mhurhangee/patent-ind-claim-en huggingface dataset:
A measurement light source comprising a solid block , in which an illumination space , a light shaping space , and a light exit space are each formed as a cavity in the block and have a diffusely reflective inner surface; wherein the illumination space is designed for light propagation in a first light propagation direction; wherein the first light propagation direction lies in a central axis of the illumination space ; wherein the light exit space is designed for light propagation in a second light propagation direction; wherein the second light propagation direction lies in a central axis of the light exits space ; wherein the illumination space opens into the light shaping space ; wherein the light shaping space opens into the light exit space ; wherein at least one light source for generating light is at least partially arranged in the illumination space ; wherein the light exit space has a light exit ; characterized in that the central axis of the illumination space and the central axis of the light exit space are arranged at a distance from one another; and wherein the light shaping space is designed for a reversal of a light propagation direction, by what the light entering the light shaping space from the illumination space undergoes a reversal of its light propagation direction as it propagates through the light shaping space , with the result that it enters the light exit space from the light shaping space with a reversed light propagation direction; wherein the first light propagation direction and the second light propagation direction are aligned opposite one another; and wherein the first light propagation direction and the second light propagation direction have an angle to one another that is 180°±30°.
A high-pressure fuel pump comprising: a discharge valve arranged on a discharge side of a pressurizing chamber; a discharge valve seat on which the discharge valve is seated; and a facing member configured independently as a separate member from the discharge valve seat and located on an opposite side of the discharge valve seat with the discharge valve interposed therebetween, wherein a stroke direction regulating portion (8D1) configured to regulate displacement of the discharge valve in a stroke direction is formed on a tapered surface of the facing member , and wherein the discharge valve is characterized by a discharge valve seat member on which the discharge valve seat is formed with a radial direction regulating portion (8A1), wherein the radial direction regulating portion (8A1) has a surface being arranged adjacent to the discharge valve seat and extending in the stroke direction, the surface accommodating the discharge valve and including at least one opening being arranged perpendicular to the stroke direction, and wherein the radial direction regulating portion (8A1) is configured to limit displacement of the discharge valve in a direction perpendicular to the stroke direction. a discharge valve arranged on a discharge side of a pressurizing chamber; a discharge valve seat on which the discharge valve is seated; and a facing member configured independently as a separate member from the discharge valve seat and located on an opposite side of the discharge valve seat with the discharge valve interposed therebetween, wherein a stroke direction regulating portion (8D1) configured to regulate displacement of the discharge valve in a stroke direction is formed on a tapered surface of the facing member , and wherein the discharge valve is characterized by a discharge valve seat member on which the discharge valve seat is formed with a radial direction regulating portion (8A1), wherein the radial direction regulating portion (8A1) has a surface being arranged adjacent to the discharge valve seat and extending in the stroke direction, the surface accommodating the discharge valve and including at least one opening being arranged perpendicular to the stroke direction, and wherein the radial direction regulating portion (8A1) is configured to limit displacement of the discharge valve in a direction perpendicular to the stroke direction.
Method for pre-programming a matrix of non-volatile resistive memory cells, said memory cells comprising a dielectric material arranged between two conductive electrodes , the dielectric material being an oxide and being in contact with each of the two conductive electrodes , said memory cells being initially in an original resistive state (original HRS) and the dielectric material being capable of being electrically modified so as to bring the memory cell from the original resistive state (original HRS) to at least one other resistive state (LRS), wherein the resistance of the memory cell is at least twice, preferably at least ten times less than the resistance of the memory cell in the original resistive state (original HRS), at least for an interval of reading voltages, the method comprising the following steps: - before assembling a component containing said matrix on a support, programming the matrix by electrically bringing a plurality of cells from the original resistive state (original HRS) to said other resistive state (LRS), said other resistive state being a second resistive state, leaving the other memory cells in the original resistive state thereof (original HRS); - assembling said matrix on a support, characterised in that during the assembly step, the memory cells are subjected to a temperature of at least 240°C, and in that the method further comprises, after the programming step and before the assembly, at least one cycle of steps carried out on the cells of said plurality of cells brought to said second resistive state, each cycle comprising: - an electrical modification of the dielectric material to bring said memory cells from said second resistive state to a third resistive state (programmed HRS), wherein the memory cells have a resistance greater than that of the memory cells in said second resistive state (LRS), then - an electrical modification of the dielectric material to bring said cells to said second resistive state. - before assembling a component containing said matrix on a support, programming the matrix by electrically bringing a plurality of cells from the original resistive state (original HRS) to said other resistive state (LRS), said other resistive state being a second resistive state, leaving the other memory cells in the original resistive state thereof (original HRS); - assembling said matrix on a support, - an electrical modification of the dielectric material to bring said memory cells from said second resistive state to a third resistive state (programmed HRS), wherein the memory cells have a resistance greater than that of the memory cells in said second resistive state (LRS), then - an electrical modification of the dielectric material to bring said cells to said second resistive state.
Dressing device for dressing a grinding tool provided with a predetermined grinding profile , the dressing device comprising at least a first dressing area and a second dressing area connected thereto, the dressing device having a longitudinal axis , and both dressing areas are arranged one behind the other in the direction of the longitudinal axis , characterized in that the first dressing area has a first specification for sharpening the grinding profile of the grinding tool and the second dressing area has a second specification deviating from the first specification for restoring the grinding profile of the grinding tool , and wherein the first dressing area has a larger volume than the second dressing area , and in that the dressing device is essentially cuboid, preferably with - a length from 150 mm to 250 mm, particularly preferably from 180 mm to 200 mm, and/or - a width from 25 mm to 75 mm, particularly preferably 50 mm, and/or - a thickness from 2.0 mm to 10.0 mm, particularly preferably 3.0 mm, 4.0 mm or 5.5 mm. - a length from 150 mm to 250 mm, particularly preferably from 180 mm to 200 mm, and/or - a width from 25 mm to 75 mm, particularly preferably 50 mm, and/or - a thickness from 2.0 mm to 10.0 mm, particularly preferably 3.0 mm, 4.0 mm or 5.5 mm.
Lifting device for the lifting and lowering of, in particular heavy, objects, comprising two frame arrangements which are placed one above the other, with respect to a vertical direction (z), and which in particular are aligned parallel to one another, of which the lower frame arrangement is arranged suspended from the upper frame arrangement via lifting-traction means (H1-H4) so that by winding up the lifting-traction means (H1-H4) the lower frame arrangement can be pulled up against the upper frame arrangement by means of a lifting-lowering device , and can be lowered relative to the upper frame arrangement by unwinding the lifting-traction means (H1-H4), wherein inclined traction means (S1a-S1d, S2a-S2d) which can be wound up and unwound by means of a tensioning device extend between the two frame arrangements , with each two crossing over with one another so that the lower frame arrangement is stabilised relative to the upper frame arrangement in at least one deflecting direction running transversely to the vertical direction (z), and wherein during winding up and unwinding of the lifting-traction means (H1-H4) each of the inclined traction means (S1a-S1d, S2a-S2d) can be held under a tensile stress by the tensioning device , wherein the frame arrangements each have at least three, in particular four, side sections (2a-2d; 3a-3d), characterised in that at least two crossing inclined traction means (S1a-S1d; S2a-S2d) extend between at least one of the side sections (2a-2d) of the lower frame arrangement and a side section (3a-3d) of the upper frame arrangement placed above same with respect to the vertical direction (z).
A tip clearance control assembly, comprising: a casing configured to guide a flow of combustion gas; a plurality of blades coupled to a rotary shaft of a gas turbine ; a labyrinth seal disposed at a front end portion of each of the plurality of blades , the labyrinth seal protruding toward an inner peripheral surface of the casing ; and a shroud configured to surround the front end portion of each of the plurality of blades , wherein the casing includes an outer casing having a dove tail slot (771-a) and an inner ring segment having a dove tail coupling portion (772-a), the inner ring segment operable to move in an axial and a radial direction (A, B) relative to the gas turbine , wherein the dove tail slot comprises a radial slot surface (771a-1) disposed in a first direction relative to the gas turbine , and an axial slot surface (771a-2) disposed in a second direction relative to the gas turbine , wherein the dove tail coupling portion comprises a radial coupling surface (772a-1) corresponding to the radial slot surface (771a-1), and an axial coupling surface (772a-2) corresponding to the axial slot surface (771a-2), wherein the radial coupling surface (772a-1) is disposed in a radial direction inclined along the axial direction relative to the gas turbine . a casing configured to guide a flow of combustion gas; a plurality of blades coupled to a rotary shaft of a gas turbine ; a labyrinth seal disposed at a front end portion of each of the plurality of blades , the labyrinth seal protruding toward an inner peripheral surface of the casing ; and a shroud configured to surround the front end portion of each of the plurality of blades , wherein the casing includes an outer casing having a dove tail slot (771-a) and an inner ring segment having a dove tail coupling portion (772-a), the inner ring segment operable to move in an axial and a radial direction (A, B) relative to the gas turbine , wherein the dove tail slot comprises a radial slot surface (771a-1) disposed in a first direction relative to the gas turbine , and an axial slot surface (771a-2) disposed in a second direction relative to the gas turbine , wherein the dove tail coupling portion comprises a radial coupling surface (772a-1) corresponding to the radial slot surface (771a-1), and an axial coupling surface (772a-2) corresponding to the axial slot surface (771a-2), wherein the radial coupling surface (772a-1) is disposed in a radial direction inclined along the axial direction relative to the gas turbine .
Carbon dioxide conversion process: • whereby carbon dioxide and water are supplied to an electrocatalytic unit (W) containing at least one cell comprising a cathode chamber (C) and an anode chamber (A), • whereby a C1 or C2 target compound selected from the group consisting of methanol, ethanol and ethylene, is produced in the cathode chamber (C) with a Faradaic Efficiency of at least 45%, said target compound being evacuated from the cathode chamber (C) in a first product stream consisting of (i) water, (ii) the target compound and (iii) a mixture containing at least unconverted carbon dioxide and hydrogen, • whereby oxygen is produced in the anode chamber (A), said oxygen being evacuated from the anode chamber (A) as part of a second product stream , • whereby target compound is extracted from the evacuated first product stream and a depleted first stream is thereby obtained, • whereby, at least a first part of the mixture of the depleted first stream and a first part of the oxygen of the second product stream are fed to a combustor (K) wherein said first part of the mixture of the depleted first stream is combusted using at least said first part of the oxygen as a combustion oxidant, thereby generating thermal energy and fumes consisting for at least 98 %vol of carbon dioxide and water, • whereby thermal energy generated in the combustor (K) is recovered and • whereby at least part and preferably all of the carbon dioxide from the fumes is fed to the electrocatalytic unit (W). • whereby carbon dioxide and water are supplied to an electrocatalytic unit (W) containing at least one cell comprising a cathode chamber (C) and an anode chamber (A), • whereby a C1 or C2 target compound selected from the group consisting of methanol, ethanol and ethylene, is produced in the cathode chamber (C) with a Faradaic Efficiency of at least 45%, said target compound being evacuated from the cathode chamber (C) in a first product stream consisting of (i) water, (ii) the target compound and (iii) a mixture containing at least unconverted carbon dioxide and hydrogen, • whereby oxygen is produced in the anode chamber (A), said oxygen being evacuated from the anode chamber (A) as part of a second product stream , • whereby target compound is extracted from the evacuated first product stream and a depleted first stream is thereby obtained, • whereby, at least a first part of the mixture of the depleted first stream and a first part of the oxygen of the second product stream are fed to a combustor (K) wherein said first part of the mixture of the depleted first stream is combusted using at least said first part of the oxygen as a combustion oxidant, thereby generating thermal energy and fumes consisting for at least 98 %vol of carbon dioxide and water, • whereby thermal energy generated in the combustor (K) is recovered and • whereby at least part and preferably all of the carbon dioxide from the fumes is fed to the electrocatalytic unit (W).
An electromagnetic device comprising: an enclosure , at least one winding in the interior of the enclosure, at least one wireless sensor for sensing at least one property or deficiency of the electromagnetic device , and at least one active communication unit comprising transceiving circuitry (14A1) and at least one antenna (14A2, 14A3), wherein the transceiving circuitry (14A1) is placed on the exterior of the enclosure and the least one antenna (14A2) is placed inside the enclosure for communication with the at least one sensor , wherein the at least one sensor comprises at least one sensor attached to the winding, and characterized in that the at least one sensor attached to the winding is a printed electronic sensor comprising electronics (PE) printed on an insulating substrate (S), where the substrate faces the at least one winding . an enclosure , at least one winding in the interior of the enclosure, at least one wireless sensor for sensing at least one property or deficiency of the electromagnetic device , and at least one active communication unit comprising transceiving circuitry (14A1) and at least one antenna (14A2, 14A3), wherein the transceiving circuitry (14A1) is placed on the exterior of the enclosure and the least one antenna (14A2) is placed inside the enclosure for communication with the at least one sensor , wherein the at least one sensor comprises at least one sensor attached to the winding, and characterized in that the at least one sensor attached to the winding is a printed electronic sensor comprising electronics (PE) printed on an insulating substrate (S), where the substrate faces the at least one winding .
Internal combustion engine having a starter motor with a drive pinion , which when starting the internal combustion engine is drive-connectable to a shaft of the internal combustion engine , - wherein the drive pinion comprises a first gear ring with first teeth located outside on the lateral surface and a first front side and is adjustable in the axial direction toward the shaft , wherein the first front side faces the shaft , - wherein the shaft of the internal combustion engine comprises a second gear ring with second teeth located outside on the lateral surface and a second front side , - wherein the first gear ring and the second gear ring are designed in such a manner that upon an axial adjusting of the drive pinion toward the shaft a first engagement situation arises, in which exclusively a first tooth engages between two second teeth or a second tooth engages between two first teeth , - the first gear ring located outside on the lateral surface or the second gear ring located outside on the lateral surface has a foot circle diameter d f and a useful tip circle diameter d a , the internal combustion engine characterised - in that the first front side or the second front side between the useful tip circle diameter d a and a radial region B about the foot circle diameter d f between d f - 6mm < B < d f + 3mm is rounded out with a radius R and because of this has a convex bevel in this region - in that an axial depth h between the first front side or the second front side and the useful tip circle diameter d a amounts to between 1mm < h < 5mm. - wherein the drive pinion comprises a first gear ring with first teeth located outside on the lateral surface and a first front side and is adjustable in the axial direction toward the shaft , wherein the first front side faces the shaft , - wherein the shaft of the internal combustion engine comprises a second gear ring with second teeth located outside on the lateral surface and a second front side , - wherein the first gear ring and the second gear ring are designed in such a manner that upon an axial adjusting of the drive pinion toward the shaft a first engagement situation arises, in which exclusively a first tooth engages between two second teeth or a second tooth engages between two first teeth , - the first gear ring located outside on the lateral surface or the second gear ring located outside on the lateral surface has a foot circle diameter d f and a useful tip circle diameter d a , the internal combustion engine characterised - in that the first front side or the second front side between the useful tip circle diameter d a and a radial region B about the foot circle diameter d f between d f - 6mm < B < d f + 3mm is rounded out with a radius R and because of this has a convex bevel in this region - in that an axial depth h between the first front side or the second front side and the useful tip circle diameter d a amounts to between 1mm < h < 5mm.
Ring filter element for filtering a liquid or gaseous medium, - with an annular filter body made of a filter material through which the medium can flow, and - with an annular inner frame made of a supporting material, which is arranged concentrically in the filter body and through which the medium can flow, - wherein the filter body is supported directly or indirectly with its radially inner body inner side radially against a radially outer cylindrical frame outer side when it is pressed from radially outside to inside against the inner frame during a flow, - wherein the ring filter element has at least one annular or spiral holder which surrounds the inner frame and is arranged on the inner side of the body, - wherein the holder has an annular or spiral adhesive body made of an adhesive, - wherein the adhesive body is radially outwardly directly bonded to the filter body by the adhesive of the adhesive body , and - wherein the holder is radially held on the radial inside of the inner frame , - wherein the holder has at least one annular or spiral reinforcement that surrounds the inner frame and is bonded directly to the adhesive body by the adhesive of the adhesive body , characterised in that the reinforcement has a lattice structure through which the adhesive of the adhesive body is interspersed, so that the adhesive body is radially internally bonded directly to the inner frame through the adhesive of the adhesive body , through the reinforcement . - with an annular filter body made of a filter material through which the medium can flow, and - with an annular inner frame made of a supporting material, which is arranged concentrically in the filter body and through which the medium can flow, - wherein the filter body is supported directly or indirectly with its radially inner body inner side radially against a radially outer cylindrical frame outer side when it is pressed from radially outside to inside against the inner frame during a flow, - wherein the ring filter element has at least one annular or spiral holder which surrounds the inner frame and is arranged on the inner side of the body, - wherein the holder has an annular or spiral adhesive body made of an adhesive, - wherein the adhesive body is radially outwardly directly bonded to the filter body by the adhesive of the adhesive body , and - wherein the holder is radially held on the radial inside of the inner frame , - wherein the holder has at least one annular or spiral reinforcement that surrounds the inner frame and is bonded directly to the adhesive body by the adhesive of the adhesive body , characterised in that