mhurhangee/patent-ind-claim-en huggingface dataset:
An electric machine for use in an aircraft, comprising: a casing containing electromechanical components; a shaft which extends outside of the casing; a seal to seal the casing around the shaft; characterised by further comprising a depressurisation system configured to depressurise the casing below an external gas pressure to prevent electrical breakdown within gas in the casing. a casing containing electromechanical components; a shaft which extends outside of the casing; a seal to seal the casing around the shaft; characterised by further comprising a depressurisation system configured to depressurise the casing below an external gas pressure to prevent electrical breakdown within gas in the casing.
A method for fabricating a semiconductor device, comprising: processing a first substrate of a first material at a first thermal budget to fabricate a p-type device surrounded by an insulator layer on the first substrate ; fabricating an interface layer on the insulator layer of the first substrate to electrically isolate the p-type device from subsequently processed devices; directly coupling a second substrate of a second material to the interface layer on the first substrate ; and processing the second substrate to fabricate an n-type device at a second thermal budget that is less than the first thermal budget, in which the p-type device and the n-type device cooperate to form a complementary device. processing a first substrate of a first material at a first thermal budget to fabricate a p-type device surrounded by an insulator layer on the first substrate ; fabricating an interface layer on the insulator layer of the first substrate to electrically isolate the p-type device from subsequently processed devices; directly coupling a second substrate of a second material to the interface layer on the first substrate ; and processing the second substrate to fabricate an n-type device at a second thermal budget that is less than the first thermal budget, in which the p-type device and the n-type device cooperate to form a complementary device.
Transverse sealing device (14a -14g) for sealing a package or a packaging material, comprising at least two sealing jaws (18a - 18g, 20a - 20g), comprising at least one movement unit (36a - 36g), which is configured for moving the at least two sealing jaws (18a - 18g, 20a - 20gl) horizontally relative to each other and comprising a guide unit (82a - 82g) to guide the at least two sealing jaws (18a - 18g, 20a - 20g) during a movement, wherein the movement unit (36a - 36g) is arranged at least substantially completely sideways relative to the at least two sealing jaws (18a - 18g, 20a - 20g), at least viewed in a direction parallel to a horizontal movement axis (38a - 38g) of the guide unit (82a - 82g), wherein at least 75% of a total volume and/or a total mass of the movement unit (36a - 36g) are arranged sideways relative to the at least two sealing jaws (18a - 18g, 20a - 20g), wherein the at least two sealing jaws (18a - 18g, 20a - 20g) are linearly movably supported along the direction parallel to the horizontal movement axis (38a - 38g) of the guide unit (82a - 82g), characterized in that the at least two sealing jaws (18a - 18g, 20a - 20g) are pullable into a sealing position by means of the movement unit (36a - 36g), wherein the movement unit (36a - 36g) is connected to the at least two sealing jaws (18a - 18g, 20a - 20g) in such a way that the movement unit (36a - 36g) is enabled to generate a direct pulling force for pulling the at least two sealing jaws (18a - 18g, 20a - 20g) relative to each other into the sealing position, wherein at least one movement element (46a - 46g) and at least one further movement element (48a - 48g) of the movement unit (36a - 36g) are movable relative to each other so as to pull the at least two sealing jaws (18a - 18g, 20a - 20g) towards each other into the sealing position.
Magnetic position transducer, comprising a magnetic transducer , a magnetic sensor, which is assigned to the magnetic transducer , for detecting the movement of the magnetic transducer , and a housing , wherein the magnetic transducer has at least two bar magnets , which are arranged in the housing with opposite polarity, wherein the poles of adjacent bar magnets are each oppositely directed, so that the two south poles or north poles of the adjacent bar magnets are closer to one another than the south pole of one of the bar magnets and the north pole of the other of the bar magnets respectively are, characterized in that at least one of the bar magnets has at least one recess and in that the housing has at least one recess , wherein the at least one recess in the housing and the at least one recess in the bar magnet are congruent.
A locking mechanism for a kitchen device having a vessel and a lid , the locking mechanism comprising: a retaining arm pivotable between a free position and a retaining position; a securing assembly adapted to engage the retaining arm and movable between a free position and a securing position; an electric motor adapted to move the securing assembly between the free position and the securing position; a processor adapted to control the electric motor using a motor controller; and a drive mechanism , wherein the electric motor is adapted to move the securing assembly using the drive mechanism, wherein the drive mechanism comprises a bridge member , and wherein the bridge member is to convert a rotary motion of the electric motor to a linear motion of the bridge member. a retaining arm pivotable between a free position and a retaining position; a securing assembly adapted to engage the retaining arm and movable between a free position and a securing position; an electric motor adapted to move the securing assembly between the free position and the securing position; a processor adapted to control the electric motor using a motor controller; and a drive mechanism , wherein the electric motor is adapted to move the securing assembly using the drive mechanism, wherein the drive mechanism comprises a bridge member , and wherein the bridge member is to convert a rotary motion of the electric motor to a linear motion of the bridge member.
A p-type oxide, wherein the p-type oxide is amorphous and is represented by the following compositional formula: xAO·yCU 2 O where x denotes a proportion by mole of AO and y denotes a proportion by mole of Cu 2 O and x and y satisfy the following expressions: 0 ≤ x < 100 and x + y = 100, and A is any one of Mg, Ca, Sr and Ba, or a mixture containing at least one selected from the group consisting of Mg, Ca, Sr and Ba.
A collar comprising: a set of collar teeth that are disposed opposite a collar hole that extends along an axis , wherein each collar tooth includes: a first end surface that extends away from the axis ; a second end surface that extends away from the axis and is disposed opposite the first end surface ; a first collar side surface that is concave from the first end surface to the second end surface ; and a second collar side surface that is concave from the first end surface to the second end surface , wherein the second collar side surface is disposed opposite the first collar side surface , and characterised in that a gap between adjacent collar teeth is bisected by a gap bisecting plane , the collar has a concave cross section in the gap bisecting plane , a root is disposed between adjacent collar teeth , and a root midpoint radius (R M ) where the gap bisecting plane intersects a transverse collar tooth plane is less than a root end radius (R E ) where the gap bisecting plane intersects the first end surface . a first end surface that extends away from the axis ; a second end surface that extends away from the axis and is disposed opposite the first end surface ; a first collar side surface that is concave from the first end surface to the second end surface ; and a second collar side surface that is concave from the first end surface to the second end surface , wherein the second collar side surface is disposed opposite the first collar side surface , and characterised in that a gap between adjacent collar teeth is bisected by a gap bisecting plane , the collar has a concave cross section in the gap bisecting plane , a root is disposed between adjacent collar teeth , and a root midpoint radius (R M ) where the gap bisecting plane intersects a transverse collar tooth plane is less than a root end radius (R E ) where the gap bisecting plane intersects the first end surface .
A test device for a body fluid analysis, the test device comprising: - a first assembly having a magnifying lens for magnifying and observing a target body fluid; - a second assembly configured to be coupled to the first assembly and having a lens transmission hole for concentrating light; and - an observation sheet for receiving the target body fluid between the first assembly and the second assembly , - wherein the observation sheet includes a body part disposed inside the first assembly and the second assembly and a handle part extending from the body part , - wherein the body part comprises a body fluid input part formed to allow the target body fluid to be injected thereinto and a body fluid guide part configured to guide the target body fluid injected into the body fluid input part , so that the target body fluid permeates an inner side of the center of the body part so as to be observed in a field of view of the magnifying lens , wherein the body fluid guide part is formed higher than a bottom of the body fluid input part , and, - wherein the first assembly further comprises a first assembly body , a seating recess formed on an inner side of the first assembly body allowing the observation sheet to be seated therein, a through hole formed in the seating recess and penetrating the first assembly body , and at least one coupling recess formed on an upper surface of the first assembly body so as to be assembled with the second assembly . - a first assembly having a magnifying lens for magnifying and observing a target body fluid; - a second assembly configured to be coupled to the first assembly and having a lens transmission hole for concentrating light; and - an observation sheet for receiving the target body fluid between the first assembly and the second assembly , - wherein the observation sheet includes a body part disposed inside the first assembly and the second assembly and a handle part extending from the body part , - wherein the body part comprises a body fluid input part formed to allow the target body fluid to be injected thereinto and a body fluid guide part configured to guide the target body fluid injected into the body fluid input part , so that the target body fluid permeates an inner side of the center of the body part so as to be observed in a field of view of the magnifying lens , wherein the body fluid guide part is formed higher than a bottom of the body fluid input part , and, - wherein the first assembly further comprises a first assembly body , a seating recess formed on an inner side of the first assembly body allowing the observation sheet to be seated therein, a through hole formed in the seating recess and penetrating the first assembly body , and at least one coupling recess formed on an upper surface of the first assembly body so as to be assembled with the second assembly .
Radially shrinkable textile hose for encasing elongated objects, comprising the following features: a) an outer layer made from shrinkable wear-resistant material and b) at least one inner layer made from thermally insulating material, the material of the at least one inner layer being swellable with heat input, characterised in that the outer layer and the at least one inner layer are joined together in places by a textile binding or by sewing or by bonding. a) an outer layer made from shrinkable wear-resistant material and b) at least one inner layer made from thermally insulating material, the material of the at least one inner layer being swellable with heat input, characterised in that the outer layer and the at least one inner layer are joined together in places by a textile binding or by sewing or by bonding. the material of the at least one inner layer being swellable with heat input, characterised in that the outer layer and the at least one inner layer are joined together in places by a textile binding or by sewing or by bonding.
A method for reproducing an injection molded part quality in injection molding in which an injection molded part is produced using an injection mold in a production cycle (Z0 to Z4) that comprises a plurality of phases (I to III), a melt is injected into a cavity of the injection mold in an injection phase (I), the melt is solidified in the cavity in a holding pressure phase (II), and at an end of a residual cooling phase (III) the melt that has continued to cool down is ejected from the cavity as the injection molded part ; wherein a variation of an internal pressure (p) of the cavity with time is detected and represented in the form of the internal pressure graph (10, 10.M0 to 10.M4); at least one internal pressure graph of a production cycle in which an injection molded part produced meets at least one predefined quality characteristic being used as the reference graph ; wherein a comparison (V0) determines whether an internal pressure graph (10.M0) of a current production cycle (Z0) exceeds at least one predefined threshold value; and if the internal pressure graph (10.M0) of the current production cycle (Z0) exceeds the threshold value, at least one current machine parameter (M0) is changed to adapt an internal pressure graph (10M1 to 10.M4) of a subsequent production cycle (Z1 to Z4) to the reference graph ; characterized in that at least one machine parameter (M1 to M4) is assigned to each phase (I to III) of the production cycle, wherein said assigned machine parameter (M1 to M4) has a higher impact on the internal pressure (p) in that phase (I to III) of the production cycle than non-assigned machine parameters; and in that said assigned machine parameters (M1 to M4) are changed in a plurality of production cycles (Z1 to Z4) in a predefined order wherein exactly one assigned machine parameter (M1 to M4) is changed per production cycle (Z0 to Z4).
An elongate vehicle reinforcement member having a U-shaped cross section, wherein the vehicle reinforcement member is disposed inside a vehicle structural member and welded to the vehicle structural member , wherein the vehicle structural member comprises opposite base lateral walls , the vehicle reinforcement member comprising: opposite reinforcement lateral walls extending in vehicle height and width directions, each having an outward edge on an outer side in vehicle width direction and an inward edge on an inner side in vehicle width direction, wherein the reinforcement lateral walls are placed along inner sides of the base lateral walls of the vehicle structural member ; and a reinforcement connecting wall connecting the outward edges of the reinforcement lateral walls , each reinforcement lateral wall together with the reinforcement connecting wall forming a ridge (L1), characterized in that each reinforcement lateral wall comprising a row of welding projections , each welding projection protruding outward over the entire width of the reinforcement lateral wall from the ridge (L1) to the inward edge of the reinforcement lateral wall , each welding projection having a raised welding surface at which the reinforcement lateral wall is welded to the base lateral wall , the welding projections in each row being arranged at intervals along vehicle height direction. opposite reinforcement lateral walls extending in vehicle height and width directions, each having an outward edge on an outer side in vehicle width direction and an inward edge on an inner side in vehicle width direction, wherein the reinforcement lateral walls are placed along inner sides of the base lateral walls of the vehicle structural member ; and a reinforcement connecting wall connecting the outward edges of the reinforcement lateral walls , each reinforcement lateral wall together with the reinforcement connecting wall forming a ridge (L1), characterized in that each reinforcement lateral wall comprising a row of welding projections , each welding projection protruding outward over the entire width of the reinforcement lateral wall from the ridge (L1) to the inward edge of the reinforcement lateral wall , each welding projection having a raised welding surface at which the reinforcement lateral wall is welded to the base lateral wall , the welding projections in each row being arranged at intervals along vehicle height direction.
A microfluidic flow device comprising: (a) a first layer comprising a plurality of gas channels ; (b) a distensible membrane coupled with the first layer; (c) a plurality of support structures embedded in the distensible membrane, the plurality of support structures distributed evenly along the length of the plurality of gas channels; and (d) a second layer comprising a plurality of blood channels and coupled with the distensible membrane, the plurality of blood channels separated from the plurality of gas channels by the distensible membrane, the plurality of blood channels comprising: (i) a cross-sectional area defined in the second layer, a shape of the cross-sectional area being configured to oscillate along a length of the plurality of blood channels by pressurizing, with a gas, the plurality of gas channels to distend the distensible membrane. (a) a first layer comprising a plurality of gas channels ; (b) a distensible membrane coupled with the first layer; (c) a plurality of support structures embedded in the distensible membrane, the plurality of support structures distributed evenly along the length of the plurality of gas channels; and (d) a second layer comprising a plurality of blood channels and coupled with the distensible membrane, the plurality of blood channels separated from the plurality of gas channels by the distensible membrane, the plurality of blood channels comprising: (i) a cross-sectional area defined in the second layer, a shape of the cross-sectional area being configured to oscillate along a length of the plurality of blood channels by pressurizing, with a gas, the plurality of gas channels to distend the distensible membrane. (i) a cross-sectional area defined in the second layer, a shape of the cross-sectional area being configured to oscillate along a length of the plurality of blood channels by pressurizing, with a gas, the plurality of gas channels to distend the distensible membrane.
A spraying apparatus for spraying a spray liquid, in particular for agricultural purposes, with at least one storage tank for a liquid and with at least one spray nozzle for spraying the spray liquid on a surface, wherein the spray liquid contains at least one carrier liquid, in particular water, and at least one spraying agent, comprising at least one measuring apparatus for determining properties of the spray liquid and/or the carrier liquid, characterized in that a determination of the water hardness and/or the microorganism load of the spray liquid and/or the carrier liquid is provided by means of the measuring apparatus and the spraying apparatus is set up for metering at least one additive with a positive effect on the spraying result and/or on the interaction of the ingredients of the spray liquid and/or their miscibility with the spray liquid on the basis of the properties determined by the measuring apparatus .
A method for range finding, the method comprising: determining a first optical signature of a spool of optical fibre wound in a winding pattern which comprises repeated changes in a winding parameter to provide a different optical response such that the signature comprises a plurality of markers representing each change in the winding parameter; despooling fibre from the spool; determining a second optical signature of the spool of optical fibre after despooling the fibre from the spool; and calculating the length of despooled fibre based on a comparison of the first and the second optical signatures. determining a first optical signature of a spool of optical fibre wound in a winding pattern which comprises repeated changes in a winding parameter to provide a different optical response such that the signature comprises a plurality of markers representing each change in the winding parameter; despooling fibre from the spool; determining a second optical signature of the spool of optical fibre after despooling the fibre from the spool; and calculating the length of despooled fibre based on a comparison of the first and the second optical signatures.
A propulsion system for an aircraft, comprising: a plenum having an intake port and an output port; a powered fan coupled to a motor configured to power the powered fan , the powered fan configured to compress ambient air entering the intake port; one or more ejectors fluidically coupled to the plenum via one or more valves ; and a nozzle disposed within the output port, the nozzle comprising a set of nozzle vanes , wherein: the propulsion system operates in a first configuration in which the nozzle vanes are closed and the compressed ambient air exits the plenum only through the one or more valves into the one or more ejectors , characterized in that the propulsion system operates in a second configuration in which the one or more valves are closed, the nozzle vanes are open and the compressed ambient air exits the plenum only through the output port. a plenum having an intake port and an output port; a powered fan coupled to a motor configured to power the powered fan , the powered fan configured to compress ambient air entering the intake port; one or more ejectors fluidically coupled to the plenum via one or more valves ; and a nozzle disposed within the output port, the nozzle comprising a set of nozzle vanes , wherein: the propulsion system operates in a first configuration in which the nozzle vanes are closed and the compressed ambient air exits the plenum only through the one or more valves into the one or more ejectors , characterized in that the propulsion system operates in a second configuration in which the one or more valves are closed, the nozzle vanes are open and the compressed ambient air exits the plenum only through the output port. the propulsion system operates in a first configuration in which the nozzle vanes are closed and the compressed ambient air exits the plenum only through the one or more valves into the one or more ejectors , characterized in that the propulsion system operates in a second configuration in which the one or more valves are closed, the nozzle vanes are open and the compressed ambient air exits the plenum only through the output port.