mhurhangee/patent-ind-claim-en huggingface dataset:
A curtain rod mounting bracket, comprising a base and a supporting rod mounted to the base , wherein a rod holding support is provided on the end of the supporting rod away from the base , wherein a mounting groove is formed in the rod holding support , wherein a curtain rod positioning clamp is detachably mounted in the mounting groove , wherein a curtain rod loading opening is formed in the curtain rod positioning clamp , wherein the opening size of the curtain rod loading opening is smaller than the internal size of the curtain rod loading opening ; wherein the base comprises a connecting base used for connecting with the supporting rod and a protecting cover sleeved on the supporting rod and covering the connecting base , wherein the connecting base is provided with a stud used for connecting with the supporting rod and with connecting holes distributed around the stud , wherein a screw hole used for forming screw connection with the stud is provided on the end of the supporting rod away from the rod holding support , characterized in that the connecting base comprises a fixing portion and a sliding portion in a slidable connection with the fixing portion , wherein the stud is positioned in the sliding portion , wherein a connector used for limiting the separation of the fixing portion and the sliding portion is provided between the fixing portion and the sliding portion , and wherein the fixing portion is provided with an X-direction adjusting assembly used for driving the sliding portion moving in the fixing portion along an X-direction and an Y-direction adjusting assembly used for driving the sliding portion moving in the fixing portion along an Y-direction.
Rotating drum for treating fibrous material , the axis of rotation of the drum being inclined by at most 30° relative to the horizontal, a fibrous material mixed with water being fed into the drum at a first end , the fibrous material being transported from the first to the second end within the drum by means of transport elements , wherein the drum is perforated, a fine fraction flows through the perforation and a coarse fraction is repelled by the latter, characterized in that the first end of the drum is closed and at least one retaining nozzle directs a water jet onto the fibrous material counter to the transport direction of the fibrous material .
A method for a string comprising a plurality of vehicles platooning by means of vehicle-to-vehicle (V2V) communication, comprising collecting (S1) from a plurality of sources values (OP1-OP3) of operational parameters related to the operation of a first of the vehicles, determining (S2) based on the operational parameter values (OP1-OP3) a plurality of values (AP1-AP3) of an acceleration parameter indicative of an acceleration of the first vehicle, where a second vehicle following behind the first vehicle is provided with a movement sensor for determining the distance to, velocity of and/or acceleration of a vehicle in front of the second vehicle, selecting (S3) from the acceleration parameter values (AP1-AP3) an extreme value (AP2) indicative of the lowest acceleration, i.e. the highest deceleration, of the first vehicle , and the second of the vehicles following behind the first vehicle determining, or receiving by means of the V2V communication, the extreme value (AP2), and initiating (S5) in dependence on the extreme value (AP2) a control of braking means for a braking action of the second vehicle , wherein the second vehicle , subsequently to the braking means control initiation, determining (S7) at least partly based on signals from the movement sensor whether to adjust the braking means control, wherein determining (S7) whether to adjust the braking means control comprises determining based on the signals from the movement sensor a further value (AP4) of the acceleration parameter indicative of the acceleration of a vehicle in front of the second vehicle , and comparing the further acceleration parameter value (AP4) with the extreme value (AP2), and adjusting the braking means control by controlling the braking means to abort the braking action if the further acceleration parameter value (AP4) is above the extreme value (AP2) by more than a tolerance amount (dAP).
A method for operating a machine component under stress, the method comprising: determining a probability of failure of the component as a function of N cycles of a cycling loading process, PoF(N); selecting a time-based acceptable risk limit for the component; selecting an operational profile for the component; converting the time-based acceptable risk limit to a cycle-based acceptable risk limit using the operational profile; comparing the cycle-based acceptable risk limit with the PoF(N) values; and operating the machine component responsive to results of the comparing step, characterized in that the step of determining comprises using a direct simulation probabilistic fracture mechanics method which defines a plurality of representations of the component based on a Monte Carlo Simulation, and the time-based acceptable risk limit comprises a first risk limit and a second risk limit, wherein the probability of failure PoF(N) equals the first risk limit when N = i and equals the second risk limit when N = j, and wherein when N = i a first action associated with the first risk limit is performed and when N = j a second action associated with the second risk limit is performed, wherein the first action in particular comprises performing an inspection of the component and the second action in particular comprises removing the component from service. determining a probability of failure of the component as a function of N cycles of a cycling loading process, PoF(N); selecting a time-based acceptable risk limit for the component; selecting an operational profile for the component; converting the time-based acceptable risk limit to a cycle-based acceptable risk limit using the operational profile; comparing the cycle-based acceptable risk limit with the PoF(N) values; and operating the machine component responsive to results of the comparing step, characterized in that the step of determining comprises using a direct simulation probabilistic fracture mechanics method which defines a plurality of representations of the component based on a Monte Carlo Simulation, and the time-based acceptable risk limit comprises a first risk limit and a second risk limit, wherein the probability of failure PoF(N) equals the first risk limit when N = i and equals the second risk limit when N = j, and wherein when N = i a first action associated with the first risk limit is performed and when N = j a second action associated with the second risk limit is performed, wherein the first action in particular comprises performing an inspection of the component and the second action in particular comprises removing the component from service.
A high-pressure fuel supply pump, comprising: a piston plunger reciprocating within a pressurizing chamber ; and an electromagnetically-driven intake valve mechanism provided at an inlet of the pressurizing chamber , wherein the electromagnetically-driven intake valve mechanism includes an anchor which pulls a plunger rod , a fixed core which attracts the anchor , and a bottomed cup-like yoke comprising a bottom part and an inner peripheral surface forming a cylindrical space ; wherein the fixed core has a cylindrical space formed inside and a bottom part; characterized in that the fixed core is rigidly fixed to the bottom part of the bottomed cup-like yoke by press-fitting, wherein a through hole is formed at the bottom part of the fixed core and wherein the fixed core is press-fitted in the inner peripheral surface) of the bottomed cup-like yoke . a piston plunger reciprocating within a pressurizing chamber ; and an electromagnetically-driven intake valve mechanism provided at an inlet of the pressurizing chamber , wherein the electromagnetically-driven intake valve mechanism includes an anchor which pulls a plunger rod , a fixed core which attracts the anchor , and a bottomed cup-like yoke comprising a bottom part and an inner peripheral surface forming a cylindrical space ; wherein the fixed core has a cylindrical space formed inside and a bottom part; characterized in that the fixed core is rigidly fixed to the bottom part of the bottomed cup-like yoke by press-fitting, wherein a through hole is formed at the bottom part of the fixed core and wherein the fixed core is press-fitted in the inner peripheral surface) of the bottomed cup-like yoke .
Applicator for applying an eyeliner to the eyelids, comprising an applicator member , the latter having, on its external surface, in side view, an indentation and a substantially flat main facet situated between the indentation and the distal end of the applicator member , the width ( l ) of the main facet , in front view, increasing with increasing distance from the indentation , at least along a major part of the length (D) of the main facet , wherein the applicator member extends along a longitudinal axis (X), the length of the main facet, measured in a direction parallel to the longitudinal axis (X) of the applicator member being between 5 mm and 15 mm, the thickness of the applicator member at the indentation being between 1 mm and 5 mm, the applicator member being made of a porous material.
A rotary press having a rotor, wherein the rotor comprises an upper and a lower punch guide and a die plate arranged between the upper and lower punch guides, furthermore having upper and lower press punches which interact with die bores in the die plate , wherein the rotary press comprises a plurality of stations, namely at least one filling station in which material to be compressed is filled into the die bores, at least one metering station in which the material filled into the die bores is metered, at least one pressing station in which the metered material filled into the die bores is compressed by the upper and lower press punches to form pellets, and at least one ejector station in which the compressed pellets are ejected, characterized in that driving means are provided, with which at least one of the stations can be automatically moved between its operating position and a resting position in which the production process of the rotary press for producing pellets is still possible with the stations that remain in each case in an operating position, but the at least one station located in the resting position has no effect on the production process.
Method for preparing esters of lactic and lactylatic acid, where the conversion of substrates is 100%, comprising: a) placement in pressure reactor polylactide (PLA) and alcohol (ROH) wherein the alcohol is selected from methyl, ethyl, n-propyl, isopropyl, n-butyl, isobutyl, sec-butyl, tert-butyl, n-pentyl, isopentyl, n-hexyl, 2-ethylhexyl, n-octyl, allyl, propargyl, benzyl alcohol or mixture of alcohols with ratio of reagents from 2 to 10 molar equivalents of alcohol for structural unit of polymer ROH/mer; b) optionally, introducing pre-catalyst to reaction mixture in situ wherein the catalyst is prepared in direct one-stage synthesis from organometallic compounds, metal halides, amides, hydrides, carboxylates, acetylacetonates, alcoholates, aryloxanes, metal oxides, metallic dusts, metallic chips, low melt metal alloys and catalytic compositions composed of mixtures of said precursors in the reaction with ROH in solvothermal conditions during the process; and wherein the catalyst is synthetized from organometallic compounds, hydroxides, metal alkoxides, salts of inorganic acids c) carrying out the alcoholysis reaction of polylactide in the presence of alcohol or mixture of alcohols, under autogenous pressure of reaction mixture components within a range from atmospheric pressure to 107 bar, in suitably selected temperature, wherein i. in non-catalyst reaction, the reaction temperature is 220-260°C, ii. while in catalyst reaction, the reaction temperature is 150-220°C, d) separating and purifying final product by filtration, evaporation and distillation. a) placement in pressure reactor polylactide (PLA) and alcohol (ROH) wherein the alcohol is selected from methyl, ethyl, n-propyl, isopropyl, n-butyl, isobutyl, sec-butyl, tert-butyl, n-pentyl, isopentyl, n-hexyl, 2-ethylhexyl, n-octyl, allyl, propargyl, benzyl alcohol or mixture of alcohols with ratio of reagents from 2 to 10 molar equivalents of alcohol for structural unit of polymer ROH/mer; b) optionally, introducing pre-catalyst to reaction mixture in situ wherein the catalyst is prepared in direct one-stage synthesis from organometallic compounds, metal halides, amides, hydrides, carboxylates, acetylacetonates, alcoholates, aryloxanes, metal oxides, metallic dusts, metallic chips, low melt metal alloys and catalytic compositions composed of mixtures of said precursors in the reaction with ROH in solvothermal conditions during the process; and wherein the catalyst is synthetized from organometallic compounds, hydroxides, metal alkoxides, salts of inorganic acids c) carrying out the alcoholysis reaction of polylactide in the presence of alcohol or mixture of alcohols, under autogenous pressure of reaction mixture components within a range from atmospheric pressure to 107 bar, in suitably selected temperature, wherein i. in non-catalyst reaction, the reaction temperature is 220-260°C, ii. while in catalyst reaction, the reaction temperature is 150-220°C, i. in non-catalyst reaction, the reaction temperature is 220-260°C, ii. while in catalyst reaction, the reaction temperature is 150-220°C, d) separating and purifying final product by filtration, evaporation and distillation.
An air-conditioning apparatus comprising: a heat medium circulating device that connects a plurality of heat medium feeding devices circulating a heat medium related to heating or cooling by heating or cooling means and a plurality of use side heat exchangers (26a to 26d) exchanging heat between air which is heat exchange target and the heat medium by piping to constitute a heat medium circulation circuit, and a control device, characterized in that the control device is configured such that it selects a use side heat exchanger (26a to 26d) absorbing heat into the heat medium and a use side heat exchanger (26a to 26d) emitting heat from the heat medium and controls to circulate the heat medium through both of the absorbing use side heat exchanger (26a to 26d) and the emitting use side heat exchanger (26a to 26d), when determining that the heating or cooling means cannot perform heating or cooling using the heat medium. a heat medium circulating device that connects a plurality of heat medium feeding devices circulating a heat medium related to heating or cooling by heating or cooling means and a plurality of use side heat exchangers (26a to 26d) exchanging heat between air which is heat exchange target and the heat medium by piping to constitute a heat medium circulation circuit, and a control device, characterized in that the control device is configured such that it selects a use side heat exchanger (26a to 26d) absorbing heat into the heat medium and a use side heat exchanger (26a to 26d) emitting heat from the heat medium and controls to circulate the heat medium through both of the absorbing use side heat exchanger (26a to 26d) and the emitting use side heat exchanger (26a to 26d), when determining that the heating or cooling means cannot perform heating or cooling using the heat medium.
Sheet processing machine comprising at least one transport means of an infeed system , the at least one transport means comprising at least one transfer element (206; 207), the infeed system comprising at least one cam mechanism comprising in each case at least one cam disk and an axis of rotation (D) of the at least one cam disk , the at least one cam mechanism being driven by at least one drive via at least one drive shaft , at least one scanning element being arranged in each case to rest against the at least one cam disk , the at least one scanning element being connected to the at least one transport means via at least one drive lever , the at least one drive lever in each case having at least one mounting point (S), the mounting point (S) and the axis of rotation (D) being configured to be adjustable and/or to be adjusted and/or to adjust relative to one another, the mounting point (S) and the axis of rotation (D) being configured to be pivotable and/or to be pivoted and/or to pivot relative to one another, characterized in that a position displacement of the mounting point (S) relative to the axis of rotation (D) is configured to compensate for at least one position error of at least one sheet , in that at least one servo drive is configured to adjust the mounting point (S) relative to the axis of rotation (D), in that the at least one servo drive is configured to intervene in a movement that is transmitted from the at least one drive shaft to the at least one transport means , in that the sheet processing machine comprises at least one transport system that is arranged downstream from the at least one infeed system in the transport direction (T), including at least two holding elements that are spaced apart from one another orthogonally to the transport direction (T), in that one of the at least two holding elements is in each case spaced apart from a respective assigned transfer element (206; 207), in a transfer position (PU), at a first distance in the transport direction (T), in that , by adjusting the mounting point (S) and the axis of rotation (D) relative to one another, the one holding element of the at least two holding elements is spaced apart from the assigned transfer element (206; 207) at a second distance in the transfer position (PU), and in that the second distance is different from the first distance.
An anti-ice system for a gas turbine engine , comprising: a first thermally conductive applique comprising a first heating circuit bonded to one or more airfoil surfaces, wherein the first thermally conductive applique comprises a metallic layer covering the first heating circuit ; and a first conductive layer electrically coupling the first heating circuit and a power generating device , the power generating device comprising: a first component configured to generate a current; a first magnet and a second magnet , wherein the first and second magnets are non-rotating structures; characterised by the first magnet being located over a first surface of the first component ; the second magnet being located over a second surface of the first component opposite the first surface of the first component ; the first component being a Faraday disk mounted to a rotor and configured to rotate in a plane perpendicular to a static magnetic field created by the first and second magnets, and wherein a first end of the first conductive layer is electrically coupled to a radially outward end of the first component , and wherein a second end of the first conductive layer is electrically coupled to a radially inward end of the first component . a first thermally conductive applique comprising a first heating circuit bonded to one or more airfoil surfaces, wherein the first thermally conductive applique comprises a metallic layer covering the first heating circuit ; and a first conductive layer electrically coupling the first heating circuit and a power generating device , the power generating device comprising: a first component configured to generate a current; a first magnet and a second magnet , wherein the first and second magnets are non-rotating structures; a first component configured to generate a current; a first magnet and a second magnet , wherein the first and second magnets are non-rotating structures; characterised by the first magnet being located over a first surface of the first component ; the second magnet being located over a second surface of the first component opposite the first surface of the first component ; the first component being a Faraday disk mounted to a rotor and configured to rotate in a plane perpendicular to a static magnetic field created by the first and second magnets, and wherein a first end of the first conductive layer is electrically coupled to a radially outward end of the first component , and wherein a second end of the first conductive layer is electrically coupled to a radially inward end of the first component .
An ullage-recirculating catalytic inerting system, the system comprising: an aircraft including a plurality of fuel tanks (200; 202; 204), the plurality of fuel tanks (200; 202; 204) having (i) respective inert gas ports (346; 348; 350; 352; 354; 356) for discharging the inert gas within a respective fuel tank (200; 202; 204), and (ii) respective ullage gas ports (302; 304; 308; 310; 322; 324) for drawing ullage gas from the respective fuel tank; and an inert gas generating system including (i) an ullage gas inlet port fluidly coupled to the respective ullage gas ports (302; 304; 308; 310; 322; 324), (ii) an inert gas outlet port (334; 336) fluidly coupled to the respective inert gas ports (346; 348; 350; 352; 354; 356), (iii) a catalytic reactor for chemically converting ullage gas received through the ullage gas inlet port to inert gas for discharge through the inert gas outlet port (334; 336), and (iv) a prime mover for moving gas through the inert gas generating system, characterized in that the ullage-recirculating catalytic inerting system is mounted with respect to the aircraft such that at least one fuel tank of the plurality of fuel tanks (200; 202; 204) includes a plurality of ullage gas ports disposed therein at different locations that correspond to respective high points of the at least one fuel tank during respective phases of flight of the aircraft, with the ullage gas ports (302; 304; 308; 310; 322; 324) being connected to the inert gas generating system via ullage gas lines . an aircraft including a plurality of fuel tanks (200; 202; 204), the plurality of fuel tanks (200; 202; 204) having (i) respective inert gas ports (346; 348; 350; 352; 354; 356) for discharging the inert gas within a respective fuel tank (200; 202; 204), and (ii) respective ullage gas ports (302; 304; 308; 310; 322; 324) for drawing ullage gas from the respective fuel tank; and an inert gas generating system including (i) an ullage gas inlet port fluidly coupled to the respective ullage gas ports (302; 304; 308; 310; 322; 324), (ii) an inert gas outlet port (334; 336) fluidly coupled to the respective inert gas ports (346; 348; 350; 352; 354; 356), (iii) a catalytic reactor for chemically converting ullage gas received through the ullage gas inlet port to inert gas for discharge through the inert gas outlet port (334; 336), and (iv) a prime mover for moving gas through the inert gas generating system, characterized in that the ullage-recirculating catalytic inerting system is mounted with respect to the aircraft such that at least one fuel tank of the plurality of fuel tanks (200; 202; 204) includes a plurality of ullage gas ports disposed therein at different locations that correspond to respective high points of the at least one fuel tank during respective phases of flight of the aircraft, with the ullage gas ports (302; 304; 308; 310; 322; 324) being connected to the inert gas generating system via ullage gas lines .