mhurhangee/ep-ind-claims huggingface dataset:
Hybrid component for a chassis of motor vehicles, composed of a connecting rod with profilings arranged at its two end regions (9b, 9c) and of two ball joints (4, 5) with plastic housings (4a, 5a) which are connected to the connecting rod by overmoulding, wherein the ball joints (4, 5) have shank-like elongations (6, 7) which surround the connecting rod and which overlap on a shank of the connecting rod, wherein, in the overlapping region of the shank-like elongations (6, 7), at least one profiling is arranged on the mutually facing surfaces, characterized in that an end region of the respective shank-like elongation (6, 7) additionally has, on its outer circumference, an undulating contour in the manner of a labyrinth seal.
A light emitting apparatus comprising: a light transmissive envelope configured to diffuse light; an LED light source being in thermal communication with a heat sink base (18, 50) housing an electronic driver; and a plurality of heat fins in thermal communication with said heat sink base and extending in a direction such that the heat fins are adjacent to said light transmissive envelope, wherein said plurality of heat fins comprises a carbon nanotube filled polymer composite; wherein said heat sink base comprises a truncated cone shape, with a receiving area for the LED light source sized approximately the same as the LED light source, and having sides angled between 15° and 30°. a light transmissive envelope configured to diffuse light; an LED light source being in thermal communication with a heat sink base (18, 50) housing an electronic driver; and a plurality of heat fins in thermal communication with said heat sink base and extending in a direction such that the heat fins are adjacent to said light transmissive envelope, wherein said plurality of heat fins comprises a carbon nanotube filled polymer composite; wherein said heat sink base comprises a truncated cone shape, with a receiving area for the LED light source sized approximately the same as the LED light source, and having sides angled between 15° and 30°.
A holder for a container of predetermined circumference and length comprising: fastener bands capable of retaining a single container therein, each band having a plurality of straps attached to and extending away from the band; each strap having a fastener (36, 38) on an end, characterized in that at least one of the fasteners (36, 38) is a first fastener comprising a G-ring base, a center strut extending away from the base and a pair of outer fingers having first portions extending in opposite directions away from the center strut and second portions extending from the first portions towards the base; the outer fingers bracketing the center strut such that a webbing is insertable between the fingers and the center strut to attach the fastener to a webbing; and a space is located between the outer fingers and the base to allow for insertion or removal of a webbing; wherein the fastener further comprises a semi-circular arch forming a D-ring with the center strut, wherein the base of the fastener includes the G-ring extending away from the center strut.
A computer-implemented method of evaluating an earth formation intersected by a borehole using signals produced at a plurality of borehole depths by an ultrasonic transducer in the borehole, the signals produced by the transducer including ringdown signals from the ultrasonic transducer and echo signals from a wall of the borehole from a plurality of azimuthal orientations, the method characterised by comprising: using peak amplitude values and arrival time values from the signals to construct a background modulation template representing background noise and corresponding to at least one depth by generating a curve representing the background modulation template by mapping each peak amplitude value with respect to a corresponding arrival time value at the at least one depth; estimating, for each respective depth of the plurality of borehole depths, an azimuthally varying interference pattern resulting from a ringdown signal for each respective depth, the azimuthally varying interference pattern for each respective depth being estimated by mapping the background modulation template to arrival time values corresponding to the respective depth; and subtracting, for each respective depth, the estimated varying interference pattern from the peak amplitude values corresponding to the respective depth to generate adjusted peak amplitudes; and generating a two-dimensional image of the earth formation using the adjusted peak amplitudes. using peak amplitude values and arrival time values from the signals to construct a background modulation template representing background noise and corresponding to at least one depth by generating a curve representing the background modulation template by mapping each peak amplitude value with respect to a corresponding arrival time value at the at least one depth; estimating, for each respective depth of the plurality of borehole depths, an azimuthally varying interference pattern resulting from a ringdown signal for each respective depth, the azimuthally varying interference pattern for each respective depth being estimated by mapping the background modulation template to arrival time values corresponding to the respective depth; and subtracting, for each respective depth, the estimated varying interference pattern from the peak amplitude values corresponding to the respective depth to generate adjusted peak amplitudes; and generating a two-dimensional image of the earth formation using the adjusted peak amplitudes.
A method of non-destructively determining the amount of ultraviolet degradation of a polymer composite material surface wherein the polymer composite material is used in a portion of an aircraft, the method comprising: irradiating said surface with infrared energy over a spectrum of wavelengths; detecting said infrared energy reflected from said surface over said spectrum of wavelengths; performing multivariate analysis on the spectrum of said reflected infrared energy; comparing results of said multivariate analysis with a predetermined calibration between model infrared energy spectra comprising said spectrum of wavelengths collected from a plurality of model material surfaces, said plurality of model material surfaces each comprising a known level of said ultraviolet degradation of said model material; and, determining said amount of said ultraviolet degradation of said surface based on said predetermined calibration. irradiating said surface with infrared energy over a spectrum of wavelengths; detecting said infrared energy reflected from said surface over said spectrum of wavelengths; performing multivariate analysis on the spectrum of said reflected infrared energy; comparing results of said multivariate analysis with a predetermined calibration between model infrared energy spectra comprising said spectrum of wavelengths collected from a plurality of model material surfaces, said plurality of model material surfaces each comprising a known level of said ultraviolet degradation of said model material; and, determining said amount of said ultraviolet degradation of said surface based on said predetermined calibration.
A waveguide for thermally assisted recording comprising: a top cladding layer made of a material having an index of refraction n 4; a core bilayer structure, the core bilayer structure comprising: a lower index core layer having an index of refraction n 3; and a higher index core layer having an index of refraction n 1, wherein the higher index core layer comprises TiO 2 and one or more than one of Nb 2 O 5, CeO 2, Ta 2 O 5, ZrO 2, HfO 2, Y 2 O 3, Sc 2 O 3, MgO, Al 2 O 3 and SiO 2, wherein the lower index core layer is adjacent the higher index core layer; and a bottom cladding layer made of a material having an index of refraction n 2, wherein the waveguide is configured with the higher index core layer of the core bilayer structure adjacent the top cladding layer and the lower index core layer of the core bilayer structure adjacent the bottom cladding layer, and wherein: n 4 is less than n 3 and n 1, and n 2 is less than n 3 and n 1, characterized in that: a near-field transducer is located in the top cladding layer; and n 4 is higher than n 2. a top cladding layer made of a material having an index of refraction n 4; a core bilayer structure, the core bilayer structure comprising: a lower index core layer having an index of refraction n 3; and a higher index core layer having an index of refraction n 1, wherein the higher index core layer comprises TiO 2 and one or more than one of Nb 2 O 5, CeO 2, Ta 2 O 5, ZrO 2, HfO 2, Y 2 O 3, Sc 2 O 3, MgO, Al 2 O 3 and SiO 2, wherein the lower index core layer is adjacent the higher index core layer; and a lower index core layer having an index of refraction n 3; and a higher index core layer having an index of refraction n 1, wherein the higher index core layer comprises TiO 2 and one or more than one of Nb 2 O 5, CeO 2, Ta 2 O 5, ZrO 2, HfO 2, Y 2 O 3, Sc 2 O 3, MgO, Al 2 O 3 and SiO 2, wherein the lower index core layer is adjacent the higher index core layer; and a bottom cladding layer made of a material having an index of refraction n 2, wherein the waveguide is configured with the higher index core layer of the core bilayer structure adjacent the top cladding layer and the lower index core layer of the core bilayer structure adjacent the bottom cladding layer, and wherein: n 4 is less than n 3 and n 1, and n 2 is less than n 3 and n 1, n 4 is less than n 3 and n 1, and n 2 is less than n 3 and n 1, characterized in that: a near-field transducer is located in the top cladding layer; and n 4 is higher than n 2. a near-field transducer is located in the top cladding layer; and n 4 is higher than n 2.
An apparatus for folding an airplane wing, in particular a wing tip of an airplane wing, comprising: a hinge pin which is supportable in a rigid wing section and is rotationally fixedly or fixedly connectable to a folding wing section; an actuator for driving the hinge pin to fold the folding wing section out of or into a main plane of the airplane wing; and an abutment element for the abutment of the folding wing section on a folding out of the folding wing section and for defining an end position of a folded-out state of the folding wing section, characterized in that the apparatus further comprises a sensor for measuring a preload torque which occurs on an abutment of the folding wing section against the abutment element, with the sensor measuring the preload torque at the hinge pin. a hinge pin which is supportable in a rigid wing section and is rotationally fixedly or fixedly connectable to a folding wing section; an actuator for driving the hinge pin to fold the folding wing section out of or into a main plane of the airplane wing; and an abutment element for the abutment of the folding wing section on a folding out of the folding wing section and for defining an end position of a folded-out state of the folding wing section, characterized in that the apparatus further comprises a sensor for measuring a preload torque which occurs on an abutment of the folding wing section against the abutment element, with the sensor measuring the preload torque at the hinge pin.
An unmanned aerial vehicle, UAV, mountable to a conductor of an aerial power transmission line system, the UAV comprising: a body having a rotor system; a motivation system attached to the body to motivate the UAV along the conductor, the motivation system comprising a single set of wheels coaxially aligned to engage a single conductor of the aerial power transmission line system; a battery carried by the body and electrically connected to at least one of the rotor system and the motivation system; a monitoring tool mounted to the body, the monitoring tool comprising a camera; and an inductive coil carried by the body and in electric connection with the battery, wherein the inductive coil is configured to harvest electricity from the aerial power transmission line system and charge the battery, characterized in that the wheels are electrically drivable to rotate and move the UAV along the single conductor. a body having a rotor system; a motivation system attached to the body to motivate the UAV along the conductor, the motivation system comprising a single set of wheels coaxially aligned to engage a single conductor of the aerial power transmission line system; a battery carried by the body and electrically connected to at least one of the rotor system and the motivation system; a monitoring tool mounted to the body, the monitoring tool comprising a camera; and an inductive coil carried by the body and in electric connection with the battery, wherein the inductive coil is configured to harvest electricity from the aerial power transmission line system and charge the battery, characterized in that the wheels are electrically drivable to rotate and move the UAV along the single conductor.
A relay platform of global navigation satellite system, GNSS, positioning signals, the relay platform having a frame of reference and comprising: - a receiver of a synchronization signal, wherein the receiver of a synchronization signal is a GNSS receiver; - a transmitter configured to condition one or more GNSS positioning signals carrying a navigation message representative of a position and time using the synchronization signal; and - an antenna assembly configured to transmit the GNSS positioning signals in an Area of Service, AoS, in at least a first mode with a radiating pattern having at least a main lobe having an aperture angle smaller than 90° in a first plane of reference comprising a vertical axis and a first horizontal axis and an aperture angle larger than 90° in a second plane of reference comprising the vertical axis and a second horizontal axis perpendicular to the first horizontal axis, wherein the AoS is a urban canyon comprising streets and obstacles such as buildings, and wherein the relay platform has a position overhanging the streets, the main lobe of the antenna assembly being directed downwards and wherein the first horizontal axis is pointed in a direction towards obstacles, so that the radiated power of the antenna assembly emitted towards said direction is minimal. - a receiver of a synchronization signal, wherein the receiver of a synchronization signal is a GNSS receiver; - a transmitter configured to condition one or more GNSS positioning signals carrying a navigation message representative of a position and time using the synchronization signal; and - an antenna assembly configured to transmit the GNSS positioning signals in an Area of Service, AoS, in at least a first mode with a radiating pattern having at least a main lobe having an aperture angle smaller than 90° in a first plane of reference comprising a vertical axis and a first horizontal axis and an aperture angle larger than 90° in a second plane of reference comprising the vertical axis and a second horizontal axis perpendicular to the first horizontal axis,
A method comprising: disposing a support layer on a surface of a wavelength converting ceramic wafer; dicing the wavelength converting ceramic wafer and the support layer to form wavelength converting members (40A, 40B, 40C); attaching a wavelength converting member (40A, 40B, 40C) to a light emitting device; and after attaching the wavelength converting member (40A, 40B, 40C,...) to the light emitting device, removing the support layer. disposing a support layer on a surface of a wavelength converting ceramic wafer; dicing the wavelength converting ceramic wafer and the support layer to form wavelength converting members (40A, 40B, 40C); attaching a wavelength converting member (40A, 40B, 40C) to a light emitting device; and after attaching the wavelength converting member (40A, 40B, 40C,...) to the light emitting device, removing the support layer.
A radiation therapy device comprising: a gantry; a first radiation source mounted on the gantry; a plurality of robotic arms mounted to the gantry, the plurality of robotic arms including a first robotic arm and a second robotic arm; a second radiation source attached to the first robotic arm; an imager attached to the second robotic arm; and a computing device, communicatively coupled to the plurality of robotic arms, the computing device executing a flexible motion control system, wherein each of the plurality of robotic arms is operable to maneuver according to a plurality of customizable acquisition trajectories, the plurality of customizable acquisition trajectories provided from the motion control system, and wherein the radiation therapy device is configured to acquire a plurality of three dimensional images taken along the plurality of customizable acquisition trajectories; wherein: the plurality of customizable acquisition trajectories includes a trajectory in which an image acquired is a composite of two half circular scan acquisitions, one clockwise and the other counter-clockwise, with an intermediate linear motion of the second radiation source and imager; and the radiation therapy device is configured to automatically combine volumes of the two half-scans. a gantry; a first radiation source mounted on the gantry; a plurality of robotic arms mounted to the gantry, the plurality of robotic arms including a first robotic arm and a second robotic arm; a second radiation source attached to the first robotic arm; an imager attached to the second robotic arm; and a computing device, communicatively coupled to the plurality of robotic arms, the computing device executing a flexible motion control system, wherein each of the plurality of robotic arms is operable to maneuver according to a plurality of customizable acquisition trajectories, the plurality of customizable acquisition trajectories provided from the motion control system, and wherein the radiation therapy device is configured to acquire a plurality of three dimensional images taken along the plurality of customizable acquisition trajectories; wherein: the plurality of customizable acquisition trajectories includes a trajectory in which an image acquired is a composite of two half circular scan acquisitions, one clockwise and the other counter-clockwise, with an intermediate linear motion of the second radiation source and imager; and the radiation therapy device is configured to automatically combine volumes of the two half-scans. the plurality of customizable acquisition trajectories includes a trajectory in which an image acquired is a composite of two half circular scan acquisitions, one clockwise and the other counter-clockwise, with an intermediate linear motion of the second radiation source and imager; and the radiation therapy device is configured to automatically combine volumes of the two half-scans.
A shrinking shock strut system for an aircraft landing gear having a retract actuator that is moveable in length to deploy or retract the landing gear, comprising: a shrink strut that is moveable between an extended length and a shrunk length, the shrink strut including a strut cylinder and a strut piston mounted coaxially, wherein a variable length strut shrink chamber is formed between the strut cylinder and the strut piston, and wherein an increase in the length of the strut shrink chamber causes a decrease in the length of the shrink strut; a transfer device configured to transfer hydraulic fluid to the strut shrink chamber independent of movement of the retract actuator; and a control device configured to cause the transfer device to transfer hydraulic fluid to the strut shrink chamber; characterised in that the transfer device further comprises a locking mechanism. a shrink strut that is moveable between an extended length and a shrunk length, the shrink strut including a strut cylinder and a strut piston mounted coaxially, wherein a variable length strut shrink chamber is formed between the strut cylinder and the strut piston, and wherein an increase in the length of the strut shrink chamber causes a decrease in the length of the shrink strut; a transfer device configured to transfer hydraulic fluid to the strut shrink chamber independent of movement of the retract actuator; and a control device configured to cause the transfer device to transfer hydraulic fluid to the strut shrink chamber; characterised in that the transfer device further comprises a locking mechanism.
A LED lighting module comprising a substrate and a plurality of LED light sources housed on the substrate, the LED light sources including: a direct emission red source; a direct emission green source; a direct emission blue source; and a direct emission cyan source; characterized in that: the LED light sources include a phosphor-converted amber source and a phosphor-converted green source; the phosphor-converted amber source and the phosphor-converted green source have equal emitting areas; and the direct emission red source, the direct emission green source and the direct emission blue source each have an emitting area equal to half the emitting area of the phosphor-converted amber source and equal to half the emitting area of the phosphor-converted green source. a direct emission red source; a direct emission green source; a direct emission blue source; and a direct emission cyan source; characterized in that: the LED light sources include a phosphor-converted amber source and a phosphor-converted green source; the phosphor-converted amber source and the phosphor-converted green source have equal emitting areas; and the direct emission red source, the direct emission green source and the direct emission blue source each have an emitting area equal to half the emitting area of the phosphor-converted amber source and equal to half the emitting area of the phosphor-converted green source. the LED light sources include a phosphor-converted amber source and a phosphor-converted green source; the phosphor-converted amber source and the phosphor-converted green source have equal emitting areas; and the direct emission red source, the direct emission green source and the direct emission blue source each have an emitting area equal to half the emitting area of the phosphor-converted amber source and equal to half the emitting area of the phosphor-converted green source.
A method for transducing a host cell, said method comprising transducing the host cell with a retroviral vector particle comprising an envelope of Friend murine leukaemia virus, wherein the envelope of Friend murine leukaemia virus is encoded by molecular clone PVC-211 (SEQ ID NO: 1) or a functional fragment thereof, and wherein the host cell recombinantly expresses a Rec1 receptor (SEQ ID No: 32) or a functional fragment thereof.
Method for pipe laying, comprising the step; - Vertically forcing a generally rigid pipe section in a substantially vertical direction downwards from a position above ground towards a desired pipe section position in the ground, wherein the pipe section maintains a substantially horizontal position upon forcing the pipe section downwards. - Vertically forcing a generally rigid pipe section in a substantially vertical direction downwards from a position above ground towards a desired pipe section position in the ground, wherein the pipe section maintains a substantially horizontal position upon forcing the pipe section downwards.
An arrangement for feeding weft yarns along several yarn paths to a jet loom, the arrangement comprising a weft creel having several cone holders (21, 21',...) and several yarn brake units (30, 30',...), wherein at least one of the several cone holders (21, 21',...) and at least one of the several yarn brake units (30, 30',...) are assigned to each yarn path, and a yarn sensor unit (40, 40',...) configured for determining at least one intrinsic characteristic of a weft yarn and being connected to a control unit for controlling a fluid feed of the jet loom, characterized in that a plurality of yarn sensor units (40, 40',...) is provided, at least one of the plurality of yarn sensor units (40, 40',...) is assigned to each of the yarn paths, and each of the plurality of yarn sensor units (40, 40',...) is mounted stationarily on the weft creel.