mhurhangee/ep-ind-claims huggingface dataset:
A termination block assembly for fluidly coupling a fluid line at a hydrocarbon production device, the termination block assembly comprising: a fluid line block with an inner surface adapted to be selectively mated to a corresponding surface of the hydrocarbon production device, the fluid line block having a protruding member extending from the inner surface; a primary seal located at an end of the protruding member, the primary seal having an inner diameter suitable for selectively circumscribing the fluid line extending from the hydrocarbon production device, and an outer diameter suitable for selectively engaging a sidewall passage surface of the hydrocarbon production device and sealing between the fluid line block and the hydrocarbon production device; a secondary seal circumscribing the protruding member, engaging both the inner surface of the fluid line block and the corresponding surface of the hydrocarbon production device and sealing between the fluid line block and the hydrocarbon production device, characterized in that the primary seal and the secondary seal define an annular cavity between the fluid line block and the hydrocarbon production device; and in that a test port is in fluid communication with the annular cavity for monitoring pressure within the annular cavity. a fluid line block with an inner surface adapted to be selectively mated to a corresponding surface of the hydrocarbon production device, the fluid line block having a protruding member extending from the inner surface; a primary seal located at an end of the protruding member, the primary seal having an inner diameter suitable for selectively circumscribing the fluid line extending from the hydrocarbon production device, and an outer diameter suitable for selectively engaging a sidewall passage surface of the hydrocarbon production device and sealing between the fluid line block and the hydrocarbon production device; a secondary seal circumscribing the protruding member, engaging both the inner surface of the fluid line block and the corresponding surface of the hydrocarbon production device and sealing between the fluid line block and the hydrocarbon production device, characterized in that the primary seal and the secondary seal define an annular cavity between the fluid line block and the hydrocarbon production device; and in that a test port is in fluid communication with the annular cavity for monitoring pressure within the annular cavity.
An improved method of making an unleavened pastry product from a pastry dough comprising an admixture consisting of 62 - 68% w/w flour, 28 - 37% w/w water, and 1 - 4% w/w salt, in a convection baking oven having a convection atmosphere, said method comprising cooking said dough in said oven, the improvement comprising (i) providing a transportable baking pan assembly comprising a baking pan, and an upper and lower water-containing reservoir means for operably releasing water vapour into said convection atmosphere during said cooking, and sheets of silicone Bakers Paper; (ii) placing said pastry dough on a sheet of said silicon Bakers Paper in said baking pan of said baking pan assembly; (iii) covering said pastry dough with an additional sheet of said silicone Bakers Paper; (iv) locating said baking pan assembly within said oven and between said upper and lower water-containing reservoir means; and (v) cooking said pastry dough at a temperature of 232°C to 252°C (450°F to 485°F) for a time of 90 minutes while maintaining the convection atmosphere as a moist atmosphere of at least 50% humidity for the duration of the cooking time, in order to maintain the moisture content of said pastry product at 25-35% w/w H 2 O. (i) providing a transportable baking pan assembly comprising a baking pan, and an upper and lower water-containing reservoir means for operably releasing water vapour into said convection atmosphere during said cooking, and sheets of silicone Bakers Paper; (ii) placing said pastry dough on a sheet of said silicon Bakers Paper in said baking pan of said baking pan assembly; (iii) covering said pastry dough with an additional sheet of said silicone Bakers Paper; (iv) locating said baking pan assembly within said oven and between said upper and lower water-containing reservoir means; and (v) cooking said pastry dough at a temperature of 232°C to 252°C (450°F to 485°F) for a time of 90 minutes while maintaining the convection atmosphere as a moist atmosphere of at least 50% humidity for the duration of the cooking time, in order to maintain the moisture content of said pastry product at 25-35% w/w H 2 O.
A mold configured to form at least one molded article having a predetermined shape by injecting a flowable self-curable molding material, the flowable self-curable molding material comprising an inorganic material powder, a dispersion medium, a gelling agent and a dispersant, the mold comprising: a cavity serving as a space configured to form a molded article by injecting the molding material; and a gate communicating with the perimeter of the bottom of the cavity and serving as a space configured to feed the cavity with the molding material characterized by an inlet arranged at a position higher than the top of the cavity and configured to feed the gate with the molding material, and a vent communicating with the top of the cavity, and serving as a space configured to partially discharge the molding material from the cavity. a cavity serving as a space configured to form a molded article by injecting the molding material; and a gate communicating with the perimeter of the bottom of the cavity and serving as a space configured to feed the cavity with the molding material characterized by an inlet arranged at a position higher than the top of the cavity and configured to feed the gate with the molding material, and a vent communicating with the top of the cavity, and serving as a space configured to partially discharge the molding material from the cavity.
A protection device for preventing a supply voltage of a microcontroller from dropping in an electronic cigarette, comprising; a microcontroller; a power supply module used to output a supply voltage to the microcontroller and a load; a field effect transistor, the source of the field effect transistor being connected to the negative electrode of the power supply module, and the drain of the field effect transistor being connected to the load; an over current or short circuit detection module, used to real-time detect an operating current of a load circuit, and to provide the microcontroller with detection signal; and an energy storage circuit connected between the microcontroller and the power supply module, and the energy storage circuit is used to supply electric power to the microcontroller and to delay the supply voltage of the microcontroller from dropping in a certain period of time when an over current or short circuit occurs in the load; and the microcontroller is used to process the over current or short circuit signal in the certain period of time and output a control signal to turn off the field effect transistor; characterized in that the energy storage circuit comprises a diode and an energy storage capacitor, the positive electrode of the diode is connected to the positive electrode of the power supply module, the negative electrode of the diode is connected to the positive supply terminal of the microcontroller and a first terminal of the storage capacitor, a second terminal of the energy storage capacitor is connected to the negative electrode of the power supply module and the negative supply terminal of the microcontroller; and when an output voltage of the power module drops caused by the over current or short circuit, the energy storage capacitor of the energy storage circuit supplies electric power to the microcontroller, and a discharging path from the energy storage capacitor following via the power module is cut off by the diode.
An integrated laminate structure adapted for optical applications in the context of wafer technology, cooling channels, greenhouse illumination, window illumination, street lighting, traffic lighting, traffic reflectors or security films, optionally configured to exhibit informative and/or commercial visual message, comprising: - a first carrier element, such as a piece of plastic or glass, configured as a flat, planar element, - a second carrier element, configured as a planar element, in which a plurality of different surface relief forms of different shapes are configured to form a number of surface relief patterns, a number of said surface relief forms of different shapes of each pattern having flat portions on laminate junction areas between the first and the second carrier elements, by which flat portions the contact surfaces between said first and said second carrier elements are formed, said first carrier element and said second carrier element being composed of an optically substantially transparent material enabling light transmission therethrough, the first carrier element and the second carrier element being laminated together to establish the integrated laminate structure such that the surface relief patterns have been embedded within the established integrated laminate structure, whereby embedded relief patterns comprising a number of related optically functional cavities (408, 410, 412) are formed at an interface established by flat portions provided as contact surfaces between the first carrier element and the second carrier element, wherein, said embedded relief patterns have at least one predetermined optical function relative to incident light selected from an incident light coupling and/or directing function, such as a collimation function, and wherein in addition to the incident light coupling and/or directing function, reflective and generally light trapping functions are achieved by the utilized patterns including cavities, their positioning, alignment and material selections, wherein light traps are formed without reflective mirror surfaces in the carrier material. - a first carrier element, such as a piece of plastic or glass, configured as a flat, planar element, - a second carrier element, configured as a planar element, in which a plurality of different surface relief forms of different shapes are configured to form a number of surface relief patterns, a number of said surface relief forms of different shapes of each pattern having flat portions on laminate junction areas between the first and the second carrier elements, by which flat portions the contact surfaces between said first and said second carrier elements are formed,
A method for protecting a resonant linear compressor, the resonant linear compressor comprising: a piston, a cylinder, a motor and a spring (7a, 7b), the resonant linear compressor further comprising: a structural resonance frequency (w E) which depends only on the dimension characteristics of the resonant linear compressor, a motor that is fed by a feed voltage (V ENT) that has an amplitude and a drive frequency (w A) both controlled according to the product A.sen(w A t), wherein the drive frequency (w A) is derived from actuation of the spring (7a, 7b) and from the amplitude of the feed voltage (V ENT) on the piston, wherein the feed voltage (V ENT) further encompasses a inductor voltage (V L (i(t)), a voltage induced in the motor, and a resistance voltage (V R), the method being characterized by comprising a step of: controlling, by means of an electronic control, a phase between an electric current i(t) of the resonant linear compressor and the piston displacement velocity in order to prevent the drive of the resonant linear compressor at drive frequencies (w A) that have at least one harmonic coinciding with the structural resonance frequency (w E) of the resonant linear compressor. a structural resonance frequency (w E) which depends only on the dimension characteristics of the resonant linear compressor, a motor that is fed by a feed voltage (V ENT) that has an amplitude and a drive frequency (w A) both controlled according to the product A.sen(w A t), wherein the drive frequency (w A) is derived from actuation of the spring (7a, 7b) and from the amplitude of the feed voltage (V ENT) on the piston, wherein the feed voltage (V ENT) further encompasses a inductor voltage (V L (i(t)), a voltage induced in the motor, and a resistance voltage (V R), the method being characterized by comprising a step of: controlling, by means of an electronic control, a phase between an electric current i(t) of the resonant linear compressor and the piston displacement velocity in order to prevent the drive of the resonant linear compressor at drive frequencies (w A) that have at least one harmonic coinciding with the structural resonance frequency (w E) of the resonant linear compressor.
A minimally invasive surgical assembly including a handpiece for removably attaching one of a plurality of probes, the handpiece comprising a housing; a mechanical actuation assembly arranged on the housing and having pivotal motion with respect thereto; a linkage assembly arranged on the housing and adapted to couple with the actuation assembly to move translationally and actuate an attached probe; an alignment feature arranged on the housing and adapted to control an orientation of an attached probe, characterized in further comprising a probe for removable attachment to the handpiece, the probe comprising a base assembly; and a procedure assembly extending from the base assembly, wherein the procedure assembly comprises an insertion member (330, 500) having a distal end with an arcuate surface and a working surface that further define a cavity therein; and a probe tool (342, 362, 372, 382) positioned on the insertion member for selective deployment from the cavity, wherein the distal end of the insertion member (330, 500) further defines a window (340, 503) in the arcuate surface forming the cavity adapted from viewing of anatomical structures on a side of the insertion member (330, 500) opposite the probe tool (342, 362, 372, 382).
Component comprising: - a substrate having a first cavity and a second cavity; - wherein a first micromechanical structure is arranged in the first cavity; - wherein a second micromechanical structure is arranged in the second cavity; - wherein the first cavity has a first gas pressure; - wherein the second cavity has a second gas pressure; - wherein the first gas pressure is provided by closing off the first cavity; - wherein a first channel opens into the second cavity, and the second gas pressure is adjustable via the first channel; and - the second gas pressure is different from the first gas pressure, characterized in that the second micromechanical structure, arranged in the second cavity, can be closed off at the wafer level by means of a wafer bonding method. - a substrate having a first cavity and a second cavity; - wherein a first micromechanical structure is arranged in the first cavity; - wherein a second micromechanical structure is arranged in the second cavity; - wherein the first cavity has a first gas pressure; - wherein the second cavity has a second gas pressure; - wherein the first gas pressure is provided by closing off the first cavity; - wherein a first channel opens into the second cavity, and the second gas pressure is adjustable via the first channel; and - the second gas pressure is different from the first gas pressure,
A steering column, comprising a steering shaft, a fixing bracket, a first cylinder, a second cylinder, an angle adjustment motor, an angle adjustment screw-nut assembly, a linkage assembly, a height adjustment motor, and a height adjustment screw-nut assembly, wherein the second cylinder is arranged in the first cylinder and is slidably sleeved with the first cylinder, the steering shaft runs through the first cylinder and the second cylinder, the steering shaft comprises an upper shaft and a lower shaft that are in splined connection, the upper shaft is supported in the second cylinder through a first bearing, the lower shaft is supported in the first cylinder through a second bearing, the first cylinder is hinged to the fixing bracket around a first hinge axis (A-A), the angle adjustment motor can drive, through the angle adjustment screw-nut assembly and the linkage assembly, the first cylinder to rotate relative to the fixing bracket, and the height adjustment motor can drive, through the height adjustment screw-nut assembly, the second cylinder to axially move relative to the first cylinder; characterized in that the steering column further comprises an angle adjustment motor base, the angle adjustment motor is fixed on the angle adjustment motor base, the angle adjustment motor base is hinged to the first cylinder around a third hinge axis (C-C), and the third hinge axis (C-C) is parallel to the first hinge axis (A-A).
A blade for a gas turbine engine, the blade characterised in that it comprises a root section having a hollow cavity, a core being positioned in the cavity, the core comprising at least two frangible parts with a shear surface between them whereby the core remains stable other than under a predetermined tension load in a plane of the root section.
An in vitro Or method for identifying a compound that modulates sterile inflammation through the modulation of the interaction of FHR1 with EMR2/ADGRE2 in a cell, comprising the steps of a) contacting at least one of FHR1, an EMR2/ADGRE2 binding fragment of FHR1, a cell expressing FHR1, and/or a cell expressing an EMR2/ADGRE2 binding fragment of FHR1 with at least one compound that potentially modulates the interaction of FHR1 with EMR2/ADGRE2 in a cell b) identifying a modulation of the binding of FHR1 or said fragment to EMR2/ADGRE2 in the presence of said at least one compound, and c) identifying a compound as identified in step b) as specifically modulating sterile inflammation. a) contacting at least one of FHR1, an EMR2/ADGRE2 binding fragment of FHR1, a cell expressing FHR1, and/or a cell expressing an EMR2/ADGRE2 binding fragment of FHR1 with at least one compound that potentially modulates the interaction of FHR1 with EMR2/ADGRE2 in a cell b) identifying a modulation of the binding of FHR1 or said fragment to EMR2/ADGRE2 in the presence of said at least one compound, and c) identifying a compound as identified in step b) as specifically modulating sterile inflammation.
A system (100, 200) for performing one or more tasks on a lightning protection system of a wind turbine, the system (100, 200) comprising: a cable having a first end attached to an up-tower anchor point, the cable extending toward a tower support surface such that a lightning receptor of the LPS is generally disposed between the up-tower anchor point and the tower support surface; a robotic testing device (102, 140, 150, 160, 170) comprising: an attachment mechanism configured for positioning about at least a portion of an outer perimeter of a rotor blade of the wind turbine and clamp thereto the rotor blade; and a LPS test probe coupled to a robotic end effector, wherein the robotic end effector is moveable to position the LPS test probe in contact with the lightning receptor of the LPS; one or more tag lines coupled to the robotic testing device (102, 140, 150, 160, 170); and a remote monitoring and control interface operable to remotely clamp the robotic testing device (102, 140, 150, 160, 170) to the rotor blade and perform the one or more LPS inspection tests, wherein the cable (!08) is coupled to the up-tower anchor point such that, the robotic testing device (102, 140, 150, 160, 170) is movable to a position at which the LPS test probe contacts the lightning receptor. a cable having a first end attached to an up-tower anchor point, the cable extending toward a tower support surface such that a lightning receptor of the LPS is generally disposed between the up-tower anchor point and the tower support surface; a robotic testing device (102, 140, 150, 160, 170) comprising: an attachment mechanism configured for positioning about at least a portion of an outer perimeter of a rotor blade of the wind turbine and clamp thereto the rotor blade; and a LPS test probe coupled to a robotic end effector, wherein the robotic end effector is moveable to position the LPS test probe in contact with the lightning receptor of the LPS; an attachment mechanism configured for positioning about at least a portion of an outer perimeter of a rotor blade of the wind turbine and clamp thereto the rotor blade; and a LPS test probe coupled to a robotic end effector, wherein the robotic end effector is moveable to position the LPS test probe in contact with the lightning receptor of the LPS; one or more tag lines coupled to the robotic testing device (102, 140, 150, 160, 170); and a remote monitoring and control interface operable to remotely clamp the robotic testing device (102, 140, 150, 160, 170) to the rotor blade and perform the one or more LPS inspection tests, wherein the cable (!08) is coupled to the up-tower anchor point such that, the robotic testing device (102, 140, 150, 160, 170) is movable to a position at which the LPS test probe contacts the lightning receptor.
An interleaving method performed by a transmitter for a communication system with spatial multiplexing over T transmit antennas employing quasi-cyclic low-density parity-check codes, T being an integer greater than 1, the interleaving method being used for applying bit permutation to bits of a codeword of a quasi-cyclic low-density parity-check code in order to generate a plurality of constellation words of one or more spatial-multiplexing blocks from the codeword, the codeword consisting of N cyclic blocks, and each cyclic block consisting of Q bits, each of the one or more spatial-multiplexing blocks consisting of B bits and consisting of T constellation words, wherein the T constellation words are simultaneously transmitted over the T transmit antennas, each constellation word indicating one of a plurality of constellation points of a predefined constellation used for constellation mapping of the constellation word, the bits of each constellation word being divisible into pairs of bits having the same robustness, characterized in that the interleaving method comprises the step of applying the bit permutation to the bits of the codeword such that: each of the one or more spatial-multiplexing blocks is made up of bits from B/2 different cyclic-blocks; each constellation word of the one or more spatial-multiplexing blocks is made up of bits from Bt/2 different cyclic blocks, Bt being the number of bits of the constellation word; and each of said pairs of bits having the same robustness of the constellation word is made up of bits from a common one of the Bt/2 different cyclic blocks. each of the one or more spatial-multiplexing blocks is made up of bits from B/2 different cyclic-blocks; each constellation word of the one or more spatial-multiplexing blocks is made up of bits from Bt/2 different cyclic blocks, Bt being the number of bits of the constellation word; and each of said pairs of bits having the same robustness of the constellation word is made up of bits from a common one of the Bt/2 different cyclic blocks.
A hydraulic system for an aircraft, the hydraulic system comprising: a flight control member, a hydraulic actuator that is operatively coupled to the flight control member; an engine driven pump that delivers hydraulic fluid to the actuator at a first pressure; characterized in that the system further comprises a boost pump that delivers hydraulic fluid to the actuator at a second pressure that is higher than the first pressure; wherein hydraulic fluid returning from the actuator to the engine driven pump is delivered to the boost pump prior to reaching the engine driven pump. a flight control member, a hydraulic actuator that is operatively coupled to the flight control member; an engine driven pump that delivers hydraulic fluid to the actuator at a first pressure; characterized in that the system further comprises a boost pump that delivers hydraulic fluid to the actuator at a second pressure that is higher than the first pressure; wherein hydraulic fluid returning from the actuator to the engine driven pump is delivered to the boost pump prior to reaching the engine driven pump.