mhurhangee/ep-ind-claims huggingface dataset:
A method for assessing aircraft interference path loss in an aircraft, the method comprising: transmitting a plurality of radio frequency signals that are stepped through a plurality of frequencies in a frequency range from a plurality of locations within an interior of the aircraft; measuring received radio frequency signals generated at a receive antenna in response to transmitting the plurality of radio frequency signals to form a plurality of measurements; performing an autocorrelation check on the plurality of measurements to determine whether a desired sample independence is present; responsive to the desired sample independence being absent, sifting the plurality of measurements or adjusting a step size to step the plurality of radio frequency signals to obtain the desired sample independence; generating an average of averages curve from the plurality of measurements; identifying a peak to average ratio; identifying field uniformity; characterised in that: the step of identifying the peak to average ratio comprises calculating a difference between the average of averages curve and an average of peaks curve; and characterised by: determining a standard error for the average of averages curve; and predicting an upper bound for the aircraft interference path loss in the aircraft using the average of averages curve, the peak to average ratio, the field uniformity, and the standard error. transmitting a plurality of radio frequency signals that are stepped through a plurality of frequencies in a frequency range from a plurality of locations within an interior of the aircraft; measuring received radio frequency signals generated at a receive antenna in response to transmitting the plurality of radio frequency signals to form a plurality of measurements; performing an autocorrelation check on the plurality of measurements to determine whether a desired sample independence is present; responsive to the desired sample independence being absent, sifting the plurality of measurements or adjusting a step size to step the plurality of radio frequency signals to obtain the desired sample independence; generating an average of averages curve from the plurality of measurements; identifying a peak to average ratio; identifying field uniformity; the step of identifying the peak to average ratio comprises calculating a difference between the average of averages curve and an average of peaks curve; and characterised by: determining a standard error for the average of averages curve; and predicting an upper bound for the aircraft interference path loss in the aircraft using the average of averages curve, the peak to average ratio, the field uniformity, and the standard error. determining a standard error for the average of averages curve; and predicting an upper bound for the aircraft interference path loss in the aircraft using the average of averages curve, the peak to average ratio, the field uniformity, and the standard error.
A thermoplastic polyester-based flame-retardant resin composition comprising 100 parts by weight of a thermoplastic polyester resin, 3 to 50 parts by weight of a bromine-containing aromatic compound, 2 to 30 parts by weight of an antimony oxide compound, 0.1 to 3 parts by weight of polytetrafluoroethylene having fibril-forming abilities, and 0.7 to 8 parts by weight of an lamellar filler, wherein the thermoplastic polyester resin is an aromatic thermoplastic polyester resin and wherein the lamellar filler is an inorganic lamellar filler.
Method for detaching elastomer particles which adhere to microvalves disposed on the inner surface of a vehicle tyre curing mould, characterized in that: a. the presence of a microvalve disposed on said inner surface of the mould is detected, and characterized in that b. said microvalve is made to vibrate with a constant amplitude of between approximately 0.05 and 0.2 mm and a frequency of between 20 000 and 30 000 Hz during the detachment of the particles from said microvalve. a. the presence of a microvalve disposed on said inner surface of the mould is detected, and characterized in that b. said microvalve is made to vibrate with a constant amplitude of between approximately 0.05 and 0.2 mm and a frequency of between 20 000 and 30 000 Hz during the detachment of the particles from said microvalve.
A method for making an antimicrobial adhesive silicone for an adhesive dressing, the method comprising mixing together; a liquid containing silicone with a silicone dispersion of polyhexamethylene biguanide hydrochloride (PHMB) and EDTA that are not soluble in said liquid and remain as particulates, and optional humectant; and allowing the mixture to cure under suitable temperature and pressure.
A process for preparing a functionalized olefin multiblock interpolymer, said process comprising: A) grafting onto the backbone of an olefin multiblock interpolymer at least one compound comprising at least one "amine-reactive" group to form a grafted olefin multiblock interpolymer; B) reacting a compound selected from a primary-secondary diamine and an alkanolamine with the grafted olefin multiblock interpolymer; and wherein step B) takes place subsequent to step A), without the isolation of the grafted olefin multiblock interpolymer, and wherein both steps A) and B) take place in a melt reaction. A) grafting onto the backbone of an olefin multiblock interpolymer at least one compound comprising at least one "amine-reactive" group to form a grafted olefin multiblock interpolymer; B) reacting a compound selected from a primary-secondary diamine and an alkanolamine with the grafted olefin multiblock interpolymer; and wherein step B) takes place subsequent to step A), without the isolation of the grafted olefin multiblock interpolymer, and wherein both steps A) and B) take place in a melt reaction.
Massdecoupling device for a motor vehicle, having: a mass-receiving element and a mass object accommodated therein, wherein the mass-receiving element and the mass object are formed point-symmetrically and mounted with respect to a body of the motor vehicle, at least one guide means which mounts the mass-receiving element and the mass object accommodated therein such that they can move along a vehicle longitudinal axis; decoupling means which are designed to decouple the mass-receiving element and the mass object accommodated therein from the body of the motor vehicle; first energy-absorbing means which are designed to transmit kinetic energy of a movement of the mass-receiving element and the mass object accommodated therein along the vehicle longitudinal axis from a first position to a second position in a predetermined time interval to the body of the motor vehicle; and second energy-absorbing means which are designed to convert the kinetic energy of the movement of the mass-receiving element and the mass object accommodated therein along the vehicle longitudinal axis at least partially into kinetic energy of a rotation of the mass-receiving element and of the mass object accommodated therein. a mass-receiving element and a mass object accommodated therein, wherein the mass-receiving element and the mass object are formed point-symmetrically and mounted with respect to a body of the motor vehicle, at least one guide means which mounts the mass-receiving element and the mass object accommodated therein such that they can move along a vehicle longitudinal axis; decoupling means which are designed to decouple the mass-receiving element and the mass object accommodated therein from the body of the motor vehicle; first energy-absorbing means which are designed to transmit kinetic energy of a movement of the mass-receiving element and the mass object accommodated therein along the vehicle longitudinal axis from a first position to a second position in a predetermined time interval to the body of the motor vehicle; and second energy-absorbing means which are designed to convert the kinetic energy of the movement of the mass-receiving element and the mass object accommodated therein along the vehicle longitudinal axis at least partially into kinetic energy of a rotation of the mass-receiving element and of the mass object accommodated therein.
A starter, comprising: a stator disposed inside a yoke; an armature, supported inside the stator, wherein an armature coil is wrapped around an armature core; a commutator connected to the armature and having a sliding surface in an outer peripheral portion; and a brush disposed opposing the commutator and having a sliding contact surface that comes into sliding contact with the sliding surface of the commutator, wherein the brush has a first member, and a second member with an electrical resistance value higher than that of the first member, the first member is disposed on an entrance side and the second member on an exit side with respect to a direction of rotation of the commutator, and the sliding contact surface of the brush has an inclined portion that is formed on the first member and a flat portion that is formed on the second member, the starter being characterized in that an origin of the inclination of the inclined portion with respect to the flat portion is disposed within a range of a width of the second member on the sliding contact surface, and in that the inclined portion inclines toward the entrance side with respect to the direction of rotation of the commutator so that the brush cannot come into sliding contact with the commutator with only the first member. a stator disposed inside a yoke; an armature, supported inside the stator, wherein an armature coil is wrapped around an armature core; a commutator connected to the armature and having a sliding surface in an outer peripheral portion; and a brush disposed opposing the commutator and having a sliding contact surface that comes into sliding contact with the sliding surface of the commutator, wherein the brush has a first member, and a second member with an electrical resistance value higher than that of the first member, the first member is disposed on an entrance side and the second member on an exit side with respect to a direction of rotation of the commutator, and the sliding contact surface of the brush has an inclined portion that is formed on the first member and a flat portion that is formed on the second member, the starter being characterized in that an origin of the inclination of the inclined portion with respect to the flat portion is disposed within a range of a width of the second member on the sliding contact surface, and in that the inclined portion inclines toward the entrance side with respect to the direction of rotation of the commutator so that the brush cannot come into sliding contact with the commutator with only the first member.
A compound helicopter comprising - a fuselage with an upper side and a lower side opposed to said upper side, - at least one engine disposed on the upper side of the fuselage, - a main rotor mounted to said upper side of said fuselage, said main rotor being driven by said at least one engine, - at least one pair of fixed wings mounted in an essentially horizontal plane on a left hand and a right hand side of the fuselage and - longitudinally oriented propulsion devices (12, 13) mounted to each of said fixed wings, said fixed wings encompassing each a drive shaft from said at least one engine, wherein the respective drive shafts drive the propulsion devices (12, 13), and wherein said propulsion devices (12, 13) are driven in operation only by means of power provided by the at least one engine, and wherein - each fixed wing comprises a lower main wing and an upper secondary wing, - said upper secondary wing is anhedral, - said upper secondary wing and said lower main wing are connected to each other within an interconnection region, - the propulsion devices (12, 13) are arranged at said interconnection region, - and said upper secondary wing houses the drive shaft from said at least one engine. - a fuselage with an upper side and a lower side opposed to said upper side, - at least one engine disposed on the upper side of the fuselage, - a main rotor mounted to said upper side of said fuselage, said main rotor being driven by said at least one engine, - at least one pair of fixed wings mounted in an essentially horizontal plane on a left hand and a right hand side of the fuselage and - longitudinally oriented propulsion devices (12, 13) mounted to each of said fixed wings, said fixed wings encompassing each a drive shaft from said at least one engine, wherein the respective drive shafts drive the propulsion devices (12, 13), and wherein said propulsion devices (12, 13) are driven in operation only by means of power provided by the at least one engine, - each fixed wing comprises a lower main wing and an upper secondary wing, - said upper secondary wing is anhedral, - said upper secondary wing and said lower main wing are connected to each other within an interconnection region, - the propulsion devices (12, 13) are arranged at said interconnection region, - and said upper secondary wing houses the drive shaft from said at least one engine.
A terminal comprising: a transmitting section configured to transmit uplink control information, UCI, by using an uplink control channel; and a control section configured to control a frequency resource for mapping the uplink control channel to use to transmit the UCI, by using a single table that defines hopping timings for each duration of the uplink control channel, wherein, in the single table, the duration of the uplink control channel may be associated with common hopping timing information, which shows a hopping timing that applies in common to a case an index of a starting symbol corresponds to the even number and a case the index of the starting symbol corresponds to the odd number and wherein a hopping timing for a specific duration defined in the single table is determined based on a ratio, which is 50%, of UCI and a demodulation reference signal mapped to a same frequency resource in the case an index of a starting symbol corresponds to the even number and in the case the index of the starting symbol corresponds to the odd number. a transmitting section configured to transmit uplink control information, UCI, by using an uplink control channel; and a control section configured to control a frequency resource for mapping the uplink control channel to use to transmit the UCI, by using a single table that defines hopping timings for each duration of the uplink control channel, wherein, in the single table, the duration of the uplink control channel may be associated with common hopping timing information, which shows a hopping timing that applies in common to a case an index of a starting symbol corresponds to the even number and a case the index of the starting symbol corresponds to the odd number and wherein a hopping timing for a specific duration defined in the single table is determined based on a ratio, which is 50%, of UCI and a demodulation reference signal mapped to a same frequency resource in the case an index of a starting symbol corresponds to the even number and in the case the index of the starting symbol corresponds to the odd number.
Method for processing a call between at least two terminals via a network, a videoconference session between said terminals being in progress, with network conditions being liable to degrade the quality of a videoconference call between said terminals, the method, which is implemented by at least one server, comprising the steps of: - when a first message, that the videoconference call quality has been degraded, is received from the server, the first message originating from at least one of said terminals and comprising network identifiers of said terminals, interrupting the videoconference call, and - using said identifiers of said terminals to transmit, to said terminals, a second message, for said terminals to be connected in the form of an audio call, the second message comprising an instruction to prevent a human-machine interface for warning of an incoming call from being activated. - when a first message, that the videoconference call quality has been degraded, is received from the server, the first message originating from at least one of said terminals and comprising network identifiers of said terminals, interrupting the videoconference call, and - using said identifiers of said terminals to transmit, to said terminals, a second message, for said terminals to be connected in the form of an audio call, the second message comprising an instruction to prevent a human-machine interface for warning of an incoming call from being activated.
An oligonucleotide set for detection of Swine Flu Virus H1 type in a sample, said set comprising the oligonucleotides as set forth in SEQ ID NO: 3 to SEQ ID NO: 8.
A building material plate comprising a non-flammable mineral base plate having two opposite main surfaces (3, 4), wherein at least one of the main surfaces (3, 4) is provided with a metal layer (5, 6) in at least some sections, which metal layer consists of aluminum or an aluminum alloy, characterized in that the metal layer (5, 6) comprises a thickness of at least 0.2 mm.
Method for determining a value of at least one geometrico-morphological parameter of a subject wearing an eyewear for precisely determining a vision correction equipment customized for this subject, said at least one geometrico-morphological parameter comprising either: - a parameter linked to both a head of the subject and said eyewear; or - a parameter linked only to the morphology of the subject; or - a parameter linked only to the geometry of the eyewear; said method being computer implemented, wherein the following steps are performed: a) obtaining at least one image of the head of the subject wearing said eyewear; b) identifying simultaneously, on said at least one image obtained in step a), a set of remarkable points of the image of the eyewear and a set of remarkable points of the image of the head of the subject, using an image processing algorithm determined based on a predetermined database comprising a plurality of reference images of heads wearing an eyewear, said image processing algorithm being based on machine learning, c) determining said at least one value of a geometrico-morphological parameter taking into account said sets of remarkable points (RPE, RPH) of the image of the eyewear and head of the subject identified in step b). - a parameter linked to both a head of the subject and said eyewear; or - a parameter linked only to the morphology of the subject; or - a parameter linked only to the geometry of the eyewear; said method being computer implemented, wherein the following steps are performed: a) obtaining at least one image of the head of the subject wearing said eyewear; b) identifying simultaneously, on said at least one image obtained in step a), a set of remarkable points of the image of the eyewear and a set of remarkable points of the image of the head of the subject, using an image processing algorithm determined based on a predetermined database comprising a plurality of reference images of heads wearing an eyewear, said image processing algorithm being based on machine learning, c) determining said at least one value of a geometrico-morphological parameter taking into account said sets of remarkable points (RPE, RPH) of the image of the eyewear and head of the subject identified in step b). a) obtaining at least one image of the head of the subject wearing said eyewear; b) identifying simultaneously, on said at least one image obtained in step a), a set of remarkable points of the image of the eyewear and a set of remarkable points of the image of the head of the subject, using an image processing algorithm determined based on a predetermined database comprising a plurality of reference images of heads wearing an eyewear, said image processing algorithm being based on machine learning, c) determining said at least one value of a geometrico-morphological parameter taking into account said sets of remarkable points (RPE, RPH) of the image of the eyewear and head of the subject identified in step b).
A configuration processing method for an antenna receiving mode, where the method comprises: when a user applies to a base station for establishing or adding radio links, determining, by a base station controller, an antenna receiving mode of the user according to resource allocation information of the user, wherein the resource allocation information of the user comprises at least one of the following information: service type of the user, priority information of the user, remaining available baseband processing resources, and the number of license channel elements, CEs, or the resource allocation information of the user comprises channel quality of the user and at least one of the following information: service type of the user, priority information of the user, remaining available baseband processing resources, and the number of license CEs; and performing, by the base station controller, user admission processing according to a CE consumption rule that is corresponding to the determined antenna receiving mode of the user. when a user applies to a base station for establishing or adding radio links, determining, by a base station controller, an antenna receiving mode of the user according to resource allocation information of the user, wherein the resource allocation information of the user comprises at least one of the following information: service type of the user, priority information of the user, remaining available baseband processing resources, and the number of license channel elements, CEs, or the resource allocation information of the user comprises channel quality of the user and at least one of the following information: service type of the user, priority information of the user, remaining available baseband processing resources, and the number of license CEs; and performing, by the base station controller, user admission processing according to a CE consumption rule that is corresponding to the determined antenna receiving mode of the user.
A method for preparing primed seed, comprising successively: - providing seed that is capable of germinating, - exposing said seed to a treatment atmosphere for an exposure time of at least 1 second, wherein the treatment atmosphere has a relative humidity of 60 % or more and a temperature of 50 °C to 100 °C, and wherein the exposure time has a duration of 30 minutes or less, and - cooling and optionally drying said seed. - providing seed that is capable of germinating, - exposing said seed to a treatment atmosphere for an exposure time of at least 1 second, wherein the treatment atmosphere has a relative humidity of 60 % or more and a temperature of 50 °C to 100 °C, and wherein the exposure time has a duration of 30 minutes or less, and - cooling and optionally drying said seed.