mhurhangee/ep-ind-claims huggingface dataset:
A method of operation of a computing system, comprising: determining a current road type for a current road segment based on a current location of a device (102, 106) located along the current road segment; generating a current zoom level of a map including the current location on the current road segment based on the current road type; generating a camera view of the map for the current zoom level based on a look ahead distance for the current road type, the camera view comprising a degree of inclination angle related to a point of view of the map and a magnification, wherein the look ahead distance is a distance between the current location and the real world location of the top edge of the map displayed in an active map area of a display interface (206, 234), and wherein the look ahead distance is calculated based on i) a minimum distance for the look ahead distance based on a current travel speed of the device (102, 106) and/or based on a speed limit of the current road segment, and ii) a look ahead distance multiplier based on a width to height ratio of the active map area; and displaying the current location along the current road segment in the active map area of the display interface (206, 234), at the current zoom level. determining a current road type for a current road segment based on a current location of a device (102, 106) located along the current road segment; generating a current zoom level of a map including the current location on the current road segment based on the current road type; generating a camera view of the map for the current zoom level based on a look ahead distance for the current road type, the camera view comprising a degree of inclination angle related to a point of view of the map and a magnification, wherein the look ahead distance is a distance between the current location and the real world location of the top edge of the map displayed in an active map area of a display interface (206, 234), and wherein the look ahead distance is calculated based on i) a minimum distance for the look ahead distance based on a current travel speed of the device (102, 106) and/or based on a speed limit of the current road segment, and ii) a look ahead distance multiplier based on a width to height ratio of the active map area; and displaying the current location along the current road segment in the active map area of the display interface (206, 234), at the current zoom level.
Method for improving an operation of a technical installation, wherein the technical process running within the installation is controlled and/or monitored by means of a process control system according to the functions specified in a function plan as part of a configuration, and wherein process-related and control-related data is recorded and written into an archive, characterised in that the archive entries, which are associated with reports, operating actions and switching operations, within a time range to be defined are analysed by a statistical relevance of the archive entries under consideration first being identified, a cause identification is performed for the statistically most relevant archive entries, using all archive entries which have occurred during the time range under consideration, by evaluating the function plans, and from the causes identified in this manner, proposed solutions for reducing the reports, operating actions and switching operations are derived, in order to improve the operation of the technical installation.
A method for providing film grain information comprising the steps of: characterizing an image information stream prior to encoding to provide information indicative of film grain within the image stream, the film grain information including at least one parameter specifying an attributes of the film grain in the image stream; characterized by: encoding the film grain information separately from encoding the image information for subsequent transmission together to enable simulation of film grain in the image stream upon decoding using the film grain information upon decoding. characterizing an image information stream prior to encoding to provide information indicative of film grain within the image stream, the film grain information including at least one parameter specifying an attributes of the film grain in the image stream; characterized by: encoding the film grain information separately from encoding the image information for subsequent transmission together to enable simulation of film grain in the image stream upon decoding using the film grain information upon decoding.
An aircraft landing gear assembly (10, 30, 40) comprising: a main shock absorbing strut arranged to be movably coupled to an aircraft so as to move between a deployed condition, for take-off and landing, and a stowed condition for flight; a support linkage (18, 28) coupled at a first anchor point (AP1, AP1') to the main shock absorbing strut and having a second anchor point (AP2, AP2') arranged to be coupled to the aircraft, the support linkage having a locked condition in which it is arranged to inhibit movement of the main shock absorbing strut from the deployed condition in one or more planes of movement and an unlocked condition in which it permits the main shock absorbing strut to move from the deployed condition to the retracted condition, wherein the support linkage comprises a split tube spring (22, 32, 42) having a longitudinal slot (23, 33, 34), the spring being biased to assume a tubular condition in which it can react axial loading thereof, and an actuator operable to radially enlarge a region of the tube for the tube to fold at the enlarged region, the support linkage being in the locked condition when the tube is in the tubular condition and being in the unlocked condition when the tube is folded. a main shock absorbing strut arranged to be movably coupled to an aircraft so as to move between a deployed condition, for take-off and landing, and a stowed condition for flight; a support linkage (18, 28) coupled at a first anchor point (AP1, AP1') to the main shock absorbing strut and having a second anchor point (AP2, AP2') arranged to be coupled to the aircraft, the support linkage having a locked condition in which it is arranged to inhibit movement of the main shock absorbing strut from the deployed condition in one or more planes of movement and an unlocked condition in which it permits the main shock absorbing strut to move from the deployed condition to the retracted condition, wherein the support linkage comprises a split tube spring (22, 32, 42) having a longitudinal slot (23, 33, 34), the spring being biased to assume a tubular condition in which it can react axial loading thereof, and an actuator operable to radially enlarge a region of the tube for the tube to fold at the enlarged region, the support linkage being in the locked condition when the tube is in the tubular condition and being in the unlocked condition when the tube is folded.
A system for determining structural characteristics of an object, comprising: a handpiece having a housing with an open end and a longitudinal axis; an energy application tool mounted inside the housing for applying energy to the object; a drive mechanism supported inside the housing, said drive mechanism adapted for moving the energy application tool; a sleeve protruding from the open end of the housing for a distance, said sleeve adapted for resting against said object with at least a portion of its open end; a sensor positioned inside said housing adapted for monitoring that a proper force is applied when the sleeve rests on the object; and a computer coupled to said handpiece adapted for determining structural characteristics of the object, wherein said energy application tool is adapted for axial movement along a longitudinal axis of the housing between a retracted form and an extended form during a measurement, the system characterized in that it further comprises a disposable feature for enveloping at least a portion of the system, the disposable feature comprising a separable tip connected to a front portion of the energy application tool by means of magnetic force, and a membrane that envelopes at least the front portion of the energy application tool; said membrane comprising a retracted form and an extended form adapted for accommodating the resting and active forms of the energy application tool during a measurement. a handpiece having a housing with an open end and a longitudinal axis; an energy application tool mounted inside the housing for applying energy to the object; a drive mechanism supported inside the housing, said drive mechanism adapted for moving the energy application tool; a sleeve protruding from the open end of the housing for a distance, said sleeve adapted for resting against said object with at least a portion of its open end; a sensor positioned inside said housing adapted for monitoring that a proper force is applied when the sleeve rests on the object; and a computer coupled to said handpiece adapted for determining structural characteristics of the object, wherein said energy application tool is adapted for axial movement along a longitudinal axis of the housing between a retracted form and an extended form during a measurement, the system characterized in that it further comprises a disposable feature for enveloping at least a portion of the system, the disposable feature comprising a separable tip connected to a front portion of the energy application tool by means of magnetic force, and a membrane that envelopes at least the front portion of the energy application tool; said membrane comprising a retracted form and an extended form adapted for accommodating the resting and active forms of the energy application tool during a measurement.
Mobile lightweight lifting device which comprises two lifting forks fastened to a plate with a double-acting hydraulic cylinder and a chassis with a support frame, wherein the plate with the lifting forks is moved in the vertical direction by means of an electrically operated hydraulic pump, in which guide devices for running rails are attached to the support frame, either rigidly or in a laterally movable manner by manual or electrical or hydraulic means, in the direction perpendicular to the support frame, and which has a steering device, characterized in that the electrical energy supply unit is integrated into the front part of the lifting forks, in that the drive and control units for the movement of the lifting forks and of the chassis, as well as the lifting forks and the double-acting hydraulic cylinder, are fastened to the plate which can be moved in the vertical direction by means of the double-acting hydraulic cylinder.
A sterilized injectable hyaluronic acid composition comprising - a crosslinked hyaluronic acid gel, - lidocaine, and - an ascorbyl glycoside in an amount which prevents or reduces the effect on the viscosity and/or elastic modulus G' of the composition caused by the lidocaine upon sterilization by heat; wherein the concentration of said ascorbyl glycoside is in the range of 0.01 to 5 mg/ml. - a crosslinked hyaluronic acid gel, - lidocaine, and - an ascorbyl glycoside in an amount which prevents or reduces the effect on the viscosity and/or elastic modulus G' of the composition caused by the lidocaine upon sterilization by heat;
An engine having an engine shaft configured to rotate and cause one or more pistons (320, 322) to reciprocate within a cylinder chamber along an axis, each piston having a first piston part and piston stem to move in unison with or separately from a second piston part to define piston strokes for different thermal functions of the engine, the engine comprising: a piston lever having a first end coupled to a movable fulcrum point and a second end coupled at a copy point to the piston stem; an actuation mechanism configured to move the piston lever and thereby the copy point; and a guide apparatus configured to dictate movement of the copy point in a direction substantially parallel to the cylinder axis, wherein a movable fulcrum comprises a roller or a slider moveable within a guide apparatus such that the movable fulcrum point is configured to move in a direction substantially perpendicular with the cylinder chamber axis. a piston lever having a first end coupled to a movable fulcrum point and a second end coupled at a copy point to the piston stem; an actuation mechanism configured to move the piston lever and thereby the copy point; and a guide apparatus configured to dictate movement of the copy point in a direction substantially parallel to the cylinder axis, wherein a movable fulcrum comprises a roller or a slider moveable within a guide apparatus such that the movable fulcrum point is configured to move in a direction substantially perpendicular with the cylinder chamber axis.
A use of a reinforcement element for monitoring strain within a railway line, wherein the reinforcement element comprises at least one single-mode sensor fiber adapted for strain measurements based on stimulated Brillouin scattering within said sensor fiber, wherein the reinforcement element is a flexible or stiff geosynthetic material or a geotextile.
A pneumatic tire for motorcycles having a tread portion formed in a part circular shape as viewed in section through a rotational axis of the tire, said tread portion having a crown portion which has a spiral belt layer in its inside in the radial direction of the tire, said spiral belt layer having an angle of 0 to 5° with respect to the equatorial direction of the tire and an arrangement width 0.5 to 0.8 times as large as the tread width, wherein said spiral belt layer is arranged in such a manner that the center of the transverse direction of said spiral belt layer coincides with the tire equator and characterized in that the curvature radius from the end portion of said spiral belt layer to the end portion of the tread portion is larger than the curvature radius from the end portion of said spiral belt layer to the tire equatorial plane.
A method for a control channel transmission by a wireless transmit/receive unit, WTRU, the method comprising: operating with a common enhanced dedicated channel, E-DCH, resource and on-going common control channel, CCCH, traffic, wherein the common E-DCH resource is associated with the on-going CCCH traffic; determining that dedicated control channel, DCCH / dedicated traffic channel, DTCH, data is available for transmission; and waiting until a CCCH resource is released before transmitting DCCH/DTCH traffic. operating with a common enhanced dedicated channel, E-DCH, resource and on-going common control channel, CCCH, traffic, wherein the common E-DCH resource is associated with the on-going CCCH traffic; determining that dedicated control channel, DCCH / dedicated traffic channel, DTCH, data is available for transmission; and waiting until a CCCH resource is released before transmitting DCCH/DTCH traffic.
A rechargeable battery, comprising: a case; an electrode assembly situated inside the case; a cap plate sealing an opening of the case; and an electrode terminal mounted at the cap plate and electrically connected to the electrode assembly; wherein the case includes a first wall that extends in a first direction and comprises a first curved portion that is curved in cross-section characterised in that the rechargeable battery further comprises a reinforcing plate bonded to the first curved portion, wherein the reinforcing plate comprises a second curved portion that is curved in cross-section; and the second curved portion is coupled with the first curved portion; further wherein the reinforcing plate comprises a plurality of plate portions and ribs that project toward or away from the first curved portion, and the plate portions and the ribs are alternately provided. a case; an electrode assembly situated inside the case; a cap plate sealing an opening of the case; and an electrode terminal mounted at the cap plate and electrically connected to the electrode assembly; wherein the case includes a first wall that extends in a first direction and comprises a first curved portion that is curved in cross-section characterised in that the rechargeable battery further comprises a reinforcing plate bonded to the first curved portion, wherein the reinforcing plate comprises a second curved portion that is curved in cross-section; and the second curved portion is coupled with the first curved portion; further wherein the reinforcing plate comprises a plurality of plate portions and ribs that project toward or away from the first curved portion, and the plate portions and the ribs are alternately provided.
A CO 2 recovery method in which a CO 2 absorption tower and an absorption-solution regeneration tower are used to reuse a lean solution, from which CO 2 has been removed in the absorption-solution regeneration tower, in the CO 2 absorption tower, the CO 2 absorption tower bringing CO 2 -containing flue gas into contact with a basic amine compound so as to remove CO 2, the absorption-solution regeneration tower separating CO 2 from the CO 2 -absorbed basic amine compound to regenerate a CO 2 absorption solution, and the method comprising: simultaneously removing basic amine compounds and aldehyde compounds by washing decarbonated flue gas with washing water in plural stages of water washing sections and supplying an aldehyde-compound removing agent including a sulfite compound, a bisulfite compound or a mixture thereof to washing water of a washing section in the plural stages of water washing sections, which is provided close to a top portion of the CO 2 absorption tower, by supplying an acid to the washing water of the washing section in the plural stages of water-washing sections to control the washing water to be acidic. simultaneously removing basic amine compounds and aldehyde compounds by washing decarbonated flue gas with washing water in plural stages of water washing sections and supplying an aldehyde-compound removing agent including a sulfite compound, a bisulfite compound or a mixture thereof to washing water of a washing section in the plural stages of water washing sections, which is provided close to a top portion of the CO 2 absorption tower, by supplying an acid to the washing water of the washing section in the plural stages of water-washing sections to control the washing water to be acidic.
A kennel for dogs or other animals including pets, or also for other uses, consisting of a structure with a base and a roof, said base being equipped with four vertical walls at least one of which being provided with an opening for the dog to pass through, at least one of said walls consisting of a pivotable wall which is hinged at its lower edge to the base characterised in that the upper edge of said at least one pivotable wall is provided with a latch mechanism which, when it is in the closed latched position, holds in place said pivotable vertical wall while, when it is in the open unlatched position, allows a rotation movement of said wall about its hinges so as to transform said wall into a platform arranged substantially at the same level as the base of the kennel.
A method for wireless communication by an apparatus (110, 120), the method comprising: determining one or more orthogonal frequency division multiplexing, OFDM, symbols to transmit channel reservation signals; determining a plurality of resources available for transmitting the channel reservation signals during the one or more OFDM symbols by determining a plurality of decoding candidates available for sending the channel reservation signals, wherein each decoding candidate comprises one or more control channel elements, CCEs; selecting one set of resources within the plurality of resources to transmit a channel reservation signal, the selecting comprising selecting one of the decoding candidates to use for sending the channel reservation signal, wherein the selected set of resources comprises the CCEs of the selected decoding candidate; and transmitting the channel reservation signal in the selected set of resources to reserve a portion of spectrum for communication. determining one or more orthogonal frequency division multiplexing, OFDM, symbols to transmit channel reservation signals; determining a plurality of resources available for transmitting the channel reservation signals during the one or more OFDM symbols by determining a plurality of decoding candidates available for sending the channel reservation signals, wherein each decoding candidate comprises one or more control channel elements, CCEs; selecting one set of resources within the plurality of resources to transmit a channel reservation signal, the selecting comprising selecting one of the decoding candidates to use for sending the channel reservation signal, wherein the selected set of resources comprises the CCEs of the selected decoding candidate; and transmitting the channel reservation signal in the selected set of resources to reserve a portion of spectrum for communication.
A method for determining a performance model of an aircraft, the flight of the aircraft being segmented into a number n_phase of flight phases, wherein each phase can be modelled by a set E of predefined equations dependent on a number p_exp of explanatory variables and on a number n_par of parameters, and which provide an observation vector of size q_mes, the method comprising the steps of: (a) determining, from data derived from a plurality of flight recordings, the content of an observation table having a number m_obs of rows and a number p_exp + q_mes of columns; the table containing points associated with flight phases; (b) determining, for a number n_par of parameters, a number of initial parameters; (c) calculating, from the number of initial parameters, a least-squares criterion for the observation table; and (d) using the least-squares criterion obtained in a parametric optimisation engine and iterating steps (b) and (c) until a predefined minimality criterion is satisfied, said minimality criterion being satisfied for a number n_par of parameters, referred to as end parameters, said end parameters determining an optimised aircraft performance model. (a) determining, from data derived from a plurality of flight recordings, the content of an observation table having a number m_obs of rows and a number p_exp + q_mes of columns; the table containing points associated with flight phases; (b) determining, for a number n_par of parameters, a number of initial parameters; (c) calculating, from the number of initial parameters, a least-squares criterion for the observation table; and (d) using the least-squares criterion obtained in a parametric optimisation engine and iterating steps (b) and (c) until a predefined minimality criterion is satisfied, said minimality criterion being satisfied for a number n_par of parameters, referred to as end parameters, said end parameters determining an optimised aircraft performance model.