mhurhangee/patent-ind-claim-en huggingface dataset:
A cabinless construction vehicle , with a roll bar , comprising a pair of vertical supports arranged in a rear region of an operator platform of the construction vehicle, each vertical support having in each case a side beam fixedly arranged on the construction vehicle and a pivoting beam , which are connected to one another via first articulated connections and are adjustable relative to one another between a protection position and a transport position of the roll bar , a weather protection device with a roof cover for the operator platform being arranged on the roll bar , the roof cover of the weather protection device being movably mounted on the roll bar in such a manner that it is adjustable together with the roll bar between a deployed weather protection position when the roll bar is in the protection position and a storage position when the roll bar is in the transport position, characterized in that the roof cover is adjustable into a rear-side position below the operator platform by releasing a first arrest of an actuator of the first articulated connections , and wherein the roof cover is arrestable in its storage position in an angular position almost parallel to the pair of pivoting beams .
A method for producing an aliphatic polyester, comprising a step of contacting a solution containing a cyclic ester with a cyclic amine catalyst and a polymerization initiator and lowering the temperature from room temperature to initiate a reaction, a step of conducting the reaction by flow-type polymerization, and a step of subjecting the product obtained in the flow-type polymerization to further reaction by postpolymerization by stirring.
Gearing assembly for torque transmission, comprising - an epicyclic gearing unit having two ring gears (3.1, 3.2) which each have a toothing (V3.1, V3.2), the number of teeth thereof being different, wherein at least three planetary gears (3.5 to 3.7) roll in the two ring gears (3.1, 3.2), wherein one of the ring gears (3.1) is stationary and the other ring gear (3.2) is designed to be movable, characterized in that two of the planetary gears (3.5, 3.6) have a two-piece design in the form of partial bearing gears (3.5.1 to 3.6.2) which are separate from one another and which roll independently in the ring gears (3.1, 3.2), and a third planetary gear (3.7) has a one-piece design and rolls in the two ring gears (3.1, 3.2) in the form of a force-transmitting gear. - an epicyclic gearing unit having two ring gears (3.1, 3.2) which each have a toothing (V3.1, V3.2), the number of teeth thereof being different, wherein at least three planetary gears (3.5 to 3.7) roll in the two ring gears (3.1, 3.2), wherein one of the ring gears (3.1) is stationary and the other ring gear (3.2) is designed to be movable,
An apparatus for actuating a rocking motion of a movable component , the apparatus comprising : • an actuator , • a lever configured to be subjected by the actuator to an angular displacement in two opposite directions with respect to a neutral positional range, • a support plate that is stationary with respect to the lever , • a movable component and a force transfer element attached to the movable component , wherein the lever is provided with a pair of oppositely placed pawls , the pawls being shaped so as to engage with the force transfer element and wherein the support plate is configured for forcing the pawls to pivot away from the force transfer element so that any interaction between the pawls and the force transfer element is prohibited, characterized in that the pawls and the support plate are configured so that: - both pawls are prohibited by the support plate from engaging with the force transfer element when the lever is within the neutral positional range, - the force transfer element and thereby the movable component is displaced in the first of the two opposite directions by the first pawl engaging with the force transfer element , when the lever exits the neutral positional range in the first direction, - the force transfer element and thereby the movable component is displaced into the second of the two opposite directions by the second pawl engaging with the force transfer element , when the lever exits the neutral positional range in the second direction, and - when the pawl that is not actuating a motion of the force transfer element approaches the support plate , the pawl is forced by the support plate to pivot away from the force transfer element . • an actuator , • a lever configured to be subjected by the actuator to an angular displacement in two opposite directions with respect to a neutral positional range, • a support plate that is stationary with respect to the lever , • a movable component and a force transfer element attached to the movable component , - both pawls are prohibited by the support plate from engaging with the force transfer element when the lever is within the neutral positional range, - the force transfer element and thereby the movable component is displaced in the first of the two opposite directions by the first pawl engaging with the force transfer element , when the lever exits the neutral positional range in the first direction, - the force transfer element and thereby the movable component is displaced into the second of the two opposite directions by the second pawl engaging with the force transfer element , when the lever exits the neutral positional range in the second direction, and - when the pawl that is not actuating a motion of the force transfer element approaches the support plate , the pawl is forced by the support plate to pivot away from the force transfer element .
Security inspection system, comprising - a luggage drop-off region having one or more drop-off stations for dropping off luggage belonging to a person into at least one load carrier , - a luggage inspection station for imaging inspection of the luggage, - a luggage pick-up region having one or more removal stations , - a transport system for transporting the load carriers laden with luggage from the luggage drop-off region via the luggage inspection station to the luggage pick-up region and for returning empty load carriers to the luggage drop-off region , characterized in that at least one first monitoring device is provided in each of the provided drop-off stations for detecting the compliance with a specified degree of loading of the load carrier as its loading state, and/or at least one second monitoring device is provided in each of the provided removal stations for detecting a load carrier that is not completely emptied as its loading state. - a luggage drop-off region having one or more drop-off stations for dropping off luggage belonging to a person into at least one load carrier , - a luggage inspection station for imaging inspection of the luggage, - a luggage pick-up region having one or more removal stations , - a transport system for transporting the load carriers laden with luggage from the luggage drop-off region via the luggage inspection station to the luggage pick-up region and for returning empty load carriers to the luggage drop-off region , characterized in that at least one first monitoring device is provided in each of the provided drop-off stations for detecting the compliance with a specified degree of loading of the load carrier as its loading state, and/or at least one second monitoring device is provided in each of the provided removal stations for detecting a load carrier that is not completely emptied as its loading state.
A method for the attachment of a component to a honeycomb structure comprising: i. forming a cavity in the honeycomb structure whereby the cavity is formed within one or more honeycomb cells; ii. placing an insert adapted to enable the attachment of the component to the honeycomb structure within the cavity whereby: a. a reformable epoxy resin adhesive is injected about the insert; or b. an expandable reformable epoxy resin adhesive is overmolded onto the insert; iii. heating the reformable epoxy resin adhesive; and iv. hardening and adhering the reformable epoxy resin adhesive to one or more interior walls of the cavity upon cooling; wherein the reformable epoxy resin adhesive is configured to debond by heating the adhesive to a temperature above its glass transition temperature, its melting temperature, or both, wherein, that the reformable epoxy resin is removed with the addition of heat, characterized in, that the reformable epoxy resin is a polyethers being prepared by refacting a diglycidyl ether of dihydric aromatic compounds, such as the diglycidyl ether of bisphenol A, or a diepoxy-functionalized poly(alkylene oxide) or mixture thereof, with a primary amine or a secondary diamine or a monoamine functionalized poly(alkylene oxide) or mixture thereof. i. forming a cavity in the honeycomb structure whereby the cavity is formed within one or more honeycomb cells; ii. placing an insert adapted to enable the attachment of the component to the honeycomb structure within the cavity whereby: a. a reformable epoxy resin adhesive is injected about the insert; or b. an expandable reformable epoxy resin adhesive is overmolded onto the insert; a. a reformable epoxy resin adhesive is injected about the insert; or b. an expandable reformable epoxy resin adhesive is overmolded onto the insert; iii. heating the reformable epoxy resin adhesive; and iv. hardening and adhering the reformable epoxy resin adhesive to one or more interior walls of the cavity upon cooling; wherein the reformable epoxy resin adhesive is configured to debond by heating the adhesive to a temperature above its glass transition temperature, its melting temperature, or both, wherein, that the reformable epoxy resin is removed with the addition of heat, characterized in, that the reformable epoxy resin is a polyethers being prepared by refacting a diglycidyl ether of dihydric aromatic compounds, such as the diglycidyl ether of bisphenol A, or a diepoxy-functionalized poly(alkylene oxide) or mixture thereof, with a primary amine or a secondary diamine or a monoamine functionalized poly(alkylene oxide) or mixture thereof.
A cryogenic liquid storage tank , comprising: a vessel for containing a cryogenic liquid ; a fill pipe in communication with the vessel wherein the vessel is filled with the cryogenic liquid via the fill pipe; a fill termination assembly associated with the fill pipe, the fill termination assembly including a valve having an open position for allowing cryogenic liquid to flow through the fill pipe and the valve during filing of the vessel and a closed position for preventing cryogenic liquid from flowing through the fill pipe and the valve when the vessel has been filled with a selected amount of cryogenic liquid; and wherein said fill termination assembly includes a chamber containing a gas, wherein the chamber includes a movable segment and a static segment , wherein the movable segment is operatively connected to the valve via an arm that is attached to a valve head of the valve so as to move the valve head to engage a valve seat of the valve to place the valve in the closed position and to disengage the valve head from the valve seat to place the valve in the open position, wherein the valve of the fill termination assembly moves from the open position to the closed position when a pressure of the gas within the chamber decreases to a threshold pressure, the pressure of the gas decreasing to the threshold pressure when the vessel is filled to the selected amount. a vessel for containing a cryogenic liquid ; a fill pipe in communication with the vessel wherein the vessel is filled with the cryogenic liquid via the fill pipe; a fill termination assembly associated with the fill pipe, the fill termination assembly including a valve having an open position for allowing cryogenic liquid to flow through the fill pipe and the valve during filing of the vessel and a closed position for preventing cryogenic liquid from flowing through the fill pipe and the valve when the vessel has been filled with a selected amount of cryogenic liquid; and wherein said fill termination assembly includes a chamber containing a gas, wherein the chamber includes a movable segment and a static segment , wherein the movable segment is operatively connected to the valve via an arm that is attached to a valve head of the valve so as to move the valve head to engage a valve seat of the valve to place the valve in the closed position and to disengage the valve head from the valve seat to place the valve in the open position, wherein the valve of the fill termination assembly moves from the open position to the closed position when a pressure of the gas within the chamber decreases to a threshold pressure, the pressure of the gas decreasing to the threshold pressure when the vessel is filled to the selected amount.
A display module and an adjacent display module , each of the display modules comprising: a substrate ; a plurality of micro light-emitting diodes, micro-LEDs, disposed on the substrate , and configured to radiate light; a plurality of electrode pads of the micro-LEDs; a plurality of connection pads on the substrate ; a plurality of soldering members configured to electrically connect the plurality of micro-LEDs and the substrate to each other and disposed between the plurality of electrode pads and the plurality of connection pads ; the display module and the adjacent display module further comprising: a reflective layer surrounding a lateral surface of each of the plurality of micro-LEDs ; and a light blocking layer disposed on the reflective layer , wherein an upper surface of the reflective layer is lower than or planar with upper surfaces of the plurality of micro-LEDs, and wherein the reflective layer comprises a first portion (90-1) surrounding and contacting lateral surfaces of the plurality of micro-LEDs, a second portion (90-2) filling spaces between the plurality of electrode pads , the plurality of connection pads and the plurality of soldering members , and a third portion (90-3) filling a space between the display module and adjacent display module , wherein the first portion (90-1), the second portion (90-2) and the third portion (90-3) of the reflective layer are integrally formed, wherein the light blocking layer is formed above the space between the display module and the adjacent display module . a substrate ; a plurality of micro light-emitting diodes, micro-LEDs, disposed on the substrate , and configured to radiate light; a plurality of electrode pads of the micro-LEDs; a plurality of connection pads on the substrate ; a plurality of soldering members configured to electrically connect the plurality of micro-LEDs and the substrate to each other and disposed between the plurality of electrode pads and the plurality of connection pads ; the display module and the adjacent display module further comprising: a reflective layer surrounding a lateral surface of each of the plurality of micro-LEDs ; and a light blocking layer disposed on the reflective layer , wherein an upper surface of the reflective layer is lower than or planar with upper surfaces of the plurality of micro-LEDs, and wherein the reflective layer comprises a first portion (90-1) surrounding and contacting lateral surfaces of the plurality of micro-LEDs, a second portion (90-2) filling spaces between the plurality of electrode pads , the plurality of connection pads and the plurality of soldering members , and a third portion (90-3) filling a space between the display module and adjacent display module , wherein the first portion (90-1), the second portion (90-2) and the third portion (90-3) of the reflective layer are integrally formed, wherein the light blocking layer is formed above the space between the display module and the adjacent display module .
A surgical instrument set comprising at least: - one storage tube having a service opening , - one sealing member configured to seal the service opening , - several surgical instruments intended for a temporary use, and - one support including several fastening elements configured to fasten the surgical instruments to the support in a detachable manner, the support and the surgical instruments forming a subset (10.12) when the surgical instruments are fastened to the support ; the storage tube being configured to house the subset (10.12), so as to store the subset (10.12) in the sterile state when the sealing member seals the service opening , and the subset (10.12) being shaped to be extracted from the storage tube through the service opening ; characterized by the support comprising a handle suitable to be manipulated by an operator, the handle having an attachment portion configured to selectively attach one of the surgical instruments in a detachable manner, fastening elements being formed by longitudinal grooves formed on the outer surface of the handle , each longitudinal groove being suitable to house a portion of a respective surgical instrument so as to fasten said surgical instrument by elastic snapfit. - one storage tube having a service opening , - one sealing member configured to seal the service opening , - several surgical instruments intended for a temporary use, and - one support including several fastening elements configured to fasten the surgical instruments to the support in a detachable manner, the support and the surgical instruments forming a subset (10.12) when the surgical instruments are fastened to the support ;
A moulding tool for reshaping hollow-body glass precursors , comprising: a forming mandrel for reshaping at least a portion of a heated zone of the glass precursor ; wherein the forming mandrel is made of an alloy comprising at least a first temperature-stable core material as the basic material of the forming mandrel and at least one further alloying element; wherein the core material is selected from the group comprising iridium, palladium, platinum, rhodium, rhenium, and/or ruthenium, or an alloy based thereon; wherein the at least one further alloying element is selected from the group comprising tungsten, zirconium, rhodium, molybdenum, ruthenium, and rhenium; and wherein tungsten is included with an amount of at least 0.01 wt%. a forming mandrel for reshaping at least a portion of a heated zone of the glass precursor ; wherein the forming mandrel is made of an alloy comprising at least a first temperature-stable core material as the basic material of the forming mandrel and at least one further alloying element; wherein the core material is selected from the group comprising iridium, palladium, platinum, rhodium, rhenium, and/or ruthenium, or an alloy based thereon; wherein the at least one further alloying element is selected from the group comprising tungsten, zirconium, rhodium, molybdenum, ruthenium, and rhenium; and wherein tungsten is included with an amount of at least 0.01 wt%.
A method for manufacturing high strength steel sheets, comprising continuous annealing of a steel sheet which includes, in terms of mass%, C at 0.01 to 0.18%, Si at 0.4 to 2.0%, Mn at 1.0 to 3.0%, Al at 0.001 to 1.0%, P at 0.005 to 0.060%, S at ≤ 0.01%, and optionally one or more elements selected from B at 0.001 to 0.005%, Nb at 0.005 to 0.05%, Ti at 0.005 to 0.05%, Cr at 0.001 to 1.0%, Mo at 0.05 to 1.0%, Cu at 0.05 to 1.0% and Ni at 0.05 to 1.0%, the balance being represented by Fe and inevitable impurities, while controlling the dew-point temperature of the atmosphere in the range of -50°C to -10°C, except for when the heating furnace inside temperature is in the range of not less than A°C and not more than B°C, and controlling the dew-point temperature of the atmosphere to become not less than -10°C when the heating furnace inside temperature is in the range of not less than A°C and not more than B°C during the course of heating wherein A is 600 ≤ A ≤ 780 and B is 800 ≤ B ≤ 900 and wherein the hydrogen concentration in the annealing furnace atmosphere is not less than 1 vol% and not more than 50 vol%.
A non-oriented electrical steel sheet, having a chemical composition containing, in mass%, C: 0.0050 % or less, Si: 2.0 % or more and 6.0 % or less, Mn: 1.0 % or more and 3.0 % or less, P: 0.20 % or less, S: 0.0050 % or less, N: 0.0050 % or less, Al: 0.0050 % or less, and one or more selected from the group consisting of B: 0.0001 % or more and 0.0050 % or less, Nb: 0.0001 % or more and 0.0050 % or less, and V: 0.0005 % or more and 0.0500 % or less, and optionally one or more selected from the group consisting of Sn: 0.01 % or more and 0.50 % or less, Sb: 0.01 % or more and 0.50 % or less, Ca: 0.0001 % or more and 0.0300 % or less, Mg: 0.0001 % or more and 0.0300 % or less, REM: 0.0001 % or more and 0.0300 % or less, Ni: 0.01 % or more and 5.00 % or less and Co: 0.01 % or more and 5.00 % or less, with a balance consisting of Fe and inevitable impurities, wherein a number density of Si-Mn nitrides with an average diameter of 50 nm or more and 500 nm or less is 1 or less per μm3 measured according to the description. a chemical composition containing, in mass%, C: 0.0050 % or less, Si: 2.0 % or more and 6.0 % or less, Mn: 1.0 % or more and 3.0 % or less, P: 0.20 % or less, S: 0.0050 % or less, N: 0.0050 % or less, Al: 0.0050 % or less, and one or more selected from the group consisting of B: 0.0001 % or more and 0.0050 % or less, Nb: 0.0001 % or more and 0.0050 % or less, and V: 0.0005 % or more and 0.0500 % or less, and optionally one or more selected from the group consisting of Sn: 0.01 % or more and 0.50 % or less, Sb: 0.01 % or more and 0.50 % or less, Ca: 0.0001 % or more and 0.0300 % or less, Mg: 0.0001 % or more and 0.0300 % or less, REM: 0.0001 % or more and 0.0300 % or less, Ni: 0.01 % or more and 5.00 % or less and Co: 0.01 % or more and 5.00 % or less, with a balance consisting of Fe and inevitable impurities, wherein a number density of Si-Mn nitrides with an average diameter of 50 nm or more and 500 nm or less is 1 or less per μm3 measured according to the description.
Method for monitoring transport securing means on a transport vehicle that operate by means of tensioning elements and preferably tensioning belts, in which at least two of the tensioning elements are provided with at least one monitoring unit in each case, which is attached thereto and comprises at least one sensor and a transmitting unit , the sensor detecting an actual value which is representative of the tensile force (F) in the tensioning element , and the transmitting unit transmitting status signals wirelessly to a control unit present on the same transport vehicle , the transmitted status signals at least comprising - the actual value together with a target value previously stored in the monitoring unit , or - a difference value derived from the actual value and the target value previously stored in the monitoring unit , characterized in that the monitoring unit automatically stores the tensile force (F), which the sensor detects as an actual value at the point in time of maximum lashing of the monitored tensioning element or immediately after this point in time, as a target value. - the actual value together with a target value previously stored in the monitoring unit , or - a difference value derived from the actual value and the target value previously stored in the monitoring unit ,