mhurhangee/ep-ind-claims huggingface dataset:
A packaging system comprising: first and second box parts (100, 101), wherein one of the first and second box parts is fittable within the other of the first and second box parts; the first box part comprising an aperture and a latch slidably disposed within the aperture; the second box part comprising a channel that comprises: a locking channel segment; and an assembly channel segment; wherein the latch is configured to slide within the aperture and the locking channel segment between first and second positions, wherein: in the first position, the latch is aligned with the assembly channel segment and is disposed within the locking channel segment, the latch thereby being able to slide within the assembly channel segment to allow the first box part to be moved with respect to the second box part; in the second position, the latch is disposed within the locking channel segment but is not aligned with the assembly channel segment such that the latch cannot slide within the assembly channel segment, the latch thereby preventing the first box part from moving with respect to the second box part. first and second box parts (100, 101), wherein one of the first and second box parts is fittable within the other of the first and second box parts; the first box part comprising an aperture and a latch slidably disposed within the aperture; the second box part comprising a channel that comprises: a locking channel segment; and an assembly channel segment; wherein a locking channel segment; and an assembly channel segment; wherein the latch is configured to slide within the aperture and the locking channel segment between first and second positions, wherein: in the first position, the latch is aligned with the assembly channel segment and is disposed within the locking channel segment, the latch thereby being able to slide within the assembly channel segment to allow the first box part to be moved with respect to the second box part; in the second position, the latch is disposed within the locking channel segment but is not aligned with the assembly channel segment such that the latch cannot slide within the assembly channel segment, the latch thereby preventing the first box part from moving with respect to the second box part. in the first position, the latch is aligned with the assembly channel segment and is disposed within the locking channel segment, the latch thereby being able to slide within the assembly channel segment to allow the first box part to be moved with respect to the second box part; in the second position, the latch is disposed within the locking channel segment but is not aligned with the assembly channel segment such that the latch cannot slide within the assembly channel segment, the latch thereby preventing the first box part from moving with respect to the second box part.
A method for enabling a high-side switch of an over-current fault detection circuit for a system comprising: a. enabling the high-side switch for a predefined pulse time in order to provide an input voltage to a capacitor to charge the capacitor, wherein the capacitor is initially not charged and the predefined pulse time is less than an over-current fault time so that an over-current fault condition will not be created while charging the capacitor; b. thereafter disabling the high-side switch for the predefined pulse time; c. repeating steps a and b such that the high-side switch is modulated on and off while the capacitor is charged and until the capacitor is sufficiently charged; d. determining if the voltage of the capacitor is such that the capacitor is sufficiently charged such that an over-current fault condition will not be created if the high-side switch is enabled for greater than the over-current fault time unless there is an over-current fault condition; and e. enabling the high-side switch for the duration of the system operation, wherein the system operation includes enabling and disabling a low-side switch to excite an external load. a. enabling the high-side switch for a predefined pulse time in order to provide an input voltage to a capacitor to charge the capacitor, wherein the capacitor is initially not charged and the predefined pulse time is less than an over-current fault time so that an over-current fault condition will not be created while charging the capacitor; b. thereafter disabling the high-side switch for the predefined pulse time; c. repeating steps a and b such that the high-side switch is modulated on and off while the capacitor is charged and until the capacitor is sufficiently charged; d. determining if the voltage of the capacitor is such that the capacitor is sufficiently charged such that an over-current fault condition will not be created if the high-side switch is enabled for greater than the over-current fault time unless there is an over-current fault condition; and e. enabling the high-side switch for the duration of the system operation, wherein the system operation includes enabling and disabling a low-side switch to excite an external load.
Navigation aid instrument for an aircraft pilot including two left and right display devices having the function of indicating the left-right angle of inclination of the aircraft wings relative to the horizontal, said angle of inclination indicating respectively whether the wings are inclined on the left side or right side of said aircraft, wherein the angle of inclination is positive when the aircraft wings are inclined on the right side, a mobile marker being able to move either along the left display device or along the right display device to indicate to the pilot on which side the aeroplane is inclined, characterized in that the two left and right display devices extend vertically relative to the instrument panel of the aircraft and at a distance from each other, the value of the inclination being larger the further the mobile marker is away from the top of the left or right display device concerned, and wherein the resolution of the angle to be displayed by the two display devices and is ± 1° relative to the position in which the aircraft wings extend horizontally.
Payment terminal comprising a smart-card reader and a radio-electric antenna characterized in that said radio-electric antenna is positioned in proximity to an insertion hole of the smart-card reader, so that said antenna absorbs a part of the electrostatic discharge of a smart card when said card is inserted into said reader.
Mould for making stuffed or filled food products, in particular Sicilian arancini, comprising a base, a sleeve and a stud, the base being provided with a cavity having an aperture facing outwards, the sleeve having a first aperture and a second aperture and being configured to be removably coupled to the base in correspondence with the aperture of the cavity of the latter so as to direct the second aperture outwards, the sleeve having an internal shape such that the second aperture has an area smaller than the area of the first aperture, the stud being configured to insert into the second aperture of the sleeve, wherein the base, the sleeve and the stud are shaped according to shapes with cylindrical symmetry, whereby the aperture of the cavity of the base and the first and the second aperture (20, 21) of the sleeve are circular apertures, the stud having a tapered end and a cylindrical central portion having a cylindrical side surface with a diameter corresponding to an internal diameter of the second aperture of the sleeve.
A steering control system comprising: a control unit configured to perform steering control using a steering torque and a steering angle detected by a steering torque sensor and a steering angle sensor of a vehicle, wherein the control unit performs the steering control in consideration that the steering torque or the steering angle is changeable by a disturbance, characterized in that the vehicle has an autonomous driving system, that the control unit is configured to perform control such that steering assistance is provided according to the autonomous driving system when the steering torque and the steering angle are changed such that the directions of change of the steering torque and the steering angle are consistent with the predetermined reference direction and the rate of change of the steering angle is constant while a driver does not grip a steering wheel, and that when the steering torque and the steering angle are changed such that the directions of change of the steering torque and the steering angle are consistent with a predetermined reference direction and the rate of change of the steering angle is constant while a driver grips a steering wheel, the control unit is configured to perform control such that steering assistance is provided according to the driver's driving operation when the vehicle is in a non-dangerous area and to perform control such that steering assistance is provided according to the autonomous driving system when the vehicle is in a dangerous area. a control unit configured to perform steering control using a steering torque and a steering angle detected by a steering torque sensor and a steering angle sensor of a vehicle, wherein the control unit performs the steering control in consideration that the steering torque or the steering angle is changeable by a disturbance, characterized in that the vehicle has an autonomous driving system, that the control unit is configured to perform control such that steering assistance is provided according to the autonomous driving system when the steering torque and the steering angle are changed such that the directions of change of the steering torque and the steering angle are consistent with the predetermined reference direction and the rate of change of the steering angle is constant while a driver does not grip a steering wheel, and that when the steering torque and the steering angle are changed such that the directions of change of the steering torque and the steering angle are consistent with a predetermined reference direction and the rate of change of the steering angle is constant while a driver grips a steering wheel, the control unit is configured to perform control such that steering assistance is provided according to the driver's driving operation when the vehicle is in a non-dangerous area and to perform control such that steering assistance is provided according to the autonomous driving system when the vehicle is in a dangerous area.
Method for setting up end-to-end communication between two networks, comprising: reception of a message from a first network, wherein the message has a first header (35; 61) and an application data portion (36; 62); and coding of data from the first header (35; 61) into a second header within the application data portion (36; 62) using a first coding scheme in order to produce a modified application data portion, characterized by the steps of: coding of the modified application data portion using a second coding scheme in order to produce a coded message (43; 80); and sending of the coded message (43; 80) to a second network. reception of a message from a first network, wherein the message has a first header (35; 61) and an application data portion (36; 62); and coding of data from the first header (35; 61) into a second header within the application data portion (36; 62) using a first coding scheme in order to produce a modified application data portion, characterized by the steps of: coding of the modified application data portion using a second coding scheme in order to produce a coded message (43; 80); and sending of the coded message (43; 80) to a second network. coding of the modified application data portion using a second coding scheme in order to produce a coded message (43; 80); and sending of the coded message (43; 80) to a second network.
A single photon avalanche diode based apparatus comprising: at least one array of single photon avalanche diodes configured to receive light generated externally to the apparatus, wherein the at least one array is configurable to be sub-divided into a plurality of sub-arrays (Rx1, Rx2, Rx3, Rx4), each sub-array comprising at least one single photon avalanche diode and being able to receive a separate free space light communication channel; and a receiver configured to receive an output from each sub-array and output data based on the received plurality of sub-array separate free space light communication channels; characterized by the array of single photon avalanche diodes being configured to deactivate at least one sub-array photodiode such that no sub-array photodiode receives more than one free space light communication channel. at least one array of single photon avalanche diodes configured to receive light generated externally to the apparatus, wherein the at least one array is configurable to be sub-divided into a plurality of sub-arrays (Rx1, Rx2, Rx3, Rx4), each sub-array comprising at least one single photon avalanche diode and being able to receive a separate free space light communication channel; and a receiver configured to receive an output from each sub-array and output data based on the received plurality of sub-array separate free space light communication channels; characterized by the array of single photon avalanche diodes being configured to deactivate at least one sub-array photodiode such that no sub-array photodiode receives more than one free space light communication channel.
A wedge lock for use with a single board computer, said wedge lock comprising: a first portion configured to move in a first direction; and a second portion configured to move in a second direction in response to the movement of said first portion, characterized in that the second portion is further configured to move in a third direction that is perpendicular to the first and second directions (301, 334). a first portion configured to move in a first direction; and a second portion configured to move in a second direction in response to the movement of said first portion, characterized in that the second portion is further configured to move in a third direction that is perpendicular to the first and second directions (301, 334).
A motor control unit that includes motor control signal output means for outputting a motor control signal, and a drive circuit that supplies three-phase driving electric power to a motor based on the motor control signal, the motor control signal output means is configured to compute an addition angle (Θa) that corresponds to an amount of change in a motor rotation angle (Θm) in each computation period and to output the motor control signal by executing current control on a rotating coordinate system (γ/δ) that rotates in accordance with a control angle (Θc) computed by adding up the addition angles (Θa) in each computation period, and the motor control unit having a first computation mode in which a value (dΘτ) obtained by executing torque feedback control based on a torque deviation (Δτ) between a target torque (τ*) that is to be generated by the motor and an actual torque (τ) is used as the addition angle (Θa), characterized by a second computation mode in which a value obtained by correcting the value (dΘτ) obtained by executing the torque feedback control, based on an estimated motor rotation angular velocity (ωm_e) is used as the addition angle, wherein the motor control signal output means is configured to change a gain (K1,K2) of the torque feedback control depending on whether a mode of computation of the addition angle (Θa) is the first computation mode or the second computation mode.
A method for acoustically generating a droplet, comprising: (a) providing a reservoir containing (i) a lower layer comprised of a first fluid, and characterised by (ii) an upper layer comprised of a second fluid, the upper layer having a curved upper surface region; and an aperture region being an area of the upper layer that exhibits a local thickness minimum; wherein the aperture region exhibits a thickness of no more than 10% of the thickness of the first fluid under the aperture region, and wherein the first and second fluids are immiscible; and (b) applying focused acoustic energy to the reservoir in a manner effective to eject a droplet from the reservoir, wherein the droplet is comprised of a predetermined volume of the first fluid propelled through the upper layer at the aperture region; wherein the aperture region has a diameter of at least twice that of the ejected droplet. (a) providing a reservoir containing (i) a lower layer comprised of a first fluid, and characterised by (ii) an upper layer comprised of a second fluid, the upper layer having a curved upper surface region; and an aperture region being an area of the upper layer that exhibits a local thickness minimum; wherein the aperture region exhibits a thickness of no more than 10% of the thickness of the first fluid under the aperture region, and wherein the first and second fluids are immiscible; and (i) a lower layer comprised of a first fluid, and characterised by (ii) an upper layer comprised of a second fluid, the upper layer having a curved upper surface region; and an aperture region being an area of the upper layer that exhibits a local thickness minimum; wherein the aperture region exhibits a thickness of no more than 10% of the thickness of the first fluid under the aperture region, and wherein the first and second fluids are immiscible; and a curved upper surface region; and an aperture region being an area of the upper layer that exhibits a local thickness minimum; wherein the aperture region exhibits a thickness of no more than 10% of the thickness of the first fluid under the aperture region, and wherein the first and second fluids are immiscible; and (b) applying focused acoustic energy to the reservoir in a manner effective to eject a droplet from the reservoir, wherein the droplet is comprised of a predetermined volume of the first fluid propelled through the upper layer at the aperture region;
A power safety system configured to provide power information for an aircraft, the aircraft including a powerplant, the power safety system comprising: a power safety instrument, comprising: a power usage indicator located on a display, the power usage indicator being configured to communicate real-time power usage of the aircraft; a power required indicator located on the display, the power required indicator being configured to communicate a power required to operate the aircraft in a hover flight mode; a power available indicator located on the display, the power available indicator being configured to communicate a power available of the powerplant in the aircraft during the hover flight mode; at least one sensor configured to measure at least one variable having an effect on the power required and the power available; at least one data input device; and a calculation unit; wherein the calculation unit is configured to perform a power available calculation comprising conducting a power assurance check of the powerplant to evaluate its health and performance. a power safety instrument, comprising: a power usage indicator located on a display, the power usage indicator being configured to communicate real-time power usage of the aircraft; a power required indicator located on the display, the power required indicator being configured to communicate a power required to operate the aircraft in a hover flight mode; a power available indicator located on the display, the power available indicator being configured to communicate a power available of the powerplant in the aircraft during the hover flight mode; at least one sensor configured to measure at least one variable having an effect on the power required and the power available; at least one data input device; and a calculation unit; a power usage indicator located on a display, the power usage indicator being configured to communicate real-time power usage of the aircraft; a power required indicator located on the display, the power required indicator being configured to communicate a power required to operate the aircraft in a hover flight mode; a power available indicator located on the display, the power available indicator being configured to communicate a power available of the powerplant in the aircraft during the hover flight mode; at least one sensor configured to measure at least one variable having an effect on the power required and the power available; at least one data input device; and a calculation unit; wherein the calculation unit is configured to perform a power available calculation comprising conducting a power assurance check of the powerplant to evaluate its health and performance.
A multivalent combination vaccine for use in a method for (i) lessening the severity of clinical symptoms associated with PCV2 infection, and/or (ii) preventing PCV2 infection, in a pig, the vaccine comprising 1.6 μg to 400 μg recombinant PCV2 ORF2 protein per dose and at least one immunogenic active component against another disease-causing organism in swine, and wherein the lessening of the severity of clinical symptoms associated with PCV2 infection, and/or the prevention of PCV2 infection, is obtained by a single administration of the vaccine to the pig. (i) lessening the severity of clinical symptoms associated with PCV2 infection, and/or (ii) preventing PCV2 infection,
An aviation gasoline composition comprising 2,2,4-tri-methylpentane and at least one C 4 or C 5 alkane wherein the amount of 2,2,4-trimethylpentane in said composition is 60 to 90 vol %, the composition comprises at least 0.01 vol% and less than 5 vol % C 4 alkane, the composition comprises at least 10 vol % C 5 alkane, the composition comprises aromatics in an amount of up to 30 vol %, the amount of lead compounds in the composition is not greater than 0.003g of lead per litre, the composition has a final boiling point of less than 170 °C, the composition has a motor octane number of at least 92 and less than 98 and the composition has a supercharge of greater than 96 ON.
An apparatus for support and movement of a camera (38; 38') relative to an operator (1; 1') of the camera, the apparatus comprising a means (10; 10'; 52) for reception of the operator, a boom (20; 20'; 56) pivotally mounted at a proximal end thereof on the reception means above, in use of the apparatus, the shoulders of the operator and having adjacent its distal end a means (32; 68) for mounting a camera, and counterbalancing means (28; 28'; 76) arranged to counterbalance the weight of the boom and a camera mounted thereon in use of the apparatus during pivotal movement of the boom relative to the reception means, the boom comprising first and second spaced members (16,18; 16, 16'; 58, 60) extending from respective pivots (12,14; 12', 14'; 62,64) on the reception means above, in use, the shoulders of the user, each of the spaced members comprising two or more telescoping sections, arranged for the said movement of the camera relative to the operator during use, and wherein the spaced members are joined by at least one cross-member adjacent the distal end of the boom and the camera-mounting means (32; 68) are on the cross-member.