mhurhangee/ep-ind-claims huggingface dataset:
A vehicle comprising: a main body; a plurality of wheels coupled to said main body, wherein one of said wheels comprises a steerable wheel; a traction motor associated with said main body and coupled to at least one of said wheels for driving said at least one wheel; control apparatus (220, 1320) coupled to said traction motor and generating a motor drive signal to said traction motor; a first sensor for generating a velocity signal indicative of a velocity of said driven wheel; a further sensor for sensing an acceleration of said main body and generating a vehicle acceleration signal; characterized in that said control apparatus (220, 1320) setting a timer to start running for a predetermined time period when one or more vehicle conditions are met and during said predetermined time period determining a measured velocity of said driven wheel from said first sensor velocity signal, calculating a velocity of said vehicle using said vehicle acceleration signal, and comparing said measured velocity of said driven wheel to said calculated velocity of said vehicle to determine wheel slip status; wherein said one or more vehicle conditions comprises a magnitude of a torque applied by said traction motor to said driven wheel being less than a predefined value, and a steer angle of said steerable wheel being less than a predetermined value. a main body; a plurality of wheels coupled to said main body, wherein one of said wheels comprises a steerable wheel; a traction motor associated with said main body and coupled to at least one of said wheels for driving said at least one wheel; control apparatus (220, 1320) coupled to said traction motor and generating a motor drive signal to said traction motor; a first sensor for generating a velocity signal indicative of a velocity of said driven wheel; a further sensor for sensing an acceleration of said main body and generating a vehicle acceleration signal; characterized in that said control apparatus (220, 1320) setting a timer to start running for a predetermined time period when one or more vehicle conditions are met and during said predetermined time period determining a measured velocity of said driven wheel from said first sensor velocity signal, calculating a velocity of said vehicle using said vehicle acceleration signal, and comparing said measured velocity of said driven wheel to said calculated velocity of said vehicle to determine wheel slip status; wherein said one or more vehicle conditions comprises a magnitude of a torque applied by said traction motor to said driven wheel being less than a predefined value, and a steer angle of said steerable wheel being less than a predetermined value.
An aircraft galley insert, comprising: a control unit including a control unit housing wherein the control unit housing comprises a base plate coupled to a control unit cover, and wherein the base plate comprises at least one of a molded aluminum structure, a casted aluminum structure, a titanium structure, or a steel structure; one or more electronic components at least partially contained within the control unit housing, wherein at least one electronic component of the one or more electronic components is coupled to the control unit housing; and one or more operating load components electrically coupled to the at least one electronic component via one or more electrical lines, wherein the control unit housing is configured to provide a grounding path for radiated emissions produced by the at least one electronic component by transferring radiated emissions back to the at least one electronic component; and characterized in that: the base plate includes one or more stand-offs, wherein the base plate is coupled to a printed circuit board at the one or more stand-offs; and wherein the control unit housing is further configured to thermally couple to the at least one electronic component and dissipate heat from the at least one electronic component. a control unit including a control unit housing wherein the control unit housing comprises a base plate coupled to a control unit cover, and wherein the base plate comprises at least one of a molded aluminum structure, a casted aluminum structure, a titanium structure, or a steel structure; one or more electronic components at least partially contained within the control unit housing, wherein at least one electronic component of the one or more electronic components is coupled to the control unit housing; and one or more operating load components electrically coupled to the at least one electronic component via one or more electrical lines, wherein the control unit housing is configured to provide a grounding path for radiated emissions produced by the at least one electronic component by transferring radiated emissions back to the at least one electronic component; and characterized in that: the base plate includes one or more stand-offs, wherein the base plate is coupled to a printed circuit board at the one or more stand-offs; and wherein the control unit housing is further configured to thermally couple to the at least one electronic component and dissipate heat from the at least one electronic component.
A method for aiding the flight management of an aircraft during a landing on an airport phase, a method according to which the aircraft flies along a final approach path which joins the runway used at an aiming point, characterized in that, automatically: a) information relative to actual conditions regarding the environment and the runway is received; b) using this information and characteristics of the the runway, a maximum shift (Dmax) is determined which corresponds to the maximum longitudinal shift along the runway, with respect to the runway threshold, of the point of passage of the aircraft at a predetermined height with respect to the runway; c) using actual conditions regarding the environment and the runway, predetermined criteria and said maximum shift, an actual shift (Deff) is determined which is less than said maximum shift (Dmax), as well as a shift point (P0f) which is shifted from the threshold of the runway along the latter in the downstream direction by the length of said actual shift (Deff); d) from said shift point (P0f), a so-called adaptive aiming point (P1f) is calculated; and e) this adaptive aiming point (P1f) is transmitted to landing aid means of the aircraft. a) information relative to actual conditions regarding the environment and the runway is received; b) using this information and characteristics of the the runway, a maximum shift (Dmax) is determined which corresponds to the maximum longitudinal shift along the runway, with respect to the runway threshold, of the point of passage of the aircraft at a predetermined height with respect to the runway; c) using actual conditions regarding the environment and the runway, predetermined criteria and said maximum shift, an actual shift (Deff) is determined which is less than said maximum shift (Dmax), as well as a shift point (P0f) which is shifted from the threshold of the runway along the latter in the downstream direction by the length of said actual shift (Deff); d) from said shift point (P0f), a so-called adaptive aiming point (P1f) is calculated; and e) this adaptive aiming point (P1f) is transmitted to landing aid means of the aircraft.
An interdental device comprising: an interdental cleaning element comprising a spinal member extending along an elongate axis; and a flexible neck extending along the elongate axis and into which an end of the spinal member is received, wherein the flexible neck comprises a plurality of hinges, the plurality of hinges comprising: a first hinge configured to enable bending of the flexible neck in a first direction perpendicular to the elongate axis; and a second hinge axially displaced from the first hinge and configured to enable bending of the flexible neck in a second direction perpendicular to the elongate axis; wherein the spinal member extends into the flexible neck to an extent such that it extends beyond at least half of the plurality of hinges. an interdental cleaning element comprising a spinal member extending along an elongate axis; and a flexible neck extending along the elongate axis and into which an end of the spinal member is received, wherein the flexible neck comprises a plurality of hinges, the plurality of hinges comprising: a first hinge configured to enable bending of the flexible neck in a first direction perpendicular to the elongate axis; and a second hinge axially displaced from the first hinge and configured to enable bending of the flexible neck in a second direction perpendicular to the elongate axis; wherein the spinal member extends into the flexible neck to an extent such that it extends beyond at least half of the plurality of hinges. a first hinge configured to enable bending of the flexible neck in a first direction perpendicular to the elongate axis; and a second hinge axially displaced from the first hinge and configured to enable bending of the flexible neck in a second direction perpendicular to the elongate axis; wherein the spinal member extends into the flexible neck to an extent such that it extends beyond at least half of the plurality of hinges.
A method for temporarily switching an uplink transmission mode in a single user multiple input communication characterized by: acquiring, by a user terminal in the single user multiple input communication, control information from a network element indicating that an uplink transmission mode is to be switched for a predetermined period between an uplink transmission mode wherein a demodulation reference signal is precoded and another uplink transmission mode wherein a demodulation reference signal is non-precoded, wherein each of the uplink transmission modes further determines an uplink transmission method, wherein the uplink transmission method denotes a way in which user data together with control data is transmitted from the user terminal to the network element, wherein the control information includes which uplink transmission mode is to be switched on; and applying a dynamic uplink transmission mode switch by switching the uplink transmission mode dynamically according to the control information. acquiring, by a user terminal in the single user multiple input communication, control information from a network element indicating that an uplink transmission mode is to be switched for a predetermined period between an uplink transmission mode wherein a demodulation reference signal is precoded and another uplink transmission mode wherein a demodulation reference signal is non-precoded, wherein each of the uplink transmission modes further determines an uplink transmission method, wherein the uplink transmission method denotes a way in which user data together with control data is transmitted from the user terminal to the network element, wherein the control information includes which uplink transmission mode is to be switched on; and applying a dynamic uplink transmission mode switch by switching the uplink transmission mode dynamically according to the control information.
A navigation satellite system, NSS, reference station for providing information to one or more NSS rover receiver(s), the NSS reference station comprising: a processing unit configured to determine one or more first range intervals representing first ambiguity windows based on estimated atmospheric effects, and determine one or more second range intervals representing second ambiguity windows smaller than each of the first ambiguity windows based on uncertainties of range measurements within a predetermined previous period; and a transmission unit configured to transmit, to the NSS rover receiver(s), first messages each comprising a range measurement modulo a first ambiguity window, and transmit between transmission of two first messages, to the NSS rover receiver(s), a plurality of second messages, each second message comprising a range measurement modulo one of the second ambiguity windows. a processing unit configured to determine one or more first range intervals representing first ambiguity windows based on estimated atmospheric effects, and determine one or more second range intervals representing second ambiguity windows smaller than each of the first ambiguity windows based on uncertainties of range measurements within a predetermined previous period; and determine one or more first range intervals representing first ambiguity windows based on estimated atmospheric effects, and determine one or more second range intervals representing second ambiguity windows smaller than each of the first ambiguity windows based on uncertainties of range measurements within a predetermined previous period; and a transmission unit configured to transmit, to the NSS rover receiver(s), first messages each comprising a range measurement modulo a first ambiguity window, and transmit between transmission of two first messages, to the NSS rover receiver(s), a plurality of second messages, each second message comprising a range measurement modulo one of the second ambiguity windows. transmit, to the NSS rover receiver(s), first messages each comprising a range measurement modulo a first ambiguity window, and transmit between transmission of two first messages, to the NSS rover receiver(s), a plurality of second messages, each second message comprising a range measurement modulo one of the second ambiguity windows.
A microcontroller device comprising: a plurality of external pins (190, 290; 420); a first microcontroller comprising a first central processing unit, CPU,, a first system bus coupled with the first CPU, first memory (150, 140) coupled with the first system bus, and a first plurality of peripheral devices (130a..n) coupled with the first system bus, a second microcontroller comprising a second central processing unit, a second system bus coupled with the second CPU, second memory (240, 250) coupled with the second system bus, and a second plurality of peripheral devices (230a..n) coupled with the second system bus, wherein the first and second microcontroller are separate from each other and communicate only via a dedicated interface (320, 330), wherein the dedicated interface comprises a bidirectional mailbox interface configured to transfer a command or short data to the respective other microcontroller, a unidirectional master-slave interface and a unidirectional slave-master interface, wherein each unidirectional interface (320; 330) comprises FIFO memory that is configured to perform a larger data transfer between the microcontrollers without a size limitation of the bidirectional mailbox interface, wherein when a data or command has been written into the bidirectional mailbox interface by one of the microcontrollers, a respective interrupt is generated within the respective other microcontroller. a plurality of external pins (190, 290; 420); a first microcontroller comprising a first central processing unit, CPU,, a first system bus coupled with the first CPU, first memory (150, 140) coupled with the first system bus, and a first plurality of peripheral devices (130a..n) coupled with the first system bus, a second microcontroller comprising a second central processing unit, a second system bus coupled with the second CPU, second memory (240, 250) coupled with the second system bus, and a second plurality of peripheral devices (230a..n) coupled with the second system bus, wherein the first and second microcontroller are separate from each other and communicate only via a dedicated interface (320, 330), wherein the dedicated interface comprises a bidirectional mailbox interface configured to transfer a command or short data to the respective other microcontroller, a unidirectional master-slave interface and a unidirectional slave-master interface, wherein each unidirectional interface (320; 330) comprises FIFO memory that is configured to perform a larger data transfer between the microcontrollers without a size limitation of the bidirectional mailbox interface, wherein when a data or command has been written into the bidirectional mailbox interface by one of the microcontrollers, a respective interrupt is generated within the respective other microcontroller.
An arrangement for the galvanically isolated control with a triggered spark gap and adjustment of the response and residual voltage of the spark gap used, which arrangement has two main electrodes (1; 2) and at least one trigger electrode, furthermore with a transformer for the galvanic isolation, wherein the spark gap is connected with its main electrodes (1; 2) to an electronic component to be protected from overvoltage events, wherein furthermore a bypass circuit connected to the main electrodes (1; 2) of the spark gap is provided which is formed as a series circuit of passive or active electronic components and a primary side (4.1) of the transformer, a secondary side (4.2) of the transformer leads to a control input of a switch which is further arranged between one of the main electrodes of the spark gap and the trigger electrode, characterized in that the switch is formed as a semiconductor switch (5; 6), and the secondary side (4.2) of the transformer is connected to means for galvanically isolated external triggering.
A structural body, comprising: an adherend; and a shaping pattern to change a shape of the adherend; wherein the shaping pattern is formed with a filament comprising: a linear core; and a covering layer covering the core; wherein: the covering layer of the filament is welded to the adherend; the core is formed with a shape memory material; the covering layer is formed with a material different from the material of the core; and the material of the covering layer is a material which is more easily welded to the adherend than to the material of the core. an adherend; and a shaping pattern to change a shape of the adherend; wherein the shaping pattern is formed with a filament comprising: a linear core; and a covering layer covering the core; wherein: the covering layer of the filament is welded to the adherend; the core is formed with a shape memory material; the covering layer is formed with a material different from the material of the core; and the material of the covering layer is a material which is more easily welded to the adherend than to the material of the core. a linear core; and a covering layer covering the core; wherein: the covering layer of the filament is welded to the adherend; the core is formed with a shape memory material; the covering layer is formed with a material different from the material of the core; and the material of the covering layer is a material which is more easily welded to the adherend than to the material of the core. the covering layer of the filament is welded to the adherend; the core is formed with a shape memory material; the covering layer is formed with a material different from the material of the core; and the material of the covering layer is a material which is more easily welded to the adherend than to the material of the core.
A brake fluid pressure retainer device for use in a vehicle incorporating a fluid pressure braking device, the brake fluid pressure retainer device comprising: an electromagnetic open-close valve disposed in a brake fluid passage between a brake pedal and a braking device provided for wheels; and a movable shutoff valve disposed in parallel with the electromagnetic open-close valve disposed in the brake fluid passage, wherein the movable shutoff valve includes: a movable valve body movable in a flowing direction of a brake fluid, the movable valve body having a rear end part and a front end part which are placed in such a way that the movable valve body extends from the rear end part towards the front end part in correspondence to a flowing direction of a brake fluid inside the movable shutoff valve when the brake fluid flows from the braking device to the brake pedal; a valve seat configured to receive the front end part of the movable valve body to shut off the brake fluid; and a spring configured to apply force to the movable valve body in a direction in which the movable valve body moves away from the valve seat. an electromagnetic open-close valve disposed in a brake fluid passage between a brake pedal and a braking device provided for wheels; and a movable shutoff valve disposed in parallel with the electromagnetic open-close valve disposed in the brake fluid passage, a movable valve body movable in a flowing direction of a brake fluid, the movable valve body having a rear end part and a front end part which are placed in such a way that the movable valve body extends from the rear end part towards the front end part in correspondence to a flowing direction of a brake fluid inside the movable shutoff valve when the brake fluid flows from the braking device to the brake pedal; a valve seat configured to receive the front end part of the movable valve body to shut off the brake fluid; and a spring configured to apply force to the movable valve body in a direction in which the movable valve body moves away from the valve seat.
A non-transitory computer-readable storage medium storing computer-executable instructions which, when executed on a modular electro surgical generator platform, carries out the steps: delivering first energy to a first target tissue via a first generator and electrodes, the first energy represented as a first waveform having a first phase; delivering second energy to a second target tissue via a second generator and electrodes, the second energy represented as a second waveform having a second phase; applying the first energy in a first energy mode in a predetermined time period; applying the second energy in a second energy mode different to the first energy mode in the predetermined time period; characterised by comparing the first phase of the first energy waveform with the second phase of the second energy waveform in one or more of a plurality of sub-periods; and adjusting a relative phase between the first and second energy waveforms based on the comparison step to offset or counteract constructive interference. delivering first energy to a first target tissue via a first generator and electrodes, the first energy represented as a first waveform having a first phase; delivering second energy to a second target tissue via a second generator and electrodes, the second energy represented as a second waveform having a second phase; applying the first energy in a first energy mode in a predetermined time period; applying the second energy in a second energy mode different to the first energy mode in the predetermined time period; characterised by comparing the first phase of the first energy waveform with the second phase of the second energy waveform in one or more of a plurality of sub-periods; and adjusting a relative phase between the first and second energy waveforms based on the comparison step to offset or counteract constructive interference.
A numerically controlled machine tool including - a machine bed capable of being installed on a flat ground surface, - a cabin supported by the machine bed, and - a form element covering a lower section of the machine bed at least between the flat ground surface and a cabin wall of the cabin, - wherein the form element is fixed to the machine tool such that a cavity is formed between the machine bed and the form element, characterized in that a rubber lip is attached along a lower edge of the form element, which is suitable to seal a gap between the lower edge of the form element and the flat ground surface. - a machine bed capable of being installed on a flat ground surface, - a cabin supported by the machine bed, and - a form element covering a lower section of the machine bed at least between the flat ground surface and a cabin wall of the cabin, - wherein the form element is fixed to the machine tool such that a cavity is formed between the machine bed and the form element,