mhurhangee/patent-ind-claim-en huggingface dataset:
Trailer platform for land cargo transport, which forms the trailer floor, the platform being in a form of a cuboid, the platform comprises an upper outer layer (1.1) and a lower outer layer (1.3) having form of an open profile, wherein each outer layer is comprised of a base laterally mounted on four sides with the arms between which a one-side open space is formed, so that the two outer layers are mutually overlapping and the core (1.2) of the platform is connected to the outer layers adjacent to the core (1.2) while the cores in located in the space formed between the connected upper outer layer (1.1) and lower outer layer (1.3) that create a space closed from the top, bottom and on the sides, wherein upper outer layer (1.1) and the lower outer layer (1.3) are made of metal, metal alloys or composite materials, while the core (1.2) has the form of a cellular material, preferably honeycomb, where the core (1.2) thickness is a minimum of 50% of the platform thickness formed by the core and the outer layers, characterized in that , the platform's corners is formed between the arms are cut through the entire thickness of the platform on a part of the length of the arms at an angle of 90 ° relative to the base.
A method for optimising the climb of an aircraft or drone, the method being computer-implemented in a flight management system FMS and comprising the steps of: - determining an optimal continuous climb strategy, the optimal continuous climb strategy being determined depending on flight-profile parameters, said flight-profile parameters comprising altitude and/or speed constraints, and/or setpoints in respect of speed and/or thrust and/or level-flight avoidance and/or gradient-variation minimisation, and allowing vertical climb predictions to be computed; - determining a lateral path, depending on lateral-path parameters comprising setpoints in respect of turn radius as a function of roll-angle setpoints, and depending on the vertical predictions computed for the flight-profile parameters; - iterating the previous two steps on each constrained segment of the aircraft or drone path, a constrained segment being a segment containing a binding constraint; then iterating the two previous steps over the entire climb, while fitting, during each iteration, said flight-profile parameters and said lateral-path parameters, until all the binding constraints have been met one by one according to a predefined strategy. - determining an optimal continuous climb strategy, the optimal continuous climb strategy being determined depending on flight-profile parameters, said flight-profile parameters comprising altitude and/or speed constraints, and/or setpoints in respect of speed and/or thrust and/or level-flight avoidance and/or gradient-variation minimisation, and allowing vertical climb predictions to be computed; - determining a lateral path, depending on lateral-path parameters comprising setpoints in respect of turn radius as a function of roll-angle setpoints, and depending on the vertical predictions computed for the flight-profile parameters; - iterating the previous two steps on each constrained segment of the aircraft or drone path, a constrained segment being a segment containing a binding constraint; then iterating the two previous steps over the entire climb, while fitting, during each iteration, said flight-profile parameters and said lateral-path parameters, until all the binding constraints have been met one by one according to a predefined strategy.
An electro-optical device comprising a first electro-optical crystal , a second electro-optical crystal and at least one layer of optically transparent glue , an input optical face and an output optical face , the output optical face of the first electro-optical crystal being made integral with the input optical face of the second electro-optical crystal by gluing using said at least one layer of glue , the first electro-optical crystal and the second electro-optical crystal being arranged in a determined orientation relative to each other and in optical series to transmit a light beam through each of the optical faces , characterized in that the electro-optical crystals are chosen in the group consisted of: sphalerite, sulphur selenide, zinc telluride, bismuth germanate, gallium arsenide, indium arsenide, gallium phosphide, cadmium telluride, potassium dihydrogen phosphate, ammonium dihydrogen phosphate, lithium niobate, lithium tantalate, barium beta-borate, deuterated potassium dihydrogen phosphate, potassium titanyl phosphate, rubidium titanyl phosphate, arsenate titanyl phosphate, potassium niobate, lithium triborate.
A method of producing a three-dimensional porous tissue in-growth structure comprising the steps of: depositing a first layer of a powder made from a metal selected from the group consisting of titanium, titanium alloys, stainless steel, cobalt chrome alloys, tantalum and niobium onto a substrate; scanning an energy beam having a power (P) for a period of time ( μ s), so as to melt said powder and form a portion of a plurality of predetermined unit cells within said first powder layer; depositing at least one additional layer of said powder onto said first powder layer; and repeating said scanning step to form additional portions of said plurality of predetermined unit cells, wherein at least some of said predetermined unit cells are any of a tetrahedron, a dodecahedron, a diamond, and an octahedron, varying porosity within said three-dimensional porous tissue in-growth structure through a random perturbation applied in any direction to vertices of said predetermined unit cells to randomize the geometry of said predetermined unit cells. depositing a first layer of a powder made from a metal selected from the group consisting of titanium, titanium alloys, stainless steel, cobalt chrome alloys, tantalum and niobium onto a substrate; scanning an energy beam having a power (P) for a period of time ( μ s), so as to melt said powder and form a portion of a plurality of predetermined unit cells within said first powder layer; depositing at least one additional layer of said powder onto said first powder layer; and repeating said scanning step to form additional portions of said plurality of predetermined unit cells, wherein at least some of said predetermined unit cells are any of a tetrahedron, a dodecahedron, a diamond, and an octahedron, varying porosity within said three-dimensional porous tissue in-growth structure through a random perturbation applied in any direction to vertices of said predetermined unit cells to randomize the geometry of said predetermined unit cells.
An apparatus comprising: a wire retaining tray comprising at least one outlet ; one or more springs ; and a plurality of wire retainers , wherein the plurality of wire retainers are coupled together and coupled to the one or more springs and at least one of the at least one outlet of the wire retaining tray , wherein the one or more springs are adapted to exert a force on one or more wire retainers to position the wire retainers relative to the wire retaining tray and wherein at least one of the wire retainers comprises a wire holding mechanism configured to hold at least a portion of a wire in a substantially straight orientation. a wire retaining tray comprising at least one outlet ; one or more springs ; and a plurality of wire retainers , wherein the plurality of wire retainers are coupled together and coupled to the one or more springs and at least one of the at least one outlet of the wire retaining tray , wherein the one or more springs are adapted to exert a force on one or more wire retainers to position the wire retainers relative to the wire retaining tray and wherein at least one of the wire retainers comprises a wire holding mechanism configured to hold at least a portion of a wire in a substantially straight orientation.
Method for providing messages which can be authenticated, having the method steps of: - determining a repeating message content (RM) of the messages (B); - calculating partial authentication codes (pMAC1, pMAC2, pMAC3, pMAC4, pMAC1A, pMAC2A) for the messages (B) on the basis of the repeating message content (RM), wherein a first authentication code for at least some of the messages (B) can be calculated from at least some of the partial authentication codes (pMAC1, pMAC2, pMAC3, pMAC4, pMAC1A, pMAC2A) for authenticating the repeating message content (RM); and - providing the messages (B), wherein the messages (B) comprise the repeating message content (RM) and at least one of the partial authentication codes (pMAC1, pMAC2, pMAC3, pMAC4, pMAC1A, pMAC2A) in each case. - determining a repeating message content (RM) of the messages (B); - calculating partial authentication codes (pMAC1, pMAC2, pMAC3, pMAC4, pMAC1A, pMAC2A) for the messages (B) on the basis of the repeating message content (RM), wherein a first authentication code for at least some of the messages (B) can be calculated from at least some of the partial authentication codes (pMAC1, pMAC2, pMAC3, pMAC4, pMAC1A, pMAC2A) for authenticating the repeating message content (RM); and - providing the messages (B), wherein the messages (B) comprise the repeating message content (RM) and at least one of the partial authentication codes (pMAC1, pMAC2, pMAC3, pMAC4, pMAC1A, pMAC2A) in each case.
A computer-implemented method for automatically fitting a haptic effect, the computer-implemented method comprising: receiving source data , wherein the source data comprises a characteristic; characterized by : comparing the source data with a plurality of haptic primitives, wherein each haptic primitive of the plurality of haptic primitives comprises a haptic parameter; selecting a haptic primitive from the plurality of haptic primitives, in which a value of the haptic parameter is most similar to a value of the characteristic of the source data, based on the comparison; and outputting a haptic effect based on the selected haptic primitive. receiving source data , wherein the source data comprises a characteristic; characterized by : comparing the source data with a plurality of haptic primitives, wherein each haptic primitive of the plurality of haptic primitives comprises a haptic parameter; selecting a haptic primitive from the plurality of haptic primitives, in which a value of the haptic parameter is most similar to a value of the characteristic of the source data, based on the comparison; and outputting a haptic effect based on the selected haptic primitive. comparing the source data with a plurality of haptic primitives, wherein each haptic primitive of the plurality of haptic primitives comprises a haptic parameter; selecting a haptic primitive from the plurality of haptic primitives, in which a value of the haptic parameter is most similar to a value of the characteristic of the source data, based on the comparison; and outputting a haptic effect based on the selected haptic primitive.
A seal system for a gas turbine engine comprising: a web plate axially disposed between a transition piece and a turbine nozzle , wherein the web plate comprises: a radial arm extending in a radial direction between an inner surface and an outer surface of the web plate , wherein the radial arm , the inner surface , and the outer surface are disposed about an axial passage configured to facilitate a flow of combustion products from the transition piece to the turbine nozzle , wherein the transition piece is disposed within a compressor discharge cavity configured to receive an oxidant , and the radial arm comprises: an upstream face in fluid communication with the compressor discharge cavity ; and at least one arm passage that extends an axial length in an axial direction from the upstream face through at least an axial depth of the radial arm , wherein the arm passage is configured to receive a portion of the oxidant through the upstream face . characterized in that the seal system further comprises: an aft frame coupled to the transition piece ; and a first sealing element disposed axially between the aft frame and the upstream face of the radial arm . a web plate axially disposed between a transition piece and a turbine nozzle , wherein the web plate comprises: a radial arm extending in a radial direction between an inner surface and an outer surface of the web plate , wherein the radial arm , the inner surface , and the outer surface are disposed about an axial passage configured to facilitate a flow of combustion products from the transition piece to the turbine nozzle , wherein the transition piece is disposed within a compressor discharge cavity configured to receive an oxidant , and the radial arm comprises: an upstream face in fluid communication with the compressor discharge cavity ; and at least one arm passage that extends an axial length in an axial direction from the upstream face through at least an axial depth of the radial arm , wherein the arm passage is configured to receive a portion of the oxidant through the upstream face . an upstream face in fluid communication with the compressor discharge cavity ; and at least one arm passage that extends an axial length in an axial direction from the upstream face through at least an axial depth of the radial arm , wherein the arm passage is configured to receive a portion of the oxidant through the upstream face . characterized in that the seal system further comprises: an aft frame coupled to the transition piece ; and a first sealing element disposed axially between the aft frame and the upstream face of the radial arm . an aft frame coupled to the transition piece ; and a first sealing element disposed axially between the aft frame and the upstream face of the radial arm .
A refrigerator comprising: a refrigerator body including a freezing compartment and a refrigerating compartment , the refrigerating compartment is arranged over the freezing compartment , an ice making compartment which is arranged in the refrigerating compartment to make ice, wherein the ice making compartment is provided at a refrigerating compartment door unit which opens or closes an inner space of the refrigerator; a heat exchanger which generates cold air for freezing food stored in the freezing compartment ; a cold air guiding device guiding cold air generated by the heat exchanger to the ice making compartment to enable the ice making compartment to make ice, wherein the cold air guiding device includes a duct unit which communicates with the ice making compartment characterized in that the duct unit includes a first opening provided at an inner wall of the refrigerating compartment , and forms one end of the duct unit connected to one side of the refrigerating compartment door unit ; the refrigerating compartment door unit includes a second opening connected to the first opening to connect the duct unit to an inner space of the ice making compartment and the refrigerator further comprises a sealing unit provided at at least one of the first and second openings to prevent air from being leaked between the first and second openings , wherein the sealing unit includes a gasket and a gasket fixer which fixes the gasket to at least one of the first and second openings . a refrigerator body including a freezing compartment and a refrigerating compartment , the refrigerating compartment is arranged over the freezing compartment , an ice making compartment which is arranged in the refrigerating compartment to make ice, wherein the ice making compartment is provided at a refrigerating compartment door unit which opens or closes an inner space of the refrigerator; a heat exchanger which generates cold air for freezing food stored in the freezing compartment ; a cold air guiding device guiding cold air generated by the heat exchanger to the ice making compartment to enable the ice making compartment to make ice, wherein the cold air guiding device includes a duct unit which communicates with the ice making compartment characterized in that the duct unit includes a first opening provided at an inner wall of the refrigerating compartment , and forms one end of the duct unit connected to one side of the refrigerating compartment door unit ; the refrigerating compartment door unit includes a second opening connected to the first opening to connect the duct unit to an inner space of the ice making compartment and the refrigerator further comprises a sealing unit provided at at least one of the first and second openings to prevent air from being leaked between the first and second openings , wherein the sealing unit includes a gasket and a gasket fixer which fixes the gasket to at least one of the first and second openings .
Machine tool system, comprising: - at least one machine tool for machining workpieces, having a workpiece holding device , wherein, during workpiece machining, one or more workpieces are held on the workpiece holding device by way of an adapter ; - a positioning device that positions workpiece blanks on adapters , - an adapter loading and transporting device , having an adapter gripping device that acts on adapters , wherein the adapter loading and transporting device moves adapters that are provided with workpiece blanks from the positioning device to the at least one machine tool , loads the at least one machine tool and unloads adapters that are provided with one or more machined workpieces from the at least one machine tool , and - a workpiece transporting device , having a workpiece gripping device that acts on workpieces, wherein, after machined workpieces have been unloaded at the at least one machine tool by the adapter loading and transporting device , the workpiece transporting device takes them up from the adapter loading and transporting device and removes them, characterized in that the workpiece holding device comprises a release system for releasing clamping of one or more machined workpieces on an adapter , and/or a clamping system for clamping one or more workpieces on the adapter , wherein machined workpieces that are positioned on adapters are unclampable from the adapter within the at least one machine tool and/or workpieces that are positioned on adapters are clampable on the adapters within the machine tool . - at least one machine tool for machining workpieces, having a workpiece holding device , wherein, during workpiece machining, one or more workpieces are held on the workpiece holding device by way of an adapter ; - a positioning device that positions workpiece blanks on adapters , - an adapter loading and transporting device , having an adapter gripping device that acts on adapters , wherein the adapter loading and transporting device moves adapters that are provided with workpiece blanks from the positioning device to the at least one machine tool , loads the at least one machine tool and unloads adapters that are provided with one or more machined workpieces from the at least one machine tool , and - a workpiece transporting device , having a workpiece gripping device that acts on workpieces, wherein, after machined workpieces have been unloaded at the at least one machine tool by the adapter loading and transporting device , the workpiece transporting device takes them up from the adapter loading and transporting device and removes them, characterized in that the workpiece holding device comprises a release system for releasing clamping of one or more machined workpieces on an adapter , and/or a clamping system for clamping one or more workpieces on the adapter , wherein machined workpieces that are positioned on adapters are unclampable from the adapter within the at least one machine tool and/or workpieces that are positioned on adapters are clampable on the adapters within the machine tool .
An antenna system comprising: a driven antenna element ; a printed circuit board, PCB, that carries on-board electronics communicatively coupled to the driven antenna element to communicate wireless signals via the driven antenna element, the PCB defining a PCB ground plane for co-operation with the driven antenna element in signal communication; and a plurality of PCB extenders (505, 510; 814, 821) comprising respective conductors electrically connected to the PCB ground plane and projecting from the PCB in mutually transverse orientations, thereby defining a plurality of mutually transverse ground planes for co-operation with the driven antenna element in signal communication, wherein one or more antenna components selected from the group comprising the driven antenna element and the plurality of PCB extenders (505, 510; 814, 821) comprises a thermally conductive element that is connected to the PCB to be in heat transfer relationship with one or more heat sources on the PCB, thereby to serve as a heat sink for the electronics on the PCB. a driven antenna element ; a printed circuit board, PCB, that carries on-board electronics communicatively coupled to the driven antenna element to communicate wireless signals via the driven antenna element, the PCB defining a PCB ground plane for co-operation with the driven antenna element in signal communication; and a plurality of PCB extenders (505, 510; 814, 821) comprising respective conductors electrically connected to the PCB ground plane and projecting from the PCB in mutually transverse orientations, thereby defining a plurality of mutually transverse ground planes for co-operation with the driven antenna element in signal communication, wherein one or more antenna components selected from the group comprising the driven antenna element and the plurality of PCB extenders (505, 510; 814, 821) comprises a thermally conductive element that is connected to the PCB to be in heat transfer relationship with one or more heat sources on the PCB, thereby to serve as a heat sink for the electronics on the PCB.
An aerospace inertial actuator, comprising: - a main gyroscopic assembly comprising a first two paired gyroscopes (CMG1) providing a first torque in two components of space, with the following conditions: - each gyroscope (CMG1) is provided with a rotor , spin motor , nutation motor and support ; - the axes of nutation of both gyroscopes are parallel, said gyroscopes producing a vector control torque of a known fixed direction, located on the plane normal to the axis of nutation thereof, - a secondary gyroscopic assembly providing a second torque in a third component of space perpendicular to the main gyroscopic assembly. - electronic computing and control means ; - mechanical support and holding means ; wherein the secondary gyroscopic assembly comprises a second two paired gyroscopes (CMG2) of the same type having a dimensional size smaller than the dimensional size of the first two paired gyroscopes (CMG1) such that the torque of the second two paired gyroscopes (CMG2) has a lower value compared to the torque of the first two paired gyroscopes (CMG1). - a main gyroscopic assembly comprising a first two paired gyroscopes (CMG1) providing a first torque in two components of space, with the following conditions: - each gyroscope (CMG1) is provided with a rotor , spin motor , nutation motor and support ; - the axes of nutation of both gyroscopes are parallel, said gyroscopes producing a vector control torque of a known fixed direction, located on the plane normal to the axis of nutation thereof, - a secondary gyroscopic assembly providing a second torque in a third component of space perpendicular to the main gyroscopic assembly. - electronic computing and control means ; - mechanical support and holding means ;
A carboxyesterase polypeptide comprising an amino acid sequence that is at least 93% or more identical to the amino acid sequence set forth in SEQ ID NO: 4, or a functional fragment thereof, wherein the residue corresponding to X198 in SEQ ID NO: 4 is L, and the carboxyesterase polypeptide has improved enzymatic activity relative to the carboxyesterase polypeptide of SEQ ID NO: 2.