mhurhangee/ep-ind-claims huggingface dataset:
Coupling device (2, 60) for a connecting rod for attaching a component to a fuselage structure of an aircraft and/or for stiffening the fuselage structure, the coupling device (2, 60) having: a first coupling element (4, 62), and a second coupling element (20, 68), which can be coupled to the first coupling element (4, 62), wherein the first coupling element (4, 62) has an elongate body (16, 64), which has a first channel structure (32, 66) on a lateral surface along a first longitudinal axis, wherein the second coupling element (20, 68) has a hollow-cylindrical portion (22, 70), which, on an inner face along a second longitudinal axis, has a second channel structure (34, 76) complementing the first channel structure (32, 66), wherein the hollow-cylindrical portion (22, 70) has a radial cutout (26, 72) through which the elongate body (16, 64) can be inserted into the second channel structure (34, 76) from outside the hollow-cylindrical portion (22, 70) in a radial direction, wherein the second coupling element (20, 68) has a closure body (36, 78), which is designed to close the radial cutout (26, 72), can be positioned removably in the cutout (26, 72) and completes the second channel structure (34, 76) on a radially internal face, and wherein the second coupling element (20, 68) also has a securing element (46, 86), which can be pushed onto the hollow-cylindrical portion (22, 70) in order to secure the closure body (36, 78) on the hollow-cylindrical portion (22, 70). a first coupling element (4, 62), and a second coupling element (20, 68), which can be coupled to the first coupling element (4, 62), wherein the first coupling element (4, 62) has an elongate body (16, 64), which has a first channel structure (32, 66) on a lateral surface along a first longitudinal axis, wherein the second coupling element (20, 68) has a hollow-cylindrical portion (22, 70), which, on an inner face along a second longitudinal axis, has a second channel structure (34, 76) complementing the first channel structure (32, 66), wherein the hollow-cylindrical portion (22, 70) has a radial cutout (26, 72) through which the elongate body (16, 64) can be inserted into the second channel structure (34, 76) from outside the hollow-cylindrical portion (22, 70) in a radial direction, wherein the second coupling element (20, 68) has a closure body (36, 78), which is designed to close the radial cutout (26, 72), can be positioned removably in the cutout (26, 72) and completes the second channel structure (34, 76) on a radially internal face, and wherein the second coupling element (20, 68) also has a securing element (46, 86), which can be pushed onto the hollow-cylindrical portion (22, 70) in order to secure the closure body (36, 78) on the hollow-cylindrical portion (22, 70).
A method for producing a flat commutator for a dynamoelectric machine, which commutator comprises an insulating support body, a plurality of carbon segments and a plurality of conductor segments connected electrically conductively therewith, wherein the carbon segments define a substantially plane brush running surface and the conductor segments each have a rotor-winding terminal, the method comprising the following steps: preparation of an annular carbon disk; molding of the support body onto the annular carbon disk by injection-molding plastic material thereon in such a way that the support body bears interlockingly and frictionally thereon in radially outward position and radially inward position as well as on the end face of the annular carbon disk opposite the brush running surface; creation, in the support body, of openings that extend from a surface of the support body opposite the brush running surface to a surface of the carbon segments or of the annular carbon disk opposite the brush running surface; mounting of the conductor segments on the support body in such a way that a contact pin of the conductor segments passes respectively through one of the openings and at its free end contacts the surface of the carbon segments or of the annular carbon disk opposite the brush running surface; and separation of the annular carbon disk into carbon segments insulated from one another. preparation of an annular carbon disk; molding of the support body onto the annular carbon disk by injection-molding plastic material thereon in such a way that the support body bears interlockingly and frictionally thereon in radially outward position and radially inward position as well as on the end face of the annular carbon disk opposite the brush running surface; creation, in the support body, of openings that extend from a surface of the support body opposite the brush running surface to a surface of the carbon segments or of the annular carbon disk opposite the brush running surface; mounting of the conductor segments on the support body in such a way that a contact pin of the conductor segments passes respectively through one of the openings and at its free end contacts the surface of the carbon segments or of the annular carbon disk opposite the brush running surface; and separation of the annular carbon disk into carbon segments insulated from one another.
A method for identifying an Uplink, UL, Hybrid Automatic Repeat Request, HARQ, process of a backhaul link, comprising: a base station and a relay node identifying the UL HARQ process of the backhaul link according to a Downlink, DL, subframe number of the backhaul link, characterized in that the method further comprises identifying the UL HARQ process of the backhaul link according to the DL subframe number of the backhaul link comprises: summing the DL subframe number of the backhaul link and an DL_UL subframe interval between a current backhaul link DL subframe and a backhaul link UL subframe corresponding to the current backhaul link DL subframe, performing a modulo operation on the summation by a total UL HARQ process number, or a preset fixed value, or the minimum UL HARQ process time value, and taking a value obtained by the modulo operation as an identifier of the UL HARQ process to identify the UL HARQ process of the backhaul link, wherein the current backhaul link DL subframe bears corresponding ACK/NACK or UL grant for the backhaul link UL subframe; or, summing the DL subframe number and the DL_UL subframe interval, performing the modulo operation on the summation by the total UL HARQ process number, or the preset fixed value, or the minimum UL HARQ process time value, and taking a sum of a value obtained by the modulo operation and an adjustment amount as the identifier of the UL HARQ process to identify the UL HARQ process of the backhaul link, wherein an absolute value of the adjustment amount is an integer between 0 and the total UL HARQ process number. a base station and a relay node identifying the UL HARQ process of the backhaul link according to a Downlink, DL, subframe number of the backhaul link, characterized in that the method further comprises identifying the UL HARQ process of the backhaul link according to the DL subframe number of the backhaul link comprises: summing the DL subframe number of the backhaul link and an DL_UL subframe interval between a current backhaul link DL subframe and a backhaul link UL subframe corresponding to the current backhaul link DL subframe, performing a modulo operation on the summation by a total UL HARQ process number, or a preset fixed value, or the minimum UL HARQ process time value, and taking a value obtained by the modulo operation as an identifier of the UL HARQ process to identify the UL HARQ process of the backhaul link, wherein the current backhaul link DL subframe bears corresponding ACK/NACK or UL grant for the backhaul link UL subframe; or, summing the DL subframe number and the DL_UL subframe interval, performing the modulo operation on the summation by the total UL HARQ process number, or the preset fixed value, or the minimum UL HARQ process time value, and taking a sum of a value obtained by the modulo operation and an adjustment amount as the identifier of the UL HARQ process to identify the UL HARQ process of the backhaul link, wherein an absolute value of the adjustment amount is an integer between 0 and the total UL HARQ process number.
Polyester according to the following formula wherein R 1 and R 2 independently of one another are X-(OC 2 H 4) n -(OC 3 H 6) m wherein X is C 1-4 alkyl and preferably methyl, the -(OC 2 H 4) groups and the -(OC 3 H 6) groups are arranged blockwise and the block consisting of the -(OC 3 H 6) groups is bound to a COO group, n is based on a molar average a number of from 40 to 50, m is based on a molar average a number of from 1 to 10 and preferably of from 1 to 7, and a is based on a molar average a number of from 5 to 8. R 1 and R 2 independently of one another are X-(OC 2 H 4) n -(OC 3 H 6) m wherein X is C 1-4 alkyl and preferably methyl, the -(OC 2 H 4) groups and the -(OC 3 H 6) groups are arranged blockwise and the block consisting of the -(OC 3 H 6) groups is bound to a COO group, n is based on a molar average a number of from 40 to 50, m is based on a molar average a number of from 1 to 10 and preferably of from 1 to 7, and a is based on a molar average a number of from 5 to 8.
Supply quantity adjustment device, comprising: a total demand quantity calculation unit that is configured to calculate a total demand quantity (CPV_1) of a product gas produced by at least one air separation apparatus and used at at least one supply destination, based on plant information acquired from the at least one supply destination; • an excess/deficit information setting unit that is configured to compare the total demand quantity (CPV_1) and a pre-set flow rate set value (SV_1) and to set a first calculated pressure value (MV_1); • a backup coefficient setting unit that is configured to set a backup coefficient set value (MV_bc) based on a pre-set supply-destination reference gasholder pressure (SV_gh), the first calculated pressure value (MV_1), a pre-set reference backup pressure set value (SV_bc), and a measured gasholder pressure value (PV_gh), which is the measured pressure value of a supply-destination gasholder; and • a production coefficient setting unit that is configured to set a production coefficient (MV_a) by comparing a production pressure set value (SV_a) obtained by adding the pre-set supply-destination reference gasholder pressure (SV_gh) and the first calculated pressure value (MV_1) with the measured gasholder pressure value (PV_gh), wherein setting the production coefficient (MV_a) is performed so as to modify a variation in the quantity of the product gas produced by the at least one air separation apparatus. • an excess/deficit information setting unit that is configured to compare the total demand quantity (CPV_1) and a pre-set flow rate set value (SV_1) and to set a first calculated pressure value (MV_1); • a backup coefficient setting unit that is configured to set a backup coefficient set value (MV_bc) based on a pre-set supply-destination reference gasholder pressure (SV_gh), the first calculated pressure value (MV_1), a pre-set reference backup pressure set value (SV_bc), and a measured gasholder pressure value (PV_gh), which is the measured pressure value of a supply-destination gasholder; and • a production coefficient setting unit that is configured to set a production coefficient (MV_a) by comparing a production pressure set value (SV_a) obtained by adding the pre-set supply-destination reference gasholder pressure (SV_gh) and the first calculated pressure value (MV_1) with the measured gasholder pressure value (PV_gh), wherein setting the production coefficient (MV_a) is performed so as to modify a variation in the quantity of the product gas produced by the at least one air separation apparatus.
A crown element for securing a packing in a mass transfer column, - comprising an elongate sheet, which comprises a roof element, a wall element and a bottom element, - wherein the wall element is arranged between the roof element and the bottom element, such that a first bending line is formed between the roof element and the wall element, and a second bending line is formed between the wall element and the bottom element, wherein a protrusion is arranged on the wall element, - wherein the roof element is disposed with a plurality of incisions, wherein the roof element is composed of a plurality of roof element segments, wherein each of the roof element segments has a length which is in the range of 40 and 120 mm, - wherein the bottom element is disposed with a plurality of grooves, - wherein the number of incisions is smaller than the number of grooves, and - wherein the wall element, the roof element and the bottom element has a thickness of 0.05 to less than 0.2 mm, and - wherein the wall element is composed of a plurality of first surfaces having the shape of a trapezoid and a plurality of second surfaces being triangular, wherein each of the first surfaces touches two neighbouring second surfaces along a pair of common edge lines (33, 34) and each of the second surfaces touches two neighbouring first surfaces along a pair of common edge lines (34, 35). - comprising an elongate sheet, which comprises a roof element, a wall element and a bottom element, - wherein the wall element is arranged between the roof element and the bottom element, such that a first bending line is formed between the roof element and the wall element, and a second bending line is formed between the wall element and the bottom element, wherein a protrusion is arranged on the wall element, - wherein the roof element is disposed with a plurality of incisions, wherein the roof element is composed of a plurality of roof element segments, wherein each of the roof element segments has a length which is in the range of 40 and 120 mm, - wherein the bottom element is disposed with a plurality of grooves, - wherein the number of incisions is smaller than the number of grooves, and - wherein the wall element, the roof element and the bottom element has a thickness of 0.05 to less than 0.2 mm, and - wherein the wall element is composed of a plurality of first surfaces having the shape of a trapezoid and a plurality of second surfaces being triangular, wherein each of the first surfaces touches two neighbouring second surfaces along a pair of common edge lines (33, 34) and each of the second surfaces touches two neighbouring first surfaces along a pair of common edge lines (34, 35).
An insulated pipe comprising: an encasement pipe and a first inner pipe arranged inside said encasement pipe, at least one vacuum insulation panel comprising a porous core material and a multi-layer envelope encasing said porous core material, wherein said multi-layer envelope comprises at least one layer comprising a metal material, wherein said at least one vacuum insulation panel is arranged around the circumference of said first inner pipe, wherein said at least one vacuum insulation panel comprises an inward-facing side facing towards a longitudinal axis of said first inner pipe, an outward-facing side facing the opposite direction, and four side faces arranged between said inward-facing side and said outward-facing side, and said insulated pipe further comprising a polymer foam filling the space between said vacuum insulation panel and said encasement pipe, wherein at least at the portion of said multi-layer envelope located at said four side faces any layer comprising a metal material is at least one metallized polymer layer. an encasement pipe and a first inner pipe arranged inside said encasement pipe, at least one vacuum insulation panel comprising a porous core material and a multi-layer envelope encasing said porous core material, wherein said multi-layer envelope comprises at least one layer comprising a metal material, wherein said at least one vacuum insulation panel is arranged around the circumference of said first inner pipe, wherein said at least one vacuum insulation panel comprises an inward-facing side facing towards a longitudinal axis of said first inner pipe, an outward-facing side facing the opposite direction, and four side faces arranged between said inward-facing side and said outward-facing side, and wherein said multi-layer envelope comprises at least one layer comprising a metal material, wherein said at least one vacuum insulation panel is arranged around the circumference of said first inner pipe, wherein said at least one vacuum insulation panel comprises an inward-facing side facing towards a longitudinal axis of said first inner pipe, an outward-facing side facing the opposite direction, and four side faces arranged between said inward-facing side and said outward-facing side, and said insulated pipe further comprising a polymer foam filling the space between said vacuum insulation panel and said encasement pipe, wherein at least at the portion of said multi-layer envelope located at said four side faces any layer comprising a metal material is at least one metallized polymer layer.
Seating assembly for a vehicle, in particular a vehicle bench, with a seating surface element which is positioned on a seating surface substructure, wherein converting means are provided, by means of which by moving away the seating surface element the seating assembly can be converted into a vehicle seat, characterised in that with said vehicle seat with a second seating surface element different from the seating surface element an adjusted seating position transverse to the seating position of the seating assembly is provided for a person in the vehicle seat, wherein the converting means are designed to form at least the backrest element of the vehicle seat by folding up the seating surface element of the seating assembly and wherein on one side of the seating surface element, which is rearward to the seating surface of the seating surface element, a backrest contour is formed for the vehicle seat.
A method for determining a lifetime of an LED gear, the method comprising the steps of: - receiving first information from the LED gear, the first information representing a thermal load on at least one electronic component, in particular an electrolytic capacitor, of the LED gear; - calculating an expected thermal lifetime of the LED gear based on the first information, characterised by - receiving second information from the LED gear, the second information representing a number of erase/write/read cycles of a memory of the LED gear and/or an amount of data transferred to/from the memory of the LED gear; calculating an expected memory lifetime of the LED gear based on the second information; and - determining the lifetime of the LED gear based on the expected thermal lifetime and the expected memory lifetime. - receiving first information from the LED gear, the first information representing a thermal load on at least one electronic component, in particular an electrolytic capacitor, of the LED gear; - calculating an expected thermal lifetime of the LED gear based on the first information, - receiving second information from the LED gear, the second information representing a number of erase/write/read cycles of a memory of the LED gear and/or an amount of data transferred to/from the memory of the LED gear; calculating an expected memory lifetime of the LED gear based on the second information; and - determining the lifetime of the LED gear based on the expected thermal lifetime and the expected memory lifetime.
A method of changing a tool attached to a spindle of a machine tool with a next tool (T') positioned at a standby position by using a tool change arm having a tool gripper at each of both ends thereof and provided to be rotated about an axis of a support shaft disposed parallel to the spindle of the machine tool and to be moved forward and backward along a direction of the axis of the support shaft, the tool attached to the spindle of the machine tool being changed with the next tool (T') positioned at the standby position by executing: a gripping operation of rotating the tool change arm about the axis of the support shaft from an original position so as to cause one of the tool grippers to grip the tool attached to the spindle and cause the other of the tool grippers to grip the next tool (T') positioned at the standby position; a pulling operation of moving the tool change arm forward along the support shaft so as to pull the tool out of the spindle, a positioning operation of rotating the tool change arm about the axis of the support shaft so as to position the next tool (T') gripped by the other of the tool grippers on an axis of the spindle; an attaching operation of moving the tool change arm backward along the support shaft so as to attach the next tool (T') gripped by the other of the tool grippers to the spindle; and a returning operation of rotating the tool change arm about the axis of the support shaft so as to return the tool change arm to the original position, characterized in that the tool change arm is rotated by 180+n∗360 degrees in the positioning operation, n being a positive integer. a gripping operation of rotating the tool change arm about the axis of the support shaft from an original position so as to cause one of the tool grippers to grip the tool attached to the spindle and cause the other of the tool grippers to grip the next tool (T') positioned at the standby position; a pulling operation of moving the tool change arm forward along the support shaft so as to pull the tool out of the spindle, a positioning operation of rotating the tool change arm about the axis of the support shaft so as to position the next tool (T') gripped by the other of the tool grippers on an axis of the spindle; an attaching operation of moving the tool change arm backward along the support shaft so as to attach the next tool (T') gripped by the other of the tool grippers to the spindle; and a returning operation of rotating the tool change arm about the axis of the support shaft so as to return the tool change arm to the original position, characterized in that the tool change arm is rotated by 180+n∗360 degrees in the positioning operation, n being a positive integer.
A composite laminate structure, comprising: a first carbon fiber reinforced plastic laminate having a first electrical impedance; a second carbon fiber reinforced plastic laminate having a second electrical impedance substantially matching the first electrical impedance; and an adhesive bondline between the first and second laminates, the adhesive bondline including an adhesive and a scrim having a third electrical impedance substantially matching the first and second electrical impedances. a first carbon fiber reinforced plastic laminate having a first electrical impedance; a second carbon fiber reinforced plastic laminate having a second electrical impedance substantially matching the first electrical impedance; and an adhesive bondline between the first and second laminates, the adhesive bondline including an adhesive and a scrim having a third electrical impedance substantially matching the first and second electrical impedances.
A hardenable two part acrylic composition comprising an acrylic polymer composition first part and an acrylic monomer composition second part, the acrylic polymer composition comprising a first type of acrylic polymer particles characterized in that each first type of acrylic polymer particle is formed of a network of coalesced emulsion polymerized acrylic microparticles, wherein the network of coalesced emulsion polymerized acrylic microparticles form a porous acrylic polymer particle and wherein the first type of acrylic polymer particles have an average particle size of 1-300 microns as determined by the measurement method according to the description.