mhurhangee/ep-ind-claims huggingface dataset:
An isolator system for a pressure transmitter, the system comprising: a port internal to the transmitter; a sensor tube connected to the port to fluidly connect a passageway through a transmitter body to a pressure sensor, the sensor tube including a first end disposed in the port, the first end having a first cross-sectional area; and a fill tube internal to the transmitter, the fill tube connected to the port to fluidly connect to the passageway, the fill tube including a second end disposed in the port, characterized in that the second end having a second cross-sectional area that is less than the first cross-sectional area of the sensor tube, wherein the first cross-sectional area is between 60% and 80% of a sum of the first cross-sectional area and the second cross-sectional area. a port internal to the transmitter; a sensor tube connected to the port to fluidly connect a passageway through a transmitter body to a pressure sensor, the sensor tube including a first end disposed in the port, the first end having a first cross-sectional area; and a fill tube internal to the transmitter, the fill tube connected to the port to fluidly connect to the passageway, the fill tube including a second end disposed in the port, characterized in that the second end having a second cross-sectional area that is less than the first cross-sectional area of the sensor tube, wherein the first cross-sectional area is between 60% and 80% of a sum of the first cross-sectional area and the second cross-sectional area.
A latch assembly, comprising: a front plate; a back plate mounted on the front plate via a pair of axles mounted between; a rotor and a catch pivotally mounted between the front and back plates; the front plate being C-shaped with opposite top and bottom flanges and a front face extending between the top and bottom flanges; a pair of axles mounted to the front face of the front plate and to the back plate to rotatably support the rotor and the catch; the front plate and the back plate are mounted together by tabs extending in one direction from one of the plates through slots on the other of the plates; and the back plate and front face having a window for receiving a striker. a front plate; a back plate mounted on the front plate via a pair of axles mounted between; a rotor and a catch pivotally mounted between the front and back plates; the front plate being C-shaped with opposite top and bottom flanges and a front face extending between the top and bottom flanges; a pair of axles mounted to the front face of the front plate and to the back plate to rotatably support the rotor and the catch; the front plate and the back plate are mounted together by tabs extending in one direction from one of the plates through slots on the other of the plates; and the back plate and front face having a window for receiving a striker.
An inspection system for controlling quality of a tube, comprising: - transporting means for transferring the tube on a transporting path being substantially perpendicular to an axis of the tube, - a radiation source (4, 4'), - a radiation receiver, and - means for altering a direction of a radiation beam, partially or totally reflecting the radiation, forming the path of the radiation beam from the radiation source (4, 4') through the interior of the tube to the radiation receiver, characterized in that: - the inspection system is configured to: - generate two radiation beams (3, 3'); - introduce (103, 105) said two radiation beams (3, 3') to the inside of the tube at two opposite ends of the tube, such that the radiation beams (3, 3') propagate through the tube in two opposite directions; - register an image generated by means of the first radiation beam after propagating through the tube; - register an image generated by means of the second radiation beam after propagating through the tube; - compare, in an inspection unit, a contour of tube ends (1A, 1B) to a circular shape; - in case of deviation of the registered shape from the circular shape, generate a signal for rejecting a faulty tube. - transporting means for transferring the tube on a transporting path being substantially perpendicular to an axis of the tube, - a radiation source (4, 4'), - a radiation receiver, and - means for altering a direction of a radiation beam, partially or totally reflecting the radiation, forming the path of the radiation beam from the radiation source (4, 4') through the interior of the tube to the radiation receiver, - the inspection system is configured to: - generate two radiation beams (3, 3'); - introduce (103, 105) said two radiation beams (3, 3') to the inside of the tube at two opposite ends of the tube, such that the radiation beams (3, 3') propagate through the tube in two opposite directions; - register an image generated by means of the first radiation beam after propagating through the tube; - register an image generated by means of the second radiation beam after propagating through the tube; - compare, in an inspection unit, a contour of tube ends (1A, 1B) to a circular shape; - in case of deviation of the registered shape from the circular shape, generate a signal for rejecting a faulty tube.
A method executed by a processor of a camera comprising a simultaneous dual-exposure HDR sensor, wherein the HDR capability is in the pixels themselves, the method comprising: capturing camera data and generating a preview image in a viewfinder based on the camera data; in response to receiving a picture request: determining one or more high dynamic range, HDR, settings and configure an HDR mode of a camera with the determined HDR settings; causing a flash to generate a pre-flash while the HDR mode of the camera is configured with the determined HDR settings; obtaining a pre-flash image from the camera after causing the flash to generate the pre-flash and while the camera is configured with the determined HDR settings; determining a plurality of camera configuration settings, wherein determining the plurality of camera configuration settings comprises determining a short exposure time based on the obtained pre-flash image, and determining a long exposure time from the preview image; configuring the camera with the determined short exposure time and long exposure time; causing the flash to generate a regular flash; obtaining, after causing the flash to generate the regular flash, an HDR image from the camera comprising the simultaneous dual exposure HDR sensor, wherein the HDR capability is in the pixels themselves; and storing the HDR image in memory. determining one or more high dynamic range, HDR, settings and configure an HDR mode of a camera with the determined HDR settings; causing a flash to generate a pre-flash while the HDR mode of the camera is configured with the determined HDR settings; obtaining a pre-flash image from the camera after causing the flash to generate the pre-flash and while the camera is configured with the determined HDR settings; determining a plurality of camera configuration settings, wherein determining the plurality of camera configuration settings comprises determining a short exposure time based on the obtained pre-flash image, and determining a long exposure time from the preview image; configuring the camera with the determined short exposure time and long exposure time; causing the flash to generate a regular flash; obtaining, after causing the flash to generate the regular flash, an HDR image from the camera comprising the simultaneous dual exposure HDR sensor, wherein the HDR capability is in the pixels themselves; and storing the HDR image in memory.
A method for registering a mobile station of a passenger with a passenger communication system of a vehicle, characterised by: receiving a message from a near field communications, NFC, module of the mobile station by an NFC terminal of the passenger communications system, the message comprising information for registering the mobile station with the passenger communications system; registering the mobile station with the passenger communications system based on the message; and enabling access to the passenger communications system for the mobile station. receiving a message from a near field communications, NFC, module of the mobile station by an NFC terminal of the passenger communications system, the message comprising information for registering the mobile station with the passenger communications system; registering the mobile station with the passenger communications system based on the message; and enabling access to the passenger communications system for the mobile station.
A medical apparatus (10,110,510,610), comprising: a catheter (20,120,220,320,420,520,620) defining a first lumen (20a,120a) and having a proximal end, a distal end, and a longitudinal axis; and at least one inflatable balloon (30,130,230, 430,530,630) located about said distal end, said at least one inflatable balloon being in communication with said first lumen and having a deflated position and an inflated position, wherein in said inflated position said at least one balloon includes first and second larger diameter areas (32a,32b,232a,232b,332a,332b,432a,432e) defining a valley (34,234,334,434a,434d) therebetween, said at least one inflatable balloon being symmetrical about said longitudinal axis, said at least one inflatable balloon adapted to being pressurized to a pressure of at least 41370Pa (6 psi), the length of said at least one inflatable balloon being between 8 cm and 16 cm and the outer diameters of said first and second spaced larger diameter areas being between 4 and 10 cm and between 20% and 40% larger than an outer diameter of said valley. a catheter (20,120,220,320,420,520,620) defining a first lumen (20a,120a) and having a proximal end, a distal end, and a longitudinal axis; and at least one inflatable balloon (30,130,230, 430,530,630) located about said distal end, said at least one inflatable balloon being in communication with said first lumen and having a deflated position and an inflated position, wherein in said inflated position said at least one balloon includes first and second larger diameter areas (32a,32b,232a,232b,332a,332b,432a,432e) defining a valley (34,234,334,434a,434d) therebetween, said at least one inflatable balloon being symmetrical about said longitudinal axis, said at least one inflatable balloon adapted to being pressurized to a pressure of at least 41370Pa (6 psi), the length of said at least one inflatable balloon being between 8 cm and 16 cm and the outer diameters of said first and second spaced larger diameter areas being between 4 and 10 cm and between 20% and 40% larger than an outer diameter of said valley.
A vibration component, comprising: a dome comprising a porous heat dissipation layer; a diaphragm covering a portion of a surface of the dome and surrounding the dome; and a voice coil connected with a side of the dome facing away from the diaphragm, wherein the porous heat dissipation layer comprises a first heat dissipation surface and a second heat dissipation surface opposite to the first heat dissipation surface, and the second heat dissipation surface is closer to the voice coil than the first heat dissipation surface; wherein the porous heat dissipation layer comprises a first heat dissipation hole, a second heat dissipation hole, and a third heat dissipation hole, characterized in that the first heat dissipation hole, the second heat dissipation hole, and the third heat dissipation hole are connected with one another, the first heat dissipation hole is connected to the first heat dissipation surface, the second heat dissipation hole is connected to the second heat dissipation surface, the third heat dissipation hole is arranged transversely, and the third heat dissipation hole is connected between the first heat dissipation hole and the second heat dissipation hole. a dome comprising a porous heat dissipation layer; a diaphragm covering a portion of a surface of the dome and surrounding the dome; and a voice coil connected with a side of the dome facing away from the diaphragm, wherein the porous heat dissipation layer comprises a first heat dissipation surface and a second heat dissipation surface opposite to the first heat dissipation surface, and the second heat dissipation surface is closer to the voice coil than the first heat dissipation surface; wherein the porous heat dissipation layer comprises a first heat dissipation hole, a second heat dissipation hole, and a third heat dissipation hole,
A method of retrofitting a mechanically controlled aircraft with a fly-by-wire system, the method comprising: removing a plurality of mechanical links between a plurality of mechanical pilot inputs and a plurality of actuators operable to drive flight surfaces; installing a plurality of vehicle management computers; coupling a plurality of electromechanical actuators between the vehicle management computers and the actuators, each of the electromechanical actuators operable to receive commands from the vehicle management computers and output a mechanical force to an input linkage of one of the actuators; characterized by coupling a plurality of electromechanical pilot input modules to the mechanical pilot inputs, each of the electromechanical pilot input modules operable to convert a pilot-driven input force of an instance of the mechanical pilot inputs into an electronic signal indicative of the pilot-driven input force; installing at least one high performance computer coupled to at least one of the vehicle management computers, the high performance computer being configured to execute one or more high level intelligence algorithms to selectively operate the aircraft autonomously; and coupling each of the electromechanical pilot input modules to a plurality of cockpit interface units, wherein each of the cockpit interface units is operable to receive an instance of the electronic signal indicative of the pilot-driven input force from each of the electromechanical pilot input modules and to communicate with at least one of the vehicle management computers. removing a plurality of mechanical links between a plurality of mechanical pilot inputs and a plurality of actuators operable to drive flight surfaces; installing a plurality of vehicle management computers; coupling a plurality of electromechanical actuators between the vehicle management computers and the actuators, each of the electromechanical actuators operable to receive commands from the vehicle management computers and output a mechanical force to an input linkage of one of the actuators; characterized by coupling a plurality of electromechanical pilot input modules to the mechanical pilot inputs, each of the electromechanical pilot input modules operable to convert a pilot-driven input force of an instance of the mechanical pilot inputs into an electronic signal indicative of the pilot-driven input force; installing at least one high performance computer coupled to at least one of the vehicle management computers, the high performance computer being configured to execute one or more high level intelligence algorithms to selectively operate the aircraft autonomously; and coupling each of the electromechanical pilot input modules to a plurality of cockpit interface units, wherein each of the cockpit interface units is operable to receive an instance of the electronic signal indicative of the pilot-driven input force from each of the electromechanical pilot input modules and to communicate with at least one of the vehicle management computers.
An inertial/video hybridization device intended to be carried on a carrier, the device comprising: - a first camera configured to acquire a first image showing a predetermined landmark attached to the carrier, - a second camera configured to acquire a second image also showing the landmark - a processing unit configured to estimate a velocity of the carrier from the acquired first image, in order to hybridize the estimated velocity with inertial data relating to the carrier produced by an inertial unit, the processing unit is further configured to: - locate a first position of the landmark in the first acquired image, - locate a second position of the landmark in the second acquired image, - determine a reference position of the landmark by applying to the second position a predetermined transformation representative of a change of reference frame from the second camera to the first camera, - calculate a deviation between the first located position and the reference position of the landmark, - compare the calculated deviation with a predetermined threshold, - signal an alert when the calculated deviation is greater than the predetermined threshold. - a first camera configured to acquire a first image showing a predetermined landmark attached to the carrier, - a second camera configured to acquire a second image also showing the landmark - a processing unit configured to estimate a velocity of the carrier from the acquired first image, in order to hybridize the estimated velocity with inertial data relating to the carrier produced by an inertial unit, - locate a first position of the landmark in the first acquired image, - locate a second position of the landmark in the second acquired image, - determine a reference position of the landmark by applying to the second position a predetermined transformation representative of a change of reference frame from the second camera to the first camera, - calculate a deviation between the first located position and the reference position of the landmark, - compare the calculated deviation with a predetermined threshold, - signal an alert when the calculated deviation is greater than the predetermined threshold.
A material for separating stem cell, which is made of fibers of combination of two or more synthetic polymer species, and which has a density K of 1.0 x 10 4 ≤ K ≤ 1.0 x 10 6 in basis weight (g/m 2)/thickness (m) and a fiber diameter of 3 to 40 μm, wherein the form of the fibers is that each of the fibers is composed of different synthetic polymer components or the fibers occur as split fibers resulting from peeling and splitting into fibers differing in component material, or the fibers result from conjugation of different single polymer fiber species respectively made of different synthetic polymers.
A method, comprising: hybrid multiplexing, with time division multiplexing and frequency division multiplexing, a relay-physical downlink control channel and relay-physical downlink shared channel of a backhaul link for a relay node as a hybrid multiplexed set of symbols, wherein the relay-physical downlink control channel comprises a searching space with parameters semi-statically configured to be searched by the relay node; and transmitting the hybrid multiplexed set of symbols to the relay node, wherein the hybrid multiplexing comprises defining the relay-physical downlink control channel searching space by a set of parameters including at least a physical resource block candidate set, a rank for the relay-physical downlink control channel, and control channel element aggregation level. hybrid multiplexing, with time division multiplexing and frequency division multiplexing, a relay-physical downlink control channel and relay-physical downlink shared channel of a backhaul link for a relay node as a hybrid multiplexed set of symbols, wherein the relay-physical downlink control channel comprises a searching space with parameters semi-statically configured to be searched by the relay node; and transmitting the hybrid multiplexed set of symbols to the relay node,
A decoder system (400; 500; 700; 1000) for decoding a bit stream signal as an audio time signal, including: a decoding section (410; 511, 512, 513; 711, 712, 713; 1011, 1013) for decoding a bit stream signal as a preliminary audio time signal by applying a decoding method adapted for speech decoding, and for estimating or extracting a pitch frequency from the bit stream signal; and a post filter (440; 540; 740; 1040) for filtering the preliminary audio time signal to attenuate noise located between harmonics of the pitch frequency to obtain an audio time signal, wherein the interharmonic noise attenuation is controlled by a post filter gain, further comprising a control section adapted to selectively disable the post filter, by setting the post filter gain to zero, responsive only to post-filtering information encoded in the bit stream signal, the post-filtering information being indicative of an encoder-side decision whether to disable post filtering, wherein the preliminary audio time signal is output as the audio time signal. a decoding section (410; 511, 512, 513; 711, 712, 713; 1011, 1013) for decoding a bit stream signal as a preliminary audio time signal by applying a decoding method adapted for speech decoding, and for estimating or extracting a pitch frequency from the bit stream signal; and a post filter (440; 540; 740; 1040) for filtering the preliminary audio time signal to attenuate noise located between harmonics of the pitch frequency to obtain an audio time signal, wherein the interharmonic noise attenuation is controlled by a post filter gain, further comprising a control section adapted to selectively disable the post filter, by setting the post filter gain to zero, responsive only to post-filtering information encoded in the bit stream signal, the post-filtering information being indicative of an encoder-side decision whether to disable post filtering, wherein the preliminary audio time signal is output as the audio time signal.
Spacecraft comprising: - a body having a face +Y and a face -Y opposite the face +Y; - a first radiator carried by at least one face out of the face +Y and the face -Y; said first radiator having an outer face; - a first supporting arm extending substantially perpendicularly to the outer face of the first radiator, said first supporting arm having a longitudinal axis (A-A); - a drive motor (50, 51) suitable for rotating the first supporting arm about said longitudinal axis (A-A) of the first supporting arm, the speed of rotation of the first supporting arm being substantially equal to the speed of revolution of the sun around the spacecraft; - a first assembly carried by the first supporting arm, said first assembly having at least one absorption face suitable for absorbing a portion of the incident solar radiation (I E) during the vernal and autumnal equinoxes, said first assembly being suitable for transmitting a heat generated by said portion of the incident solar radiation absorbed to the first radiator; said absorption face being inclined with respect to the outer face of the first radiator by an angle (α) substantially between 20° and 26°, characterised in that said first assembly comprises at least two slats attached one above the other and separated from each other by a free space (e), said slats being stationary with respect to the first supporting arm. - a body having a face +Y and a face -Y opposite the face +Y; - a first radiator carried by at least one face out of the face +Y and the face -Y; said first radiator having an outer face; - a first supporting arm extending substantially perpendicularly to the outer face of the first radiator, said first supporting arm having a longitudinal axis (A-A); - a drive motor (50, 51) suitable for rotating the first supporting arm about said longitudinal axis (A-A) of the first supporting arm, the speed of rotation of the first supporting arm being substantially equal to the speed of revolution of the sun around the spacecraft; - a first assembly carried by the first supporting arm, said first assembly having at least one absorption face suitable for absorbing a portion of the incident solar radiation (I E) during the vernal and autumnal equinoxes, said first assembly being suitable for transmitting a heat generated by said portion of the incident solar radiation absorbed to the first radiator; said absorption face being inclined with respect to the outer face of the first radiator by an angle (α) substantially between 20° and 26°,