mhurhangee/ep-ind-claims huggingface dataset:
A protection system including a shunt resistor for measuring a value of current flowing from a battery to a load unit; a current detection sensor composed of a threshold detection unit, a monitoring unit and a CAN communication unit; a pyro-switch for cutting the shunt resistor based on a predetermined signal; and a suppression unit connected between the shunt resistor and the load unit; wherein the suppression unit suppresses energy generated by cutting the shunt resistor by the pyro-switch; the pyro-switch comprising a heater ignition unit; the monitoring unit being configured to monitor the electrical connection state between an output of the threshold detection unit and the heater ignition unit and to transmit the electrical connection state through the CAN communication unit to a vehicle ECU. a shunt resistor for measuring a value of current flowing from a battery to a load unit; a current detection sensor composed of a threshold detection unit, a monitoring unit and a CAN communication unit; a pyro-switch for cutting the shunt resistor based on a predetermined signal; and a suppression unit connected between the shunt resistor and the load unit; wherein the suppression unit suppresses energy generated by cutting the shunt resistor by the pyro-switch; the pyro-switch comprising a heater ignition unit; the monitoring unit being configured to monitor the electrical connection state between an output of the threshold detection unit and the heater ignition unit and to transmit the electrical connection state through the CAN communication unit to a vehicle ECU.
Time-of-flight vision camera with N capture phases, where N is an integer of at least 2, comprising within a camera housing: - an electronic control circuit (C-MOD) receiving a carrier clock signal with a carrier frequency (fp) defined for the camera, and configured to output a modulation clock signal (fe) at the said carrier frequency; - a light source (S-LED) modulated by the said modulation clock signal (fe) to emit a series of light pulses towards a target scene, the pulse duration (Tp) and the interval between two pulses (Toff 0) defining a cycle ratio less than or equal to 50%; - a matrix image sensor (Cl) configured to control N image capture phases (STO, ST1, ST2, ST3) per integration period (TINT), synchronously with the light pulses emitted by the source, where the integration period corresponds to the carrier clock period (fp); characterised in that: the electronic control circuit comprises a modulation circuit for modulating the carrier clock signal, applying a camera-specific pulse position modulation function (k(t)), synthesised by a periodic frequency signal lower than the carrier frequency, such that the pulses of the said modulation clock fe applied as a signal to modulate the light source and to control the N capture phases of the sensor have a constant pulse duration Tp, fixed by the carrier frequency fp, with Tp=1/2fp, and a variable time interval (Toff) between two successive pulses, modulated by the said modulation function (k(t)), the said time interval being at least equal to the pulse duration, defining a modulation clock cycle ratio that is variable but less than or equal to 50%. - an electronic control circuit (C-MOD) receiving a carrier clock signal with a carrier frequency (fp) defined for the camera, and configured to output a modulation clock signal (fe) at the said carrier frequency; - a light source (S-LED) modulated by the said modulation clock signal (fe) to emit a series of light pulses towards a target scene, the pulse duration (Tp) and the interval between two pulses (Toff 0) defining a cycle ratio less than or equal to 50%; - a matrix image sensor (Cl) configured to control N image capture phases (STO, ST1, ST2, ST3) per integration period (TINT), synchronously with the light pulses emitted by the source, where the integration period corresponds to the carrier clock period (fp); the electronic control circuit comprises a modulation circuit for modulating the carrier clock signal, applying a camera-specific pulse position modulation function (k(t)), synthesised by a periodic frequency signal lower than the carrier frequency, such that the pulses of the said modulation clock fe applied as a signal to modulate the light source and to control the N capture phases of the sensor have a constant pulse duration Tp, fixed by the carrier frequency fp, with Tp=1/2fp, and a variable time interval (Toff) between two successive pulses, modulated by the said modulation function (k(t)), the said time interval being at least equal to the pulse duration, defining a modulation clock cycle ratio that is variable but less than or equal to 50%.
Use of a composition comprising: a) a probe wrapper for hybridization to a nucleic acid probe wherein the probe wrapper comprises a first probe wrapper segment and a second probe wrapper segment that is downstream to the first; and b) a nucleic acid probe for detecting a target sequence wherein the probe comprises a FRET pair, wherein the probe comprises a first probe segment and a second probe segment downstream to the first probe segment; wherein the sequence of the first probe wrapper segment is at least 90% homologous to the reverse complement of the sequence of the first probe segment, wherein the sequence of the second probe wrapper segment is at least 90% homologous to the reverse complement of the sequence of the second probe segment; wherein the melting temperature (Tm) of the probe/target complex is greater than the melting temperature of the probe/probe wrapper complex, to determine the presence of a target nucleic acid in a sample. a) a probe wrapper for hybridization to a nucleic acid probe wherein the probe wrapper comprises a first probe wrapper segment and a second probe wrapper segment that is downstream to the first; and b) a nucleic acid probe for detecting a target sequence wherein the probe comprises a FRET pair, wherein
A munition guidance system, comprising: an generally tubular enclosure, having an internal cavity adapted for receiving a munition, wherein an outer diameter of said enclosure is at most the largest outer diameter of said munition; a plurality of guidance wings; and a processing and control unit enclosed within said enclosure and being configured for controlling said guidance wings so as to maneuver said munition while flying; characterized in that: said enclosure comprises a collapsing member for triggering an impact fuse in said munition upon impact, and the system is an add-on kit to an existing, unmodified, munition. an generally tubular enclosure, having an internal cavity adapted for receiving a munition, wherein an outer diameter of said enclosure is at most the largest outer diameter of said munition; a plurality of guidance wings; and a processing and control unit enclosed within said enclosure and being configured for controlling said guidance wings so as to maneuver said munition while flying; said enclosure comprises a collapsing member for triggering an impact fuse in said munition upon impact, and the system is an add-on kit to an existing, unmodified, munition.
Method for establishing a duplex connection for data transmission between two transmission units (TR1, TR2), each having a transmit unit (Txl, Tx2) and a receive unit (Rxl, Rx2), wherein the duplex connection has two opposingly directed, unidirectional transmission channels (DC12, DC21), by which a communications link for data transmission between the respective transmit unit (Txl, Tx2) and the respective receive unit (Rxl, Rx2) of the two transmission units (TR1, TR2) is established in each case, characterised in that during a synchronisation phase the transmit units (Txl, Tx2) of the two transmission units (TR1, TR2) independently emit in a periodically repeated manner a first synchronisation signal (P11, P21) respectively, in that following detection and synchronisation with the respective first synchronisation signal (P11, P21) by the respective receive unit (Rxl, Rx2), the transmit unit (Txl, Tx2) belonging to the same transmission unit (TR1, TR2) respectively is instructed to emit at least one time a second synchronisation signal (P12, P22) respectively, in that the second synchronisation signal (P12, P22) respectively is derived from the first synchronisation signal (P11, P21) respectively of the transmit unit (Txl, Tx2) of the respective transmission unit (TR1, TR2) by modulation of a respective repetition period (T11, T21) of the first synchronisation signal (P11, P21), or by changing an amplitude of the first synchronisation signal (P11, P21) and/or a polarity of the first synchronisation signal (P11, P21), and in that following at least one-time detection of the second synchronisation signal (P12, P22) respectively by the receive units (Rxl, Rx2) of the two transmission units (TR1, TR2), a changeover to data transmission is implemented.
A measurement system for a construction machine, in particular a road construction machine, comprising: a temperature measuring device configured to determine a first surface temperature for a first area (22_1) of a measuring field (41m, 41m') of the temperature measuring device as well as a second surface temperature for a second area (22_2) of the measuring field (41m, 41m') of the temperature measuring device, the temperature measuring device being directed to a reference surface, in relation to which the construction machine is moving, and the measuring field (41m, 41m') of the temperature measuring device being shifted as a function of a movement of the construction machine along the reference surface; and an evaluation device configured to determine a movement parameter by means of a shift in a first temperature zone (22_1, 22_1'), defined for a first point in time by the first surface temperature within the first area (22_1), in relation to the first and/or second area(s) (22_2) or in relation to the measuring field (41m, 41m') of the temperature measuring device. a temperature measuring device configured to determine a first surface temperature for a first area (22_1) of a measuring field (41m, 41m') of the temperature measuring device as well as a second surface temperature for a second area (22_2) of the measuring field (41m, 41m') of the temperature measuring device, the temperature measuring device being directed to a reference surface, in relation to which the construction machine is moving, and the measuring field (41m, 41m') of the temperature measuring device being shifted as a function of a movement of the construction machine along the reference surface; and an evaluation device configured to determine a movement parameter by means of a shift in a first temperature zone (22_1, 22_1'), defined for a first point in time by the first surface temperature within the first area (22_1), in relation to the first and/or second area(s) (22_2) or in relation to the measuring field (41m, 41m') of the temperature measuring device.
A ferrite controller (200, 402, 406), comprising: a single array of two or more ferrite control elements, wherein the ferrite control elements each include: a radio frequency path assembly including a RF path ferrite element and a RF path dielectric element; a magnetizing ferrite assembly including: a magnetizing ferrite element configured to control the magnetization state of the control element; one or more structural dielectric elements; and a flexible insulated waveguide wall; wherein the magnetizing ferrite element is attached to the one or more structural dielectric elements, wherein the flexible insulated waveguide wall surrounds the magnetizing ferrite element and the structural dielectric elements, wherein the RF path ferrite element and the magnetizing ferrite element are attached to form a ferrite toroid; and two tapered impedance matching transformers attached to the RF path assembly and the magnetizing ferrite assembly. a single array of two or more ferrite control elements, wherein the ferrite control elements each include: a radio frequency path assembly including a RF path ferrite element and a RF path dielectric element; a magnetizing ferrite assembly including: a magnetizing ferrite element configured to control the magnetization state of the control element; one or more structural dielectric elements; and a flexible insulated waveguide wall; wherein the magnetizing ferrite element is attached to the one or more structural dielectric elements, wherein the flexible insulated waveguide wall surrounds the magnetizing ferrite element and the structural dielectric elements, wherein the RF path ferrite element and the magnetizing ferrite element are attached to form a ferrite toroid; and a radio frequency path assembly including a RF path ferrite element and a RF path dielectric element; a magnetizing ferrite assembly including: a magnetizing ferrite element configured to control the magnetization state of the control element; one or more structural dielectric elements; and a flexible insulated waveguide wall; wherein the magnetizing ferrite element is attached to the one or more structural dielectric elements, wherein the flexible insulated waveguide wall surrounds the magnetizing ferrite element and the structural dielectric elements, wherein the RF path ferrite element and the magnetizing ferrite element are attached to form a ferrite toroid; and a magnetizing ferrite element configured to control the magnetization state of the control element; one or more structural dielectric elements; and a flexible insulated waveguide wall; wherein the magnetizing ferrite element is attached to the one or more structural dielectric elements, wherein the flexible insulated waveguide wall surrounds the magnetizing ferrite element and the structural dielectric elements, wherein the RF path ferrite element and the magnetizing ferrite element are attached to form a ferrite toroid; and two tapered impedance matching transformers attached to the RF path assembly and the magnetizing ferrite assembly.
Pressure sensor module comprising: - a base electrode surrounding at least a part of a bottom electrode, - an anchor arrangement on top of the base electrode, - an electrically conductive layer that covers at least the bottom electrode and the anchor arrangement such that a cavity is formed between the bottom electrode, the anchor arrangement and the electrically conductive layer, - characterized in that the anchor arrangement comprises at least two electrically conductive walls that both surround at least a part of the bottom electrode, and - on at least one side of the cavity a proportionate area of the at least two electrically conductive walls in a cross section extending from the surface of the inner wall of the anchor arrangement facing the cavity to the surface of the outermost wall of the anchor arrangement facing away from the cavity in a plane parallel to the plane of the bottom electrode is equal to or less than 10 %. - a base electrode surrounding at least a part of a bottom electrode, - an anchor arrangement on top of the base electrode, - an electrically conductive layer that covers at least the bottom electrode and the anchor arrangement such that a cavity is formed between the bottom electrode, the anchor arrangement and the electrically conductive layer, - characterized in that the anchor arrangement comprises at least two electrically conductive walls that both surround at least a part of the bottom electrode, and - on at least one side of the cavity a proportionate area of the at least two electrically conductive walls in a cross section extending from the surface of the inner wall of the anchor arrangement facing the cavity to the surface of the outermost wall of the anchor arrangement facing away from the cavity in a plane parallel to the plane of the bottom electrode is equal to or less than 10 %.
A UAV for detecting cracks in a wall of a building, the UAV comprising - a propulsion means for flying the UAV, - a digital camera for capturing pictures of the wall, - a flight control module, the flight control module being operative to control the propulsion means based on image data of the digital camera, such that the UAV flies along the wall of the building along a pre-determined flight path (20,24), - an image capturing module, wherein the flight control module is operative to control the propulsion means and wherein the image capturing module is operative to control the digital camera such that adjacent pictures captured by the digital camera have an overlap in a predetermined range, the UAV further comprises a processor for identifying at least one no-scan area of the wall to determine the pre-determined flight path (20,24), characterised in that the overlap of the adjacent pictures is between 5% and 10%. - a propulsion means for flying the UAV, - a digital camera for capturing pictures of the wall, - a flight control module, the flight control module being operative to control the propulsion means based on image data of the digital camera, such that the UAV flies along the wall of the building along a pre-determined flight path (20,24), - an image capturing module, wherein the flight control module is operative to control the propulsion means and wherein the image capturing module is operative to control the digital camera such that adjacent pictures captured by the digital camera have an overlap in a predetermined range, the UAV further comprises a processor for identifying at least one no-scan area of the wall to determine the pre-determined flight path (20,24), characterised in that the overlap of the adjacent pictures is between 5% and 10%.
Apparatus suitable for housing premature infants, the apparatus comprising: an incubator housing; a warming system comprising a temperature controller connected to control a temperature within the incubator housing; a humidifier connected to maintain a desired humidity level within the incubator housing; a platform within the housing, the platform dimensioned to support an infant and one or more actuators connected to the platform and operable to move the platform in at least a vertical direction with an oscillating motion; a controller connected to control the actuators to move the platform to oscillate in the vertical direction at a frequency in the range of 5 to 25 oscillations per minute; characterized by a blood oxygen sensor connected to supply a blood-oxygen signal representing blood oxygen content to the controller wherein the controller is configured to adjust one or both of a frequency and amplitude of oscillation of the platform based on the blood-oxygen signal; or a heart monitor associated with a signal processor configured to process an output signal of the heart monitor signal to yield a HRV signal indicative of heart rate variability wherein the controller is configured to adjust one or both of a frequency and amplitude of oscillation of the platform based on the HRV signal. an incubator housing; a warming system comprising a temperature controller connected to control a temperature within the incubator housing; a humidifier connected to maintain a desired humidity level within the incubator housing; a platform within the housing, the platform dimensioned to support an infant and one or more actuators connected to the platform and operable to move the platform in at least a vertical direction with an oscillating motion; a controller connected to control the actuators to move the platform to oscillate in the vertical direction at a frequency in the range of 5 to 25 oscillations per minute; characterized by a blood oxygen sensor connected to supply a blood-oxygen signal representing blood oxygen content to the controller wherein the controller is configured to adjust one or both of a frequency and amplitude of oscillation of the platform based on the blood-oxygen signal; or a heart monitor associated with a signal processor configured to process an output signal of the heart monitor signal to yield a HRV signal indicative of heart rate variability wherein the controller is configured to adjust one or both of a frequency and amplitude of oscillation of the platform based on the HRV signal.
An antenna array assembly, comprising: a dielectric film carrying an array of conductive patch radiator elements and a plurality of conductive feed tracks; and a ground plate, a face of the ground plate having a contoured shape, the contoured shape comprising a first part configured to be in contact with the dielectric film, and a second part comprising sunken sections with respect to the first part arranged to underlie the conductive feed tracks and conductive patch radiator elements, and the ground plate having locating protrusions protruding from the first part, wherein the dielectric film is attached to the ground plate by location of holes in the dielectric film with the locating protrusions, such that the dielectric film is held under tension, whereby to maintain spacing of the dielectric film from the sunken sections of the ground plate without the use of a dielectric spacer layer between the dielectric film and the ground plate, wherein each said hole in the dielectric film has a respective diameter, before assembly, that is less than the diameter of the corresponding locating protrusion, and the dielectric film is attached such that the dielectric film in the region of each hole is raised away from the first part of the ground plate and parts of the dielectric film more distant from each hole are urged against the first part of the ground plate and held in tension. a dielectric film carrying an array of conductive patch radiator elements and a plurality of conductive feed tracks; and a ground plate, a face of the ground plate having a contoured shape, the contoured shape comprising a first part configured to be in contact with the dielectric film, and a second part comprising sunken sections with respect to the first part arranged to underlie the conductive feed tracks and conductive patch radiator elements, and the ground plate having locating protrusions protruding from the first part, wherein the dielectric film is attached to the ground plate by location of holes in the dielectric film with the locating protrusions, such that the dielectric film is held under tension, whereby to maintain spacing of the dielectric film from the sunken sections of the ground plate without the use of a dielectric spacer layer between the dielectric film and the ground plate, wherein each said hole in the dielectric film has a respective diameter, before assembly, that is less than the diameter of the corresponding locating protrusion, and the dielectric film is attached such that the dielectric film in the region of each hole is raised away from the first part of the ground plate and parts of the dielectric film more distant from each hole are urged against the first part of the ground plate and held in tension.
A method of cutting a tubular, comprising: disposing a rotatable cutter assembly in the tubular, the cutter assembly including a blade having a cutting portion; engaging the tubular using an integral stabilizer disposed on at least a portion of an outer surface of the blade body; engaging the tubular using a trailing cutting structure of the cutting portion; engaging the tubular using an intermediate cutting structure of the cutting portion; forming a window in the tubular; and longitudinally extending the window using a leading cutting structure of the cutting portion. disposing a rotatable cutter assembly in the tubular, the cutter assembly including a blade having a cutting portion; engaging the tubular using an integral stabilizer disposed on at least a portion of an outer surface of the blade body; engaging the tubular using a trailing cutting structure of the cutting portion; engaging the tubular using an intermediate cutting structure of the cutting portion; forming a window in the tubular; and longitudinally extending the window using a leading cutting structure of the cutting portion.