mhurhangee/patent-ind-claim-en huggingface dataset:
A Method of manufacturing a wind turbine blade said blade for a wind turbine having a blade shell body made of a composite material, said composite material comprising reinforcement fibres and a thermosetting resin, said wind turbine blade comprising a tip end and a root end , as well as a leading edge and a trailing edge , said method comprising the steps of: - placing a first thermoplastic material in a mould for moulding at least a part of the blade shell body, said first thermoplastic material being placed in the mould to form at least part of the leading edge of the outer surface of the wind turbine blade, - placing reinforcement fibres in the mould, - contacting the first thermoplastic material and the reinforcement fibres with thermosetting resin, - curing said resin to form at least a part of the shell body, - and joining blade shell body parts to form a complete blade shell body and attaching to said first thermoplastic material a second thermoplastic material. wherein said wind turbine blade further comprises an erosion shield said erosion shield extending along at least a part of said leading edge along an outer surface of the wind turbine blade, said erosion shield comprising an inner layer comprising a first thermoplastic material, and an outer layer comprising a second thermoplastic material and being attached to the first thermoplastic material of the inner layer said first thermoplastic material of the inner layer being an integral part of the shell body. - placing a first thermoplastic material in a mould for moulding at least a part of the blade shell body, said first thermoplastic material being placed in the mould to form at least part of the leading edge of the outer surface of the wind turbine blade, - placing reinforcement fibres in the mould, - contacting the first thermoplastic material and the reinforcement fibres with thermosetting resin, - curing said resin to form at least a part of the shell body, - and joining blade shell body parts to form a complete blade shell body and attaching to said first thermoplastic material a second thermoplastic material.
A method of forming a decorative wear resistant layer, the method comprising: • providing a substrate (4; 4a; 5) comprising a thermoplastic material and a transparent layer comprising a thermoplastic material, • providing a continuous print layer comprising particles on the substrate (4; 4a; 5) or on the transparent layer , wherein the print layer comprises loose particles, and wherein the particles comprise a thermoplastic powder , • printing a digital image comprising colour pigments on the print layer , and • bonding the print layer with the colour pigments to the transparent layer and to the substrate (4; 4a; 5) with heat and pressure such that the digital image is located between the transparent layer and the substrate (4; 4a; 5), wherein the transparent layer is a thermoplastic foil, and wherein the substrate is a thermoplastic foil . • providing a substrate (4; 4a; 5) comprising a thermoplastic material and a transparent layer comprising a thermoplastic material, • providing a continuous print layer comprising particles on the substrate (4; 4a; 5) or on the transparent layer , wherein the print layer comprises loose particles, and wherein the particles comprise a thermoplastic powder , • printing a digital image comprising colour pigments on the print layer , and • bonding the print layer with the colour pigments to the transparent layer and to the substrate (4; 4a; 5) with heat and pressure such that the digital image is located between the transparent layer and the substrate (4; 4a; 5),
A flight control method of an Unmanned Aerial Vehicle, UAV, comprising: Determining a flight track of the UAV; receiving a remote control signal sent by a remote control apparatus which is operated manually; converting the remote control signal into a flight controlled quantity of the UAV; generating a flight adjustment controlled quantity of the UAV according to a current location, the flight track and the flight controlled quantity, of the UAV; and executing a flight mission according to an action indicated by the flight adjustment controlled quantity, as to enable the UAV to run on the flight track; wherein the flight controlled quantity comprises a pitching flight controlled quantity and a transverse flight controlled quantity, and generating the flight adjustment controlled quantity of the UAV according to the current location, the flight track and the flight controlled quantity, of the UAV comprises: when the transverse flight controlled quantity is zero, determining a transverse adjustment controlled quantity according to the current location of the UAV and the flight track; and generating a flight adjustment controlled quantity according to the pitching flight controlled quantity and the transverse adjustment controlled quantity, the flight adjustment controlled quantity comprising a flight speed magnitude and a flight direction. Determining a flight track of the UAV; receiving a remote control signal sent by a remote control apparatus which is operated manually; converting the remote control signal into a flight controlled quantity of the UAV; generating a flight adjustment controlled quantity of the UAV according to a current location, the flight track and the flight controlled quantity, of the UAV; and executing a flight mission according to an action indicated by the flight adjustment controlled quantity, as to enable the UAV to run on the flight track; wherein the flight controlled quantity comprises a pitching flight controlled quantity and a transverse flight controlled quantity, and generating the flight adjustment controlled quantity of the UAV according to the current location, the flight track and the flight controlled quantity, of the UAV comprises: when the transverse flight controlled quantity is zero, determining a transverse adjustment controlled quantity according to the current location of the UAV and the flight track; and generating a flight adjustment controlled quantity according to the pitching flight controlled quantity and the transverse adjustment controlled quantity, the flight adjustment controlled quantity comprising a flight speed magnitude and a flight direction. when the transverse flight controlled quantity is zero, determining a transverse adjustment controlled quantity according to the current location of the UAV and the flight track; and generating a flight adjustment controlled quantity according to the pitching flight controlled quantity and the transverse adjustment controlled quantity, the flight adjustment controlled quantity comprising a flight speed magnitude and a flight direction.
A method of manufacturing a lithium ion battery module by means of a manufacturing system , which comprises a control system having a control logic and a pick and place system controlled by the control system , the control logic causing the pick and place system to perform the following steps: - engaging, with a capture mechanism of the pick and place system, a low or no swelling prismatic battery cell of an assembled group of prismatic battery cells having dimensions within manufacturing tolerances of prismatic battery cell dimensions; - removing the engaged prismatic battery cell from the group of prismatic battery cells ; and - placing the removed prismatic battery cell into a floating arrangement into a housing of the lithium ion battery module , wherein the floating arrangement includes an arrangement in which each prismatic battery cell is suspended within the housing by a plurality of fixed protrusions holding the prismatic battery cell along at least a portion of its periphery, wherein the method does not comprise cell grading, wherein cell grading includes determining a size, degree of variation, state of charge, or any combination thereof, for each prismatic battery cell , and wherein each prismatic battery cell comprises Li 4 Ti 5 O 12 (LTO) as an anode active material and LiNi 1/3 Co 1/3 Mn 1/3 O 2 (NMC) as a cathode active material. - engaging, with a capture mechanism of the pick and place system, a low or no swelling prismatic battery cell of an assembled group of prismatic battery cells having dimensions within manufacturing tolerances of prismatic battery cell dimensions; - removing the engaged prismatic battery cell from the group of prismatic battery cells ; and - placing the removed prismatic battery cell into a floating arrangement into a housing of the lithium ion battery module , wherein the floating arrangement includes an arrangement in which each prismatic battery cell is suspended within the housing by a plurality of fixed protrusions holding the prismatic battery cell along at least a portion of its periphery,
An electrical cabinet, comprising a cabinet body and a door movable on the cabinet body between a cabinet closing position and an opening position, circuit breakers mounted to the door and extending in the cabinet when the door is closed, and electrical circuits each comprising a first part attached to the cabinet body, and a second part passing through a respective circuit breaker comprising second connectors , connectable to second complementary connectors attached to the circuit breaker , characterised in that the second parts are fastened to the door and extend between first connectors (33, 34, 36; 13), connectable to first complementary connectors , attached to the first parts of the circuits, in the door closing position.
A method for encoding or decoding a bitstream representing a 3D model, comprising: accessing a plurality of instance information associated with the 3D model, each instance being associated with a corresponding pattern and transformation data; the method being characterized by encoding, or decoding, the plurality of instance information for transmission in a bitstream in one of first and second modes, wherein the bitstream comprises a header buffer, and wherein in the first mode, the transformation information associated with each respective instance is grouped in the bitstream with the respective instance on an instance by instance basis, and in the second mode, the transformation information is grouped in the bitstream on a transformation information type by transformation type basis; wherein the header buffer comprises information indicating whether the instance information is grouped in the first mode or in the second mode; determining whether there is a part of the 3D model not included in any repetitive structure; and in response to determining that there is a part of the 3D model not included in any repetitive structure, encoding, or decoding, the part of the 3D model not included in any repetitive structure in the bitstream, wherein information in the header buffer is used to indicate whether there is a part of the 3D model not included in any repetitive structure. accessing a plurality of instance information associated with the 3D model, each instance being associated with a corresponding pattern and transformation data; the method being characterized by encoding, or decoding, the plurality of instance information for transmission in a bitstream in one of first and second modes, wherein the bitstream comprises a header buffer, and wherein in the first mode, the transformation information associated with each respective instance is grouped in the bitstream with the respective instance on an instance by instance basis, and in the second mode, the transformation information is grouped in the bitstream on a transformation information type by transformation type basis; wherein the header buffer comprises information indicating whether the instance information is grouped in the first mode or in the second mode; determining whether there is a part of the 3D model not included in any repetitive structure; and in response to determining that there is a part of the 3D model not included in any repetitive structure, encoding, or decoding, the part of the 3D model not included in any repetitive structure in the bitstream, wherein information in the header buffer is used to indicate whether there is a part of the 3D model not included in any repetitive structure.
A pin spanner tool for use with a driver having a center of rotation, comprising: an arm assembly comprising a driven arm , and a a floating arm , said arm assembly having a center of rotation ; a bolt connecting said driven arm and said floating arm, characterised in that when the bolt is turned, the driven arm turns, the floating arm being free to rotate independently from the bolt rotation; and wherein the bolt is provided at the centre of rotation of said arm assembly, so that when a driver is used to exert force about the centre of rotation of the bolt , said force is exerted upon the centre of rotation of the arm assembly.. an arm assembly comprising a driven arm , and a a floating arm , said arm assembly having a center of rotation ; a bolt connecting said driven arm and said floating arm, characterised in that when the bolt is turned, the driven arm turns, the floating arm being free to rotate independently from the bolt rotation; and wherein the bolt is provided at the centre of rotation of said arm assembly, so that when a driver is used to exert force about the centre of rotation of the bolt , said force is exerted upon the centre of rotation of the arm assembly..
A method of joining two components using a hybrid metal extrusion and bonding process, the method comprising: providing the two components, wherein the components each have a joining surface which is to be joined to the other component; providing an aluminium extrusion material for use in a hybrid metal extrusion and bonding process, wherein the aluminium extrusion material is made of 2xxx, 5xxx, 6xxx, 7xxx or 8xxx aluminium alloy, wherein the composition of the extrusion material comprises: 0 to 0.25 wt% iron; at least 0.05 wt% dispersoid-forming elements, wherein the dispersoid-forming elements comprise 0 to 1.2 wt% manganese, 0 to 0.25 wt% chromium, 0 to 0.25 wt% zirconium and 0 to 0.25 wt% scandium; and, except when the aluminium alloy of the aluminium extrusion material is in the 2xxx series, 0 to 0.05 wt% copper, wherein the microstructure of the extrusion material is a deformed microstructure, and wherein the nanostructure of the extrusion material comprises an aluminium matrix with dislocations and dispersoids , and wherein at least 50% of the alloying elements other than the dispersoid-forming elements and the iron are in solid solution in the aluminium matrix; removing oxide from the joining surfaces of the two components, and extruding the aluminium extrusion material between the joining surfaces of the two components. providing the two components, wherein the components each have a joining surface which is to be joined to the other component; providing an aluminium extrusion material for use in a hybrid metal extrusion and bonding process, wherein the aluminium extrusion material is made of 2xxx, 5xxx, 6xxx, 7xxx or 8xxx aluminium alloy, wherein the composition of the extrusion material comprises: 0 to 0.25 wt% iron; at least 0.05 wt% dispersoid-forming elements, wherein the dispersoid-forming elements comprise 0 to 1.2 wt% manganese, 0 to 0.25 wt% chromium, 0 to 0.25 wt% zirconium and 0 to 0.25 wt% scandium; and, except when the aluminium alloy of the aluminium extrusion material is in the 2xxx series, 0 to 0.05 wt% copper, 0 to 0.25 wt% iron; at least 0.05 wt% dispersoid-forming elements, wherein the dispersoid-forming elements comprise 0 to 1.2 wt% manganese, 0 to 0.25 wt% chromium, 0 to 0.25 wt% zirconium and 0 to 0.25 wt% scandium; and, except when the aluminium alloy of the aluminium extrusion material is in the 2xxx series, 0 to 0.05 wt% copper, wherein the microstructure of the extrusion material is a deformed microstructure, and wherein the nanostructure of the extrusion material comprises an aluminium matrix with dislocations and dispersoids , and wherein at least 50% of the alloying elements other than the dispersoid-forming elements and the iron are in solid solution in the aluminium matrix; removing oxide from the joining surfaces of the two components, and extruding the aluminium extrusion material between the joining surfaces of the two components.
A curable composition for stereolithography, comprising a photopolymerizable component and a photopolymerization initiator, the photopolymerizable component comprising a (meth)acrylic monomer at a proportion of 80% by mass or more with respect to the total photopolymerizable component, the photopolymerizable component comprising a difunctional (meth)acrylic monomer and a monofunctional (meth)acrylic monomer, the monofunctional (meth)acrylic monomer comprising a compound represented by the following Formula : wherein in Formula R 1 represents a monovalent hydrocarbon group of 1 to 40 carbon atoms or a monovalent hydrocarbon group of 1 to 40 carbon atoms from which a part of the carbon atoms is substituted by an oxygen atom or a nitrogen atom, which may have a substituent; and R 2 represents a hydrogen atom or a methyl group, and wherein a cured product of the curable composition has a minimum value of a storage elastic modulus, in a range of from 25°C to 300°C, of not greater than 1.20×10 7 Pa, and a storage elastic modulus at 25°C of greater than 1.0×10 9 Pa, wherein the storage elastic modulus is determined according to the method specified in the passage of the specification titled "Measurement of storage elastic modulus". the photopolymerizable component comprising a (meth)acrylic monomer at a proportion of 80% by mass or more with respect to the total photopolymerizable component, the photopolymerizable component comprising a difunctional (meth)acrylic monomer and a monofunctional (meth)acrylic monomer, the monofunctional (meth)acrylic monomer comprising a compound represented by the following Formula : wherein in Formula R 1 represents a monovalent hydrocarbon group of 1 to 40 carbon atoms or a monovalent hydrocarbon group of 1 to 40 carbon atoms from which a part of the carbon atoms is substituted by an oxygen atom or a nitrogen atom, which may have a substituent; and R 2 represents a hydrogen atom or a methyl group, and wherein a cured product of the curable composition has a minimum value of a storage elastic modulus, in a range of from 25°C to 300°C, of not greater than 1.20×10 7 Pa, and a storage elastic modulus at 25°C of greater than 1.0×10 9 Pa, wherein the storage elastic modulus is determined according to the method specified in the passage of the specification titled "Measurement of storage elastic modulus".
A system for supporting operation of an X-ray imaging apparatus (IA) having a plurality of non-ionizing radiation based cameras mounted at different locations on to the apparatus, the apparatus being capable of assuming different imaging geometries, comprising: an input interface (IN) for receiving a specification of a path extending at least partly into an object; a camera sampler (CS) configured to compute, for at least one of the plurality of non-ionizing radiation based cameras (OC) of the X-ray imaging apparatus (IM), a respective imaging geometry of the X-ray imaging apparatus in which a non-ionizing radiation based camera achieves a plan view on the object, an optical axis of said camera being aligned with said path in said plan view. an input interface (IN) for receiving a specification of a path extending at least partly into an object; a camera sampler (CS) configured to compute, for at least one of the plurality of non-ionizing radiation based cameras (OC) of the X-ray imaging apparatus (IM), a respective imaging geometry of the X-ray imaging apparatus in which a non-ionizing radiation based camera achieves a plan view on the object, an optical axis of said camera being aligned with said path in said plan view.
A brushing system , including a brush , and a hydraulic motor , comprising meshed gears housed in a closed package, for not allowing pressurized water entering an inlet of said package to flow between said meshed gears , thereby directing the water to flow around said gears , for rotating said brush , said brushing system characterized in administering said pressurized water by water outlets of said brush , whereby said water outlets of said brush rotate with said brush , wherein an inner volume of said one of said two gears comprises a piping for communicating therethrough an outlet of said hydraulic motor to said water outlets of said brush .
A trolley for a cable transportation system transportation unit; the trolley extending along a longitudinal axis (A1) and comprising a frame ; a clamp supported by the frame and designed to connect the trolley to a cable ; and a first and second guide which are mounted and project on opposite sides of the clamp , taper towards their respective free ends, and have respective bottom faces designed to contact the cable ; wherein the bottom face of the second guide has a first portion adjacent to the clamp, and a second portion located at the free end of the second guide and sloping upwards with respect to the first portion ; characterised in that the second guide comprises an end portion bent upwards to define the first and second portion along the bottom face , and being designed to allow the first guide of a further trolley , adjacent to and aligned with the trolley along the longitudinal axis (A1), to fit beneath the second guide .
A method of operating a control node adapted to provide mobility management in a wireless network, the method comprising: retrieving from a directory a list of data functions correlated to corresponding gateway nodes , wherein each gateway node comprises at least one data function to route packets containing traffic data between a radio access network and an external data network , wherein the directory is implemented in a node separate from the gateway nodes and separate from control nodes adapted to provide mobility management in the wireless network; receiving a message from a mobile station requesting activation of a connection, the mobile station being wirelessly connected to the radio access network ; in response to the received message, selecting, in dependence upon the retrieved list of data functions , a first and a second gateway nodes coupled between the radio access network and the external data network if no data functions from the retrieved list of data functions serve a particular access point name, APN, and are normally loaded; and sending commands to the selected first and second gateway nodes to establish a session between the control node and the selected first and second gateway nodes and to establish a data path between the radio access network and the selected first and second gateway nodes , wherein the data path bypasses the control node . retrieving from a directory a list of data functions correlated to corresponding gateway nodes , wherein each gateway node comprises at least one data function to route packets containing traffic data between a radio access network and an external data network , wherein the directory is implemented in a node separate from the gateway nodes and separate from control nodes adapted to provide mobility management in the wireless network; receiving a message from a mobile station requesting activation of a connection, the mobile station being wirelessly connected to the radio access network ; in response to the received message, selecting, in dependence upon the retrieved list of data functions , a first and a second gateway nodes coupled between the radio access network and the external data network if no data functions from the retrieved list of data functions serve a particular access point name, APN, and are normally loaded; and sending commands to the selected first and second gateway nodes to establish a session between the control node and the selected first and second gateway nodes and to establish a data path between the radio access network and the selected first and second gateway nodes , wherein the data path bypasses the control node .
A method for preventing bacterial infection in a process for fermenting a sugar-containing material, characterized in that a disinfectant comprising performic acid is used.