mhurhangee/patent-ind-claim-en huggingface dataset:
An exhaust gas purification system of a gasoline-fueled engine , the exhaust gas purification system comprising: a stainless steel support made of stainless steel; a first layer containing ceria and at least one type of noble metal selected from the group consisting of Pt, Pd, Ir, Ru, and Os; and a second layer containing at least one type of noble metal selected from the group consisting of Rh, Ir, Ru, Pt, Pd, Au, Ag, and Os, the second layer having a ceria content lower than a ceria content in the first layer or having a ceria content of 0 wt%, the first layer being provided between the second layer and the stainless steel support so as to be in contact with the second layer and the stainless steel support , the second layer being provided on the first layer , wherein of the first layer and the second layer , at least the first layer contains a noble metal and a composite in which alumina and a ceria-zirconia solid solution doped with a rare earth element are combined, wherein the composite has an alumina portion and a ceria-zirconia portion whose average primary particle diameter is smaller than the average primary particle diameter of the alumina portion, and wherein the composite has an average secondary particle diameter of 6 μm or more and less than 10 μm. a stainless steel support made of stainless steel; a first layer containing ceria and at least one type of noble metal selected from the group consisting of Pt, Pd, Ir, Ru, and Os; and a second layer containing at least one type of noble metal selected from the group consisting of Rh, Ir, Ru, Pt, Pd, Au, Ag, and Os, the second layer having a ceria content lower than a ceria content in the first layer or having a ceria content of 0 wt%, the first layer being provided between the second layer and the stainless steel support so as to be in contact with the second layer and the stainless steel support , the second layer being provided on the first layer , wherein of the first layer and the second layer , at least the first layer contains a noble metal and a composite in which alumina and a ceria-zirconia solid solution doped with a rare earth element are combined, wherein the composite has an alumina portion and a ceria-zirconia portion whose average primary particle diameter is smaller than the average primary particle diameter of the alumina portion, and wherein the composite has an average secondary particle diameter of 6 μm or more and less than 10 μm.
Method for selecting, for a motor vehicle traveling on a roundabout , a traffic lane of said roundabout that comprises a number (L) of traffic lanes , the method comprising a step of: - detecting the traffic lanes of the roundabout and other vehicles driving on said traffic lanes , the method being characterized in that it also comprises steps of: - determining, for each traffic lane under consideration from among at least some of the detected traffic lanes , a first item of data (p i ) relating to the occupancy of the traffic lane under consideration (i) by the other vehicles , and a second item of data (R j->i ) relating to the number of traffic lanes to be crossed in the event of changing traffic lane from a current traffic lane (j) to the traffic lane under consideration (i), - calculating the value of a cost function (J j->i ) for each traffic lane under consideration (i), on the basis of the first item of data (p i ) and of the second item of data (R j->i ), and - selecting one of the traffic lanes under consideration on the basis of each calculated value of the cost function (J j->i ). - detecting the traffic lanes of the roundabout and other vehicles driving on said traffic lanes , - determining, for each traffic lane under consideration from among at least some of the detected traffic lanes , a first item of data (p i ) relating to the occupancy of the traffic lane under consideration (i) by the other vehicles , and a second item of data (R j->i ) relating to the number of traffic lanes to be crossed in the event of changing traffic lane from a current traffic lane (j) to the traffic lane under consideration (i), - calculating the value of a cost function (J j->i ) for each traffic lane under consideration (i), on the basis of the first item of data (p i ) and of the second item of data (R j->i ), and - selecting one of the traffic lanes under consideration on the basis of each calculated value of the cost function (J j->i ).
A photomask unit comprising a pellicle membrane , a pellicle fram having a frame-like shape onto one surface of which a region of the pellicle membrane in the vicinity of side portions thereof is fixed, a photomask , and a stage onto one surface of which the photomask and the pellicle frame are fixed, wherein the pellicle frame is fixed onto the stage at a region outside of a region of the stage onto which the photomask is fixed and the pellicle membrane through which exposure light transmits is provided to cover an entire region of one of the openings formed by the pellicle frame.
Vibratory conveyer, comprising a vibrating rail , on which goods can be conveyed in the direction of a first position on the vibrating rail by a vibration of the vibrating rail , and at least one excitation element for exciting the vibration, wherein the excitation element is an ultrasonic transducer coupled to the vibrating rail at the first position, by which the vibrating rail can be excited to vibrate at the first position as a function of a control signal provided by a control device , a damping element, characterized in that the damping element is formed as a lateral boundary extending parallel to a conveying direction of the vibrating rail , which bounds a conveying surface of the vibrating rail , at least on one side, wherein the boundary is formed as a separate component which is fixed to the vibrating rail at at least two points and/or is in rubbing contact with the vibrating rail , so that the amplitude of the vibration decreases along the vibrating rail with increasing distance from the first position .
Household refrigeration appliance with an outer housing , in which an inner container of the household refrigeration appliance is arranged, and with a receiving space for foodstuffs, which is limited by walls of the inner container , and with at least one separate heat-conducting element arranged outside the receiving space , with which heat from a heat source separate from the heat-conducting element can be conducted to a condensation-critical point of the refrigeration appliance , wherein the heat-conducting element is arranged on a front flange of the inner container and extends from the front flange to the condensation-critical point , wherein thermal insulation foam is introduced in an intermediate space between the outer housing and the inner container and the heat-conducting element is embedded in foam in this intermediate space , characterised in that the heat-conducting element is embodied in a brace-like manner, so that a clamping self-retaining effect is achieved at the front flange and the condensation-critical point , at least in part.
A die-cast aluminum alloy, comprising the following components in mass percentages: magnesium: 0.1%-7%, zinc: 12%-35%, manganese: 0.2%-0.8%, iron: 0.1%-0.7%, titanium and/or zirconium: 0.07%-0.2%, optionally silicon: 0%-2.3% and/or copper: 0%-2.6%, inevitable impurities ≤ 0.3%, and aluminum. magnesium: 0.1%-7%, zinc: 12%-35%, manganese: 0.2%-0.8%, iron: 0.1%-0.7%, titanium and/or zirconium: 0.07%-0.2%, optionally silicon: 0%-2.3% and/or copper: 0%-2.6%, inevitable impurities ≤ 0.3%, and aluminum.
A method of transferring materials in space, the method comprising: launching a spacecraft comprising a storage container ; positioning the spacecraft in a first orbit, transferring the spacecraft to a second orbit; docking the spacecraft with a satellite in the second orbit; transferring material between the storage container and the satellite ; and undocking the spacecraft from the satellite ; characterised in that transferring material to the satellite comprises deploying a flexible container on the satellite to receive the material; and wherein deploying the flexible container comprises extending the flexible container away from the satellite . launching a spacecraft comprising a storage container ; positioning the spacecraft in a first orbit, transferring the spacecraft to a second orbit; docking the spacecraft with a satellite in the second orbit; transferring material between the storage container and the satellite ; and undocking the spacecraft from the satellite ; characterised in that transferring material to the satellite comprises deploying a flexible container on the satellite to receive the material; and wherein deploying the flexible container comprises extending the flexible container away from the satellite .
A catering trolley retrieval device for a galley compartment for stowing multiple trolleys , the device comprising a cassette which is rectangular and extending lengthwise from a front end to a back end , and arranged to be mounted to the compartment above where the trolleys are to be stowed so as to be slidable lengthwise in the direction of the stowage of the trolleys , the cassette further comprising a downwardly-extending claw mounted to the back end of the cassette and extending perpendicular to a plane of the cassette , and arranged such that, when the cassette is slid out of the compartment , the claw will engage a rear trolley stowed within the compartment to move it forward, the catering trolley retrieval device further comprises a retention latch mounted on the cassette at a first lengthwise position from the back end of the cassette , the retention latch movably mounted on the cassette , and arranged to extend downward so as to engage the rear trolley .
Tin-nickel layer having an NiSn phase, wherein the tin-nickel layer has a hardness of at least HV 750 (Vickers hardness) and a layer thickness, determined by X-ray fluorescence analysis in accordance with DIN EN ISO 3497, of 5 to 250 μm.
Reaction chamber comprising a device for distributing a light phase in a heavy phase inside said reaction chamber containing said heavy phase in the fluidized state, said device comprising a pipe for conveying the light phase entering the reaction chamber in its lower part, said pipe being cylindrical and substantially centred along the axis of symmetry of the reaction chamber , and being open in its upper part via first and second rectangular openings pierced in the lateral wall of said pipe , the second openings being extended by branches perpendicular to the axis of symmetry of the reaction chamber , and the pipe being surmounted at its upper part by a convex head which has notches uniformly distributed all along its lower edge, and allows the passage of the branches which protrude beyond the circumference of said head .
A semiconductor light emitting diode comprising: a sapphire substrate having a plurality of sapphire protrusions provided directly on a surface thereof; and semiconductor layers made of material different from that of said substrate and formed on the surface of said substrate , wherein a side face of each protrusion has an apex and includes, below said apex, a lower part and, above said apex, an upper part having different inclination angles (θ 1 , θ 2 ) between the inner side surface of the side face and a respective horizontal plane; wherein the plurality of protrusions have a circular shape in a plan view configuration. a sapphire substrate having a plurality of sapphire protrusions provided directly on a surface thereof; and semiconductor layers made of material different from that of said substrate and formed on the surface of said substrate , wherein a side face of each protrusion has an apex and includes, below said apex, a lower part and, above said apex, an upper part having different inclination angles (θ 1 , θ 2 ) between the inner side surface of the side face and a respective horizontal plane; wherein the plurality of protrusions have a circular shape in a plan view configuration.
An axial flow blower , comprising: a propeller fan ; and a driving unit configured to rotate the propeller fan , the propeller fan comprising: a hub ; and a plurality of blades supported by the hub , wherein a pressure surface of each of the blades comprises a protruding portion curved so as to swell to a suction side, wherein a height (H) of the protruding portion of the each of the blades on a trailing edge side is larger than a height of the protruding portion on a leading edge side, and the axial flow blower being characterized in that : a radial position of an apex of the protruding portion on the trailing edge side is located on a radially inner side with respect to a radial position of the apex of the protruding portion on the leading edge side, and a position of an inner end of the protruding portion on the,trailing edge side is located on the radially inner side with respect to a position of the inner end of the protruding portion on the leading edge side. a propeller fan ; and a driving unit configured to rotate the propeller fan , the propeller fan comprising: a hub ; and a plurality of blades supported by the hub , a hub ; and a plurality of blades supported by the hub , wherein a pressure surface of each of the blades comprises a protruding portion curved so as to swell to a suction side, wherein a height (H) of the protruding portion of the each of the blades on a trailing edge side is larger than a height of the protruding portion on a leading edge side, and the axial flow blower being characterized in that : a radial position of an apex of the protruding portion on the trailing edge side is located on a radially inner side with respect to a radial position of the apex of the protruding portion on the leading edge side, and a position of an inner end of the protruding portion on the,trailing edge side is located on the radially inner side with respect to a position of the inner end of the protruding portion on the leading edge side. a radial position of an apex of the protruding portion on the trailing edge side is located on a radially inner side with respect to a radial position of the apex of the protruding portion on the leading edge side, and a position of an inner end of the protruding portion on the,trailing edge side is located on the radially inner side with respect to a position of the inner end of the protruding portion on the leading edge side.
Anti-sinking and anti-fire safety system for boats, said system is constituted by a plurality of inflatable devices , of substantially rectangular flattened form, when deflated, whose four perimeter edges are connectable to a portion of two longitudinal members , preferably consecutive, and to a portion of two crosspieces , preferably consecutive, of any one hull ; each inflatable device is initially installed in a first deflated configuration, it occupies the least possible space, and said inflatable devices being susceptible of assuming a second inflated configuration, with a volume considerably greater than said first deflated configuration; each of said inflatable devices being connected to at least one dispenser , adapted to fill the corresponding inflatable device with a predetermined quantity of non-inflammable foam adapted to be expanded within said inflatable device until it is allowed to assume the maximum desired preestablished volume in said second inflated configuration; said non-inflammable foam being constituted by any one polymer that can be found on the market, preferably expanded polyurethane, adapted to quickly increase volume once outside said dispenser , and adapted to maintain over time the characteristics of fire resistance and buoyancy; each of said dispensers being connected to at least one activation means adapted to activate the corresponding dispenser by means of remote control of the user, sent by means of a common control system ; said safety system being characterized in that it is constituted by a plurality of dispensers , connected to the corresponding activation means , adapted to expand, by means of remote control of the user sent by means of said control system , a predetermined quantity of non-inflammable foam (106.a) within the lower internal technical space and, especially, between the free spaces present between the inflatable devices that are already inflated, and in any other internal space of the ship considered to be a fire risk space ; said non-inflammable foam (106.a) being adapted to sublimate after a known time interval from its expansion; said control system being constituted by a common processor adapted to allow the user, by means of a communication interface , to actuate a part or all of said activation means in case of opening of a leak on the hull or in case of risk of fire on board.
Method for controlling a percussion apparatus for an extended life of operation, the method comprising: operating the percussion apparatus at a first stroke length and at a first frequency, wherein the first stroke length and the first frequency generate a low stress level to reduce fatigue in the percussion apparatus ; receiving a user selection for a second stroke length and a second frequency, wherein the second stroke length is longer than the first stroke length and the second frequency is lower than the first frequency such that a high stress level increases fatigue in the percussion apparatus when the percussion apparatus has yet engaged with an operation target ; providing a feed forward pressure to a sliding selector controlling a piston hammer stroke length and frequency according to the user selection and in response to an actuation input, wherein the actuation input is provided in response to an operation of the percussion apparatus and wherein in response to the actuation input, the feed forward pressure increases and becomes greater than a threshold value to change the mode of operation when the percussion apparatus presses against a target surface; in response to the feed forward pressure lower than the threshold level, maintaining the first stroke length and the first frequency; and in response to the feed forward pressure higher than the threshold level, increasing the first stroke length to the second stroke length and reducing the first frequency to the second frequency. operating the percussion apparatus at a first stroke length and at a first frequency, wherein the first stroke length and the first frequency generate a low stress level to reduce fatigue in the percussion apparatus ; receiving a user selection for a second stroke length and a second frequency, wherein the second stroke length is longer than the first stroke length and the second frequency is lower than the first frequency such that a high stress level increases fatigue in the percussion apparatus when the percussion apparatus has yet engaged with an operation target ; providing a feed forward pressure to a sliding selector controlling a piston hammer stroke length and frequency according to the user selection and in response to an actuation input, wherein the actuation input is provided in response to an operation of the percussion apparatus and wherein in response to the actuation input, the feed forward pressure increases and becomes greater than a threshold value to change the mode of operation when the percussion apparatus presses against a target surface; in response to the feed forward pressure lower than the threshold level, maintaining the first stroke length and the first frequency; and in response to the feed forward pressure higher than the threshold level, increasing the first stroke length to the second stroke length and reducing the first frequency to the second frequency.
A vehicle comprising a lighting arrangement , the lighting arrangement comprising a left-hand lighting assembly and a right-hand lighting assembly , and a controller for controlling the activation of the light sources (S 11 , ..., S 26 ) of the lighting assemblies so as to adjust the swivel angles (σ 1 , σ 2 ) of the front beams (B L , B R ) of each one of the lighting assemblies, wherein each lighting assembly comprises a projection lens and a light source array of light sources (S 11 , ..., S 26 ) distributed symmetrically about an optical axis (X 1 , X 2 ) of that lighting assembly , wherein, in each lighting assembly , the light sources (S 11 , ..., S 26 ) are individually controlled to adjust a swivel angle (σ1, σ2) of a front beam (B L , B R ) generated by that lighting assembly to illuminate the area in front of the vehicle when the vehicle is directed into a turn, characterized in that , the optical axis (X 1 ) of the left-hand lighting assembly is arranged at a positive fixed angle (Φ 1 ) to the longitudinal axis (L) of the vehicle so as to point somewhat to the left, and the optical axis (X 2 ) of the right-hand lighting assembly is arranged at a negative fixed angle (Φ 2 ) to the longitudinal axis (L) of the vehicle so as to point somewhat to the right.
A device for analyzing and managing data generated by a sensor-equipped braking system for vehicles, comprising a support element for a block of friction material and a sensor means interposed between the block of friction material and the support element , said sensor means comprising at least a temperature sensor, at least one piezoceramic pressure sensor and at least one piezoceramic shear force sensor provided between said block of friction material and said support element , further comprising at least a central control unit configured to receive in real time from said sensor means at least basic data related to the pressure of the activated braking system, the temperature of the activated braking system, the braking torque and the residual torque when the braking system is deactivated and the wear on the braking system during and after the activation thereof, said at least a central control unit being connected to a GPS and to an accelerometer so as to receive first auxiliary data on the position and kinematic state of said vehicle, said basic data and said first auxiliary data being analyzed simultaneously with all the onboard data on the state of the vehicle acquired directly from an onboard system of the vehicle, and furhter comprising at least a recording unit connected to said central control unit for the simultaneous real-time recording of said basic data, said first auxiliary data, said onboard data analyzed by said central control unit , said recording unit being connected on one side to a black box for storing all said data and on the other side to a long-range communication unit .
A lipid nanoparticle comprising an ionizable lipid in which a 6-membered heterocyclic amine and an alkyl-epoxide are bonded; a phospholipid; cholesterol; and a ceramide-PEG (polyethyleneglycol) conjugate, wherein the 6-membered heterocyclic amine is wherein the ceramide-PEG conjugate comprised in 0.5 to 5 mol%. wherein the 6-membered heterocyclic amine is wherein the ceramide-PEG conjugate comprised in 0.5 to 5 mol%.