mhurhangee/ep-ind-claims huggingface dataset:
Voltage supply device having a first and a second main channel arrangement (6a, b), wherein the first main channel arrangement has a first voltage input for a first input DC voltage and a first main voltage output for a first output DC voltage, wherein the first main channel arrangement has a first DC/DC converter device for converting the first input DC voltage into the first output DC voltage, wherein the first DC/DC converter device has a first output inductor which is arranged in series with the first main voltage output, wherein the second main channel arrangement has a second voltage input for a second input DC voltage and a second main voltage output for a second output DC voltage, wherein the second main channel arrangement has a second DC/DC converter device for converting the second input DC voltage into the second output DC voltage, wherein the second DC/DC converter device has a second output inductor which is arranged in series with the second main voltage output, characterized in that the voltage supply device has a first and a second output transformer (17a, b), wherein the first output inductor is designed as a primary winding of the first output transformer, and the second output inductor is designed as a primary winding of the second output transformer; and in that the voltage supply device has at least a first secondary channel arrangement, wherein the first secondary channel arrangement has a first secondary voltage output and a first secondary winding of the first output transformer and a first secondary winding of the second output transformer, wherein the first secondary voltage output is connected to the first secondary windings (19a, b) which are connected in parallel, wherein the first secondary windings (19a, b) are arranged in parallel with one another by having one end connected to a ground and having their second outputs interconnected at a node, the node being in series with the first secondary voltage output.
A method in a computing system that implements a video decoder, the method comprising: receiving and parsing a syntax element that indicates a maximum size of frame memory for reordering, wherein the maximum size of frame memory for reordering is expressed in terms of a maximum count of frames that can precede any frame of a video sequence in coded order but follow that frame in output order; receiving and parsing one or more different syntax elements that indicate a constraint on frame reordering latency, wherein the constraint on frame reordering latency is expressed in terms of a maximum count of frames that can precede any frame of the video sequence in output order but follow that frame in coded order; receiving encoded data for plural frames of the video sequence; with the video decoder, decoding at least some of the encoded data to reconstruct one of the plural frames; and outputting the reconstructed frame. receiving and parsing a syntax element that indicates a maximum size of frame memory for reordering, wherein the maximum size of frame memory for reordering is expressed in terms of a maximum count of frames that can precede any frame of a video sequence in coded order but follow that frame in output order; receiving and parsing one or more different syntax elements that indicate a constraint on frame reordering latency, wherein the constraint on frame reordering latency is expressed in terms of a maximum count of frames that can precede any frame of the video sequence in output order but follow that frame in coded order; receiving encoded data for plural frames of the video sequence; with the video decoder, decoding at least some of the encoded data to reconstruct one of the plural frames; and outputting the reconstructed frame.
A unmanned aerial vehicle comprising: a frame; a propulsion mechanism coupled to the frame that propels the frame through the air; one or more airbags (302, 304) coupled to the frame; and an inflation device (210, 211) coupled to the frame and to at least one of the one or more airbags, characterized in that the inflation device inflates the one or more airbags based upon receipt of an activation signal such that the one or more airbags engulf the frame and propulsion mechanism. a frame; a propulsion mechanism coupled to the frame that propels the frame through the air; one or more airbags (302, 304) coupled to the frame; and an inflation device (210, 211) coupled to the frame and to at least one of the one or more airbags, characterized in that the inflation device inflates the one or more airbags based upon receipt of an activation signal such that the one or more airbags engulf the frame and propulsion mechanism.
An injection molding device for fabricating a part that is a body of revolution, the device comprising: - an injection mold (1, 1', 1", 16), the mold being a body of revolution constituted by a support (2, 12) and a countermold (3, 13) that are distinct and that define between them a mold cavity (4, 17) presenting a first shape that is circular; and - at least one injection means for injecting a fluid material into the mold cavity; the device being characterized in that it includes deformation elements configured to modify the shape of the mold cavity to a second shape that is of oval section and different from the first shape. - an injection mold (1, 1', 1", 16), the mold being a body of revolution constituted by a support (2, 12) and a countermold (3, 13) that are distinct and that define between them a mold cavity (4, 17) presenting a first shape that is circular; and - at least one injection means for injecting a fluid material into the mold cavity;
A method for performing an assembly operation, the method comprising: macro-positioning a tool relative to an exterior of a fuselage assembly, wherein macro-positioning the tool comprises driving an external mobile platform carrying the tool into a position relative to an assembly fixture supporting the fuselage assembly; micro-positioning the tool relative to a particular location on the exterior of the fuselage assembly; performing the assembly operation at the particular location using the tool; and autonomously coupling the external mobile platform to the assembly fixture to form an interface such that a number of utilities may flow from the assembly fixture to the external mobile platform. macro-positioning a tool relative to an exterior of a fuselage assembly, wherein macro-positioning the tool comprises driving an external mobile platform carrying the tool into a position relative to an assembly fixture supporting the fuselage assembly; micro-positioning the tool relative to a particular location on the exterior of the fuselage assembly; performing the assembly operation at the particular location using the tool; and autonomously coupling the external mobile platform to the assembly fixture to form an interface such that a number of utilities may flow from the assembly fixture to the external mobile platform.
A device for the separation of solids from gases having a raw gas chamber with the top connectible to a raw gas channel and the bottom connectible to a discharge hopper, and with at least one filter arranged in the raw gas chamber, whose flow channel, which is enclosed by a filter shell and can be perfused from the bottom to the top, is connected to a clean gas chamber, wherein the filter is connected to clean gas line, which runs through the raw gas chamber, whose top and bottom are open, and which opens into the clean gas chamber laterally adjacent to the raw gas chamber, wherein further the filter comprises vertical cartridges, which are arranged in at least one row and held in openings of an insertion part and abutting directly thereon, the insertion part engages with a guide associated with the floor of the clean gas line, and wherein, in the insertion position of the insertion part, the filter cartridges are pressed firmly onto the floor, being provided with corresponding floor openings, of the clean gas line, with intermediate placement of a seal, when the insertion part is held pressed onto the floor of the clean gas line in the front region of the clean gas line with the aid of a tension lock, characterized in that the insertion part engages with the guide and said guide rises in the direction of insertion in order to create said sealing abutment with the floor.
A method of manufacturing a gallium nitride crystal having an hexagonal shaped or an almost hexagonal shaped cross section orthogonal to the c-axis, a length L of the c-axis of 9 mm or more, and a ratio L/d of the length L of the c-axis to the crystal diameter d of the cross section orthogonal to the c-axis of 7 or more, characterized in that the method includes: a molten mixture forming process to form a molten mixture containing at least sodium and gallium in a reactor vessel, bring gas containing nitrogen into contact with the molten mixture, and dissolve the nitrogen from the gas into the molten mixture; and a crystal growth process to grow the gallium nitride crystal toward -c-axis direction of the crystal from the gallium in the molten mixture and the nitrogen dissolved in the molten mixture, wherein in the molten mixture forming process, a mol ratio of sodium to a total amount of gallium and sodium in the molten mixture is in a range of 75 % to 90 %, a temperature of the molten mixture is in a range of 860 degrees Celsius to 900 degrees Celsius, and a nitrogen partial pressure of the gas is in a range of 5 MPa to 8 MPa. a molten mixture forming process to form a molten mixture containing at least sodium and gallium in a reactor vessel, bring gas containing nitrogen into contact with the molten mixture, and dissolve the nitrogen from the gas into the molten mixture; and a crystal growth process to grow the gallium nitride crystal toward -c-axis direction of the crystal from the gallium in the molten mixture and the nitrogen dissolved in the molten mixture, wherein in the molten mixture forming process, a mol ratio of sodium to a total amount of gallium and sodium in the molten mixture is in a range of 75 % to 90 %, a temperature of the molten mixture is in a range of 860 degrees Celsius to 900 degrees Celsius, and a nitrogen partial pressure of the gas is in a range of 5 MPa to 8 MPa.
A method performed by a vehicle system for handling configuration of a vehicle, the method comprising: obtaining a request for a service to be provided on-board the vehicle; comparing a current configuration of the vehicle's network capabilities with a required configuration of network capabilities that the vehicle is required to have to be capable of hosting the requested service, wherein the network capabilities comprise one or more containers and/or one or more logical networks connecting containers to one another and/or to one or more offboard resources, wherein the container is a logical structure representing a segmented part of the vehicle's operating system resources assigned to the service and that are separated from other operating system resources of the vehicle; and when a result of the comparing indicates that the current configuration of the network capabilities is different than the required configuration of the network capabilities, triggering the vehicle to reconfigure its current configuration of network capabilities such that the vehicle comprises the required configuration of the network capabilities and is thereby capable of hosting the service. obtaining a request for a service to be provided on-board the vehicle; comparing a current configuration of the vehicle's network capabilities with a required configuration of network capabilities that the vehicle is required to have to be capable of hosting the requested service, wherein the network capabilities comprise one or more containers and/or one or more logical networks connecting containers to one another and/or to one or more offboard resources, wherein the container is a logical structure representing a segmented part of the vehicle's operating system resources assigned to the service and that are separated from other operating system resources of the vehicle; and when a result of the comparing indicates that the current configuration of the network capabilities is different than the required configuration of the network capabilities, triggering the vehicle to reconfigure its current configuration of network capabilities such that the vehicle comprises the required configuration of the network capabilities and is thereby capable of hosting the service.
An information processing terminal system comprising: an information processing terminal (4, 6, 10, 10', 16, 16'); and a transmitting and receiving unit (3, 5, 7, 9, 11, 13, 15) which can be attached to or detached from said information processing terminal (4, 6, 10, 10', 16, 16'), wherein said transmitting and receiving unit (3, 5, 7, 9, 11, 13, 15) comprises: a transmission and reception processing section (21, 37); a demodulation section (22, 42); a modulation section and a baseband processing section, when said transmitting and receiving unit (3, 5, 7, 9, 11, 13, 15) is attached to said information processing terminal (4, 6, 10, 10', 16, 16'), said transmission and reception processing section (21, 37) is configured to output a reception modulation wave signal from a network to said demodulation section (22, 42) and to transmit a transmission modulation wave signal from said modulation section to the network, said demodulation section (22, 42) being configured to convert the reception modulation wave signal from said transmission and reception processing section (21, 37) into a reception analog baseband signal, said baseband processing section being configured to convert the reception analog baseband signal into a reception digital signal to output to said information processing terminal (4, 6, 10, 10', 16, 16'), and to convert a transmission digital signal from said information processing terminal (4, 6, 10, 10', 16, 16') into a transmission analog baseband signal, said modulation section being configured to convert the transmission analog baseband signal into the transmission modulation wave signal, wherein said information processing terminal (4, 6, 10, 10', 16, 16') comprises: an interface (47, 34, 102, 104), and a control unit (48, 26), said baseband processing section, said interface (47, 34, 102, 104) and said control unit (48, 26) being configured to operate in synchronization with a clock, and the reception digital signal containing a reception data, and the transmission digital signal containing a transmission data. an information processing terminal (4, 6, 10, 10', 16, 16'); and a transmitting and receiving unit (3, 5, 7, 9, 11, 13, 15) which can be attached to or detached from said information processing terminal (4, 6, 10, 10', 16, 16'), a transmission and reception processing section (21, 37); a demodulation section (22, 42); a modulation section and a baseband processing section, an interface (47, 34, 102, 104), and a control unit (48, 26),
A cylinder liner for insert casting including a base and a plurality of protrusions on the outer periphery of the base, wherein the molten metal running index YI defined by the following Formula is 2.2 or more and 14.5 or less. Molten metal running index YI = area ratio S t % of top portions of protrusions × molten metal infiltration volume V mm 3 / outer peripheral surface area A mm 2 of cylinder liner base / average surface − to − surface distance P av mm between top portions of protrusions In the Formula, the area ratio S t of the top portions of the protrusions is the projected area ratio of the protrusions viewed from the outer peripheral side of the cylinder liner in the height direction of the protrusions. In the Formula, the molten metal infiltration volume V is represented by V = α - β - (γ × δ), where α = π × (outermost diameter d max (mm) of cylinder liner including protrusions/2) 2 × axial length L (mm) of cylinder liner, β = π × (outer diameter d (mm) of cylinder liner base/2) 2 × axial length L (mm) of cylinder liner, γ = Number of protrusions per unit area × [(outer diameter d (mm) of cylinder liner base × π × axial length L (mm) of cylinder liner)/unit area (mm 2)], and δ = π × (average diameter d pav (mm) of top portion of protrusion/2) 2 × average protrusion height H av (mm). When both ends of the cylinder liner are chamfered, the axial length L of the cylinder liner is defined as the length of the cylinder liner minus the length of the chamfered portions. In the Formula, the area ratio S t of the top portions of the protrusions is the projected area ratio of the protrusions viewed from the outer peripheral side of the cylinder liner in the height direction of the protrusions. In the Formula, the molten metal infiltration volume V is represented by V = α - β - (γ × δ), where α = π × (outermost diameter d max (mm) of cylinder liner including protrusions/2) 2 × axial length L (mm) of cylinder liner, β = π × (outer diameter d (mm) of cylinder liner base/2) 2 × axial length L (mm) of cylinder liner, γ = Number of protrusions per unit area × [(outer diameter d (mm) of cylinder liner base × π × axial length L (mm) of cylinder liner)/unit area (mm 2)], and δ = π × (average diameter d pav (mm) of top portion of protrusion/2) 2 × average protrusion height H av (mm). α = π × (outermost diameter d max (mm) of cylinder liner including protrusions/2) 2 × axial length L (mm) of cylinder liner, β = π × (outer diameter d (mm) of cylinder liner base/2) 2 × axial length L (mm) of cylinder liner, γ = Number of protrusions per unit area × [(outer diameter d (mm) of cylinder liner base × π × axial length L (mm) of cylinder liner)/unit area (mm 2)], and δ = π × (average diameter d pav (mm) of top portion of protrusion/2) 2 × average protrusion height H av (mm). When both ends of the cylinder liner are chamfered, the axial length L of the cylinder liner is defined as the length of the cylinder liner minus the length of the chamfered portions.
Method for printing electric or electronic structures by means of cold-foil transfer, characterized in that desired breaking points are created in the transfer layer.
An article, preferably a gas turbine engine component, comprising: a) a substrate formed of a silicon-comprising material; b) an environmental barrier layer comprising an alkaline earth metal aluminosilicate; or mullite or mixtures thereof with yttrium silicate or an alkaline earth metal aluminosilicate material, or a rare earth silicate having a formula selected from the group consisting of RE 2 O 3.SiO 2, 2RE 2 O 3.3SiO 2, RE 2 O 3.2SiO 2 and combinations thereof wherein RE is a rare earth element selected from the group consisting of Sc, Y, Dy, Ho, Er, Tm, Yb, Lu, Eu, Gd, Tb and combinations thereof overlying the substrate; and c) a transition layer overlying the environmental barrier layer, the transition layer comprising zirconia or hafnia stabilized with up to 10 mole % of an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals; and a low CTE oxide selected from the group consisting of niobia and tantala; and mixtures thereof; and d) a top coat overlying the transition layer, the top coat comprising zirconia or hafnia stabilized with up to 10 mole % of an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals, and mixtures thereof. a) a substrate formed of a silicon-comprising material; b) an environmental barrier layer comprising an alkaline earth metal aluminosilicate; or mullite or mixtures thereof with yttrium silicate or an alkaline earth metal aluminosilicate material, or a rare earth silicate having a formula selected from the group consisting of RE 2 O 3.SiO 2, 2RE 2 O 3.3SiO 2, RE 2 O 3.2SiO 2 and combinations thereof wherein RE is a rare earth element selected from the group consisting of Sc, Y, Dy, Ho, Er, Tm, Yb, Lu, Eu, Gd, Tb and combinations thereof overlying the substrate; and c) a transition layer overlying the environmental barrier layer, the transition layer comprising zirconia or hafnia stabilized with up to 10 mole % of an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals; and a low CTE oxide selected from the group consisting of niobia and tantala; and mixtures thereof; and d) a top coat overlying the transition layer, the top coat comprising zirconia or hafnia stabilized with up to 10 mole % of an oxide of a metal selected from the group consisting of magnesium, calcium, scandium, yttrium, and lanthanide metals, and mixtures thereof.
A rope grab comprising: a housing having an elongated member guide forming an elongated member passage, the elongated member passage configured and arranged to receive an elongated member; a locking cam pivotally coupled to the housing, the locking cam configured and arranged to selectively engage an elongated member received in the elongated member passage; a cam biasing member positioned to provide a relatively slight biasing force on the locking cam towards an elongated member received in the elongated member passage, the relatively slight biasing force being countered by gravity during normal operations of the rope grab_to allow the rope grab to move both up and down on the elongated member without the locking cam locking onto the elongated member during normal operations while inertial loads on the locking cam and the slight biasing force of the cam biasing member during a fall event work in tandem to rotate the locking cam onto the elongated member to lock the locking cam onto the elongated member in the elongated member passage; and a locking arm pivotally coupled to the housing, the locking arm having a first end configured and arranged to be coupled to a safety harness of a user and a second end configured and arranged to selectively engage the locking cam to selectively lock the locking cam onto the elongated member in the elongated member passage during a fall event. a housing having an elongated member guide forming an elongated member passage, the elongated member passage configured and arranged to receive an elongated member; a locking cam pivotally coupled to the housing, the locking cam configured and arranged to selectively engage an elongated member received in the elongated member passage; a cam biasing member positioned to provide a relatively slight biasing force on the locking cam towards an elongated member received in the elongated member passage, the relatively slight biasing force being countered by gravity during normal operations of the rope grab_to allow the rope grab to move both up and down on the elongated member without the locking cam locking onto the elongated member during normal operations while inertial loads on the locking cam and the slight biasing force of the cam biasing member during a fall event work in tandem to rotate the locking cam onto the elongated member to lock the locking cam onto the elongated member in the elongated member passage; and a locking arm pivotally coupled to the housing, the locking arm having a first end configured and arranged to be coupled to a safety harness of a user and a second end configured and arranged to selectively engage the locking cam to selectively lock the locking cam onto the elongated member in the elongated member passage during a fall event.
A component composed at least to some extent of a layer structure, where the layer structure comprises the following layers: (a) an elastomer layer with density greater than 800 g/L, (b) a thermoset layer comprising at least 50% by weight of a first polyurethane, where the shore hardness of the elastomer layer is less than 95 shore A in accordance with DIN ISO 7619-1:2010. (a) an elastomer layer with density greater than 800 g/L, (b) a thermoset layer comprising at least 50% by weight of a first polyurethane,