mhurhangee/ep-ind-claims huggingface dataset:
Process for production of a container by blowing starting from a pre-form made of plastics material within a production unit, the production unit comprising a mold defining an impression for the container to be formed, and a nozzle which is designed to close the mold hermetically, the production process comprising: - a sequence of forming by blowing, with a blowing phase (S2; S3; S5) comprising at least the injection and maintenance of a gas under pressure in the pre-form, via the nozzle, in order to deform the pre-form until it matches the impression of the mold, and obtain a container; - a phase of degassing (D2; D3; D5) of the container formed, consisting of discharging the gas contained in the container at the end of the forming sequence, in order to take the interior of the container to atmospheric pressure, characterized in that, during the degassing phase (D2; D3; D5), the nozzle is spaced (ET2; ET3; ET5) from the mold in order to interrupt the hermetic closure, so as to put the interior of the container into direct fluid communication with the atmosphere, the spacing of the nozzle being begun: - after the beginning of the degassing phase (D2; D3), when the pressure in the interior of the container has dropped and has reached an intermediate pressure which is lower than the pressure at the end of the forming sequence, and is between 14 and 3 bars; or after completion of the blowing phase (S2; S3; S5), at a predetermined instant which takes place within an interval of time of between 0 and 200 ms after the stoppage of the injection of gas into the container. - a sequence of forming by blowing, with a blowing phase (S2; S3; S5) comprising at least the injection and maintenance of a gas under pressure in the pre-form, via the nozzle, in order to deform the pre-form until it matches the impression of the mold, and obtain a container; - a phase of degassing (D2; D3; D5) of the container formed, consisting of discharging the gas contained in the container at the end of the forming sequence, in order to take the interior of the container to atmospheric pressure, - after the beginning of the degassing phase (D2; D3), when the pressure in the interior of the container has dropped and has reached an intermediate pressure which is lower than the pressure at the end of the forming sequence, and is between 14 and 3 bars;
A resin vehicle door structure comprising: an outer panel to be disposed at a vehicle compartment outer side of a vehicle door; an inner panel made from resin and to be disposed at a vehicle compartment inner side of the outer panel; the resin vehicle door structure being characterized by a bent portion (36, 38; 52, 54) that is a portion of the resin vehicle door structure which is formed by the outer panel and the inner panel and that is provided at a join portion (30; 50) where the outer panel and the inner panel are joined to each other by an adhesive, whereby the outer panel and the inner panel are bent into a crank shape when forming the bent portion (36, 38; 52, 54); and a rib (40; 56) that is formed at least at a corner portion of the bent portion (36, 38; 52, 54) on a face of one of the outer panel and the inner panel that is coated with the adhesive, and that projects out from said face of the corner portion. an outer panel to be disposed at a vehicle compartment outer side of a vehicle door; an inner panel made from resin and to be disposed at a vehicle compartment inner side of the outer panel; the resin vehicle door structure being characterized by a bent portion (36, 38; 52, 54) that is a portion of the resin vehicle door structure which is formed by the outer panel and the inner panel and that is provided at a join portion (30; 50) where the outer panel and the inner panel are joined to each other by an adhesive, whereby the outer panel and the inner panel are bent into a crank shape when forming the bent portion (36, 38; 52, 54); and a rib (40; 56) that is formed at least at a corner portion of the bent portion (36, 38; 52, 54) on a face of one of the outer panel and the inner panel that is coated with the adhesive, and that projects out from said face of the corner portion.
A system with adjustable levelling feet for furniture with a bottom and shoulders which terminate in correspondence with said bottom, of the type including, in combination: at least one pair of feet (35,35'), front and rear, respectively, which are operatively interconnected by means of a return and regulation rod, and wherein each foot (35, 35') comprises a regulation mechanism, said rod and said mechanism being accessible from the outside of the foot (35,35') and manoeuvrable by means of a tool, the foot (35, 35') being assembled on a plaque (34,34') fixed outside the bottom of said piece of furniture, a series of passages (49, 49';43, 43'; 44, 44') for said rod and for said tool being envisaged in said plaque (34,34') characterized in that said plaque (34, 34') has a square configuration defining wings substantially positioned at 90°, said foot (35,35') being situated in the vertex defined by said wings, whose regulation mechanism is accessible through said passages (43, 43'; 44, 44') situated in said wings radially with respect to said foot (35, 35') said first of said passages being substantially parallel to the second of said passages, and substantially perpendicular to the third of said passages, whereas the fourth of said passages is substantially parallel to the fifth of said passages, and substantially perpendicular to the sixth of said passages.
A bellows (4, 104, 204, 304, 404) for a vacuum interrupter (8, 8A, 8B, 8C) having an evacuated envelope, the bellows in a free state comprising: a plurality of convolution elements and a plurality of support elements alternately connected together and being symmetric about an axis (16, 116, 216, 316, 416) that extends centrally through the bellows, each adjacent pair of convolution elements being connected with and spaced apart by an intervening support element, and each adjacent pair of support elements being connected with and spaced apart by an intervening convolution element; each convolution element being of a convolution length (28, 128A, B, C, D, 228A, B, C, D, 328A, B, C, D, 428A, B, C, D) along the axis and being of a convolution height (32A, B, C, D, 132A, D, 232A, D, 332A, B, C, D, E, 432) perpendicular to the axis; each support element being of a spacing length (36, 136A, B, C, D, 236A, B, C, D, 336A, B, C, D, E, 436A, B, C, D) along the axis; and at least one of: at least a first convolution element having a convolution length different than that of another convolution element situated adjacent the at least first convolution element, and at least a first support element having a spacing length different than that of another support element situated adjacent the at least first support element. a plurality of convolution elements and a plurality of support elements alternately connected together and being symmetric about an axis (16, 116, 216, 316, 416) that extends centrally through the bellows, each adjacent pair of convolution elements being connected with and spaced apart by an intervening support element, and each adjacent pair of support elements being connected with and spaced apart by an intervening convolution element; each convolution element being of a convolution length (28, 128A, B, C, D, 228A, B, C, D, 328A, B, C, D, 428A, B, C, D) along the axis and being of a convolution height (32A, B, C, D, 132A, D, 232A, D, 332A, B, C, D, E, 432) perpendicular to the axis; each support element being of a spacing length (36, 136A, B, C, D, 236A, B, C, D, 336A, B, C, D, E, 436A, B, C, D) along the axis; and at least one of: at least a first convolution element having a convolution length different than that of another convolution element situated adjacent the at least first convolution element, and at least a first support element having a spacing length different than that of another support element situated adjacent the at least first support element. at least a first convolution element having a convolution length different than that of another convolution element situated adjacent the at least first convolution element, and at least a first support element having a spacing length different than that of another support element situated adjacent the at least first support element.
A crankshaft assembly for an air compressor for a vehicle comprising: a crankshaft, the crankshaft comprising: a first segment; a second segment having an outside diameter at a distal end; a cavity extending into the second segment at the distal end, the cavity comprising: a first portion having first inner diameter; and a second portion having a second inner diameter, wherein the second inner diameter is less than the first inner diameter, characterized by a linear passage in the second segment, wherein the linear passage does not intersect the cavity; and an insert (20; 20') having a first end (21; 21') with a first insert diameter and a second end (26; 26') with a second insert diameter, wherein the insert (20; 20') is sized to be matingly engaged in the cavity, and where the insert (20; 20') is substantially flush with the distal end of the second segment of the crankshaft. a crankshaft, the crankshaft comprising: a first segment; a second segment having an outside diameter at a distal end; a cavity extending into the second segment at the distal end, the cavity comprising: a first portion having first inner diameter; and a second portion having a second inner diameter, wherein the second inner diameter is less than the first inner diameter, a first segment; a second segment having an outside diameter at a distal end; a cavity extending into the second segment at the distal end, the cavity comprising: a first portion having first inner diameter; and a second portion having a second inner diameter, wherein the second inner diameter is less than the first inner diameter, a first portion having first inner diameter; and a second portion having a second inner diameter, wherein the second inner diameter is less than the first inner diameter, characterized by a linear passage in the second segment, wherein the linear passage does not intersect the cavity; and an insert (20; 20') having a first end (21; 21') with a first insert diameter and a second end (26; 26') with a second insert diameter, wherein the insert (20; 20') is sized to be matingly engaged in the cavity, and where the insert (20; 20') is substantially flush with the distal end of the second segment of the crankshaft.
An aircraft fuselage wall comprising: at least first and second frame members, wherein the first and second frame members extend approximately parallel to one another, a panel assembly comprising: a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface, wherein the second panel includes at least first and second rib members formed therein that extend inwardly and each define an outer rib cavity, wherein the first and second rib members each include an inner surface and an outer surface, wherein at least a first panel portion is defined between the first and second rib members, wherein the first panel portion includes an inner surface and an outer surface, wherein the inner surfaces of the first and second rib members are secured to the inner surface of the first panel, and wherein the inner surface of the first panel portion is spaced apart from the inner surface of the first panel to define at least a first cavity, wherein the first and second frame members are received in and extend longitudinally along the first and second outer rib cavities, respectively. at least first and second frame members, wherein the first and second frame members extend approximately parallel to one another, a panel assembly comprising: a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface, wherein the second panel includes at least first and second rib members formed therein that extend inwardly and each define an outer rib cavity, wherein the first and second rib members each include an inner surface and an outer surface, wherein at least a first panel portion is defined between the first and second rib members, wherein the first panel portion includes an inner surface and an outer surface, wherein the inner surfaces of the first and second rib members are secured to the inner surface of the first panel, and wherein the inner surface of the first panel portion is spaced apart from the inner surface of the first panel to define at least a first cavity, wherein the first and second frame members are received in and extend longitudinally along the first and second outer rib cavities, respectively. a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface, wherein the second panel includes at least first and second rib members formed therein that extend inwardly and each define an outer rib cavity, wherein the first and second rib members each include an inner surface and an outer surface, wherein at least a first panel portion is defined between the first and second rib members, wherein the first panel portion includes an inner surface and an outer surface, wherein the inner surfaces of the first and second rib members are secured to the inner surface of the first panel, and wherein the inner surface of the first panel portion is spaced apart from the inner surface of the first panel to define at least a first cavity, wherein the first and second frame members are received in and extend longitudinally along the first and second outer rib cavities, respectively.
A magnetic bearing comprising: a rotor to be supported for rotation about an axis, the rotor comprising a metallic core (160, 28) having a radially outward extending flange, wherein the flange has first and second axial end faces (170, 172); a stator extending from a first end to a second end and comprising: one or more first permanent magnet rings; one or more second permanent magnet rings of polarity substantially opposite to a polarity of the one or more first permanent magnet rings; a first axial winding circumscribing the axis; a second axial winding circumscribing the axis; a first end pole; and a second end pole; wherein the first and second axial end faces (170, 172) of the flange are separated from the first and second end poles (120, 122) by gaps (190, 192) wherein the magnetic bearing is a thrust bearing without radial windings. a rotor to be supported for rotation about an axis, the rotor comprising a metallic core (160, 28) having a radially outward extending flange, wherein the flange has first and second axial end faces (170, 172); a stator extending from a first end to a second end and comprising: one or more first permanent magnet rings; one or more second permanent magnet rings of polarity substantially opposite to a polarity of the one or more first permanent magnet rings; a first axial winding circumscribing the axis; a second axial winding circumscribing the axis; a first end pole; and a second end pole; wherein the first and second axial end faces (170, 172) of the flange are separated from the first and second end poles (120, 122) by gaps (190, 192) wherein the magnetic bearing is a thrust bearing without radial windings. one or more first permanent magnet rings; one or more second permanent magnet rings of polarity substantially opposite to a polarity of the one or more first permanent magnet rings; a first axial winding circumscribing the axis; a second axial winding circumscribing the axis; a first end pole; and a second end pole; wherein the first and second axial end faces (170, 172) of the flange are separated from the first and second end poles (120, 122) by gaps (190, 192) wherein the magnetic bearing is a thrust bearing without radial windings.
Process for the preparation of a copolymer in semicontinuous operation in a polymerization apparatus, comprising a polymerization reactor connected to a metering device, in each case acid monomer being initially taken in the metering device and polyether macromonomer and water in the polymerization reactor, acid monomer being metered from the metering device via an acid metering line into the polymerization reactor, free radical polymerization initiator being passed into the polymerization reactor before and/or during the metering of the acid monomer into the polymerization reactor so that an aqueous medium in which acid monomer and polyether macromonomer are reacted with formation of the copolymer by free radical polymerization forms in the polymerization reactor, the molar ratio of acid monomer used altogether to polyether macromonomer used altogether being 20: 1 to 1: 1, the molar ratio of acid monomer initially taken in the polymerization reactor to the acid monomer metered into the polymerization reactor being 3: 1 to 1: 10, a portion of the copolymer-containing aqueous medium being passed continuously during the free radical polymerization from the polymerization reactor via a reaction mixture line which is connected via a mixing device to the acid monomer metering line, the discharged copolymer-containing aqueous medium being mixed with the acid monomer in the mixing device during the metering of the acid monomer and being recycled to the polymerization reactor after the mixing via the acid monomer metering line.
A method for providing a measurement report from a User Equipment, in the following referred to as UE, to a network in a wireless communication system, the method comprising: being configured with carrier aggregation at the UE or being configured with at least one Secondary Cell, in the following referred to as SCells, at the UE; triggering a measurement report; characterized by omitting an additional measurement result in the measurement report if the measurement report is triggered by inter-Radio Access Technology measurement, in the following referred to as inter-RAT measurement,, wherein the additional measurement results include the measurement result for best non-serving cells. being configured with carrier aggregation at the UE or being configured with at least one Secondary Cell, in the following referred to as SCells, at the UE; triggering a measurement report; characterized by omitting an additional measurement result in the measurement report if the measurement report is triggered by inter-Radio Access Technology measurement, in the following referred to as inter-RAT measurement,, wherein the additional measurement results include the measurement result for best non-serving cells.
A method for regulating the thrust of an aircraft turbomachine, for an aircraft turbomachine comprising: - a propeller comprising a plurality of blades; - a blade variable pitch setting system for varying the pitch of said blades; - successively along an engine axle: • a low-pressure compressor comprising at least one straightener equipped with a vane variable pitch setting system for changing an orientation of vanes of the straightener, • a high-pressure compressor, • a combustion chamber, • one or more turbines (140, 150); the method being characterised in that it comprises the following steps: (i) varying a pitch setting of vanes of the straightener by means of the vane variable pitch setting system to regulate in an open loop the thrust of the turbomachine; (ii) regulating a pitch setting of blades of the propeller in a closed loop based on a rotational speed of the propeller, by means of the blade variable pitch setting system. - a propeller comprising a plurality of blades; - a blade variable pitch setting system for varying the pitch of said blades; - successively along an engine axle: • a low-pressure compressor comprising at least one straightener equipped with a vane variable pitch setting system for changing an orientation of vanes of the straightener, • a high-pressure compressor, • a combustion chamber, • one or more turbines (140, 150); • a low-pressure compressor comprising at least one straightener equipped with a vane variable pitch setting system for changing an orientation of vanes of the straightener, • a high-pressure compressor, • a combustion chamber, • one or more turbines (140, 150); (i) varying a pitch setting of vanes of the straightener by means of the vane variable pitch setting system to regulate in an open loop the thrust of the turbomachine; (ii) regulating a pitch setting of blades of the propeller in a closed loop based on a rotational speed of the propeller, by means of the blade variable pitch setting system.
Pneumatic vehicle tyre with a tread, a tyre sidewall and a tyre bead with a bead core, a bead filler and a bead outer profile, the bead filler enclosing the bead core rotationally symmetrically in relation to the axial axis of the pneumatic vehicle tyre and at least one carcass insert being turned up around the bead core with the bead filler, and a bead reinforcement being turned up around the outer side of the carcass ply, characterized in that the end of the bead outer profile that is lying on the outside in the radial direction with respect to the vehicle tyre lies against the bead filler in a cupped manner and is arranged below the outer end of the bead filler, the bead outer profile lying on the outside against the carcass ply turn-up and the bead reinforcement.
Method to increase growth or differentiation in vitro in a cell or tissue culture comprising culturing said cell or tissue and applying pulsed radiofrequency to said cell or tissue, wherein the cell or tissue is derived from a plant, and wherein the parameters for PRF are as follows: a. Frequency: 50,000 - 1,000,000 Hz, preferably 150,000 - 500,000 Hz b. Pulse duration: 0.1 - 100 msec, preferably 5-20 msec. c. Pulse frequency: 1 - 20/sec, preferably 1 - 3/sec d. Voltage: 1-100 V per cm distance between electrodes e. Exposure time: 2-180 minutes. a. Frequency: 50,000 - 1,000,000 Hz, preferably 150,000 - 500,000 Hz b. Pulse duration: 0.1 - 100 msec, preferably 5-20 msec. c. Pulse frequency: 1 - 20/sec, preferably 1 - 3/sec d. Voltage: 1-100 V per cm distance between electrodes e. Exposure time: 2-180 minutes.
Method for processing an analogue channel signal deriving from a transmission channel, the analogue channel signal conveying symbol frames, and the transmission channel being considered to be linear and cyclo-stationary for the entire duration of at least one frame, the method comprising an analogue-digital conversion of the analogue channel signal so as to obtain a digital channel signal, and a plurality of channel estimations performed for the said at least one frame on the basis of the digital channel signal so as to formulate a sequence of N transfer functions (HF k) of the transmission channel which are respectively associated with N successive time slices (TR k), the total duration of the N time slices being equal to almost the whole of the cyclo-stationarity period of the channel or to the whole of the said period, and a decoding of at least some of the symbols of the said at least one frame by using for each of these symbols the transfer function associated with the time slice containing the said symbol, the formulation of the sequence of N transfer functions comprising a formulation of an initial sequence of M transfer functions (H i) respectively associated with M successive reference symbols of the said at least one frame, the M reference symbols temporally covering a duration equal to or slightly greater than the whole of the said cyclo-stationarity period, the N transfer functions (HF k) being derived from these M transfer functions (Hi), characterized in that the analogue channel signal derives from a digital-analogue conversion of an initial digital signal, and when the sampling frequency of the digital channel signal is different from the sampling frequency of the initial digital signal, the said plurality of channel estimations comprise estimations of M base transfer functions (HB i) respectively performed on the basis of the M reference symbols of the said received frame, and a processing for correcting these M base transfer functions with a phase shift (DPHC) corresponding to this shift of sampling frequency so as to obtain the said M transfer functions (H i).