mhurhangee/ep-ind-claims huggingface dataset:
A vacuum heat performance testing device for a two-phase fluid loop comprising a heat radiation plate, temperature-controlled heaters, multilayer heat insulation assemblies, temperature sensors, a simulated heat source and a loop support, wherein the heat radiation plate is mounted at the upper part of the loop support in a way of heat insulation realized by a heat insulation cushion; a condensation pipeline of the two-phase fluid loop is embedded in the heat radiation plate, and a liquid reservoir of the two-phase fluid loop is semi-embedded in the heat radiation plate; an evaporator of the two-phase fluid loop is mounted at the lower part of the loop support in a heat insulation way; the temperature-controlled heaters are mounted on a steam pipeline, the liquid reservoir, a control valve and a liquid pipeline of the two-phase fluid loop; the temperature sensors are mounted on edge regions of the evaporator, the steam pipeline, the condensation pipeline, the liquid reservoir, the control valve, the liquid pipeline, the simulated heat source and the heat radiation plate; the steam pipeline, the liquid reservoir, the control valve and the liquid pipeline are wrapped by the multilayer heat insulation assemblies; the simulated heat source is an RHU isotopic electric simulated heat source and is fixedly mounted in the evaporator; a heat radiation plate heater for providing a working temperature for the heat radiation plate is mounted, and the heat radiation plate heater is an infrared heater mounted in a space at the outer side of the heat radiation plate or heating fins stuck to the heat radiation plate; the loop support is placed in a vacuum cabin; wherein the evaporator is mounted on a heat insulation plate, the simulated heat source is placed inside the evaporator, a lug of a tool of the simulated heat source is fixedly arranged on the heat insulation plate by a screw and a heat insulation cushion, and the heat insulation plate is fixedly mounted on the loop support by four heat insulation columns; the simulated heat source is used for controlling the temperature of the evaporator and maintaining the temperature of the evaporator at -55-50 ° C; the heat radiation plate heater is used for controlling the temperature of the heat radiation plate and maintaining the temperature of the heat radiation plate at -60-50 ° C; and the temperature-controlled heaters are used for preventing the steam pipeline, the liquid reservoir, the control valve and the liquid pipeline from being frozen, and self-control thresholds of the temperature-controlled heaters are set to be -55 to -30 ° C.
A metal complex represented by the following Formula: wherein M represents palladium or platinum; L represents a ligand selected from carbon monoxide, an olefin compound, an amine compound, a phosphine compound, an N-heterocyclic carbene compound, a nitrile compound and an isocyanide compound; n represents an integer of 0 to 2 showing the number of the ligand; and each of R 1 to R 4 represents an organic group.
A current collector arrangement arranged to be mounted on a vehicle and to transmit electric power between a current conductor (130; 230; 330; 430; 530) located in the surface of a road and the vehicle, wherein the current collector arrangement comprises a current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050) that is arranged to be controllable for at least vertical displacement relative to a longitudinal axis of the vehicle, in order to position the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050) to allow power transmission from the current conductor (130; 230; 330; 430; 530); the current collector arrangement comprising; - controllable actuators arranged to effect at least the vertical displacement of the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050); and - an electronic control unit for controlling at least power transmission in and displacement of the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050); characterized in that the current collector arrangement further comprises - a first actuator (481; 581; 681; 781; 881; 981; 1081) arranged to lower the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050) from a retracted position into a deployed position where electric power can be transmitted from the current conductor to the current collector; - a second actuator (482; 582; 682; 782; 882; 982; 1082) arranged to lift the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050) from the deployed position into the retracted position; and that during a vertical displacement effected by one of the first or second actuators, the other actuator is arranged to act as a damper. - controllable actuators arranged to effect at least the vertical displacement of the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050); and - an electronic control unit for controlling at least power transmission in and displacement of the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050); characterized in that the current collector arrangement further comprises - a first actuator (481; 581; 681; 781; 881; 981; 1081) arranged to lower the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050) from a retracted position into a deployed position where electric power can be transmitted from the current conductor to the current collector; - a second actuator (482; 582; 682; 782; 882; 982; 1082) arranged to lift the current collector arm (150; 250; 350; 450; 550; 650; 750; 850; 950; 1050) from the deployed position into the retracted position; and
A process for preparing a racemic cyclopentenone of Formula I wherein P 1 a protecting group for the phenol group, comprising the steps of: (a) reacting furan with an acyl donor of the acid compound of Formula V to form a 2-acylfuran of Formula IV (b) reacting the 2-acylfuran of Formula IV with a reducing agent to form the corresponding furancarbinol compound of formula III: and (c) subjecting the furancarbinol compound of formula III to a rearrangement and isomerization to form the racemic compound of Formula I. (a) reacting furan with an acyl donor of the acid compound of Formula V to form a 2-acylfuran of Formula IV (b) reacting the 2-acylfuran of Formula IV with a reducing agent to form the corresponding furancarbinol compound of formula III: and (c) subjecting the furancarbinol compound of formula III to a rearrangement and isomerization to form the racemic compound of Formula I.
A leading edge high-lift device deployable from a wing of an aircraft, the leading edge high-lift device comprising: a leading edge; a trailing edge; a lower surface and an upper surface both extending between the leading edge and the trailing edge; a trailing edge region being defined by the trailing edge and an adjacent region thereto; and a shaping device disposed at the trailing edge region, the shaping device moveable between a non-activated position and an activated position; wherein the shaping device is hingedly coupled to the lower surface at the trailing edge region, characterized in that the shaping device is configured to be activated via aerodynamic forces, wherein the shaping device engages a stop in the activated position. a leading edge; a trailing edge; a lower surface and an upper surface both extending between the leading edge and the trailing edge; a trailing edge region being defined by the trailing edge and an adjacent region thereto; and a shaping device disposed at the trailing edge region, the shaping device moveable between a non-activated position and an activated position;
A method for manufacturing sintered ore comprising: charging sintering raw material comprising fine ore and carbon material on a circulatively moving pallet to form a raw material layer; igniting the carbon material on a surface of the raw material layer and sucking air from above the raw material layer down to below the palette so that the air is introduced into the raw material layer; and combusting the carbon material in the raw material layer to thereby manufacture sintered ore, wherein fuel gas is discharged from a nozzle at a flow speed of 40 Nm/s or more, the discharged fuel gas is combusted to generate combustion gas, and the combustion gas is used for the igniting the carbon material, wherein the combustion gas is generated using a burner comprising: a main burner part having a fuel gas nozzle configured to discharge the fuel gas and an air nozzle configured to discharge air for combustion; and a sub burner part positioned further outward than the main burner part and configured to combust the fuel gas discharged from the main burner part. charging sintering raw material comprising fine ore and carbon material on a circulatively moving pallet to form a raw material layer; igniting the carbon material on a surface of the raw material layer and sucking air from above the raw material layer down to below the palette so that the air is introduced into the raw material layer; and combusting the carbon material in the raw material layer to thereby manufacture sintered ore, wherein fuel gas is discharged from a nozzle at a flow speed of 40 Nm/s or more, the discharged fuel gas is combusted to generate combustion gas, and the combustion gas is used for the igniting the carbon material, wherein the combustion gas is generated using a burner comprising: a main burner part having a fuel gas nozzle configured to discharge the fuel gas and an air nozzle configured to discharge air for combustion; and a sub burner part positioned further outward than the main burner part and configured to combust the fuel gas discharged from the main burner part. a main burner part having a fuel gas nozzle configured to discharge the fuel gas and an air nozzle configured to discharge air for combustion; and a sub burner part positioned further outward than the main burner part and configured to combust the fuel gas discharged from the main burner part.
Seating device, in particular airplane seating device, with at least one lateral baggage bar (10a; 10b), which is configured to be mounted underneath a seat (12a; 12b) on a side of the seat (12a; 12b) facing toward an aisle of a passenger cabin, the lateral baggage bar (10a; 10b) extending from its front end (34a; 34b) at least substantially parallel to the cabin floor toward a rear region of the seat (12a; 12b), and with at least one carrier element (14a; 14b) that is configured to receive a support force, characterised in that the carrier element (14a; 14b) is realized by a step element providing a stepping zone that is elevated with respect to the cabin floor, and that the carrier element (14a; 14b) and the baggage bar (10a; 10b) have at least one coupling point (16a; 16b) via which the baggage bar (10a; 10b) and the carrier element (14a; 14b) are connected to each other in a form-fit and/or force-fit manner and/or by substance-to-substance bond, the coupling point (16a; 16b) being configured to transfer at least a portion of the support force from the carrier element (14a; 14b) to the baggage bar (10a; 10b). with at least one lateral baggage bar (10a; 10b), which is configured to be mounted underneath a seat (12a; 12b) on a side of the seat (12a; 12b) facing toward an aisle of a passenger cabin, the lateral baggage bar (10a; 10b) extending from its front end (34a; 34b) at least substantially parallel to the cabin floor toward a rear region of the seat (12a; 12b), and with at least one carrier element (14a; 14b) that is configured to receive a support force, characterised in that the carrier element (14a; 14b) is realized by a step element providing a stepping zone that is elevated with respect to the cabin floor, and that the carrier element (14a; 14b) and the baggage bar (10a; 10b) have at least one coupling point (16a; 16b) via which the baggage bar (10a; 10b) and the carrier element (14a; 14b) are connected to each other in a form-fit and/or force-fit manner and/or by substance-to-substance bond, the coupling point (16a; 16b) being configured to transfer at least a portion of the support force from the carrier element (14a; 14b) to the baggage bar (10a; 10b).
Process for producing bakery produce with the steps of: 1. producing a first dough for a first dough layer, producing a second dough for a second dough layer, wherein the first and the second doughs have different colouring: 2. rolling out of the first dough to a first thickness and generating incisions that at least in part span the first thickness, subsequent stretching of the first dough for dilating or opening of the incisions for producing a first dough layer having dilated or opened incisions; 3. rolling out of the first dough to a second thickness for producing a second dough layer; 4. arranging the first dough layer that has dilated or opened incisions, adjacent to the second dough layer; 5. rolling out of the arrangement comprising the first and the adjacent second dough layers (10, 16) for producing a flat dough composite of uniform thickness having a first and a second dough layer (1, 2) which has a continuous surface in which recesses formed of the dilated or opened incisions in the first dough layer are filled by the second dough layer. 1. producing a first dough for a first dough layer, producing a second dough for a second dough layer, wherein the first and the second doughs have different colouring: 2. rolling out of the first dough to a first thickness and generating incisions that at least in part span the first thickness, subsequent stretching of the first dough for dilating or opening of the incisions for producing a first dough layer having dilated or opened incisions; 3. rolling out of the first dough to a second thickness for producing a second dough layer; 4. arranging the first dough layer that has dilated or opened incisions, adjacent to the second dough layer; 5. rolling out of the arrangement comprising the first and the adjacent second dough layers (10, 16) for producing a flat dough composite of uniform thickness having a first and a second dough layer (1, 2) which has a continuous surface in which recesses formed of the dilated or opened incisions in the first dough layer are filled by the second dough layer.
Combustion system comprising at least one combustion module and at least one source of at least one combustible gas and one oxidizing gas, said combustion module comprising: - a one-piece body including several combustion chambers (C1, C2, C3, C4) intended to be supplied by the source of at least one combustible gas and one oxidizing gas, - means for initiating combustion in combustion chambers, characterized in that the combustion system also comprises: - a first connector in contact with a first end of the body, said first connector being made of a material that is heat insulating relative to that of the body, the first connector including conduits for supplying combustible gas and connected to the source of at least one combustible gas and one oxidizing gas, and conduits for evacuating combustion gas, the first connector including as many conduits for supplying and conduits for evacuating as combustion chambers, - a second connector in contact with a second end of the body, said second connector being made of a material that is heat insulating relative to that of the body, said second connector including conduits for supplying combustible gas and oxidizing gas and connected to the source of at least one combustible gas and one oxidizing gas, and conduits for evacuating combustion gas, the second connector including as many conduits for supplying and conduits for evacuating as combustion chambers. - a one-piece body including several combustion chambers (C1, C2, C3, C4) intended to be supplied by the source of at least one combustible gas and one oxidizing gas, - means for initiating combustion in combustion chambers, - a first connector in contact with a first end of the body, said first connector being made of a material that is heat insulating relative to that of the body, the first connector including conduits for supplying combustible gas and connected to the source of at least one combustible gas and one oxidizing gas, and conduits for evacuating combustion gas, the first connector including as many conduits for supplying and conduits for evacuating as combustion chambers, - a second connector in contact with a second end of the body, said second connector being made of a material that is heat insulating relative to that of the body, said second connector including conduits for supplying combustible gas and oxidizing gas and connected to the source of at least one combustible gas and one oxidizing gas, and conduits for evacuating combustion gas, the second connector including as many conduits for supplying and conduits for evacuating as combustion chambers.
Method of control of an SDN network, known as an IP core network, said IP core network including at least one first and one second router connected to an external packet data network and a plurality of switches capable of connecting at least one base station of a network for access to the first and second routers, said packet data network being capable of transmitting data streams through the IP core network destined for terminals attached to the at least one base station, data streams currently being routed between the external network and at least one terminal, the method including a step (E301, E302, E303) for establishing one stream processing rule per stream received by the first router, characterized in that the method of control further includes: • a step of assigning the second router as backup router for the first router; • a step (E201, E202) of transmitting to the external packet data network an item of information relating to said assignment of the backup router; • a step of detecting an event relating to a failure of the first router; • a step of transmitting to the backup router all of the established processing rules for the first router, intended to be applied by the backup router, the transmission step being triggered by the step of detecting an event relating to a failure of the first router. • a step of assigning the second router as backup router for the first router; • a step (E201, E202) of transmitting to the external packet data network an item of information relating to said assignment of the backup router; • a step of detecting an event relating to a failure of the first router; • a step of transmitting to the backup router all of the established processing rules for the first router, intended to be applied by the backup router, the transmission step being triggered by the step of detecting an event relating to a failure of the first router.
A control unit for a node of a network, comprising: a phase-adaptation module for adjusting at least one operation parameter of the node based on a current network phase out of a plurality of network phases; and wherein a node is adapted to be switched to one of the plurality of network phases; a phase-aware module for processing a received data packet based on the operation parameter, wherein the node is switchable to an intermediate network phase, wherein the intermediate network phase is time or area limited. a phase-adaptation module for adjusting at least one operation parameter of the node based on a current network phase out of a plurality of network phases; and wherein a node is adapted to be switched to one of the plurality of network phases; a phase-aware module for processing a received data packet based on the operation parameter, wherein the node is switchable to an intermediate network phase, wherein the intermediate network phase is time or area limited.
A duplex stainless steel having a chemical composition of, in mass %: up to 0.03 % C; 0.1 to 0.8 % Si; lower than 2.0 % Mn; up to 0.040 % P; up to 0.010 % S; up to 0.040 % sol. Al; 3 to 7 % Ni; 20 to 28 % Cr; 0.5 to 2.0 % Mo; more than 2.0 % and not more than 4.0 % Cu; 0.02 to 0.5 % Co; 0.1 to 0.35 % N; up to 0.010 % O; 0 to 1.5 % V; 0 to 0.02 % Ca; 0 to 0.02 % Mg; 0 to 0.02 % B; 0 to 0.2 % REM; and the balance being Fe and impurities, the duplex stainless steel having a microstructure including an austenite phase and a ferrite phase, the ferrite phase having an area percentage of 30 to 60 %, the duplex stainless steel satisfying the following Formula,: 0.70 × Ni L ≤ Ni H where Ni H and Ni L are obtained by using an electron-beam microanalyzer using electron beams with an acceleration voltage of 15kV to measure Ni content at points separated by 0.6 μm in an area of 300×300 μm 2 and, in a distribution histogram of Ni content with a class width of 0.05 mass %, two maximum values appear, which correspond to the austenite phase and ferrite phase, and treating the one with a higher Ni content as Ni H and treating the one with a lower Ni content as Ni L wherein the following Formula,, is satisfied: 1 − AE − 60 / AE − 20 × 100 ≤ 8 where AE- 60 and AE- 20 indicate values of absorbed energy of the steel at -60 °C and -20 °C, respectively, as measured by the testing method in accordance with ASTM A370, and a shear fracture percentage of the steel at -20 °C is 100%. up to 0.03 % C; 0.1 to 0.8 % Si; lower than 2.0 % Mn; up to 0.040 % P; up to 0.010 % S; up to 0.040 % sol. Al; 3 to 7 % Ni; 20 to 28 % Cr; 0.5 to 2.0 % Mo; more than 2.0 % and not more than 4.0 % Cu; 0.02 to 0.5 % Co; 0.1 to 0.35 % N; up to 0.010 % O; 0 to 1.5 % V; 0 to 0.02 % Ca; 0 to 0.02 % Mg; 0 to 0.02 % B; 0 to 0.2 % REM; and the balance being Fe and impurities, the duplex stainless steel having a microstructure including an austenite phase and a ferrite phase, the ferrite phase having an area percentage of 30 to 60 %, the duplex stainless steel satisfying the following Formula,: 0.70 × Ni L ≤ Ni H where Ni H and Ni L are obtained by using an electron-beam microanalyzer using electron beams with an acceleration voltage of 15kV to measure Ni content at points separated by 0.6 μm in an area of 300×300 μm 2 and, in a distribution histogram of Ni content with a class width of 0.05 mass %, two maximum values appear, which correspond to the austenite phase and ferrite phase, and treating the one with a higher Ni content as Ni H and treating the one with a lower Ni content as Ni L wherein the following Formula,, is satisfied: 1 − AE − 60 / AE − 20 × 100 ≤ 8 where AE- 60 and AE- 20 indicate values of absorbed energy of the steel at -60 °C and -20 °C, respectively, as measured by the testing method in accordance with ASTM A370, and a shear fracture percentage of the steel at -20 °C is 100%. where AE- 60 and AE- 20 indicate values of absorbed energy of the steel at -60 °C and -20 °C, respectively, as measured by the testing method in accordance with ASTM A370, and a shear fracture percentage of the steel at -20 °C is 100%.