mhurhangee/ep-ind-claims huggingface dataset:
A method for displaying aircraft engine information, comprising: receiving a plurality of signals corresponding to the plurality of engine operating parameters; and if all the engine operating parameters are within corresponding ranges, determining that the overall operational state of the aircraft engine is a first overall operational state; or if fewer than all the engine operating parameters are within the corresponding ranges, determining that the overall operational state of the aircraft engine is a second overall operational state; directing the display (430;530) of an icon (431;531) that indicates a qualitative overall operational state of an aircraft engine, the overall operational state being determined from the plurality of engine operating parameters; and directing a change in the display of the icon when the overall operational state of the aircraft engine changes from the first overall operational state to the second overall operational state, wherein the change includes changing a color of the icon from a first color to a second color different than the first color; and characterised by directing the display of a text message (435;535) at least proximate to the icon corresponding to the cause of the change from the first overall operational state to the second overall operational state. receiving a plurality of signals corresponding to the plurality of engine operating parameters; and if all the engine operating parameters are within corresponding ranges, determining that the overall operational state of the aircraft engine is a first overall operational state; or if fewer than all the engine operating parameters are within the corresponding ranges, determining that the overall operational state of the aircraft engine is a second overall operational state; if all the engine operating parameters are within corresponding ranges, determining that the overall operational state of the aircraft engine is a first overall operational state; or if fewer than all the engine operating parameters are within the corresponding ranges, determining that the overall operational state of the aircraft engine is a second overall operational state; directing the display (430;530) of an icon (431;531) that indicates a qualitative overall operational state of an aircraft engine, the overall operational state being determined from the plurality of engine operating parameters; and directing a change in the display of the icon when the overall operational state of the aircraft engine changes from the first overall operational state to the second overall operational state, wherein the change includes changing a color of the icon from a first color to a second color different than the first color; and characterised by directing the display of a text message (435;535) at least proximate to the icon corresponding to the cause of the change from the first overall operational state to the second overall operational state.
A tail cutter comprising • a tail knife with a longitudinal cutting blade for cutting free part of the tail at the base part of the tail, characterized in that the tail cutter is suitable for being connected to a cutting device for splitting animal carcasses, the tail cutter being capable of partly cutting free the tail of an animal carcass while the cutting device is cutting the back of an animal carcass into two halves, that the tail cutter further comprises: • a finger connected to the tail knife, the finger being capable of directing the loose part of the tail to a predetermined side of the animal carcass, • the finger is bent to the right or left relative to the longitudinal direction of the cutting blade of the tail knife, and • that the tail cutter is configured such that, when the tail cutter is connected to a cutting device, the cutting blade of the tail knife is located in line with and/or in the same plane as the cutting device when the tail knife is located on this cutting device. • a tail knife with a longitudinal cutting blade for cutting free part of the tail at the base part of the tail, • a finger connected to the tail knife, the finger being capable of directing the loose part of the tail to a predetermined side of the animal carcass, • the finger is bent to the right or left relative to the longitudinal direction of the cutting blade of the tail knife, and • that the tail cutter is configured such that, when the tail cutter is connected to a cutting device, the cutting blade of the tail knife is located in line with and/or in the same plane as the cutting device when the tail knife is located on this cutting device.
A non-porous molded article for a polishing layer, the non-porous molded article comprising a thermoplastic polyurethane, characterised in that the thermoplastic polyurethane has a maximum value of a loss tangent, tan δ, in a range of -70 to -50°C of 4.00 × 10 -2 or less.
A two-part insertion tool comprising: (i) a guide sheath comprising a proximal end and a distal end, the proximal end being flared, the guide sheath comprising an inner surface defining a central lumen, the guide sheath further comprising a locking notch disposed on the inner surface between the proximal end and the distal end; and (ii) a protection tube comprising a proximal end and a distal end, the proximal end being flared; wherein a portion of the protection tube is situated within the central lumen of the guide sheath; and wherein the flared proximal end of the protection tube is sized to fit within the locking notch and has an outer diameter larger than portions of the inner surface immediately adjacent to the locking notch. (i) a guide sheath comprising a proximal end and a distal end, the proximal end being flared, the guide sheath comprising an inner surface defining a central lumen, the guide sheath further comprising a locking notch disposed on the inner surface between the proximal end and the distal end; and (ii) a protection tube comprising a proximal end and a distal end, the proximal end being flared; wherein a portion of the protection tube is situated within the central lumen of the guide sheath; and wherein the flared proximal end of the protection tube is sized to fit within the locking notch and has an outer diameter larger than portions of the inner surface immediately adjacent to the locking notch. wherein a portion of the protection tube is situated within the central lumen of the guide sheath; and wherein the flared proximal end of the protection tube is sized to fit within the locking notch and has an outer diameter larger than portions of the inner surface immediately adjacent to the locking notch.
An electronic device, comprising: a system unit; an internal power supplying unit, coupled to the system unit, and supplying a system voltage to the system unit; and a power controller, coupled to the system unit and the internal power supplying unit, receiving an external voltage from external of the electronic device, the electronic device being characterized in that the power controller is using a voltage value of the external voltage to determine a source of the external voltage, wherein when the power controller determines that the source of the external voltage is a mobile power supply device, the power controller supplies the external voltage to the system unit, and does not charge the internal power supplying unit with the external voltage. a system unit; an internal power supplying unit, coupled to the system unit, and supplying a system voltage to the system unit; and a power controller, coupled to the system unit and the internal power supplying unit, receiving an external voltage from external of the electronic device, the electronic device being characterized in that the power controller is using a voltage value of the external voltage to determine a source of the external voltage,
A catheter adapted to carry a position sensor, comprising: an elongated catheter body; a distal section distal the catheter body, the distal section having a longitudinal axis and a composite construction comprising: a plurality of deflectable members extending along the longitudinal axis; a plurality of support members extending along the longitudinal axis with a respective ring electrode being mounted on each support member, wherein the plurality of deflectable members and the plurality of support members are arranged in an alternating sequence along the longitudinal axis of the distal section; and a tip electrode, wherein a distal irrigation fluid path is provided axially through the plurality of deflectable members and the plurality of support members to deliver irrigation fluid to the respective ring electrode and the tip electrode; wherein each support member is constructed of a first material; wherein each deflectable member is constructed of a second material that is less rigid than the first material; wherein each support member also carries a respective coil sensor that is wound around an outer surface of the support member and wherein the coil sensor is wound in a groove formed in the outer surface of the support member. an elongated catheter body; a distal section distal the catheter body, the distal section having a longitudinal axis and a composite construction comprising: a plurality of deflectable members extending along the longitudinal axis; a plurality of support members extending along the longitudinal axis with a respective ring electrode being mounted on each support member, wherein the plurality of deflectable members and the plurality of support members are arranged in an alternating sequence along the longitudinal axis of the distal section; and a tip electrode, a plurality of deflectable members extending along the longitudinal axis; a plurality of support members extending along the longitudinal axis with a respective ring electrode being mounted on each support member, wherein the plurality of deflectable members and the plurality of support members are arranged in an alternating sequence along the longitudinal axis of the distal section; and a tip electrode, wherein a distal irrigation fluid path is provided axially through the plurality of deflectable members and the plurality of support members to deliver irrigation fluid to the respective ring electrode and the tip electrode; wherein each support member is constructed of a first material; wherein each deflectable member is constructed of a second material that is less rigid than the first material; wherein each support member also carries a respective coil sensor that is wound around an outer surface of the support member and wherein the coil sensor is wound in a groove formed in the outer surface of the support member.
A process for producing expanded particles comprising at least one polyolefin, which comprises at least the steps production of a suspension comprising a pelletized material comprising at least one polyolefin in water, impregnation of the pelletized material comprised in the suspension from step with at least one blowing agent in order to obtain a pelletized material loaded with blowing agent in suspension, and depressurization of the suspension obtained in step in order to obtain expanded particles, wherein the phase ratio of pelletized material used in step to water is >0.5 and nitrogen is used as blowing agent in step, where the bulk density of the expanded particles is from 80 to 300 g/l. production of a suspension comprising a pelletized material comprising at least one polyolefin in water, impregnation of the pelletized material comprised in the suspension from step with at least one blowing agent in order to obtain a pelletized material loaded with blowing agent in suspension, and depressurization of the suspension obtained in step in order to obtain expanded particles,
A system for removing speckle from an image frame of a surgical site comprising: an endoscopic device comprising a distal end; an imaging device comprising a CMOS image sensor, wherein the CMOS image sensor comprises a pixel array located at the distal end of the endoscopic device; a pulsing coherent light source for providing light to a surgical site, wherein the pulsing coherent light source is pulsed at an interval that corresponds in time to the operation and functionality of the pixel array of the CMOS image sensor; a control unit comprising circuitry for sending data to the CMOS image sensor and receiving data from the CMOS image sensor to create an image frame of the surgical site; a display that allows a user to visualize the surgical site; a first fiber optic bundle connected to the pulsing coherent light source; a second fiber optic bundle connected to the first fiber optic bundle at a junction; and a vibrating mechanism located at the junction that causes the light to lose coherence momentarily as the geometry of its path is changed, thereby substantially removing any speckle from the image frame of the surgical site; wherein the pulsing coherent light source is pulsed in a plurality of electromagnetic partitions, such that the pixel array receives electromagnetic energy and produces a data set that corresponds in time with each of the plurality of electromagnetic partitions. an endoscopic device comprising a distal end; an imaging device comprising a CMOS image sensor, wherein the CMOS image sensor comprises a pixel array located at the distal end of the endoscopic device; a pulsing coherent light source for providing light to a surgical site, wherein the pulsing coherent light source is pulsed at an interval that corresponds in time to the operation and functionality of the pixel array of the CMOS image sensor; a control unit comprising circuitry for sending data to the CMOS image sensor and receiving data from the CMOS image sensor to create an image frame of the surgical site; a display that allows a user to visualize the surgical site; a first fiber optic bundle connected to the pulsing coherent light source; a second fiber optic bundle connected to the first fiber optic bundle at a junction; and a vibrating mechanism located at the junction that causes the light to lose coherence momentarily as the geometry of its path is changed, thereby substantially removing any speckle from the image frame of the surgical site; wherein the pulsing coherent light source is pulsed in a plurality of electromagnetic partitions, such that the pixel array receives electromagnetic energy and produces a data set that corresponds in time with each of the plurality of electromagnetic partitions.
A motorcycle tire comprising: a tread portion having a pair of tread edges (Te) and a tread surface therebetween, and comprising a crown region (Cr) including a tire equator and a pair of shoulder regions (Sh) respectively including the tread edges (Te); a pair of axially spaced bead portions; a pair of sidewall portions extending from the tread edges (Te) to the bead portions; a bias-ply carcass extending between the bead portions through the tread portion and the sidewall portions, and comprising a plurality of carcass plies of carcass cords, including an outer carcass ply which is radially outermost in the tread portion in the carcass plies; a band disposed radially outside the carcass in the tread portion, and comprising a jointless band ply composed of at least one band cord wound spirally and circumferentially of the tire at 5 degrees or less with respect to the tire circumferential direction; and a tread rubber disposed radially outside the band, characterized in that a loss tangent of the tread rubber at a temperature of 0 deg C is larger in the crown region (Cr) than in the shoulder regions (Sh), wherein the loss tangent is measured under the conditions frequency 5 Hz, initial strain 10%, and dynamic strain +/-2.5%, and angles of the carcass cords of the outer carcass ply with respect to the tire circumferential direction are smaller in the crown region (Cr) than in the shoulder regions (Sh). a tread portion having a pair of tread edges (Te) and a tread surface therebetween, and comprising a crown region (Cr) including a tire equator and a pair of shoulder regions (Sh) respectively including the tread edges (Te); a pair of axially spaced bead portions; a pair of sidewall portions extending from the tread edges (Te) to the bead portions; a bias-ply carcass extending between the bead portions through the tread portion and the sidewall portions, and comprising a plurality of carcass plies of carcass cords, including an outer carcass ply which is radially outermost in the tread portion in the carcass plies; a band disposed radially outside the carcass in the tread portion, and comprising a jointless band ply composed of at least one band cord wound spirally and circumferentially of the tire at 5 degrees or less with respect to the tire circumferential direction; and a tread rubber disposed radially outside the band, characterized in that a loss tangent of the tread rubber at a temperature of 0 deg C is larger in the crown region (Cr) than in the shoulder regions (Sh), wherein the loss tangent is measured under the conditions frequency 5 Hz, initial strain 10%, and dynamic strain +/-2.5%, and angles of the carcass cords of the outer carcass ply with respect to the tire circumferential direction are smaller in the crown region (Cr) than in the shoulder regions (Sh).
A composite compressed gas tank for a gas, comprising an outer casing and a liner which is enveloped by the outer casing and comprises a light metal, more especially aluminium or an aluminium alloy, into the feed and discharge opening of which is inserted a closure element which has at least one channel (2a, 2b) for the feed and/or discharge of gas and which comprises light metal, more especially aluminium or an aluminium alloy and which is connected to the liner by a welded joint and wherein a component is provided which is composed of individual elements (4a, 4b) and is prefabricated away from the compressed gas tank, the first end portion of the component comprises light metal, more especially aluminium or an aluminium alloy and the other end portion thereof comprises a steel material, is connected by its first end portion to the closure element of the compressed gas tank by a welded joint, characterised in that at least one connection line (5a, 5b), comprising a steel material is welded to the other end portion, comprising a steel material, of the mentioned component.
An unmanned aerial vehicle, UAV, comprising one or more image sensors (212, 214, 216); a propulsion mechanism; and one or more processors configured by executable instructions to perform operations comprising: capturing, with the one or more image sensors (212, 214, 216), while the UAV is in flight, a plurality of images of a scan target; using distance information determined based on the plurality of images for determining respective locations in three-dimensional, 3D, space of a plurality of points of a 3D model, the plurality of points representative of a surface of the scan target; comparing a first image of the plurality of images with a second image of the plurality of images to determine a difference between a position for the UAV in a current frame of reference and a position for the UAV in an estimate of an actual frame of reference; and based at least on the difference, determining, while the UAV is in flight, an update to the 3D model including at least one of: an updated location of at least one point in the 3D model, or a location of a new point in the 3D model. one or more image sensors (212, 214, 216); a propulsion mechanism; and one or more processors configured by executable instructions to perform operations comprising: capturing, with the one or more image sensors (212, 214, 216), while the UAV is in flight, a plurality of images of a scan target; using distance information determined based on the plurality of images for determining respective locations in three-dimensional, 3D, space of a plurality of points of a 3D model, the plurality of points representative of a surface of the scan target; comparing a first image of the plurality of images with a second image of the plurality of images to determine a difference between a position for the UAV in a current frame of reference and a position for the UAV in an estimate of an actual frame of reference; and based at least on the difference, determining, while the UAV is in flight, an update to the 3D model including at least one of: an updated location of at least one point in the 3D model, or a location of a new point in the 3D model. capturing, with the one or more image sensors (212, 214, 216), while the UAV is in flight, a plurality of images of a scan target; using distance information determined based on the plurality of images for determining respective locations in three-dimensional, 3D, space of a plurality of points of a 3D model, the plurality of points representative of a surface of the scan target; comparing a first image of the plurality of images with a second image of the plurality of images to determine a difference between a position for the UAV in a current frame of reference and a position for the UAV in an estimate of an actual frame of reference; and based at least on the difference, determining, while the UAV is in flight, an update to the 3D model including at least one of: an updated location of at least one point in the 3D model, or a location of a new point in the 3D model.
A modified heterophasic copolymer polypropylene for the preparation of thermoformed articles, obtained by modification via reactive extrusion of a polypropylene comprising from 0% to 6% comonomer in the synthesis thereof, a rubber phase comprising propene and at least one alpha-olefin or ethene comonomer at a ratio of 3 to 70% by weight and having 3 to 18 carbons, characterized in that the polypropylene matrix comprises from 0.3 to 2 long-chain branches per 1,000 carbon atoms, and in that the modified heterophasic copolymer polypropylene has a MFR greater than 1.5 g/10 min, a melt strength of between 12cN and 40 cN at 190°, an extensibility greater than 11 cm/s and an impact strength higher than 100 J/m at room temperature.
A composition of transgenic factor VII (FVII), each molecule of factor VII of the composition exhibiting two N-glycosylation sites, characterized in that: - among all the molecules of FVII of the composition, the rate of Galα1,3Gal glycan moieties is comprised between 0 and 4%, the rate of Galα1,3Gal glycan moieties being measured by lectin-blot with exposure to 4-chloro-1-naphtol, and - all of the sialic acids of the FVII imply α2-6 links, and - factor VII of the composition is produced by transgenic female rabbits. - among all the molecules of FVII of the composition, the rate of Galα1,3Gal glycan moieties is comprised between 0 and 4%, the rate of Galα1,3Gal glycan moieties being measured by lectin-blot with exposure to 4-chloro-1-naphtol, and - all of the sialic acids of the FVII imply α2-6 links, and - factor VII of the composition is produced by transgenic female rabbits.