mhurhangee/patent-ind-claim-en huggingface dataset:
Plug-in device for an arrangement for displaying merchandise, having a socket , which can be mounted on a supporting structure , and a plug-in part , which is separate from the socket , wherein the plug-in part has a plug-in portion which can be plugged into a receptacle of the socket in a plug-in direction along a plug-in axis until a connected state of the plug-in device is reached, with the result that, in the connected state, the plug-in part and the socket are releasably connected to each other, wherein the plug-in portion has an end region and an outer lateral region , and wherein the receptacle of the socket has an end region , which is situated at the front in the plug-in direction, and an inner lateral region , wherein, in the connected state, the lateral region of the plug-in portion and the lateral region of the receptacle come into contact with each other, wherein an electrification arrangement is provided in order, in the connected state of the plug-in device , to supply electrical power to an electrical load via the plug-in device , wherein, for supplying electrical power, an electrical connection is established via the socket and the plug-in part by way of electrically conductive contact being established by galvanic contacting between a first contact point of a contact portion of the electrification arrangement on the socket and a second contact point of a contact portion of the electrification arrangement on the plug-in portion , wherein the first contact point is formed on the socket in the lateral region of the receptacle , and in that the second contact point is formed on the plug-in portion in the lateral region of the plug-in portion , with the result that, in the connected state, the first contact point in the lateral region of the socket and the second contact point in the lateral region of the plug-in portion are electrically contacted with each other, wherein the contact portion of the electrification arrangement on the socket has two spaced-apart first contact points , and the contact portion of the electrification arrangement on the plug-in portion has two spaced-apart second contact points , wherein a first contact point and a second contact point , which are connected to each other, belong to a common electrical pole, wherein the contact points are situated radially opposite each other with respect to the plug-in axis, characterized in that an outwardly open opening is present in the lateral region of the receptacle , wherein, in the connected state of the plug-in device , the galvanic contacting of the first contact point with the second contact point is established via the opening , wherein the opening in the lateral region of the receptacle is present in an associated wall portion which encloses the receptacle .
A deformable heating element, comprising at least one heating conductor which is laid and fastened on a flat base material at the one side thereof, called front-side layer , wherein the base material is divided into a front-side layer and a rear-side layer which connects the front-side layer on the side opposite the heat conductor , wherein the front-side layer on which the heating conductor is laid and fastened has a lower compression hardness and/or volume density than in the area of the opposite rear-side layer , characterized in that in comparison with the rear-side layer the front-side layer occupies a volume that is 50 to100% greater at the same volume weight.
An articulated tracked vehicle (IV) comprising a first vehicle unit and a second vehicle unit controllably connected by means of a control member , wherein the first vehicle unit comprises a combustion engine , wherein the combustion engine is arranged to drive a generator for electric generation, wherein the generator is arranged to transfer power via power electronic means to at least one electric motor (401; 403) of at least one electric propulsion unit (400a-b), wherein transmission of power between said vehicle units is arranged to be effected only electrically, characterized in that the vehicle has an electric motor per vehicle unit, wherein the vehicle has an electric motor per pair of first and second, and third and fourth drive shaft (6a-b, 6c-d) respectively, wherein the respective electric motor is arranged to drive a shaft running in the longitudinal direction of the vehicle.
A gas turbine engine system , comprising: a nacelle ; a fan casing within the nacelle ; and a fan section within said fan casing , said fan section including multiple airfoils ; a variable area fan nozzle ; and a controller that is operable to move said variable area fan nozzle to influence a discharge airflow area associated with said variable area fan nozzle ; characterised by further comprising a gear train configured to reduce the speed of the fan section ; a sensor which detects a flutter condition of said airfoils , said sensor being configured to detect an arrival time at which each of said multiple of airfoils passes said sensor during operation of said fan section ; and in that: the controller communicates with said sensor , and is operable to move said variable area fan nozzle to influence the discharge airflow area associated with said variable area fan nozzle in response to the detection of said airfoil flutter condition, said controller being programmed to differentiate between which of said arrival times correlate to said airfoil flutter condition and which of said arrival times correlate to an airfoil non-flutter condition. a nacelle ; a fan casing within the nacelle ; and a fan section within said fan casing , said fan section including multiple airfoils ; a variable area fan nozzle ; and a controller that is operable to move said variable area fan nozzle to influence a discharge airflow area associated with said variable area fan nozzle ; characterised by further comprising a gear train configured to reduce the speed of the fan section ; a sensor which detects a flutter condition of said airfoils , said sensor being configured to detect an arrival time at which each of said multiple of airfoils passes said sensor during operation of said fan section ; and in that: the controller communicates with said sensor , and is operable to move said variable area fan nozzle to influence the discharge airflow area associated with said variable area fan nozzle in response to the detection of said airfoil flutter condition, said controller being programmed to differentiate between which of said arrival times correlate to said airfoil flutter condition and which of said arrival times correlate to an airfoil non-flutter condition.
A wind turbine blade for a rotor of a wind turbine having a substantially horizontal rotor shaft and a hub connected to the rotor shaft, the blade extending in a substantially radial direction from the hub , when mounted to the hub , wherein the blade comprises: - a profiled contour comprising a pressure side and a suction side and a leading edge and a trailing edge connecting the pressure side and the suction side, - a lift regulating device comprising one or more surface mounted flaps , and - an operation device comprising an electromagnet configured to operate the lift regulating device between a first state and a second state, and - the lift regulating device comprises a magnetisable material, characterised in that - the operation device is not mechanically engaged with the surface mounted flap(s) . - a profiled contour comprising a pressure side and a suction side and a leading edge and a trailing edge connecting the pressure side and the suction side, - a lift regulating device comprising one or more surface mounted flaps , and - an operation device comprising an electromagnet configured to operate the lift regulating device between a first state and a second state, and - the lift regulating device comprises a magnetisable material, characterised in that - the operation device is not mechanically engaged with the surface mounted flap(s) .
An unmanned aerial system for transporting and delivering packages (P i B j D k ), comprising: - at least one unmanned motorized aircraft (D k ), - at least one non-motorized aerostatic device (B j ) having aerostatic lift and being able to be coupled to said at least one motorized aircraft, said at least one motorized aircraft and said at least one non-motorized aerostatic device cooperating to transport at least one package (P i ) from a take-off site to a delivery site , characterized in that said at least one aerostatic device (B j ) (i) is made up of j aerostatic modules each having a predetermined modular aerostatic lift and secured therebetween by coupling means, so that said at least one aerostatic device (B j ) has a static lift substantially greater than or equal to the overall weight of the package (P i ) to be transported and of said aerostatic device (B j ), said j aerostatic modules being adapted to be delivered on demand by a site for storing and distributing aerostatic modules (B), said storage and distribution site being located close to the take-off site . - at least one unmanned motorized aircraft (D k ), - at least one non-motorized aerostatic device (B j ) having aerostatic lift and being able to be coupled to said at least one motorized aircraft, said at least one motorized aircraft and said at least one non-motorized aerostatic device cooperating to transport at least one package (P i ) from a take-off site to a delivery site , characterized in that said at least one aerostatic device (B j ) (i) is made up of j aerostatic modules each having a predetermined modular aerostatic lift and secured therebetween by coupling means, so that said at least one aerostatic device (B j ) has a static lift substantially greater than or equal to the overall weight of the package (P i ) to be transported and of said aerostatic device (B j ), said j aerostatic modules being adapted to be delivered on demand by a site for storing and distributing aerostatic modules (B), said storage and distribution site being located close to the take-off site .
A device for unitary dosage of tablets or pills, characterized in that it comprises: - a hollow body ; - a container housed in the hollow body configured to house tablets or pills, the container comprising an outlet channel through which the tablets or pills exit said container ; - a rotation mechanism connected to the container and configured to make the same rotate; - a dispensing mechanism connected to the hollow body and operatively connected to the rotation mechanism , configured to house and dispense a tablet or pill, as well as to actuate the rotation mechanism ; and - stirring means , connected to the hollow body and to the container ; such that the actuation of the dispensing mechanism causes the rotation of the container by means of the rotation mechanism , the tablets or pills being stirred by the operative combination of the rotation of the stirring means ; and wherein the actuation of the dispensing mechanism dispenses a tablet or pill and/or houses another to be dispensed. - a hollow body ; - a container housed in the hollow body configured to house tablets or pills, the container comprising an outlet channel through which the tablets or pills exit said container ; - a rotation mechanism connected to the container and configured to make the same rotate; - a dispensing mechanism connected to the hollow body and operatively connected to the rotation mechanism , configured to house and dispense a tablet or pill, as well as to actuate the rotation mechanism ; and - stirring means , connected to the hollow body and to the container ; such that the actuation of the dispensing mechanism causes the rotation of the container by means of the rotation mechanism , the tablets or pills being stirred by the operative combination of the rotation of the stirring means ; and wherein the actuation of the dispensing mechanism dispenses a tablet or pill and/or houses another to be dispensed.
A process for processing VxLAN data units in an environment that includes an operating system configured for processing VxLAN data units, and a fast path environment dedicated to processing incoming packets arriving on an inbound interface, wherein the fast path environment is configured for receiving incoming VxLAN data units and is capable of processing such VxLAN data units, the process comprising: • obtaining VxLAN processing configuration parameters used by the operating system, wherein the obtained parameters comprise a VxLAN forward table; • configuring the fast path environment for processing received VxLAN data units based on the obtained parameters; and • selecting, at the fast path environment, at least one received VxLAN data unit for processing by the operating system outside of the fast path environment. • obtaining VxLAN processing configuration parameters used by the operating system, wherein the obtained parameters comprise a VxLAN forward table; • configuring the fast path environment for processing received VxLAN data units based on the obtained parameters; and • selecting, at the fast path environment, at least one received VxLAN data unit for processing by the operating system outside of the fast path environment.
A method for manufacturing an aerodynamic seal for fixed or mobile aerodynamic surfaces in aircrafts or a combination of both, of complex geometry comprising the steps of: selecting a material from the family of vulcanised thermoplastic elastomers suitable for the requirements to be met by aerodynamic seals and for additive manufacturing by means of 3D printing; designing the aerodynamic seal that enables manufacturing by means of the 3D printing technique and the selected material; selecting the manufacturing parameters for the aerodynamic seal design carried out and material selected; manufacturing the aerodynamic seal using the selected material, design and manufacturing parameters, by means of additive manufacturing by means of 3D printing; the method being characterised in that it further comprises the steps of: heat treatment of the aerodynamic seal manufactured according to the preceding steps, wherein the aerodynamic seal is subjected to a heat treatment in a climatic chamber consisting of a preheating cycle, introduction of the seal into the chamber, maintenance at a temperature equal to or less than 200 °C and cooling to room temperature, and mechanical shaping to obtain the final geometry of the aerodynamic seal in accordance with the dimensional and assembly requirements that apply thereto. selecting a material from the family of vulcanised thermoplastic elastomers suitable for the requirements to be met by aerodynamic seals and for additive manufacturing by means of 3D printing; designing the aerodynamic seal that enables manufacturing by means of the 3D printing technique and the selected material; selecting the manufacturing parameters for the aerodynamic seal design carried out and material selected; manufacturing the aerodynamic seal using the selected material, design and manufacturing parameters, by means of additive manufacturing by means of 3D printing; the method being characterised in that it further comprises the steps of: heat treatment of the aerodynamic seal manufactured according to the preceding steps, wherein the aerodynamic seal is subjected to a heat treatment in a climatic chamber consisting of a preheating cycle, introduction of the seal into the chamber, maintenance at a temperature equal to or less than 200 °C and cooling to room temperature, and mechanical shaping to obtain the final geometry of the aerodynamic seal in accordance with the dimensional and assembly requirements that apply thereto. heat treatment of the aerodynamic seal manufactured according to the preceding steps, wherein the aerodynamic seal is subjected to a heat treatment in a climatic chamber consisting of a preheating cycle, introduction of the seal into the chamber, maintenance at a temperature equal to or less than 200 °C and cooling to room temperature, and mechanical shaping to obtain the final geometry of the aerodynamic seal in accordance with the dimensional and assembly requirements that apply thereto.
A process for producing a resist solvent for producing electronic parts or a rinsing liquid for producing electronic parts consisting of an organic acid ester-type liquid containing an organic peroxide at a peroxide-value (POV) of 0.5 mmoL/kg or less, measured in accordance with ISO 3960:2007 fourth edition, 9968, said process comprising contacting an organic peroxide-containing organic acid ester-type liquid with a platinum group metal catalyst carried on a synthetic resin to remove said organic peroxide from said organic acid ester-type liquid.
A microwave coupler/combiner device for coupling and combining at least two microwave sources , comprising a waveguide provided with: - a sleeve extending longitudinally along a main axis (X) and having two opposite ends comprising a first end provided with a short-circuit element and an open second end ; and - at least one transverse bar (3a; 3b; 3c; 3d) extending inside the sleeve along a transverse axis (Y) orthogonal to the main axis (X); said microwave coupler/combiner device further comprising at least two coaxial connectors (4a; 4b; 4c; 4d) provided to be respectively connected to microwave sources , wherein each coaxial connector (4a; 4b; 4c; 4d) is externally mounted on the sleeve and has a central conductive core connected to and extended by a conductive antenna extending inside the sleeve and ending by an end, which end of the conductive antenna being fixed on a transverse bar (3a; 3b; 3c; 3d), wherein said central conductive core and said conductive antenna are aligned and extend in a direction orthogonal to the transverse axis (Y) and to the main axis (X); and wherein the at least two coaxial connectors comprise two contiguous coaxial connectors (4a; 4b; 4c; 4d) whose conductive antennas are fixed on a same transverse bar (3a; 3b; 3c; 3d), said contiguous coaxial connectors (4a; 4b; 4c; 4d) being disposed side by side in a direction parallel to the transverse axis (Y) of the transverse bar (3a; 3b; 3c; 3d). - a sleeve extending longitudinally along a main axis (X) and having two opposite ends comprising a first end provided with a short-circuit element and an open second end ; and - at least one transverse bar (3a; 3b; 3c; 3d) extending inside the sleeve along a transverse axis (Y) orthogonal to the main axis (X); said microwave coupler/combiner device further comprising at least two coaxial connectors (4a; 4b; 4c; 4d) provided to be respectively connected to microwave sources , wherein each coaxial connector (4a; 4b; 4c; 4d) is externally mounted on the sleeve and has a central conductive core connected to and extended by a conductive antenna extending inside the sleeve and ending by an end, which end of the conductive antenna being fixed on a transverse bar (3a; 3b; 3c; 3d), wherein said central conductive core and said conductive antenna are aligned and extend in a direction orthogonal to the transverse axis (Y) and to the main axis (X); and wherein the at least two coaxial connectors comprise two contiguous coaxial connectors (4a; 4b; 4c; 4d) whose conductive antennas are fixed on a same transverse bar (3a; 3b; 3c; 3d), said contiguous coaxial connectors (4a; 4b; 4c; 4d) being disposed side by side in a direction parallel to the transverse axis (Y) of the transverse bar (3a; 3b; 3c; 3d).
An implantable hearing prosthesis pillow charger, comprising: at least one coil antenna configured to emit one or more magnetic fields; and an electrically non-conductive coil safeguard enclosure disposed around the at least one coil antenna and configured to shield the implantable hearing prosthesis from exposure to densities of the one or more magnetic fields that exceed a predetermined threshold, characterized by an electromagnetic compatibility (EMC) screen surrounding at least the coil safeguard enclosure and configured to block harmonics of the one or more magnetic fields above certain frequencies. at least one coil antenna configured to emit one or more magnetic fields; and an electrically non-conductive coil safeguard enclosure disposed around the at least one coil antenna and configured to shield the implantable hearing prosthesis from exposure to densities of the one or more magnetic fields that exceed a predetermined threshold, characterized by an electromagnetic compatibility (EMC) screen surrounding at least the coil safeguard enclosure and configured to block harmonics of the one or more magnetic fields above certain frequencies.
A polyurethane adhesive composition comprising a polyurethane dispersion and from 1.2% to 20%, by dry weight based on total dry weight of the polyurethane dispersion, a polyisocyanate crosslinker; wherein the polyurethane dispersion is a reaction product of, by dry weight, based on total dry weight of the polyurethane dispersion, from 10% to 40% of a monomeric aromatic diisocyanate, from 30% to 65% of a polyether polyol, from 15% to 30% of a polyester polyol having at least one aromatic group and one aliphatic group, from 0.1% to 8% of a polyamine, and from 0.5% to 10% of an ionic surfactant.
A monomer for use in making a homopolymer or a copolymer for stabilizing a biomolecule, the monomer having the general structure: R 1 R 2 C = CR 3 R 4 , wherein R 1 and R 2 are hydrogen, R 3 is hydrogen or methyl and R 4 is a side chain of the formula -L-trehalose, wherein L is a linker that links trehalose to the monomer and L-trehalose has a structure selected from:
Floating support structure for photovoltaic modules, comprising at least two floating bodies and supports arranged next to one another, in particular parallel to one another, on which PV modules are mounted, characterized in that the supports have two portions of which the longitudinal axes enclose an angle (β), the angle (β) being less than 180° and greater than 135°, and in that a membrane is provided between two or more than two supports or floating bodies arranged next to one another, and in that at least two supports or floating bodies and the membrane form a membrane-reinforced supporting structure. characterized in that the supports have two portions of which the longitudinal axes enclose an angle (β), the angle (β) being less than 180° and greater than 135°, and in that a membrane is provided between two or more than two supports or floating bodies arranged next to one another, and in that at least two supports or floating bodies and the membrane form a membrane-reinforced supporting structure.
A refrigerated transport container comprising: a cargo space for containing an interior gas; a gas transfer membrane comprising a selectively permeable membrane configured to transfer component gases at different rates, the gas transfer membrane having an interior side to receive interior gas from the cargo space and an exterior side in communication with a gas exchange portion of an exterior gas pathway ; an air mover configured to drive an exterior gas flow along the exterior gas pathway for gas transfer over the membrane; a flow controller configured to selectively activate the air mover to control transfer of a controlled component gas across the gas transfer membrane from the interior side to the exterior side; characterized by a heater upstream of the gas exchange portion of the exterior gas pathway to heat the exterior gas flow. a cargo space for containing an interior gas; a gas transfer membrane comprising a selectively permeable membrane configured to transfer component gases at different rates, the gas transfer membrane having an interior side to receive interior gas from the cargo space and an exterior side in communication with a gas exchange portion of an exterior gas pathway ; an air mover configured to drive an exterior gas flow along the exterior gas pathway for gas transfer over the membrane; a flow controller configured to selectively activate the air mover to control transfer of a controlled component gas across the gas transfer membrane from the interior side to the exterior side; characterized by a heater upstream of the gas exchange portion of the exterior gas pathway to heat the exterior gas flow.