal and an ultrasound receiver configured to receive a reflected ultrasound signal for determining a location of a target treatment site within a nasal cavity of the patient, and wherein the cryo-ablation element is configured to be positioned at the target treatment site location to cryogenically ablate the target treatment site in order to ablate at least one nasal nerve to reduce at least one symptom of rhinitis, characterized in that the probe shaft includes a cryo-ablation element portion along the probe shaft , and the ultrasound transducer is coupled to the probe shaft towards the distal end of the probe shaft and distal of the cryo-ablation element , and the probe shaft comprises an articulation joint configured to facilitate articulation of the ultrasound transducer relative to the cryo-ablation element .
A system , comprising: a support structure including a cavity surface and an aperture , the cavity surface at least partially forming a boundary of a cavity , and the aperture extending partially into the support structure from the cavity surface ; and a nozzle including a mount , a neck and a head , the mount seated within the aperture , the neck connected to the mount and extending axially along a centerline away from the surface to the head , and the head configured to inject fluid out of the nozzle and into the cavity , wherein the system further comprises a turbine engine component in the cavity , wherein the nozzle comprises a lubricant nozzle, and wherein the nozzle is configured to direct lubricant onto the turbine engine component. a support structure including a cavity surface and an aperture , the cavity surface at least partially forming a boundary of a cavity , and the aperture extending partially into the support structure from the cavity surface ; and a nozzle including a mount , a neck and a head , the mount seated within the aperture , the neck connected to the mount and extending axially along a centerline away from the surface to the head , and the head configured to inject fluid out of the nozzle and into the cavity , wherein the system further comprises a turbine engine component in the cavity , wherein the nozzle comprises a lubricant nozzle, and wherein the nozzle is configured to direct lubricant onto the turbine engine component.
A spacecraft (120A-120F) system , comprising: a plurality of spacecraft (120A-120F) in a stack , wherein the stack has a plurality of layers (124A-124C), each layer (124A-124C) includes at least two spacecraft (120A-120F) of the plurality of spacecraft (120A-120F), and each spacecraft (120A-120F) is releasably coupled to two or more adjacent spacecraft (120A-120F) of the plurality of spacecraft (120A-120F) in the stack ; a plurality of biasing devices (138A-138I) between adjacent layers (124A-124C) in the stack , wherein the plurality of biasing devices (138A-138I) apply a biasing force between the adjacent layers (124A-124C) to facilitate separating each layer (124A-124C) from the stack after the layer (124A-124C) releases from the stack , wherein, for each layer (124A-124C) of the stack , at least one of the plurality of biasing devices (138A-138I) applies a different biasing force to the layer (124A-124C) than at least another of the plurality of biasing devices (138A-138I) such that the layer (124A-124C) rotates as the layer (124A-124C) separates from the stack ; and a controller configured to, for each layer (124A-124C): cause the layer (124A-124C) to release from the stack , and after the layer (124A-124C) releases from the stack , cause the at least two spacecraft (120A-120F) in the layer (124A-124C) to release from each other. a plurality of spacecraft (120A-120F) in a stack , wherein the stack has a plurality of layers (124A-124C), each layer (124A-124C) includes at least two spacecraft (120A-120F) of the plurality of spacecraft (120A-120F), and each spacecraft (120A-120F) is releasably coupled to two or more adjacent spacecraft (120A-120F) of the plurality of spacecraft (120A-120F) in the stack ; a plurality of biasing devices (138A-138I) between adjacent layers (124A-124C) in the stack , wherein the plurality of biasing devices (138A-138I) apply a biasing force between the adjacent layers (124A-124C) to facilitate separating each layer (124A-124C) from the stack after the layer (124A-124C) releases from the stack , wherein, for each layer (124A-124C) of the stack , at least one of the plurality of biasing devices (138A-138I) applies a different biasing force to the layer (124A-124C) than at least another of the plurality of biasing devices (138A-138I) such that the layer (124A-124C) rotates as the layer (124A-124C) separates from the stack ; and a controller configured to, for each layer (124A-124C): cause the layer (124A-124C) to release from the stack , and after the layer (124A-124C) releases from the stack , cause the at least two spacecraft (120A-120F) in the layer (124A-124C) to release from each other. cause the layer (124A-124C) to release from the stack , and after the layer (124A-124C) releases from the stack , cause the at least two spacecraft (120A-120F) in the layer (124A-124C) to release from each other.
An inductive power transmitter comprising: a converter configured to generate at least two object detection signals, wherein a first object detection signal of the at least two object detection signals is generated at a first frequency and a second object detection signal of the at least two object detections signals is generated at a second frequency, the first frequency and the second frequency being substantially different frequencies, at least one transmitting coil configured to generate a magnetic field based on the at least two object detection signals, and a controller configured to determine or measure circuit parameter(s) representing an inductance of the transmitting coil at each of the at least two frequencies, and determine whether an object is present or what kind of object is present depending on a difference between the inductances of the transmitting coil at the first frequency and the second frequency. a converter configured to generate at least two object detection signals, wherein a first object detection signal of the at least two object detection signals is generated at a first frequency and a second object detection signal of the at least two object detections signals is generated at a second frequency, the first frequency and the second frequency being substantially different frequencies, at least one transmitting coil configured to generate a magnetic field based on the at least two object detection signals, and a controller configured to determine or measure circuit parameter(s) representing an inductance of the transmitting coil at each of the at least two frequencies, and determine whether an object is present or what kind of object is present depending on a difference between the inductances of the transmitting coil at the first frequency and the second frequency.
Landing gear provided with a first skid and a second skid , the landing gear comprising at least two first ground-contact rollers mounted on two respective first free-wheels that are connected to the first skid , each first free-wheel being configured to lock during an elastic return phase when the first skid moves in a first direction and to be free during a sink phase when the first skid moves in a second direction opposite to the first direction , the first direction extending from the first skid towards the second skid , the landing gear comprising at least two second ground-contact rollers mounted on two respective second free-wheels that are connected to the second skid , each second free-wheel being configured to lock during the elastic return phase when the second skid moves in the second direction and to be free during the sink phase when the second skid moves in the first direction .
An orthodontic appliance , comprising: - a body ; - at least one ring-shaped member ; - at least one connecting portion extending between and connecting to the body and to the at least one ring-shaped member; and - wherein the body and the at least one ring-shaped member are held apart from one another by the at least one connecting portion, and wherein, in an unloaded state, the body and the at least one ring-shaped member are substantially parallel, and, wherein the at least one connecting portion is oriented orthogonally to both of the at least one ring-shaped member and the body, and wherein the body includes a surface , and wherein the surface includes at least one of: a number, a letter, a symbol, a logo, a printed image, a pattern, an indicia, and a raised element. - a body ; - at least one ring-shaped member ; - at least one connecting portion extending between and connecting to the body and to the at least one ring-shaped member; and - wherein the body and the at least one ring-shaped member are held apart from one another by the at least one connecting portion, and
A method, comprising: at a multifunction device with a touch-sensitive display: detecting a gesture on the touch-sensitive display; in response to detecting the gesture on the touch-sensitive display: when the gesture is a first swipe gesture in a first direction, displaying a plurality of open application icons that corresponds to at least some of a plurality of concurrently open applications; when the gesture is a second swipe gesture in a second direction distinct from the first direction, displaying one or more settings icons, characterised in that the one or more settings icons include a remote media controls icon , which when activated, causes the multifunction device to concurrently display: controls (5042-1, 5042-2, 5042-3, 5042-4) for selecting a plurality of remote devices, other than the multifunction device, on which to play media content; and one or more media player controls for controlling the media content played on the plurality of selected remote devices. detecting a gesture on the touch-sensitive display; in response to detecting the gesture on the touch-sensitive display: when the gesture is a first swipe gesture in a first direction, displaying a plurality of open application icons that corresponds to at least some of a plurality of concurrently open applications; when the gesture is a second swipe gesture in a second direction distinct from the first direction, displaying one or more settings icons, characterised in that the one or more settings icons include a remote media controls icon , which when activated, causes the multifunction device to concurrently display: controls (5042-1, 5042-2, 5042-3, 5042-4) for selecting a plurality of remote devices, other than the multifunction device, on which to play media content; and one or more media player controls for controlling the media content played on the plurality of selected remote devices. when the gesture is a first swipe gesture in a first direction, displaying a plurality of open application icons that corresponds to at least some of a plurality of concurrently open applications; when the gesture is a second swipe gesture in a second direction distinct from the first direction, displaying one or more settings icons, characterised in that the one or more settings icons include a remote media controls icon , which when activated, causes the multifunction device to concurrently display: controls (5042-1, 5042-2, 5042-3, 5042-4) for selecting a plurality of remote devices, other than the multifunction device, on which to play media content; and one or more media player controls for controlling the media content played on the plurality of selected remote devices. controls (5042-1, 5042-2, 5042-3, 5042-4) for selecting a plurality of remote devices, other than the multifunction device, on which to play media content; and one or more media player controls for controlling the media content played on the plurality of selected remote devices.
A 3D data analysis apparatus comprising: a data storage unit configured to store measurement data of microparticles; an input unit configured to select four independent variables from the measurement data; a data processing unit configured to calculate a position in a coordinate space using three variables of the selected variables as coordinate axes, the three variables showing optical characteristics of the microparticles, a display unit configured to display a 3D stereoscopic image , the 3D data analysis apparatus being characterized in that the data processing unit is configured to calculate from the residual variable a figure corresponding to a microparticle, wherein the residual variable is a variable showing electrical characteristics of the microparticle, calculate the shape, size and/or color of the figure from the measurement data of the residual variable, wherein the figure is a polyhedron formed of a combination of polygons having a predetermined shape, and create the 3D stereoscopic image showing a plurality of polyhedron formed figures corresponding to a characteristic distribution of the microparticles. a data storage unit configured to store measurement data of microparticles; an input unit configured to select four independent variables from the measurement data; a data processing unit configured to calculate a position in a coordinate space using three variables of the selected variables as coordinate axes, the three variables showing optical characteristics of the microparticles, a display unit configured to display a 3D stereoscopic image , the 3D data analysis apparatus being characterized in that the data processing unit is configured to calculate from the residual variable a figure corresponding to a microparticle, wherein the residual variable is a variable showing electrical characteristics of the microparticle, calculate the shape, size and/or color of the figure from the measurement data of the residual variable, wherein the figure is a polyhedron formed of a combination of polygons having a predetermined shape, and create the 3D stereoscopic image showing a plurality of polyhedron formed figures corresponding to a characteristic distribution of the microparticles. calculate from the residual variable a figure corresponding to a microparticle, wherein the residual variable is a variable showing electrical characteristics of the microparticle, calculate the shape, size and/or color of the figure from the measurement data of the residual variable, wherein the figure is a polyhedron formed of a combination of polygons having a predetermined shape, and create the 3D stereoscopic image showing a plurality of polyhedron formed figures corresponding to a characteristic distribution of the microparticles.
A radio frequency electronic tag which comprises: a radio frequency chip , the radio frequency chip comprises antenna pins arranged on the radio frequency chip ; antennas ; and a sleeve in which the radio frequency chip is packaged; characterized in that, the antennas are connected to the antenna pins ; the antenna pins are formed as a rod, and one end of each of the antenna pins is arranged inside the sleeve and this end is connected to the radio frequency chip , external screw threads or internal screw threads are provided on an opposite end of the antenna pins , and ends of the antennas are provided with screw connection structures matching the external screw threads or internal screw threads of the antenna pins . a radio frequency chip , the radio frequency chip comprises antenna pins arranged on the radio frequency chip ; antennas ; and a sleeve in which the radio frequency chip is packaged; characterized in that, the antennas are connected to the antenna pins ; the antenna pins are formed as a rod, and one end of each of the antenna pins is arranged inside the sleeve and this end is connected to the radio frequency chip , external screw threads or internal screw threads are provided on an opposite end of the antenna pins , and ends of the antennas are provided with screw connection structures matching the external screw threads or internal screw threads of the antenna pins .
A container security system comprising - force sensors and acceleration sensors to be attached to a so-called lifting beam of a container handling device or to some other part of a frame of the container handling device, - an electronics unit of the system, - an oscillation device , attached to the so-called lifting beam of the container handling device or to some other part of the frame of the container handling device, and characterized in that a first code (25.1) is created for an empty container based on the elasticity of the container, the elasticity being determined by an oscillation measurement of the empty container before loading in a prior container handling stage and retrieved from the database of the system , and that during a container handling stage ending the logistics chain, the oscillation device is arranged to create oscillation onto the container, which is empty, and the system is arranged (i) to generate a second code (25.9) for the container based on elasticity of the container, the elasticity being determined by measurement of the created oscillation by the force sensors and acceleration sensors and analysis of results of the measurement, and (ii) to recognize a change in elasticity of the empty container by comparison of the second code (25.9) to the first code (25.1). - force sensors and acceleration sensors to be attached to a so-called lifting beam of a container handling device or to some other part of a frame of the container handling device, - an electronics unit of the system, - an oscillation device , attached to the so-called lifting beam of the container handling device or to some other part of the frame of the container handling device, and
Method for tracking a hand-guided robot for a medical minimally invasive intervention on a patient , the hand-guided robot comprising a control unit and at least one manipulator coupled to an end effector , wherein the manipulator comprises a plurality of joints and links and the end effector is manually displaceable within an operational volume , comprising the steps: determining (S2) by the control unit at least one movement information of each joint during and/or after a manual displacement of the end effector , determining (S3) by the control unit a position and orientation information of the end effector inside the operational volume during and/or after the displacement of the end effector using the determined movement information of each joint and a software-based kinematic and dynamic model of the manipulator stored in a memory of the control unit , determining by the control unit a displacement trajectory of the end effector during displacement by determining the position and orientation information at different points in time during displacement, calculating (S4) by the control unit at each point in time a deviation information respectively describing the deviation between the displacement trajectory and a target trajectory, which is stored in the memory of the control unit , providing an image data set of the patient by an X-ray apparatus, a computer tomography apparatus or a magnetic resonance tomography apparatus, and displaying (S6) the deviation information and/or the displacement trajectory and/or the target trajectory and the image data set of the patient on a screen . determining (S2) by the control unit at least one movement information of each joint during and/or after a manual displacement of the end effector , determining (S3) by the control unit a position and orientation information of the end effector inside the operational volume during and/or after the displacement of the end effector using the determined movement information of each joint and a software-based kinematic and dynamic model of the manipulator stored in a memory of the control unit , determining by the control unit a displacement trajectory of the end effector during displacement by determining the position and orientation information at different points in time during displacement, calculating (S4) by the control unit at each point in time a deviation information respectively describing the deviation between the displacement trajectory and a target trajectory, which is stored in the memory of the control unit , providing an image data set of the patient by an X-ray apparatus, a computer tomography apparatus or a magnetic resonance tomography apparatus, and displaying (S6) the deviation information and/or the displacement trajectory and/or the target trajectory and the image data set of the patient on a screen .
An apparatus, comprising: a cylinder having an outer wall characterized as having four quadrants and further having a central longitudinal axis; a separate winding located on each quadrant , wherein the positive output (52, 54; 62, 66) of the windings (41, 43; 42, 44) located on geometrically opposite quadrants (1, 3; 2, 4) are connected together; a rotor configured to rotate around said cylinder ; and a Halbach array attached to the inner wall of said rotor and configured to concentrate its magnetic field near the inner surface of the array ; a first inductor connected between the positive output of a first set of windings located on geometrically opposite quadrants and a second inductor connected between the positive output of a second set of windings located on geometrically opposite quadrants ; wherein the inductance of said first inductor is different from that of said second inductor ; the apparatus being further arranged for monitoring change in at least one of the ratio and waveforms of the voltage outputs of the first and second sets of windings. a cylinder having an outer wall characterized as having four quadrants and further having a central longitudinal axis; a separate winding located on each quadrant , wherein the positive output (52, 54; 62, 66) of the windings (41, 43; 42, 44) located on geometrically opposite quadrants (1, 3; 2, 4) are connected together; a rotor configured to rotate around said cylinder ; and a Halbach array attached to the inner wall of said rotor and configured to concentrate its magnetic field near the inner surface of the array ; a first inductor connected between the positive output of a first set of windings located on geometrically opposite quadrants and a second inductor connected between the positive output of a second set of windings located on geometrically opposite quadrants ; wherein the inductance of said first inductor is different from that of said second inductor ; the apparatus being further arranged for monitoring change in at least one of the ratio and waveforms of the voltage outputs of the first and second sets of windings.