mhurhangee/ep-ind-claims huggingface dataset:
Steering gear with a gear housing, in which a rack is mounted such that it can be displaced in a longitudinal direction, and comprising a first steering pinion and a second steering pinion which are mounted in each case rotatably in the gear housing and have a toothing region which is in engagement with at least one toothing system (6, 7) which is provided on the rack, the first steering pinion being operatively connected to a steering shaft (2, 3) which supports a steering wheel, and the second steering pinion being operatively connected via a worm gear mechanism (24, 25) to an electric motor, and the second steering pinion having a first free end and a second free end, the first free end being mounted in a first anti-friction bearing in the gear housing such that it can be rotated about a rotational axis, and the second free end supporting a worm gear of the gear, the second steering pinion being mounted in a second anti-friction bearing between the toothing region and the worm gear, the second anti-friction bearing comprising an outer ring, and the outer ring of the second anti-friction bearing being fixed by means of a securing ring in the gear housing in the direction of the rotational axis, characterized in that the securing ring is a circlip which has a ring part, provided with an interruption or a gap at one point, and two limbs which protrude radially on both sides from the interruption, project radially outwards and serve to prestress the securing ring, the second anti-friction bearing being arranged in an integrally formed region of the gear housing.
An elevator comprising a force application assembly provided for applying a force to an elevator car when the elevator car and a counterweight are in a balanced state, the force application assembly comprising: a first attachment portion, which is configured to be removably attached to an elevator hoistway; a second attachment portion, one end of which is removably fixed relative to the elevator car or the counterweight, and which is configured to be at least partially elastic; an actuation portion connected between the first attachment portion and the second attachment portion, wherein the first attachment portion is configured to be fixed relative to the actuation portion, and the second attachment portion is configured to be movable relative to the actuation portion; and an operation portion, which is associated with the actuation portion and is operable to move the second attachment portion away from or close to the actuation portion; wherein the actuation portion applies a force to the second attachment portion, and the force is stored as elastic potential energy in the second attachment portion before the balanced state of the elevator car and the counterweight is broken; and wherein the operation portion is sized in such a way that an operator can operate the operation portion when the operator is located outside the elevator hoistway. a first attachment portion, which is configured to be removably attached to an elevator hoistway; a second attachment portion, one end of which is removably fixed relative to the elevator car or the counterweight, and which is configured to be at least partially elastic; an actuation portion connected between the first attachment portion and the second attachment portion, wherein the first attachment portion is configured to be fixed relative to the actuation portion, and the second attachment portion is configured to be movable relative to the actuation portion; and an operation portion, which is associated with the actuation portion and is operable to move the second attachment portion away from or close to the actuation portion; wherein the actuation portion applies a force to the second attachment portion, and the force is stored as elastic potential energy in the second attachment portion before the balanced state of the elevator car and the counterweight is broken; and wherein the operation portion is sized in such a way that an operator can operate the operation portion when the operator is located outside the elevator hoistway.
A method for forming a sealant layer in a tire, the method comprising the steps of: providing a tire; and applying a plurality of strip-shaped windings (201, 214, 220, 230, 240, 250, 260) of a sealant material to form a sealant layer to the inside of the tire under the crown of the tire, wherein each winding (201, 214, 220, 230, 240, 250, 260) has a straight portion aligned at a zero degree angle with respect to the tire mid-circumferential plane; characterized in that the sealant material is sprayed or extruded onto the inside of the tire in a continuous manner, wherein a number of 5 to 30 strip-shaped windings (201, 214, 220, 230, 240, 250, 260) are applied, and wherein the strip-shaped windings (201, 214, 220, 230, 240, 250, 260) are applied in an abutting manner such that the windings do not overlap or are applied in a spaced manner such that the windings do not overlap and that there is a gap between adjacent windings. providing a tire; and applying a plurality of strip-shaped windings (201, 214, 220, 230, 240, 250, 260) of a sealant material to form a sealant layer to the inside of the tire under the crown of the tire, wherein each winding (201, 214, 220, 230, 240, 250, 260) has a straight portion aligned at a zero degree angle with respect to the tire mid-circumferential plane; characterized in that the sealant material is sprayed or extruded onto the inside of the tire in a continuous manner, wherein a number of 5 to 30 strip-shaped windings (201, 214, 220, 230, 240, 250, 260) are applied, and wherein the strip-shaped windings (201, 214, 220, 230, 240, 250, 260) are applied in an abutting manner such that the windings do not overlap or are applied in a spaced manner such that the windings do not overlap and that there is a gap between adjacent windings.
A fabric conditioner composition comprising: a) a branched amine functional silicone, wherein the branched amine functional silicone has a structure of R is C 1 -C 4 alkyl group, R' is an amine or salt thereof, R" is (R 2 SiO) x or (R 2 SiO) y (RSiO) w [(CH 2) 3 R'] z, a is 1 to 10, optionally 1 to 5, 1 to 3, or 3, m is 1 to 5, n is 3 to 20, p is 300 to 500, x is 50 to 200, y is 20 to 100, w is 0 to 10, z is 0 to 5; and x + y + w + z + p = 500 to 700; and b) cetyl trimethyl ammonium chloride present in an emulsion of the branched amine functional silicone. a) a branched amine functional silicone, wherein the branched amine functional silicone has a structure of R is C 1 -C 4 alkyl group, R' is an amine or salt thereof, R" is (R 2 SiO) x or (R 2 SiO) y (RSiO) w [(CH 2) 3 R'] z, a is 1 to 10, optionally 1 to 5, 1 to 3, or 3, m is 1 to 5, n is 3 to 20, p is 300 to 500, x is 50 to 200, y is 20 to 100, w is 0 to 10, z is 0 to 5; and x + y + w + z + p = 500 to 700; and R is C 1 -C 4 alkyl group, R' is an amine or salt thereof, R" is (R 2 SiO) x or (R 2 SiO) y (RSiO) w [(CH 2) 3 R'] z, a is 1 to 10, optionally 1 to 5, 1 to 3, or 3, m is 1 to 5, n is 3 to 20, p is 300 to 500, x is 50 to 200, y is 20 to 100, w is 0 to 10, z is 0 to 5; and x + y + w + z + p = 500 to 700; and b) cetyl trimethyl ammonium chloride present in an emulsion of the branched amine functional silicone.
Method of controlling an aircraft autopilot, the method comprising a succession of steps comprising at least: • a selection step for selecting a flight parameter to be servo-controlled by the autopilot, • a modification step for modifying a setpoint of the flight parameter to be servo-controlled by the autopilot, the modification step being performed by the at least one pilot of the aircraft by turning a first manually operated rotatable control element (25, 28), the first control element (25, 28) having a degree of rotational mobility relative to a fixed frame about an axis of rotation, and • a mode engagement step for engaging the autopilot in a mode corresponding to the modified setpoint at the modification step of the flight parameter, the mode engaging step being carried out by the at least one pilot of the aircraft by pressing on a second manually operated translatable control element (35, 38), the second control element (35, 38) having a degree of translational mobility with respect to the fixed frame along an axis of translation between an initial rest position and an activated engagement position, characterised in that the selection step is at least performed by at least one pilot of the aircraft by touching a touch zone arranged on a touch surface of a control screen bringing about a display of at least two flight parameters of the aircraft, in that the modification step is performed by means of the first control element (25, 28) arranged in close proximity to the control screen by rotating the first control element (25, 28) with respect to the fixed frame about the axis of rotation arranged perpendicular to the control screen and in that the mode engagement step is performed by pressing the second control element (35, 38) cooperating with elastic return means allowing the second control element (35, 38) to return to the initial rest position once the at least one pilot of the aircraft ceases pressing. • a selection step for selecting a flight parameter to be servo-controlled by the autopilot, • a modification step for modifying a setpoint of the flight parameter to be servo-controlled by the autopilot, the modification step being performed by the at least one pilot of the aircraft by turning a first manually operated rotatable control element (25, 28), the first control element (25, 28) having a degree of rotational mobility relative to a fixed frame about an axis of rotation, and • a mode engagement step for engaging the autopilot in a mode corresponding to the modified setpoint at the modification step of the flight parameter, the mode engaging step being carried out by the at least one pilot of the aircraft by pressing on a second manually operated translatable control element (35, 38), the second control element (35, 38) having a degree of translational mobility with respect to the fixed frame along an axis of translation between an initial rest position and an activated engagement position,
A cooling device for a Gas Insulated Switchgear comprising a condenser arranged outside a gas chamber, further comprising an evaporation part arranged in the gas chamber, a gas filling the gas chamber, and at least one fluid conduit connecting the evaporation part and the condenser; wherein the fluid conduit is heat conductive and is filled with liquid to transfer heat from the evaporation part to the condenser, and wherein the evaporation part is in contact with the gas filling the gas chamber on all sides, the fluid conduit comprising a hollow part at a gas chamber end to increase the contact of the fluid conduit with the gas in the gas chamber; and wherein the evaporation part and the at least one fluid conduit are integrated together, and the evaporation part is the gas chamber end of the at least one fluid conduit.
Prosthetic band, in particular for repairing a mitral valve, comprising an elongate band made of a flexible material for the fixation of artificial cords, characterized in that a plurality of separable pads is included that are joined to said elongate band along the trajectory of said elongate band and protrude with respect thereto, and that are separable from said elongate band, said pads being separated from each other and capable of receiving such artificial cords.
An enclosure for packaging products of the type comprising a contoured laminar element which is folded onto itself, wherein said laminar element comprises, at an intermediate portion thereof, a transverse folding line which defines two mutually opposite flaps (4, 5), a first flap comprising at least one slot, which extends in a direction that is perpendicular to the direction of said folding line, in the configuration for use said laminar element being folded onto itself along said folding line characterised in that said at least one slot is adjacent to an end border which is substantially parallel to said folding line, and in that said end border is coupled to said second flap, so that the strips which delimit the at least one slot are folded so as to define a substantially polygonal protruding shape, an end band of said second flap being juxtaposed and associated stably with the bottom of said strips for the partial closure of said at least one slot.
A radome for an aircraft, the radome comprising: a shell, the shell forming an outer surface of an enclosure when mounted on an aircraft, the enclosure being sized and shaped to house a first radio antenna configured to transmit and receive in a first frequency, wherein the shell includes a first portion that has mechanical properties that are different from the mechanical properties of the remaining portions of the shell and a second portion forming a transmission/reception window for the first radio antenna, the second portion having a reduced radio signal attenuation property of the first radio frequency when compared to the first portion, characterized in that the enclosure is sized and shaped to house a second radio antenna configured to transmit and receive in a second frequency, and the shell includes a third portion forming a transmission/reception window for the second radio antenna, the third portion having a reduced radio signal attenuation property of the second radio frequency when compared to the first portion and to the second portion, the first radio frequency and the second radio frequency being different radio frequencies. a shell, the shell forming an outer surface of an enclosure when mounted on an aircraft, the enclosure being sized and shaped to house a first radio antenna configured to transmit and receive in a first frequency, wherein the shell includes a first portion that has mechanical properties that are different from the mechanical properties of the remaining portions of the shell and a second portion forming a transmission/reception window for the first radio antenna, the second portion having a reduced radio signal attenuation property of the first radio frequency when compared to the first portion, characterized in that the enclosure is sized and shaped to house a second radio antenna configured to transmit and receive in a second frequency, and the shell includes a third portion forming a transmission/reception window for the second radio antenna, the third portion having a reduced radio signal attenuation property of the second radio frequency when compared to the first portion and to the second portion, the first radio frequency and the second radio frequency being different radio frequencies.
A polyarylene sulfide resin composition, including: 60 to 95 wt% of a polyarylene sulfide resin of which at least part of the end group of the polyarylene sulfide main chain is substituted by a carboxyl group; and 5 to 40 wt% of an epoxy-containing olefin-based elastomer, wherein the polyarylene sulfide resin is prepared by a method including: melt-polymerizing a reactant including a diiodioaromatic compound and sulfur element; and adding a compound having a carboxyl group while carrying out the melt-polymerization step. 60 to 95 wt% of a polyarylene sulfide resin of which at least part of the end group of the polyarylene sulfide main chain is substituted by a carboxyl group; and 5 to 40 wt% of an epoxy-containing olefin-based elastomer, wherein the polyarylene sulfide resin is prepared by a method including: melt-polymerizing a reactant including a diiodioaromatic compound and sulfur element; and adding a compound having a carboxyl group while carrying out the melt-polymerization step.
A cylindrical sleeve for a sheave for a passenger conveyor system, the cylindrical sleeve comprising: an outer surface (110, 406) comprising a groove arranged to receive a belt; and an inner surface defining a cylindrical cavity; wherein the cylindrical sleeve is substantially made of a polymer-based composite material including a polymeric material with fibre reinforcement, and wherein the cylindrical sleeve is made by disc gate injection moulding; further wherein the cylindrical sleeve comprises: a core made of the polymeric material with a first weight percentage of fibre reinforcement; and characterized in that the sleeve further comprises: two surface layers (460, 462) defining the outer surface (110, 406) and the inner surface (115, 405), respectively, wherein the surface layers (460, 462) are made of the polymeric material with a second weight percentage of fibre reinforcement; wherein the second weight percentage of fibre reinforcement is lower than the first weight percentage of fibre reinforcement. an outer surface (110, 406) comprising a groove arranged to receive a belt; and an inner surface defining a cylindrical cavity; wherein the cylindrical sleeve is substantially made of a polymer-based composite material including a polymeric material with fibre reinforcement, and wherein the cylindrical sleeve is made by disc gate injection moulding; further wherein the cylindrical sleeve comprises: a core made of the polymeric material with a first weight percentage of fibre reinforcement; and characterized in that the sleeve further comprises: two surface layers (460, 462) defining the outer surface (110, 406) and the inner surface (115, 405), respectively, wherein the surface layers (460, 462) are made of the polymeric material with a second weight percentage of fibre reinforcement; wherein the second weight percentage of fibre reinforcement is lower than the first weight percentage of fibre reinforcement. two surface layers (460, 462) defining the outer surface (110, 406) and the inner surface (115, 405), respectively, wherein the surface layers (460, 462) are made of the polymeric material with a second weight percentage of fibre reinforcement; wherein the second weight percentage of fibre reinforcement is lower than the first weight percentage of fibre reinforcement.
A recorder device for recording physiological data from a patient disposed in a high magnetic field, the recorder device comprising: a printer assembly configured to print the physiological data from the patient disposed in the high magnetic field; a piezoelectric motor for use in the high magnetic field configured to feed paper through the printer assembly as the physiological data from the patient in the high magnetic field is printed; a primary control board that is configured to generate electromechanical stepper motor drive signals based on clock signals; and a secondary control board operatively connected to the primary control board and the piezoelectric motor to receive the stepper motor drive signals from the primary control board and generate piezoelectric motor drive signals that drive the piezoelectric motor. a printer assembly configured to print the physiological data from the patient disposed in the high magnetic field; a piezoelectric motor for use in the high magnetic field configured to feed paper through the printer assembly as the physiological data from the patient in the high magnetic field is printed; a primary control board that is configured to generate electromechanical stepper motor drive signals based on clock signals; and a secondary control board operatively connected to the primary control board and the piezoelectric motor to receive the stepper motor drive signals from the primary control board and generate piezoelectric motor drive signals that drive the piezoelectric motor.
Data processing unit for a receiver of signals carrying data, said unit including: - a clock and data recovery circuit, which is clocked by a local clock signal and which includes a numerical phase lock loop, in which there is arranged a numerically controlled oscillator to generate at output at least one pulse signal (I P, Q P), the phase and frequency of which can be adapted on the basis of a data signal (D OUT) received at the input of the clock and data recovery circuit, and - a processor circuit connected to the clock and data recovery circuit, characterized in that the processor circuit is arranged to be able to calculate the mean and variance over time of the numerical input signal (NCO IN) of the numerically controlled oscillator so as to determine the coherence of the data signal (D OUT) if the calculated mean and variance are below a predefined coherence threshold, and to be able to perform a complete reset of the receiver if the calculated mean or variance of the numerical input signal (NCO in) of the numerically controlled oscillator are above the predefined coherence threshold. - a clock and data recovery circuit, which is clocked by a local clock signal and which includes a numerical phase lock loop, in which there is arranged a numerically controlled oscillator to generate at output at least one pulse signal (I P, Q P), the phase and frequency of which can be adapted on the basis of a data signal (D OUT) received at the input of the clock and data recovery circuit, and - a processor circuit connected to the clock and data recovery circuit, characterized in that the processor circuit is arranged to be able to calculate the mean and variance over time of the numerical input signal (NCO IN) of the numerically controlled oscillator so as to determine the coherence of the data signal (D OUT) if the calculated mean and variance are below a predefined coherence threshold, and to be able to perform a complete reset of the receiver if the calculated mean or variance of the numerical input signal (NCO in) of the numerically controlled oscillator are above the predefined coherence threshold.
Use of a clotting composition in the preparation of a serum sample for analyte detection, wherein the clotting composition consists essentially of purified prothrombin activator or comprises prothrombin activator purified or partially purified from snake venom.
A starry projection lamp, comprising an upper shell, a lower shell, a light-emitting light path system used for emitting water ripple light, a laser light path system used for emitting starriness light, and a main control board, wherein the lower shell is provided with a first accommodating cavity; the light-emitting light path system is rotatably disposed; the light-emitting light path system and the laser light path system are arranged in the first accommodating cavity; the upper shell is provided with a first light outlet and a second light outlet; the first light outlet is provided with a light-transmittance optical lens; a plurality of polyhedral vertebral prisms are distributed on an inner surface of the optical lens; a light-emitting surface of the light-emitting light path system faces the polyhedral vertebral prisms; a light-emitting surface of the laser light path system faces the second light outlet; a loudspeaker is also arranged in the first accommodating cavity; a communication module and an audio module are arranged on the main control board; and the loudspeaker is electrically connected to the main control board, wherein a motor fixing seat is also arranged in the first accommodating cavity; the motor fixing seat is provided with a second accommodating cavity; a groove and a boss arranged on the groove are arranged in the second accommodating cavity; a motor is arranged on the groove; the light-emitting light path system is arranged on the boss by a aluminum base plate; when the upper shell covers the lower shell, the upper shell presses the optical lens on the motor fixing seat; and the motor fixing seat is fixed on the lower shell; the motor fixing seat is also symmetrically provided with sound cavities; the sound cavities are arranged on two sides of the second accommodating cavity; and two loudspeakers are provided, and are respectively arranged in the sound cavities; each polyhedral vertebral prism is formed by splicing a plurality of triangular mirrors; the mirrors of the polyhedral vertebral prism are divided into a plurality of groups of triangles which are distributed towards an edge along a center of the spherical inner surface of the optical lens, and bottom sides of each group of triangles are spliced to form a dodecagon.