mhurhangee/patent-ind-claim-en huggingface dataset:
Valve shaft guide for a steam expander having a housing ; having at least one opening extending in the housing for receiving a valve shaft ; wherein a sliding bushing is inserted into the opening , which sliding bushing has an inner guide surface for forming a sliding bearing for the valve shaft ; the sliding bushing is screwed directly or indirectly into the housing ; wherein a valve seat ring is inserted coaxially to the sliding bushing into the opening in the housing ; characterized in that the sliding bushing is only plugged into the valve seat ring . having a housing ; having at least one opening extending in the housing for receiving a valve shaft ; wherein a sliding bushing is inserted into the opening , which sliding bushing has an inner guide surface for forming a sliding bearing for the valve shaft ; the sliding bushing is screwed directly or indirectly into the housing ; wherein a valve seat ring is inserted coaxially to the sliding bushing into the opening in the housing ; characterized in that the sliding bushing is only plugged into the valve seat ring .
A propulsion unit having a propeller for an aircraft comprising: - a nacelle configured to be attached to a structural element of the aircraft ; - a propeller which is rotatably mounted in the nacelle about a longitudinal axis of rotation (X) by means of a hub , the propeller comprising blades each of which is mounted in a pivotally fixed manner to an associated blade cuff which is pivotally mounted about a radial pitch axis (Y) with respect to the hub , and each blade being pivotally mounted with respect to the blade cuff about a folding axis (Z) orthogonal to the radial pitch axis (Y); - a folding device which comprises a folding actuator controlling the pivoting of each blade relative to its blade cuff between a deployed position in which the blades extend radially with respect to the axis (X) of rotation and a folded position in which the blades extend generally longitudinally against the nacelle ; the folding device comprising a transmission associated with each blade , each transmission comprising: - a movable control member which is mounted in a rotationally fixed manner to the blade cuff and which is moved by the folding actuator , and - a link comprising a first end pivotally mounted on a root of the associated blade eccentrically with respect to the folding axis (Z) and a second end pivotally mounted on the movable control member , characterised in that the movable control member is formed by a crank which is pivotally mounted in the blade cuff around of a control axis (Z1) parallel to the folding axis (Z) and in that the pivoting of the movable control member is actuated by means of a gearing between a toothed sector of the crank and a rack which is mounted so as to slide longitudinally and driven by the folding actuator . - a nacelle configured to be attached to a structural element of the aircraft ; - a propeller which is rotatably mounted in the nacelle about a longitudinal axis of rotation (X) by means of a hub , the propeller comprising blades each of which is mounted in a pivotally fixed manner to an associated blade cuff which is pivotally mounted about a radial pitch axis (Y) with respect to the hub , and each blade being pivotally mounted with respect to the blade cuff about a folding axis (Z) orthogonal to the radial pitch axis (Y); - a folding device which comprises a folding actuator controlling the pivoting of each blade relative to its blade cuff between a deployed position in which the blades extend radially with respect to the axis (X) of rotation and a folded position in which the blades extend generally longitudinally against the nacelle ; - a movable control member which is mounted in a rotationally fixed manner to the blade cuff and which is moved by the folding actuator , and - a link comprising a first end pivotally mounted on a root of the associated blade eccentrically with respect to the folding axis (Z) and a second end pivotally mounted on the movable control member ,
A method for the automated adjustment of a scale having an automated adjustment weight circuit, comprising the following steps performed automatically: - placing an adjustment weight (JG I ) selected from an adjustment weight stock comprising a plurality of adjustment weights (JG I ) onto an adjustment weight holder which is connected to a load support in a gravimetrically effective manner, - detecting a measurement value (M k ) representative of the loading of the load support, and - calculating, from the representative measurement value (M k ), a corresponding adjustment value (K k ), which should be used as a basis in the determination of weight values from the associated measurement values in subsequent weighings, characterized in that , immediately before the adjustment weight (JG I ) is placed on, a weight value (W 0 , W k-1 ) is determined and a maximum possible additional weight (Δ) within a specified loading range of the load support is calculated, and that, the adjustment weight (JG I ) having a nominal weight (N I ) that is the greatest of all those adjustment weights (JG I ) that have a nominal weight (N I ) less than the calculated maximum possible additional weight (Δ) is selected and is placed onto the adjustment weight holder. - placing an adjustment weight (JG I ) selected from an adjustment weight stock comprising a plurality of adjustment weights (JG I ) onto an adjustment weight holder which is connected to a load support in a gravimetrically effective manner, - detecting a measurement value (M k ) representative of the loading of the load support, and - calculating, from the representative measurement value (M k ), a corresponding adjustment value (K k ), which should be used as a basis in the determination of weight values from the associated measurement values in subsequent weighings, characterized in that , immediately before the adjustment weight (JG I ) is placed on, a weight value (W 0 , W k-1 ) is determined and a maximum possible additional weight (Δ) within a specified loading range of the load support is calculated, and that, the adjustment weight (JG I ) having a nominal weight (N I ) that is the greatest of all those adjustment weights (JG I ) that have a nominal weight (N I ) less than the calculated maximum possible additional weight (Δ) is selected and is placed onto the adjustment weight holder. characterized in that , immediately before the adjustment weight (JG I ) is placed on, a weight value (W 0 , W k-1 ) is determined and a maximum possible additional weight (Δ) within a specified loading range of the load support is calculated, and that, the adjustment weight (JG I ) having a nominal weight (N I ) that is the greatest of all those adjustment weights (JG I ) that have a nominal weight (N I ) less than the calculated maximum possible additional weight (Δ) is selected and is placed onto the adjustment weight holder.
An electromagnetic positioning device having anchor means which are realized for actuating a positioning partner and which are movable in an anchor space relative to stationary core means , which conduct magnetic flux, as a reaction to an energization of stationary coil means , the coil means, which have a coil support provided with a winding and at least one external contactable connector , being embedded at least in sections in the core means and/or being surrounded by said core means and the core means realizing an end surface , which is planar at least in sections, for interacting with the anchor means, the core means and the coil means being embedded in and/or surrounded by a one-piece pot-like and/or cup-like housing made of a material suitable for deep-drawing in such a manner that the core means rest on a membrane-like, continuous and closed base section of the housing, the base section realizing a boundary surface of the anchor space, characterized in that the core means are surrounded by a preferably cylindrical encapsulation , the outer diameter of said encapsulation being adapted to a clear inside width of the pot-like or cup-like housing. anchor means which are realized for actuating a positioning partner and which are movable in an anchor space relative to stationary core means , which conduct magnetic flux, as a reaction to an energization of stationary coil means , the coil means, which have a coil support provided with a winding and at least one external contactable connector , being embedded at least in sections in the core means and/or being surrounded by said core means and the core means realizing an end surface , which is planar at least in sections, for interacting with the anchor means, the core means and the coil means being embedded in and/or surrounded by a one-piece pot-like and/or cup-like housing made of a material suitable for deep-drawing in such a manner that the core means rest on a membrane-like, continuous and closed base section of the housing, the base section realizing a boundary surface of the anchor space, characterized in that the core means are surrounded by a preferably cylindrical encapsulation , the outer diameter of said encapsulation being adapted to a clear inside width of the pot-like or cup-like housing.
A liquid pharmaceutical composition suitable for parenteral administration comprising: a. pemetrexed diacid; b. arginine; c. at least one monothiolic antioxidant; d. 10-200 mg/ml of propylene glycol, and e. one or more parenteral solvents, wherein the preparation thereof is conducted in an atmosphere of inert gas and wherein arginine is present in an amount sufficient to reach a pH of the composition in the range from 8.3 to 9.1. a. pemetrexed diacid; b. arginine; c. at least one monothiolic antioxidant; d. 10-200 mg/ml of propylene glycol, and e. one or more parenteral solvents,
A space propulsion module, characterized in that it comprises a solid propellant chemical thruster , possessing a main body made in composite material, and at least one electric thruster , and in that the electric thruster is mounted on the main body of the solid propellant chemical thruster via a fastener structure comprising a top flange provided at the top end of the main body of the solid propellant chemical thruster , and a bottom flange provided at the bottom end of the main body of the solid propellant chemical thruster . characterized in that it comprises a solid propellant chemical thruster , possessing a main body made in composite material, and at least one electric thruster , and in that the electric thruster is mounted on the main body of the solid propellant chemical thruster via a fastener structure comprising a top flange provided at the top end of the main body of the solid propellant chemical thruster , and a bottom flange provided at the bottom end of the main body of the solid propellant chemical thruster .
A blender comprising: a main body ; a jar configured to be seated on the main body and provided with a blade device for crushing food; a motor assembly provided inside the main body and configured to generate rotation power of the blade device ; a main PCB device provided inside the main body , wherein a knob rotation shaft is mounted on the main PCB device , and wherein the main PCB device includes a plurality of LEDs for emitting light toward the knob assembly ; and a knob assembly for operation of the blender by a user, the knob assembly is mounted on the knob rotation shaft and the knob assembly is protruding outwardly through the main body , wherein the knob assembly includes: a knob coupled with the knob rotation shaft and configured to be rotationally manipulated by the user; and a knob ring penetrated by the knob and mounted on the main body ; and characterized in that the LEDs include: at least one inner LED disposed to emit light toward a rear end of the knob , and at least one outer LED provided on the outside of the inner LED to emit light toward the knob ring . a main body ; a jar configured to be seated on the main body and provided with a blade device for crushing food; a motor assembly provided inside the main body and configured to generate rotation power of the blade device ; a main PCB device provided inside the main body , wherein a knob rotation shaft is mounted on the main PCB device , and wherein the main PCB device includes a plurality of LEDs for emitting light toward the knob assembly ; and a knob assembly for operation of the blender by a user, the knob assembly is mounted on the knob rotation shaft and the knob assembly is protruding outwardly through the main body , a knob coupled with the knob rotation shaft and configured to be rotationally manipulated by the user; and a knob ring penetrated by the knob and mounted on the main body ; and characterized in that the LEDs include: at least one inner LED disposed to emit light toward a rear end of the knob , and at least one outer LED provided on the outside of the inner LED to emit light toward the knob ring . at least one inner LED disposed to emit light toward a rear end of the knob , and at least one outer LED provided on the outside of the inner LED to emit light toward the knob ring .
A method, comprising: preparing a random access message at a user equipment ; transmitting the random access message from the user equipment on a common resource, wherein the common resource comprises a resource known by a plurality of access nodes or a resource shared by a plurality of access nodes ; and receiving multiple joint random access responses with same content, in response to the random access message, wherein the multiple joint random access responses relate to at least two of the plurality of access nodes . preparing a random access message at a user equipment ; transmitting the random access message from the user equipment on a common resource, wherein the common resource comprises a resource known by a plurality of access nodes or a resource shared by a plurality of access nodes ; and receiving multiple joint random access responses with same content, in response to the random access message, wherein the multiple joint random access responses relate to at least two of the plurality of access nodes .
An outdoor unit for an air conditioner, comprising: a casing , including a portion defining an outlet through which air is discharged from the outdoor unit ; an axial flow fan disposed in the casing for blowing air through the outlet, wherein the axial flow fan comprises: a hub ; a plurality of main wings extending from the hub ; and a rim connecting the main wings to one other and rotating integrally with the main wings ; and a plurality of auxiliary wings disposed at a clearance space between the rim and the portion of the casing defining the outlet, wherein the rim includes a front edge, a rear edge, an inner surface and an outer surface, wherein the front edge is closer to the outlet than the rear edge, and wherein the plurality of auxiliary wings are formed on the outer surface of the rim , wherein each auxiliary wing has a leading edge at which air flow begins and a trailing edge opposite the leading edge , wherein the leading edge is positioned further forward towards the direction of rotation than the trailing edge , wherein the trailing edge is positioned further forward towards the front of the rim than the leading edge , wherein an outer radius of the front of the rim is less than an outer radius of the back of the rim , wherein a distance between the leading edge of the auxiliary wing and the axis of the axial flow fan is greater than a distance between the trailing edge of the auxiliary wing and the axis of the axial flow fan . a casing , including a portion defining an outlet through which air is discharged from the outdoor unit ; an axial flow fan disposed in the casing for blowing air through the outlet, wherein the axial flow fan comprises: a hub ; a plurality of main wings extending from the hub ; and a rim connecting the main wings to one other and rotating integrally with the main wings ; and a hub ; a plurality of main wings extending from the hub ; and a rim connecting the main wings to one other and rotating integrally with the main wings ; and a plurality of auxiliary wings disposed at a clearance space between the rim and the portion of the casing defining the outlet, wherein the rim includes a front edge, a rear edge, an inner surface and an outer surface, wherein the front edge is closer to the outlet than the rear edge, and wherein the plurality of auxiliary wings are formed on the outer surface of the rim , wherein each auxiliary wing has a leading edge at which air flow begins and a trailing edge opposite the leading edge , wherein the leading edge is positioned further forward towards the direction of rotation than the trailing edge , wherein the trailing edge is positioned further forward towards the front of the rim than the leading edge , wherein an outer radius of the front of the rim is less than an outer radius of the back of the rim , wherein a distance between the leading edge of the auxiliary wing and the axis of the axial flow fan is greater than a distance between the trailing edge of the auxiliary wing and the axis of the axial flow fan .
A sorting machine for objects configured to receive objects from one or more infeed stations (i) and move them towards respective predetermined outfeed stations (u), comprising a plurality of conveyors located in the form of a matrix or chequerboard on a movement area, wherein each conveyor is configured to move at least one object between a plurality of respective receiving/unloading stations (rs) arranged one after another along a conveying trajectory, said conveyors being configured and/or arranged in such a way that said conveying trajectories lie on a same plane, preferably horizontal, wherein each conveyor is positioned adjacent to at least one other conveyor of said plurality of conveyors in such a way that at least one receiving/unloading station (rs) of a conveyor is shared with a respective adjacent conveyor ; wherein each conveyor has one or more movement means configured for transferring an object, in movement on said conveying trajectory, from and towards a conveyor adjacent to said at least one shared receiving/unloading station (rs); and wherein each conveyor comprises a motor-driven carousel rotatable about a respective axis of rotation (X) and the movement means of each conveyor comprise respective conveyor belts moved by said carousel about said axis of rotation (X) and defining respective radial directions of movement relative to said axis of rotation (X); the machine being characterized in that said carousel comprises a supporting ring extending around the respective axis of rotation (X), said conveyor belts being rigidly mounted on said supporting ring . wherein each conveyor is positioned adjacent to at least one other conveyor of said plurality of conveyors in such a way that at least one receiving/unloading station (rs) of a conveyor is shared with a respective adjacent conveyor ; wherein each conveyor has one or more movement means configured for transferring an object, in movement on said conveying trajectory, from and towards a conveyor adjacent to said at least one shared receiving/unloading station (rs); and wherein each conveyor comprises a motor-driven carousel rotatable about a respective axis of rotation (X) and the movement means of each conveyor comprise respective conveyor belts moved by said carousel about said axis of rotation (X) and defining respective radial directions of movement relative to said axis of rotation (X); the machine being characterized in that said carousel comprises a supporting ring extending around the respective axis of rotation (X), said conveyor belts being rigidly mounted on said supporting ring .
Device in a liquid for damping and scattering of hydrosound in the liquid, particularly water , by means of an envelope body containing a gas, wherein the liquid can flow through the device , in particular in the direction of sound propagation, and the device has a plurality of envelope bodies each containing a gas and that are at a distance from one another and are each surrounded by the liquid, wherein the device has a carrier element and a mass body, wherein the envelope bodies are arranged at a distance from one another on the carrier element , characterized in that the envelope bodies are positioned horizontally in a plane on the floor of the liquid.
A system for assessing a geometry of a surface comprising a joint formed between adjacent drywall panels , the system comprising: an assembly comprising a laser that projects a laser line at an angle of incidence of 1 degree to 60 degrees relative to a mean plane defined by the surface and perpendicularly across the joint , wherein the laser line enables user visualization of non-planar distortion in the joint ; and a camera that digitally images the laser line and a reference guide located or simulated on the surface adjacent to the laser line; and a computer coupled to the camera , wherein the computer quantifies the geometry of the surface based on the digital images, parameters of the laser line , the reference guide, and a distance between the camera and the surface to determine a quality of the joint , and wherein the geometry of the surface is quantified by expressing the non-planar distortion of the joint along the laser line , defining a width of the joint , measuring a slope of edges of the joint , or a combination thereof. an assembly comprising a laser that projects a laser line at an angle of incidence of 1 degree to 60 degrees relative to a mean plane defined by the surface and perpendicularly across the joint , wherein the laser line enables user visualization of non-planar distortion in the joint ; and a camera that digitally images the laser line and a reference guide located or simulated on the surface adjacent to the laser line; and a computer coupled to the camera , wherein the computer quantifies the geometry of the surface based on the digital images, parameters of the laser line , the reference guide, and a distance between the camera and the surface to determine a quality of the joint , and wherein the geometry of the surface is quantified by expressing the non-planar distortion of the joint along the laser line , defining a width of the joint , measuring a slope of edges of the joint , or a combination thereof.
A process for the production of a plasma etched organic polymer surface or SiO 2 surface, with carbonyl or carboxyl groups, wherein the process comprises the step of etching the surface with oxygen or fluorine or fluorocarbon containing and polymer depositing plasmas or mixtures thereof, under anisotropic etching conditions, in the presence of an etching inhibitor, characterized in that after the plasma etching step the surface is subjected to a thermal annealing step by heating for 10 - 120 min at a temperature 5 to 40 degrees below the glass transition temperature of the organic polymer or the plasma deposited polymer.