mhurhangee/ep-ind-claims huggingface dataset:
A fan assembly comprising: a nozzle having at least one first air inlet, at least one first air outlet, a first interior passage for conveying air from said at least one first air inlet to said at least one first air outlet, at least one second air inlet, at least one second air outlet, and a second interior passage for conveying air from said at least one second air inlet to said at least one second air outlet, the nozzle defining a bore about which the interior passages (48, 54) extend and through which air from outside the fan assembly is drawn by air emitted from the air outlets (44, 52); a body on which the nozzle is mounted, the body comprising flow generating means for generating a first air flow through the first interior passage and a second air flow through the second interior passage, a first air passageway for conveying the first air flow to said at least one first air inlet, and a second air passageway for conveying the second air flow to said at least one second air inlet, the second air passageway being arranged to receive air from the first air passageway downstream from the flow generating means, and means for changing one of the temperature, humidity, composition and electrical charge of the second air flow. a nozzle having at least one first air inlet, at least one first air outlet, a first interior passage for conveying air from said at least one first air inlet to said at least one first air outlet, at least one second air inlet, at least one second air outlet, and a second interior passage for conveying air from said at least one second air inlet to said at least one second air outlet, the nozzle defining a bore about which the interior passages (48, 54) extend and through which air from outside the fan assembly is drawn by air emitted from the air outlets (44, 52); a body on which the nozzle is mounted, the body comprising flow generating means for generating a first air flow through the first interior passage and a second air flow through the second interior passage, a first air passageway for conveying the first air flow to said at least one first air inlet, and a second air passageway for conveying the second air flow to said at least one second air inlet, the second air passageway being arranged to receive air from the first air passageway downstream from the flow generating means, and means for changing one of the temperature, humidity, composition and electrical charge of the second air flow.
A method for actively damping a ship's motion while the ship is sailing by driving at least one first rotatable damping element that extends from the ship's hull, below the water line, on a side of the ship, comprising the steps of: i) sensing the ship's motion and sailing speed, ii) generating and delivering control signals on the basis of step i), iii) rotatably driving the stabilisation elements (4a,4b) on the basis of step ii), iv) determining, on the basis of step i), the current frictional resistance experienced by the stabilisation elements at the sensed motion and sailing speed of the ship, v) setting the stabilisation element at an angle relative to a longitudinal axis of the ship on the basis of the determined current frictional resistance and a desired minimum frictional resistance. i) sensing the ship's motion and sailing speed, ii) generating and delivering control signals on the basis of step i), iii) rotatably driving the stabilisation elements (4a,4b) on the basis of step ii), iv) determining, on the basis of step i), the current frictional resistance experienced by the stabilisation elements at the sensed motion and sailing speed of the ship, v) setting the stabilisation element at an angle relative to a longitudinal axis of the ship on the basis of the determined current frictional resistance and a desired minimum frictional resistance.
An Ethernet base, comprising a USB unit, a USB drive unit, an Ethernet drive unit, and an Ethernet unit, wherein the USB unit is configured to receive first service data which is in a USB format and sent by a 3G router; the USB drive unit is configured to convert the first service data in the USB format into second service data in an Ethernet format, and is further configured to perform software configuration on the USB unit, so as to enable the USB unit to fulfill a hardware time sequence function of a USB host device; the Ethernet drive unit is configured to send the second service data in the Ethernet format to the Ethernet unit; and the Ethernet unit is configured to send the second service data in the Ethernet format to a fixed network router; and the USB drive unit comprises a serial interface and an Ethernet network card; the serial interface is configured to run control signaling; the Ethernet network card is configured to run service data; and the control signaling comprises signaling that identifies a device and determines whether a function of an Ethernet interface is a function of a local area network or a function of a wide area network.
A system for communicating information to and from a user of a surgical instrument comprising: a surgical instrument having a motor, a power source, a microprocessor to control the motor and a memory; a separate mobile wireless device; the surgical instrument further having a means for transmitting first information to the mobile wireless device; a remote computer in communication with the mobile wireless device, the remote computer having information stored thereon; wherein the mobile wireless device is capable of receiving and storing the first information transmitted from the surgical instrument, and further capable of soliciting second information from a user and transmitting the first and second information to the remote computer; and wherein the computer is configured to compare the transmitted first and second information with the stored information and to generate user alert information based upon the result of the comparison; and the computer is further configured to transmit the user alert information to the mobile wireless device. a surgical instrument having a motor, a power source, a microprocessor to control the motor and a memory; a separate mobile wireless device; the surgical instrument further having a means for transmitting first information to the mobile wireless device; a remote computer in communication with the mobile wireless device, the remote computer having information stored thereon; wherein the mobile wireless device is capable of receiving and storing the first information transmitted from the surgical instrument, and further capable of soliciting second information from a user and transmitting the first and second information to the remote computer; and wherein the computer is configured to compare the transmitted first and second information with the stored information and to generate user alert information based upon the result of the comparison; and the computer is further configured to transmit the user alert information to the mobile wireless device.
An electrostatic chuck, comprising: a thermally conductive layer configured to carry a wafer and provided therein with a heating element; and a heat insulating layer group disposed below the thermally conductive layer and configured to control a temperature of a bottom of the heat insulating layer group within a set range; and the heat insulating layer group comprises at least two heat insulating layers (81,82), which are sequentially arranged from top to bottom in descending order of thermal conductivity coefficient; both a material of the thermally conductive layer and a material of an uppermost heat insulating layer of the at least two heat insulating layers comprise aluminum nitride, and the thermally conductive layer and the uppermost heat insulating layer are connected into an integral body by sintering; at least one of the thermally conductive layer and the uppermost heat insulating layer is doped with at least one trace element in a predetermined proportion, so that a thermal conductivity coefficient of the uppermost heat insulating layer is less than a thermal conductivity coefficient of the thermally conductive layer; and a material of a lowermost heat insulating layer of the at least two heat insulating layers comprises quartz. a thermally conductive layer configured to carry a wafer and provided therein with a heating element; and a heat insulating layer group disposed below the thermally conductive layer and configured to control a temperature of a bottom of the heat insulating layer group within a set range; and the heat insulating layer group comprises at least two heat insulating layers (81,82), which are sequentially arranged from top to bottom in descending order of thermal conductivity coefficient;
A hose or belt incorporating a hybrid cable comprising a core and a wrap; the core comprising a carbon fiber yarn or bundle of carbon fiber yarns and comprising a twist; and the wrap comprising a plurality of metal wires helically wrapped around the core, the plurality of metal wires laid side by side without crossing each other.
A fluid dispenser comprising: · a fluid reservoir containing fluid; · a fluid suction chamber of variable volume that includes an extraction and application space, the space defining an open end and a closed end, the space communicating with the remainder of the chamber via the open end; · a dip tube that connects the reservoir to the chamber at an injection orifice that defines an injection axis; and · suction means (25, 75) for sucking, during a suction stage, fluid from the reservoir into the chamber through the injection orifice; the dispenser being characterized in that the extraction and application space is formed by a blind tube of volume that is constant defining the open end and the closed end, the injection orifice being situated at the open end of the blind tube, such that the fluid is injected in the form of an axial jet into the extraction and application space and fills it, at least in part, without the injection orifice penetrating into the space. · a fluid reservoir containing fluid; · a fluid suction chamber of variable volume that includes an extraction and application space, the space defining an open end and a closed end, the space communicating with the remainder of the chamber via the open end; · a dip tube that connects the reservoir to the chamber at an injection orifice that defines an injection axis; and · suction means (25, 75) for sucking, during a suction stage, fluid from the reservoir into the chamber through the injection orifice;
Air suspension system of a motor vehicle, comprising at least two spring bellows (3, 4) which are associated with air springs arranged on opposite vehicle sides of a vehicle axle and can be connected to and shut off from a main pressure line via respective connecting lines (7, 8) each provided with a level-regulating valve (5, 6), the main pressure line being connectable via a main pressure valve alternately to a compressed air source and to a compressed air sink and the connecting lines (7, 8) of the at least two spring bellows (3, 4) being connected to one another via a connecting line which is provided with a throttle and can be shut off by a shut-off valve, characterized in that the shut-off valve is configured to be activatable mechanically and is coupled to the level-regulating valve of the spring bellows arranged on the nearside of the vehicle in such a way that the shut-off valve is open when the level-regulating valve is closed and is closed when the level-regulating valve is open.
Fuselage section comprising: - at least two frames, each comprising: - a central element adapted to be located within the perimeter of the fuselage, - a portion of a longitudinal structure arranged to form a portion of a lifting surface and of a torsion box of a lifting structure for attaching the engines of an aircraft, - two lateral extensions adapted to project outside the perimeter of the fuselage from both sides of the central element that are the portion of the longitudinal structure, the central element and the two lateral extensions being configured as an integrated piece manufactured as a single part, and - a skin portion continuously extending over said two frames, wherein each central element comprises an upper portion and a lower portion respectively located at the upper part and lower part of the fuselage section, the upper portion having an inner perimeter edge, characterised in that the inner perimeter edge is aligned with the lower edge of the lateral extensions. - at least two frames, each comprising: - a central element adapted to be located within the perimeter of the fuselage, - a portion of a longitudinal structure arranged to form a portion of a lifting surface and of a torsion box of a lifting structure for attaching the engines of an aircraft, - two lateral extensions adapted to project outside the perimeter of the fuselage from both sides of the central element that are the portion of the longitudinal structure, the central element and the two lateral extensions being configured as an integrated piece manufactured as a single part, and - a central element adapted to be located within the perimeter of the fuselage, - a portion of a longitudinal structure arranged to form a portion of a lifting surface and of a torsion box of a lifting structure for attaching the engines of an aircraft, - two lateral extensions adapted to project outside the perimeter of the fuselage from both sides of the central element that are the portion of the longitudinal structure, the central element and the two lateral extensions being configured as an integrated piece manufactured as a single part, and - a skin portion continuously extending over said two frames,
A detector device, adapted to receive an incident signal being a terahertz signal, comprising: a body comprising a photoconductive material; a first antenna element connected to a first portion of the body and a second antenna element connected to a second portion of the body, wherein the first antenna element and the second antenna element are arranged to induce an electric field in the body in response to an incident signal; a waveguide arranged to couple light into the photoconductive material via a coupling interface between the waveguide and the body, the coupling interface facing away from the first portion and the second portion of the body and being closer to the first portion than to the second portion; and an electrode pair arranged to allow a photocurrent to be measured, the photocurrent resulting from the induced electrical field and the light coupled into the body; and wherein the first portion and the second portion form part of a top portion of the body, and wherein the coupling interface forms part of a side portion of the body. a body comprising a photoconductive material; a first antenna element connected to a first portion of the body and a second antenna element connected to a second portion of the body, wherein the first antenna element and the second antenna element are arranged to induce an electric field in the body in response to an incident signal; a waveguide arranged to couple light into the photoconductive material via a coupling interface between the waveguide and the body, the coupling interface facing away from the first portion and the second portion of the body and being closer to the first portion than to the second portion; and an electrode pair arranged to allow a photocurrent to be measured, the photocurrent resulting from the induced electrical field and the light coupled into the body; and wherein the first portion and the second portion form part of a top portion of the body, and wherein the coupling interface forms part of a side portion of the body.
A decoder, wherein the decoder is configured to receive an encoded data stream, the encoded data stream including data representing a picture and a classification mode parameter, the classification mode parameter specifying a certain classification to be applied to samples in the picture, the certain classification selected from a plurality of classifications, wherein the decoder is configured to decode the encoded data stream to obtain a reconstructed picture and the classification mode parameter, to classify samples of the reconstructed picture into one of a plurality of classes using the certain classification specified by the classification mode parameter, and to filter samples of the reconstructed picture, a sample being filtered using a filter for the class into which the sample has been classified, wherein the decoder includes an in-loop filter stage, the in-loop filter stage including a deblocking filter, DBF, to reduce blocking artifacts, a nonlinear sample adaptive offset, SAO, filter to reduce coding artifacts after the DBF, and an adaptive loop filter to minimize the mean square errors between original samples and reconstructed samples from the SAO filter, and wherein the adaptive loop filter is based on a geometry transformation-based adaptive loop filter, GALF, using multiple classifiers, the GALF configured to classify samples of the reconstructed picture into one of a plurality of classes using the certain classification specified by the classification mode parameter.. wherein the decoder is configured to receive an encoded data stream, the encoded data stream including data representing a picture and a classification mode parameter, the classification mode parameter specifying a certain classification to be applied to samples in the picture, the certain classification selected from a plurality of classifications, wherein the decoder is configured to decode the encoded data stream to obtain a reconstructed picture and the classification mode parameter, to classify samples of the reconstructed picture into one of a plurality of classes using the certain classification specified by the classification mode parameter, and to filter samples of the reconstructed picture, a sample being filtered using a filter for the class into which the sample has been classified, wherein the decoder includes an in-loop filter stage, the in-loop filter stage including a deblocking filter, DBF, to reduce blocking artifacts, a nonlinear sample adaptive offset, SAO, filter to reduce coding artifacts after the DBF, and an adaptive loop filter to minimize the mean square errors between original samples and reconstructed samples from the SAO filter, and wherein the adaptive loop filter is based on a geometry transformation-based adaptive loop filter, GALF, using multiple classifiers, the GALF configured to classify samples of the reconstructed picture into one of a plurality of classes using the certain classification specified by the classification mode parameter..
An optical fiber which is imparted with a twist to reduce polarization mode dispersion due to external factors after a glass portion of the optical fiber is hardened, the twist being an elastic torsion with stress, wherein a twist rate, which is the number of rotations per unit length by the twist, is represented by f(z) as a function of a position z in a longitudinal direction of the optical fiber, the f(z) having a predetermined twist cycle L and being defined such that a twist rotation angle in one direction and a twist rotation angle in the opposite direction become equal to each other in the twist cycle, and wherein when a rotation coefficient serving as a proportionality coefficient representing circular birefringence per twist rate is denoted by g, an angular frequency is denoted by ω, external linear birefringence due to a bending and a lateral pressure is denoted by β e, a variable k is denoted by a relational expression, a sum q̂ k ( ρ) of rotation angles over one twist cycle is denoted by a relational expression (1 b), a change ratio d e of β e to a change ratio of w is denoted by a relational expression, a change ratio d t of g to a change ratio of w is denoted by a relational expression, an average twist amplitude γ av is denoted by a relational expression, and a ratio ρ of the mean amplitude of a waveform to the peak amplitude thereof is denoted by a relational expression, a twist condition for the optical fiber satisfies a first condition that a twist error amount A from the optimum number of twist rotations defined by a relational expression is 8π (rad) or less, where k = 1, 2, 3, ⋯ q̂ k ( ρ): k-th zero point x from the smallest one among F x = gx 4 + d e d t ρ 4 + 0.42 d e 1 − ρ 4 − 1 tan gx 4 x > 0 d e = ω β e ∂ β e ∂ ω d t = ω g ∂ g ∂ ω γ av = 〈 f z 〉 = 1 L ∮ f z dz ρ = 〈 f z 〉 / max f z A = min k γ av L − q ^ k ρ / 1.014
A continuous process of preparing brominated styrenic polymer having a bromine content of at least 60 wt% after a bromination time of 20 minutes or less, which process comprises maintaining in a reaction zone, reaction mixture continuously formed from (i) a brominating agent, (ii) a solution formed from a solvent and styrenic polymer made by anionic polymerization, and (iii) aluminum halide catalyst in which the halogen atoms are bromine or chlorine with at least one such halogen atom being a bromine atom, in which (i), (ii), and (iii) are fed continuously but separately from each other, a mixture of (i) and (iii) and separately (ii) are fed continuously, or a mixture of (ii) and (iii) and separately (i) are fed continuously, at one or more temperatures in the range of -20 to +20°C and terminating the bromination of the polymer in the reaction mixture continuously exiting from the reaction zone.
An auxiliary device system of an aircraft engine, the auxiliary device system comprising: a motor generator configured to drive the aircraft engine; at least one auxiliary device motor configured to drive an auxiliary device mounted on the aircraft engine; a converter configured to convert electric power generated by the motor generator; at least one inverter provided separately from the converter and configured to drive the motor generator and the auxiliary device motor; at least one switch configured to be switched between a motor generator control state in which the inverter controls the motor generator and an auxiliary device motor control state in which the inverter controls the auxiliary device motor; and a controller configured to control the switch, wherein: when a condition in which a motor generator drive command has been generated is satisfied, the controller sets the switch to the motor generator control state; and when the condition is not satisfied, the controller sets the switch to the auxiliary device motor control state. a motor generator configured to drive the aircraft engine; at least one auxiliary device motor configured to drive an auxiliary device mounted on the aircraft engine; a converter configured to convert electric power generated by the motor generator; at least one inverter provided separately from the converter and configured to drive the motor generator and the auxiliary device motor; at least one switch configured to be switched between a motor generator control state in which the inverter controls the motor generator and an auxiliary device motor control state in which the inverter controls the auxiliary device motor; and a controller configured to control the switch, wherein: when a condition in which a motor generator drive command has been generated is satisfied, the controller sets the switch to the motor generator control state; and when the condition is not satisfied, the controller sets the switch to the auxiliary device motor control state. when a condition in which a motor generator drive command has been generated is satisfied, the controller sets the switch to the motor generator control state; and when the condition is not satisfied, the controller sets the switch to the auxiliary device motor control state.