mhurhangee/patent-ind-claim-en huggingface dataset:
A cleaning system for a heat exchanger, adapted to generate supersonic shock waves from a gas and project the same against the surface of the exchanger, said system being characterised in that it comprises at least one cleaning device comprising a high pressure first chamber to be fluidly connected to a pressurised gas tank to supply said high pressure first chamber with gas, a low pressure second chamber comprising a port for exhausting the shock wave , and a trigger device reversibly actuatable between a closing position preventing fluid communication between said first and second chambers , and an opening position placing said chambers in fluid communication, the opening speed of the trigger device being, when using this system, greater than or equal to 1.5 m 2 per second.
Heat flux sensor comprising: a body with six or more sensor pairs, each pair consisting of one radiation absorbing, absorptive, sensor for measuring a combined radiative and convective heat flux and one radiation reflecting, reflective, sensor for substantially measuring a convective heat flux, the body exhibiting three axes of heat flux measurement, the axes being substantially perpendicular, with two sensor pairs per axis facing substantially in opposite directions, a heating member that is in heat conducing contact with the body, capable of heating the body uniformly within 2 °C for body temperatures between 25 and 40 °C at ambient air temperatures between 20 and 25 °C at air speeds < 1 m/s and a temperature sensor thermally coupled with the body for measuring the body temperature T sen . a body with six or more sensor pairs, each pair consisting of one radiation absorbing, absorptive, sensor for measuring a combined radiative and convective heat flux and one radiation reflecting, reflective, sensor for substantially measuring a convective heat flux, the body exhibiting three axes of heat flux measurement, the axes being substantially perpendicular, with two sensor pairs per axis facing substantially in opposite directions, a heating member that is in heat conducing contact with the body, capable of heating the body uniformly within 2 °C for body temperatures between 25 and 40 °C at ambient air temperatures between 20 and 25 °C at air speeds < 1 m/s and a temperature sensor thermally coupled with the body for measuring the body temperature T sen .
A roller blind structure, comprising a casing made up of a plurality of side walls that define an inner chamber intended to incorporate drive means therein linked to a blind or similar, and guide profiles able to be located at opposite ends of the casing , which are configured to guide the blind or similar, the guide profiles being intended to extend in a downward direction with respect to the positioning of the casing , including an attachment system to attach each one of the guide profiles and the casing , in that the attachment system is provided with a first interconnection member able to be coupled to an end of the casing by means of fixing means and a connector member able to be coupled to the first interconnection member by means of first releasable quick-fit means and able to be coupled to a respective guide profile by means of second releasable quick-fit means, and wherein the first releasable quick-fit means consist of a flexible retaining flange able to be fitted in a housing having shapes and dimensions complementary to the retaining flange, the housing being made in an upper region of the connector member , characterised in that the second releasable quick-fit means consist of a male extension able to be coupled to a female region present in the guide profile .
A multi-well fluorescence standard , comprising: a cured and solidified adhesive ; a selected quantity of substantially non-photobleaching fluorescent quantum dots dispersed in the adhesive ; and a multi-well format plate having a plurality of sample wells , wherein at least one sample well of the multi-well format plate has a selected quantity of the adhesive and the quantum dots disposed therein; wherein the quantum dots are in a colloidal suspension within the adhesive and are evenly suspended in the adhesive. a cured and solidified adhesive ; a selected quantity of substantially non-photobleaching fluorescent quantum dots dispersed in the adhesive ; and a multi-well format plate having a plurality of sample wells , wherein at least one sample well of the multi-well format plate has a selected quantity of the adhesive and the quantum dots disposed therein; wherein the quantum dots are in a colloidal suspension within the adhesive and are evenly suspended in the adhesive.
A beverage composition comprising collagen and vitamin C, or a derivative thereof and methyl sulphonyl methane, wherein said collagen is present in an amount between about 2 and about 10 g/100 ml and said vitamin C, or derivative thereof, is present in an amount between about 50 and about 400 mg/100 ml, and the weight ratio of collagen to vitamin C is between about 10:1 and about 50:1, and said methyl sulphonyl methane is present in an amount between about 300 and about 800 mg/100 mL.
A process for forming an asymmetric hollow fiber carbon membrane using precursor pre-treatment comprising: providing an aromatic imide polymer precursor; pre-treating at least a portion of the polymer precursor by contacting the polymer precursor with a modifying agent comprising a silane having the formula R 1 R 2 R 3 R 4 Si, where each of R 1 , R 2 , R 3 , and R 4 are independently vinyl, C 1 -C 6 alkyl, -O-alkyl, or halide, with the proviso that the silane contain at least one vinyl group and at least one -O-alkyl or halide; and subjecting the pre-treated polymer precursor to pyrolysis; wherein the step of pre-treating at least a portion of the polymer precursor provides at least a 300% increase in the gas permeance of the carbon membrane in contrast to the carbon membrane without precursor pre-treatment, measured with pure at 689 kPa (100 psia) and 35 °C. providing an aromatic imide polymer precursor; pre-treating at least a portion of the polymer precursor by contacting the polymer precursor with a modifying agent comprising a silane having the formula R 1 R 2 R 3 R 4 Si, where each of R 1 , R 2 , R 3 , and R 4 are independently vinyl, C 1 -C 6 alkyl, -O-alkyl, or halide, with the proviso that the silane contain at least one vinyl group and at least one -O-alkyl or halide; and subjecting the pre-treated polymer precursor to pyrolysis; wherein the step of pre-treating at least a portion of the polymer precursor provides at least a 300% increase in the gas permeance of the carbon membrane in contrast to the carbon membrane without precursor pre-treatment, measured with pure at 689 kPa (100 psia) and 35 °C.
Process for the dehydration of at least one oxygenated compound, preferably selected from saturated alcohols, unsaturated alcohols, diols, ethers, comprising feeding to a reactor including at least a first catalytic bed comprising silica (SiO 2 ), or at least a first catalytic bed comprising at least one catalyst for the dissociation of ammonia (NH 3 ) selected from catalysts comprising silica (SiO 2 ), preferably at least a first catalytic bed comprising silica (SiO 2 ), and at least a second catalytic bed comprising at least one dehydration catalyst selected from cerium oxide (CeO 2 ), aluminum oxide (γ-Al 2 O 3 ), aluminium silicate, silica-aluminas (SiO 2 -Al 2 O 3 ), aluminas, zeolites, sulfonate resins, ion exchange resins, metal oxides (such as lanthanum oxide, zirconium oxide, tungsten oxide, thallium oxide, magnesium oxide, zinc oxide), a mixture comprising said at least one oxygenated compound and at least one basic agent selected from ammonia (NH 3 ), or from inorganic or organic compounds containing nitrogen capable of developing ammonia (NH 3 ) during said dehydration process, said mixture being fed to said reactor so as to pass first through said first catalytic bed and subsequently through said second catalytic bed.
Aircraft light for a foldable wing tip of an aircraft , comprising: a first lighting structure , comprising at least one first light source and a first optical system , with the at least one first light source and the first optical system in operation generating a first light output, a second lighting structure , comprising at least one second light source and a second optical system , with the at least one second light source and the second optical system in operation generating a second light output, wherein the aircraft light is an aircraft navigation light , and the first light output is a first navigation light output and the second light output is a second navigation light output, wherein the first light output and the second light output are of the same color, characterised in that the first light output and the second light output are angled with respect to each other such that the aircraft navigation light is able to provide lateral emission of a navigation light output, both when the foldable wing tip is in a folded up position and when the foldable wing tip is in a laterally extending position, and the aircraft light is configured to control the at least one first light source and the at least one second light source depending on a wing tip orientation signal, which is indicative of an orientation of the foldable wing tip . a first lighting structure , comprising at least one first light source and a first optical system , with the at least one first light source and the first optical system in operation generating a first light output, a second lighting structure , comprising at least one second light source and a second optical system , with the at least one second light source and the second optical system in operation generating a second light output, wherein the aircraft light is an aircraft navigation light , and the first light output is a first navigation light output and the second light output is a second navigation light output, wherein the first light output and the second light output are of the same color, characterised in that the first light output and the second light output are angled with respect to each other such that the aircraft navigation light is able to provide lateral emission of a navigation light output, both when the foldable wing tip is in a folded up position and when the foldable wing tip is in a laterally extending position, and the aircraft light is configured to control the at least one first light source and the at least one second light source depending on a wing tip orientation signal, which is indicative of an orientation of the foldable wing tip .
Safety switch arrangement for a power connector of a personal care appliance , the arrangement comprising: - a housing portion , - a power connector unit comprising a connector receptacle , - an operating switch , and - an actuation portion , wherein the actuation portion is mounted to the housing portion and arranged to be moved between a first state and a second state, wherein the power connector unit is arranged at the housing portion , wherein the actuation portion , in the first state, enables an operation of the personal care appliance and prevents a contact with the connector receptacle , wherein the operating switch is switched on by the actuation portion in the first state, and wherein the actuation portion , in the second state, prevents an operation of the personal care appliance and enables a contact with the connector receptacle , wherein the actuation portion blocks an access for a connector plug to the connector receptacle in the first state by at least partially covering an insertion recess of the connector receptacle in the first state, and wherein the actuation portion enables an access for a connector plug to the connector receptacle in the second state. - a housing portion , - a power connector unit comprising a connector receptacle , - an operating switch , and - an actuation portion ,
A method for reestablishing and recovering a Long Term Evolution, LTE-based, trunking communication system, characterized by comprising: monitoring, by a user terminal, first resource configuration information of a serving cell where the user terminal is located and second resource configuration information of a neighbor cell which are issued by a network side, configuring the user terminal according to the first resource configuration information to allow access of the user terminal serving as a trunking listening user, and storing the second resource configuration information (S10); establishing, by the user terminal, a Radio Resource Control, RRC, link and a service bearer with the network side to allow access of the user terminal serving as a trunking speaking user and a LTE service user (S20); selecting, when the user terminal detects abnormality of a radio link, one cell as a target cell from the serving cell where the user terminal is located and the neighbor cell, and sending, by the user terminal, a reestablishment request to the target cell, such that when receiving the reestablishment request, the target cell initiates a reestablishment process according to the reestablishment request to recover a LTE service or both of a LTE service and a trunking speaking user service, and recover a trunking listening user service according to the second resource configuration information (S30). monitoring, by a user terminal, first resource configuration information of a serving cell where the user terminal is located and second resource configuration information of a neighbor cell which are issued by a network side, configuring the user terminal according to the first resource configuration information to allow access of the user terminal serving as a trunking listening user, and storing the second resource configuration information (S10); establishing, by the user terminal, a Radio Resource Control, RRC, link and a service bearer with the network side to allow access of the user terminal serving as a trunking speaking user and a LTE service user (S20); selecting, when the user terminal detects abnormality of a radio link, one cell as a target cell from the serving cell where the user terminal is located and the neighbor cell, and sending, by the user terminal, a reestablishment request to the target cell, such that when receiving the reestablishment request, the target cell initiates a reestablishment process according to the reestablishment request to recover a LTE service or both of a LTE service and a trunking speaking user service, and recover a trunking listening user service according to the second resource configuration information (S30).
A magnet actuator for use in an electronic device , said magnet actuator comprising - a coil , - a magnet , - a first housing and a second housing , said coil being at least partially located within, and fixed to, said first housing , said magnet being at least partially located within, and fixed to, said second housing , said first housing comprising a magnetic material, a magnetic field, generated by said magnet and said first housing causing an attractive force (F) between said magnet and said first housing , said magnet and said first housing being in a force equilibrium state, wherein an air gap is provided between said magnet and said coil , and wherein manipulating electrical current in said coil causes a change in said attractive force (F), thereby causing a displacement between said magnet and said first housing , the magnet actuator further comprising at least one compressible spacer , said spacer being arranged to maintain said magnet and said first housing in a force equilibrium state by acting as a counterforce to the force (F) caused by said magnetic field, characterized in that said spacer interconnects said first housing and said magnet . - a coil , - a magnet , - a first housing and a second housing , said coil being at least partially located within, and fixed to, said first housing , said magnet being at least partially located within, and fixed to, said second housing , said first housing comprising a magnetic material, a magnetic field, generated by said magnet and said first housing causing an attractive force (F) between said magnet and said first housing , said magnet and said first housing being in a force equilibrium state, wherein an air gap is provided between said magnet and said coil , and wherein manipulating electrical current in said coil causes a change in said attractive force (F), thereby causing a displacement between said magnet and said first housing , the magnet actuator further comprising at least one compressible spacer , said spacer being arranged to maintain said magnet and said first housing in a force equilibrium state by acting as a counterforce to the force (F) caused by said magnetic field, characterized in that said spacer interconnects said first housing and said magnet .
A spinal implant , comprising: a body extending in direction at least substantially along a body axis , between a first end portion and a second end portion ; a first bearing surface disposed relative to the first end portion , and defining a first relief pattern that is configured to inhibit movement of the spinal implant relative to one or more vertebrae in at least substantially all directions wherein the plurality of protrusions each have an at least generally conical shape, and each defining a base integrally connected to the first bearing surface , and a tip at a distal end of the respective protrusion wherein the plurality of protrusions are oriented in a plurality of different directions relative to the body axis . a body extending in direction at least substantially along a body axis , between a first end portion and a second end portion ; a first bearing surface disposed relative to the first end portion , and defining a first relief pattern that is configured to inhibit movement of the spinal implant relative to one or more vertebrae in at least substantially all directions wherein the plurality of protrusions each have an at least generally conical shape, and each defining a base integrally connected to the first bearing surface , and a tip at a distal end of the respective protrusion wherein the plurality of protrusions are oriented in a plurality of different directions relative to the body axis .
A motor comprising: a stator including a stator core and teeth respectively protruding from the stator core in predetermined directions of protrusion; and coils respectively wound onto the teeth n (n is an integer of 3 or greater) turns including first to n-th turns in a concentrated manner, characterized in that a k-th (k is an integer, 1 < k < n) turn of each of the coils is defined as a center turn among the first to n-th turns, and when each of the coils is cut in a corresponding one of the predetermined directions of protrusion of the teeth, each of the first turn and the n-th turn is greater in cross-sectional area than the k-th turn. a stator including a stator core and teeth respectively protruding from the stator core in predetermined directions of protrusion; and coils respectively wound onto the teeth n (n is an integer of 3 or greater) turns including first to n-th turns in a concentrated manner, characterized in that a k-th (k is an integer, 1 < k < n) turn of each of the coils is defined as a center turn among the first to n-th turns, and when each of the coils is cut in a corresponding one of the predetermined directions of protrusion of the teeth, each of the first turn and the n-th turn is greater in cross-sectional area than the k-th turn.
A method comprising: a joint modulation controller of a transmitter receiving at least one operating condition parameter of the transmitter, channel state information, and channel rank information; the joint modulation controller determining at least one diversity order and antenna selection factor based on the received at least one operating condition parameter; receiving as input at the transmitter a set of information bits; dividing the set of information bits into a plurality of groups, wherein at least one group is either a signal space keying group or a radiation pattern/polarization group having a size limited by the diversity order determined by the joint modulation controller; mapping a first group to a plurality of signal space based modulation formats; mapping the at least one group and each other group to a control signal for a configurable feature of a transmitter system; generating and modulating a plurality of base signals according to the mapping of the first group onto the modulation format, each of the plurality of base signals generated by a selected number of transmit radio frequency chains using spatial multiplexing, the selected number of transmit radio frequency chains being based on the channel rank information; configuring at least one configurable feature of a configurable antenna of the transmitter system based on the control signal; and transmitting the modulated signal from the configured at least one configurable antenna. a joint modulation controller of a transmitter receiving at least one operating condition parameter of the transmitter, channel state information, and channel rank information; the joint modulation controller determining at least one diversity order and antenna selection factor based on the received at least one operating condition parameter; receiving as input at the transmitter a set of information bits; dividing the set of information bits into a plurality of groups, wherein at least one group is either a signal space keying group or a radiation pattern/polarization group having a size limited by the diversity order determined by the joint modulation controller; mapping a first group to a plurality of signal space based modulation formats; mapping the at least one group and each other group to a control signal for a configurable feature of a transmitter system; generating and modulating a plurality of base signals according to the mapping of the first group onto the modulation format, each of the plurality of base signals generated by a selected number of transmit radio frequency chains using spatial multiplexing, the selected number of transmit radio frequency chains being based on the channel rank information; configuring at least one configurable feature of a configurable antenna of the transmitter system based on the control signal; and transmitting the modulated signal from the configured at least one configurable antenna.
A method for differentiating mesenchymal stem cells into neurons, comprising the steps of: (a) adding an Ecklonia cava extract to a cell culture medium; (b) dedifferentiating mesenchymal stem cells into induced pluripotent stem cells in the medium; and (c) differentiating the induced pluripotent stem cells into neurons. (a) adding an Ecklonia cava extract to a cell culture medium; (b) dedifferentiating mesenchymal stem cells into induced pluripotent stem cells in the medium; and (c) differentiating the induced pluripotent stem cells into neurons.