mhurhangee/ep-ind-claims huggingface dataset:
A method for producing hydrogen gas and optionally a carbonaceous product from a hydrocarbon fuel, comprising: introducing a flowing stream of said fuel into a reaction chamber of a reactor through one or more fuel inlet, wherein said reaction chamber has at least one wall and wherein a heating zone, which is heated by a heat source, is present in the reaction chamber, the heating zone beginning at, or shortly after, the fuel inlet(s) extending for at least a portion of the reaction chamber and being bounded by the reaction chamber wall(s), heating said fuel in said heating zone to effect pyrolytic decomposition of said hydrocarbon fuel to produce said hydrogen gas and optionally said carbonaceous product; wherein the ratio of C:O (mol/mol) in the reaction chamber is greater than 20:1; characterized in that the heat source heats the hydrocarbon fuel in the heating zone by radiated heat to an average temperature of greater than 2000 °C, the difference between the minimum and maximum fuel gas temperatures throughout the heating zone is no more than 250 °C, and the fuel gas flow through the heating zone is laminar. introducing a flowing stream of said fuel into a reaction chamber of a reactor through one or more fuel inlet, wherein said reaction chamber has at least one wall and wherein a heating zone, which is heated by a heat source, is present in the reaction chamber, the heating zone beginning at, or shortly after, the fuel inlet(s) extending for at least a portion of the reaction chamber and being bounded by the reaction chamber wall(s), heating said fuel in said heating zone to effect pyrolytic decomposition of said hydrocarbon fuel to produce said hydrogen gas and optionally said carbonaceous product; wherein the ratio of C:O (mol/mol) in the reaction chamber is greater than 20:1; characterized in that the heat source heats the hydrocarbon fuel in the heating zone by radiated heat to an average temperature of greater than 2000 °C, the difference between the minimum and maximum fuel gas temperatures throughout the heating zone is no more than 250 °C, and the fuel gas flow through the heating zone is laminar.
An assembly of a container and a lid in plastic material, comprising: a container having a side wall provided with an outer skirt configured with an upwardly open annular channel and an annular hooking rib inside the annular channel; a lid provided with a peripheral skirt downwardly extending from an annular channel, along a peripheral rim of the lid; in which the peripheral skirt of the container and the peripheral skirt of the lid are provided with snap engaging annular locking ribs (16, 17; 30, 32); characterised in that: the skirt of the lid is provided with a hooking crown to the annular rib of the channel of the skirt of the container, in which the hooking crown is outwardly extending from a peripheral rim of the skirt of the lid, and in which the hooking crown comprised a plurality of side by side arranged tabs separated by cross slits, each hooking tab being connected to the peripheral rim of the skirt of the lid by an elastically flexible hinge. a container having a side wall provided with an outer skirt configured with an upwardly open annular channel and an annular hooking rib inside the annular channel; a lid provided with a peripheral skirt downwardly extending from an annular channel, along a peripheral rim of the lid; in which the peripheral skirt of the container and the peripheral skirt of the lid are provided with snap engaging annular locking ribs (16, 17; 30, 32); characterised in that: the skirt of the lid is provided with a hooking crown to the annular rib of the channel of the skirt of the container, in which the hooking crown is outwardly extending from a peripheral rim of the skirt of the lid, and in which the hooking crown comprised a plurality of side by side arranged tabs separated by cross slits, each hooking tab being connected to the peripheral rim of the skirt of the lid by an elastically flexible hinge.
A locking device having a locking cylinder and a cylinder key, wherein the locking cylinder has a cylinder housing and a locking core supported rotatably in the cylinder housing, in which locking core at least one core pin is provided, which is supported in the locking core displaceably in the direction toward the cylinder key, and wherein a blocking element is provided in the locking cylinder, which blocking element engages at least one core pin and blocks it in such a way that the core pin can no longer be displaced in the direction of the cylinder key and in such a way that the blocking element is deactivatable by means of a magnet, and wherein the at least one core pin is formed by the first core pin oriented toward a key stop of the cylinder key, characterized in that the blocking element includes a tapered pin; that the core pin has an encompassing notch or an encompassing bead; and that the tapered pin engages the notch or rests on the bead.
A transparent, dyed cooktop with improved colour indication capability, made of a glass ceramic with high quartz solid solution as the predominant crystal phase, wherein the glass ceramic does not contain any of the chemical refining agents arsenic oxide and antimony oxide except for unavoidable traces, wherein the composition of the glass ceramic (in wt% on an oxide basis) substantially consists of Li 2 O 3.0 - 4.2 ∑ Na 2 O+K 2 O 0.2 - 1.5 MgO 0 - 1.5 ∑ CaO+SrO+BaO 0 - 4 ZnO 0 - 2 B 2 O 3 0 - 2 Al 2 O 3 19 - 23 SiO 2 60 - 69 TiO 2 2.5 - 4 ZrO 2 0.5 - 2 P 2 O 5 0 - 3 SnO 2 0.1 - < 0.6 ∑ TiO 2 +ZrO 2 +SnO 2 3.8 - 6 V 2 O 5 0.01 - 0.06 Fe 2 O 3 0.03 - 0.2; under the condition: 1 < Fe 2 O 3 / V 2 O 5 < 8; characterised by transmittance values of greater than 0.1 % within the range of visible light in the entire wavelength range greater than 450 nm, a light transmittance in the visible from 0.8 to 2.5 %, and a transmittance in the infrared at 1600 nm from 45 to 85 %.
A wing tip device for an aircraft wing, comprising: an upper winglet configured to extend upwardly from the aircraft wing; and a lower element extending downwardly from the upper winglet, and configured to form a closed loop below the aircraft wing, the closed loop having a hollow interior wherein the lower element comprises a lower loop mounted to a wing lower surface. an upper winglet configured to extend upwardly from the aircraft wing; and a lower element extending downwardly from the upper winglet, and configured to form a closed loop below the aircraft wing, the closed loop having a hollow interior wherein the lower element comprises a lower loop mounted to a wing lower surface.
A vertical falling film heat transfer tube for falling film evaporation of spent liquor, the heat transfer tube having: - a heating medium surface arranged to be heated by a heating medium; and - a falling film surface opposite and facing away from said heating medium surface, which falling film surface is arranged to have spent liquor containing lignin and other dissolved components from cellulosic material and/or inorganics from the cellulosic material and chemicals used passing over it as a falling film while evaporating solvent from the falling film and thus increasing the dry matter content; said heat transfer tube being made from a sheet metal material, e.g. an iron based high alloy stainless steel material with an alloy content above 16.00% for Chromium and above 1% for Nickel, preferably corresponding to corrosion resistant steel qualities at least like AISI 316 or AISI 304 characterized in that the falling film surface of the heat transfer tube is equipped with a multitude of wire bumps, each wire bump being spaced apart along the longitudinal axis of the heat transfer tube from a neighbouring wire bump by 3-300 mm; said wire bumps having a height (h) in the range 0,3-5.0 mm; said wire bumps having a width (w) in the range 0,3-5,0 mm; and said wire bumps having an inclination angle (α) versus a plane orthogonal to a longitudinal axis of the heat transfer tube in a range of 0-70 degrees. - a heating medium surface arranged to be heated by a heating medium; and - a falling film surface opposite and facing away from said heating medium surface, which falling film surface is arranged to have spent liquor containing lignin and other dissolved components from cellulosic material and/or inorganics from the cellulosic material and chemicals used passing over it as a falling film while evaporating solvent from the falling film and thus increasing the dry matter content; said heat transfer tube being made from a sheet metal material, e.g. an iron based high alloy stainless steel material with an alloy content above 16.00% for Chromium and above 1% for Nickel, preferably corresponding to corrosion resistant steel qualities at least like AISI 316 or AISI 304 characterized in that the falling film surface of the heat transfer tube is equipped with a multitude of wire bumps, each wire bump being spaced apart along the longitudinal axis of the heat transfer tube from a neighbouring wire bump by 3-300 mm; said wire bumps having a height (h) in the range 0,3-5.0 mm; said wire bumps having a width (w) in the range 0,3-5,0 mm; and said wire bumps having an inclination angle (α) versus a plane orthogonal to a longitudinal axis of the heat transfer tube in a range of 0-70 degrees.
A joint arrangement, comprising a hollow cylindrical receiving cylinder that extends in a cylinder axis direction and is designed to receive one end of a chair column of an active-dynamic wobble chair, the latter being movably mounted in a substantially hollow cylindrical outer joint shell that is composed of two or more parts made up of joint shell segments, the movable mounting of the receiving cylinder being achieved by means of deformable elastic elements that are arranged in a bearing gap between respectively an outer wall portion (21, 22) of the receiving cylinder and an inner wall portion (41, 42) of the joint shell and the receiving cylinder can be actuated in a force-dependent manner, which changes the shape and/or position of the elastic elements as a result of a change, preferably a reduction, in the clearance of the bearing gap as viewed in a radial direction (Rs) when the receiving cylinder is actuated in a cylinder axis direction.
A cleaning nozzle unit comprising: an inner liquid passage guiding a cleaning solution; an inner air passage feeding air to an outlet of the inner liquid passage; and an injection port that mixes the cleaning solution guided by the inner liquid passage and the air fed by the inner air passage and injects a mixture of the cleaning solution and the air to a surface of an object, wherein a plurality of the injection ports are provided, are disposed at predetermined intervals, characterized in that the plurality of the injection ports injects the mixtures in directions such that the mixtures hits each other in the surface at a substantially predetermined angle in a front view of the surface, wherein the cleaning nozzle unit comprises a lid body that closes the outlet of the inner liquid passage and opens the outlet of the inner liquid passage by elastically deforming by hydraulic pressure of the cleaning solution when the cleaning solution is fed to the inner liquid passage. an inner liquid passage guiding a cleaning solution; an inner air passage feeding air to an outlet of the inner liquid passage; and an injection port that mixes the cleaning solution guided by the inner liquid passage and the air fed by the inner air passage and injects a mixture of the cleaning solution and the air to a surface of an object, wherein a plurality of the injection ports are provided, are disposed at predetermined intervals, characterized in that the plurality of the injection ports injects the mixtures in directions such that the mixtures hits each other in the surface at a substantially predetermined angle in a front view of the surface, wherein the cleaning nozzle unit comprises a lid body that closes the outlet of the inner liquid passage and opens the outlet of the inner liquid passage by elastically deforming by hydraulic pressure of the cleaning solution when the cleaning solution is fed to the inner liquid passage.
Plug comprising a contact carrier which can be connected or is connected to a core of a cable and which supports contact elements extending in the direction of a plug axis, and comprising a shield contact arrangement which forms separate shield contact tongues formed by a sheet metal strip, which shield contact tongues extend on a first circular arc line about the plug axis and in the direction of the plug axis and can be connected or are connected to a cable shield, the shield contact tongues having contact springs which point radially outwards in an end portion lying in front of the contact elements and the contact carrier in the direction of the plug axis, characterised in that the contact springs are cut free from the shield contact tongues, forming an annularly enclosed window in each case, such that said springs are fastened to the shield contact tongue at a bending edge, which extends transversely to the plug axis and is associated with the free end of the shield contact tongue, and form two legs (6, 8) which are interconnected at an apex line, the apex lines extending on a common second circular arc line about the plug axis, which is radially outside the first circular arc line.
An integrated circuit device testing system comprising: a socket configured to receive an integrated circuit device, characterized in that the socket comprises at least one conductive trace made of a material with a resistivity that is a function of temperature, and wherein the socket is configured such that, when the integrated circuit device is located in the socket, the at least one conductive trace extends along a surface of the integrated circuit device; and a controller or active circuit configured to determine a temperature at the surface of the integrated circuit device based on a measured resistance of the at least one conductive trace. a socket configured to receive an integrated circuit device, characterized in that the socket comprises at least one conductive trace made of a material with a resistivity that is a function of temperature, and wherein the socket is configured such that, when the integrated circuit device is located in the socket, the at least one conductive trace extends along a surface of the integrated circuit device; and a controller or active circuit configured to determine a temperature at the surface of the integrated circuit device based on a measured resistance of the at least one conductive trace.
A method for generating a plurality of potential treatment plans, each treatment plan specifying a distribution of radiation to a target volume, the method being performed by a treatment planning system and comprising the steps of: performing multi-criteria optimization based on a set of optimization functions, wherein at least one optimization function depends on the distribution of the product of radiation dose and linear energy transfer, LET, in a specified region of the patient, yielding a plurality of treatment plans.
A method of disinfecting a room comprising a surface, the method comprising: - moving an irradiating unit to a first position in the room, - emitting radiation from the irradiating unit toward the surface, during a period of time, while determining an intensity of emitted radiation emitted to the surface, - determining a dose of radiation launched on the surface from the determined intensity and the period of time, - outputting information relating to the position and the determined dose, characterized in that the intensity delivered to the surface is determined from an intensity output from the emitter, a distance to the surface, and an angle between the radiation and the surface. - moving an irradiating unit to a first position in the room, - emitting radiation from the irradiating unit toward the surface, during a period of time, while determining an intensity of emitted radiation emitted to the surface, - determining a dose of radiation launched on the surface from the determined intensity and the period of time, - outputting information relating to the position and the determined dose,
Drop tower having - an inner space which extends in the tower, and - a payload carrier (25, 125, 125', 161, 171) for experimental constructions which can be moved in the inner space in a vertical direction in such a manner that during the movement a state of reduced gravitational force exists at least temporarily, - an acceleration capsule which is constructed to surround the payload carrier (25, 125, 125', 161, 171) and which can be moved so as to be controlled in a vertical manner by means of a linear drive, characterised by a coupling device (121, 121') which is configured to automatically couple the payload carrier (25, 125, 125', 161, 171) and the acceleration capsule in a positive-locking and/or non-positive-locking manner when the drive force which is controlled by the linear drive counter to gravitational force assumes a value greater than zero and to automatically decouple them from each other when the drive force controlled by the linear drive counter to gravitational force assumes a value which is less than or equal to zero, wherein the coupling device (121, 121') has a damping and/or resilient element (141, 141'), wherein the payload carrier (25, 125, 125', 161, 171) can be coupled by means of the damping and/or resilient element (141, 141') to the acceleration capsule so as to absorb acceleration forces, and wherein the damping and/or resilient element (141, 141') is constructed as a deformation member which can be compressed and decompressed in accordance with the acceleration forces acting thereon, and wherein the deformation member is a hollow member which has a connection for a fluid-conducting connection line to a storage container. - an inner space which extends in the tower, and - a payload carrier (25, 125, 125', 161, 171) for experimental constructions which can be moved in the inner space in a vertical direction in such a manner that during the movement a state of reduced gravitational force exists at least temporarily, - an acceleration capsule which is constructed to surround the payload carrier (25, 125, 125', 161, 171) and which can be moved so as to be controlled in a vertical manner by means of a linear drive,
A composition of triglycerides comprising in weight percent based on the weight of the composition: A. 30 to 70% C18:1 fatty acids; B. 10 to 55% of a mixture of C8 and C10 fatty acids in which the mixture comprises 50 to 70 wt%, based on the weight of the mixture, of C8 fatty acids; C. No more than 13% polyunsaturated fatty acids; and D. No more than 7% of saturated fatty acids of which each contains at least 12 carbon atoms. A. 30 to 70% C18:1 fatty acids; B. 10 to 55% of a mixture of C8 and C10 fatty acids in which the mixture comprises 50 to 70 wt%, based on the weight of the mixture, of C8 fatty acids; C. No more than 13% polyunsaturated fatty acids; and D. No more than 7% of saturated fatty acids of which each contains at least 12 carbon atoms.
Fastening system for mounting insulating elements, comprising an expansion nail and a dowel, wherein the expansion nail comprises an expansion nail head and an expansion nail shank, and wherein the dowel comprises a dowel shank and a connected thrust piece, characterized in that, the thrust piece is integrally connected with the dowel shank by means of a peripherally formed connecting element, wherein the connecting element is so designed that it breaks off circumferentially upon introducing the expansion nail into the dowel shank.
Injection-moulding device, comprising a. a first mould half and a second mould half, which is arranged to be moveable linearly in a first direction with respect to the first mould half, and b. a third mould half, which is arranged between the first mould half and the second mould half, and which interacts with the first mould half in the region of a first parting line in order to form first cavities, and which interacts with the second mould half in the region of a second parting line in order to form second cavities, wherein c. the third mould half has an upper part and a lower part spaced from each other by a slot, characterized in that d. a first drive shaft is arranged in the interior of the third mould half, wherein e. on the drive shaft, at least one carrier for an injection-moulded part is arranged adjustably in a radial direction via an arm, and wherein f. the first drive shaft is supported both with respect to the upper part and with respect to the lower part by at least one bearing (14, 15, 16, 17), and is thereby provided for centring the lower part with respect to the upper part. a. a first mould half and a second mould half, which is arranged to be moveable linearly in a first direction with respect to the first mould half, and b. a third mould half, which is arranged between the first mould half and the second mould half, and which interacts with the first mould half in the region of a first parting line in order to form first cavities, and which interacts with the second mould half in the region of a second parting line in order to form second cavities, wherein c. the third mould half has an upper part and a lower part spaced from each other by a slot, characterized in that d. a first drive shaft is arranged in the interior of the third mould half, wherein e. on the drive shaft, at least one carrier for an injection-moulded part is arranged adjustably in a radial direction via an arm, and wherein f. the first drive shaft is supported both with respect to the upper part and with respect to the lower part by at least one bearing (14, 15, 16, 17), and is thereby provided for centring the lower part with respect to the upper part.
A polycarbonate resin composition for a thin optical component, comprising, per 100 mass parts of a polycarbonate resin, 0.1 to 4 mass parts of a polyalkylene glycol copolymer having a linear alkylene ether unit given by general formula below and a branched alkylene ether unit selected from units given by general formulas (II-1) to (II-4) below, 0.005 to 0.5 mass parts of a phosphorus stabilizer, and 0.0005 to 0.2 mass parts of an epoxy compound [Chemical 1] -[-(CH 2) n -O-]- ··· wherein n in the formula is an integer from 3 to 6 [Chemical 2] -[-CR 1 R 2 -CR 3 R 4 -O-]- ··· (II-1) -[-CR 1 R 2 -CR 3 R 4 -CR 5 R 6 -O]- ··· (II-2) -[-CR 1 R 2 -CR 3 R 4 -CR 5 R 6 -CR 7 R 8 -O-]- ··· (II-3) -[-CR 1 R 2 -CR 3 R 4 -CR 5 R 6 -CR 7 R 8 -CR 9 R 10 -O-]- ··· (II-4) wherein, in formulas (II-1) to (II-4), R 1 to R 10 represent a hydrogen atom or an alkyl group having 1 to 3 carbons, and in each of formulas (II-1) to (II-4), at least one of R 1 to R 10 is an alkyl group having 1 to 3 carbons.