mhurhangee/ep-ind-claims huggingface dataset:
A surgical instrument manipulator assembly comprising: a low backlash coupler and a drive output disk; the low backlash coupler comprising a central body with a central lumen, a first beam, a second beam, a third beam, and a fourth beam; each of the first beam, the second beam, the third beam, and the fourth beam being stiff in torsion about an axis extending through the central lumen, but flexible relative to lateral offsets; each of the first beam, the second beam, the third beam, and the fourth beam comprising a first end and a second end; each of the first ends of the first beam, the second beam, the third beam, and the fourth beam being connected to the central body; the second end of the first beam comprising a first driven cylinder; the second end of the second beam comprising a second driven cylinder; the second end of the third beam comprising a first driving cylinder; the second end of the fourth beam comprising a second driving cylinder; the drive output disk being coupled to the low backlash coupler via input pins of the drive output disk mounted in central bores of the first driving cylinder and the second driving cylinder; and the low backlash coupler being coupled to a drive unit via output pins of the drive unit mounted in central bores of the first driven cylinder and the second driven cylinder such that the low backlash coupler transfers torque from the drive unit to the drive output disk. a low backlash coupler and a drive output disk; the low backlash coupler comprising a central body with a central lumen, a first beam, a second beam, a third beam, and a fourth beam; each of the first beam, the second beam, the third beam, and the fourth beam being stiff in torsion about an axis extending through the central lumen, but flexible relative to lateral offsets; each of the first beam, the second beam, the third beam, and the fourth beam comprising a first end and a second end; each of the first ends of the first beam, the second beam, the third beam, and the fourth beam being connected to the central body; the second end of the first beam comprising a first driven cylinder; the second end of the second beam comprising a second driven cylinder; the second end of the third beam comprising a first driving cylinder; the second end of the fourth beam comprising a second driving cylinder; the drive output disk being coupled to the low backlash coupler via input pins of the drive output disk mounted in central bores of the first driving cylinder and the second driving cylinder; and the low backlash coupler being coupled to a drive unit via output pins of the drive unit mounted in central bores of the first driven cylinder and the second driven cylinder such that the low backlash coupler transfers torque from the drive unit to the drive output disk.
Frame (1, 100, 200) for the attachment of animal skins for a plant or chamber for drying the skins themselves, wherein said frame (1, 100, 200) comprises a perimeter framework (10, 110, 210), at least one panel (2, 2a, 2b, 102, 102a, 102b, 202), an upper portion (17, 117) in use and a lower portion (18, 118) in use, wherein said upper portion (17, 117) comprises at least one first panel (2a, 102a, 202) and/or said lower portion (18, 118) comprises at least one second panel (2b, 102b, 202), wherein said at least one first panel (2a, 102a, 202) is separable and/or moveable away from said lower portion (18, 118) in use and/or from said at least one second panel (2b, 102b, 202) along a first direction or vertical direction in use for a distance, said frame (1, 100, 200) comprising movement means (30, 300) adapted to move said at least one panel (2, 2a, 2b, 102, 102a, 102b, 202) along a second direction or a longitudinal or horizontal direction in use of the frame (1, 100, 200) for a displacement so as to widen the extension of the skin in use attached to said frame (1, 100, 200) both along said first direction and along said second direction or along a diagonal direction resulting from the displacement along said first direction or vertical direction in use and said second direction or horizontal or longitudinal direction in use in the passage for the frame (1, 100, 200) from a first operating position to a second operating position, characterized in that said movement means adapted to move at least one first panel (2a, 202) placed in said upper portion of said frame (1, 200) comprise at least one bar (31, 31') and at least one plate (32, 32'), wherein said at least one plate (32, 32') is constrained to said perimeter framework (10, 210) in at least one constraint point or pin (A, A') and in that said at least one bar (31, 31') is constrained to said lower portion of said frame (1, 200) and to said at least one plate (32, 32') in at least one rotating constraint point (B, B').
A container filling system comprising: a beverage product reservoir; multiple beverage container filling valves connected to the reservoir and configured to hot fill containers with beverage product from the reservoir; a product recirculation flow path connected to each of the filling valves and configured to maintain a flow of beverage product through each of the filling valves when each of the filling valves is closed; characterized in that a flow meter is located in a portion of the recirculation flow path and configured to output flow meter signals indicative of flow rates through the flow meter; and a controller is configured to receive the flow meter signals and to generate, based on the received flow meter signals, control signals to maintain a flow rate through the product recirculation flow path at a target flow value. a beverage product reservoir; multiple beverage container filling valves connected to the reservoir and configured to hot fill containers with beverage product from the reservoir; a product recirculation flow path connected to each of the filling valves and configured to maintain a flow of beverage product through each of the filling valves when each of the filling valves is closed; characterized in that a flow meter is located in a portion of the recirculation flow path and configured to output flow meter signals indicative of flow rates through the flow meter; and a controller is configured to receive the flow meter signals and to generate, based on the received flow meter signals, control signals to maintain a flow rate through the product recirculation flow path at a target flow value.
Steam turbine comprising a shaft and a diverter device, wherein the shaft has a cooling steam section which is designed to cause cooling steam to flow over the shaft surface, wherein the cooling steam section is arranged below the diverter device, wherein the diverter device is arranged in the steam inlet region, characterized in that the shaft surface is coated with a thermal barrier coating in the cooling steam section.
Method for modifying the installation configuration of an aircraft comprising a compartment, called engine compartment, with an engine installed in said engine compartment, in which method: - an engine control device: • connected to command cables, said command cables being adapted to be connected to a command device and • connected to a first extremity of transmission cables adapted to transmit electrical signals in the aircraft, • is disconnected from both the command cables and the transmission cables, - a jumper connector is connected in lieu of the engine control device between the command cables and the transmission cables, - an engine control device is: • installed in the engine compartment, • connected to > a second extremity of the transmission cables and > sensing cables connected to sensors (24,25). - an engine control device: • connected to command cables, said command cables being adapted to be connected to a command device and • connected to a first extremity of transmission cables adapted to transmit electrical signals in the aircraft, • is disconnected from both the command cables and the transmission cables, • connected to command cables, said command cables being adapted to be connected to a command device and • connected to a first extremity of transmission cables adapted to transmit electrical signals in the aircraft, • is disconnected from both the command cables and the transmission cables, - a jumper connector is connected in lieu of the engine control device between the command cables and the transmission cables, - an engine control device is: • installed in the engine compartment, • connected to > a second extremity of the transmission cables and > sensing cables connected to sensors (24,25). • installed in the engine compartment, • connected to > a second extremity of the transmission cables and > sensing cables connected to sensors (24,25). > a second extremity of the transmission cables and > sensing cables connected to sensors (24,25).
A method for assembling a re-workable heat dissipation device, comprising: applying a first surface of a removable adhesive layer to a first surface of a first interposer layer; applying a heat dissipation device to a second surface of the removable adhesive layer; applying a non-removable adhesive layer to a first surface of a device to be cooled; bonding, after applying the heat dissipation device to the second surface of the removable adhesive layer, a second surface of the first interposer layer to the non-removable adhesive layer; removing the removable adhesive layer and the heat dissipation device from the first surface of the first interposer layer; applying a first surface of a second removable adhesive layer to a first surface of a second interposer layer; applying a second heat dissipation device to a second surface of the second removable adhesive layer; applying a second non-removable adhesive layer to the first surface of the first interposer layer; and bonding a second surface of the second interposer layer to the second non-removable adhesive layer, wherein the removable adhesive layer and the second removable adhesive layer are higher pressure adhesive layers, and wherein the non-removable adhesive layer and the second non-removable adhesive layer are low or no-pressure adhesive layers. applying a first surface of a removable adhesive layer to a first surface of a first interposer layer; applying a heat dissipation device to a second surface of the removable adhesive layer; applying a non-removable adhesive layer to a first surface of a device to be cooled; bonding, after applying the heat dissipation device to the second surface of the removable adhesive layer, a second surface of the first interposer layer to the non-removable adhesive layer; removing the removable adhesive layer and the heat dissipation device from the first surface of the first interposer layer; applying a first surface of a second removable adhesive layer to a first surface of a second interposer layer; applying a second heat dissipation device to a second surface of the second removable adhesive layer; applying a second non-removable adhesive layer to the first surface of the first interposer layer; and bonding a second surface of the second interposer layer to the second non-removable adhesive layer, wherein the removable adhesive layer and the second removable adhesive layer are higher pressure adhesive layers, and wherein the non-removable adhesive layer and the second non-removable adhesive layer are low or no-pressure adhesive layers.
A fiber structure for reinforcing a composite material part, said structure being obtained by multilayer weaving between a plurality of layers of warp yarns and a plurality of layers of weft yarns, the fiber structure including, at least on one of its faces, one or more fastener elements (12; 13), characterized in that each fastener element comprises a body (121; 131) arranged at least in part under yarns (101 1, 101 2) present on a face of said fiber structure, and at least one fastener portion (122; 132) situated over said yarns.
A method of conducting blood-brain barrier penetration studies of nanoparticles in an insect, said method comprising the steps: • optionally anesthetizing the insect; • fixing the head of the insect; • dissecting out the dorsal part of the insect head so as to expose the brain, eyes, antennas, and nerve associations; • optionally removing the neural lamella; • treating the brain with the nanoparticles; • washing and homogenising or ultra sound disintegrating the brain; and • determining the concentration of the nanoparticles in the homogenised brain material, wherein hemolymph and/or albumin is added to the nanoparticles.. • optionally anesthetizing the insect; • fixing the head of the insect; • dissecting out the dorsal part of the insect head so as to expose the brain, eyes, antennas, and nerve associations; • optionally removing the neural lamella; • treating the brain with the nanoparticles; • washing and homogenising or ultra sound disintegrating the brain; and • determining the concentration of the nanoparticles in the homogenised brain material, wherein hemolymph and/or albumin is added to the nanoparticles..
Casting mold for the manufacture of hard or soft contact lenses, comprising a male mold half made of highly finished glass having a generally convexly shaped male mold surface shaped by precision glass molding and a female mold half made of highly finished glass having a generally concavely shaped female mold surface shaped by precision glass molding, each of the male and female mold surfaces (20, 30) comprising a lens-forming surface (21, 31) which is encircled by a non-lens-forming annular edge surface (22, 32), the lens-forming surface (21, 31) comprising a central optical zone (210, 310) and a non-optical peripheral zone (211, 311) surrounding the central optical zone (210, 310), at least one of the male and female mold halves (2, 3) being provided with at least one permanent marking (10; 12; 110, 111) which is arranged only on the non-lens-forming annular edge surface (22, 32).
A method for creating an elevator shaft of an elevator system, wherein the elevator shaft is mainly vertically aligned and forms a travelway for a car of the elevator system (10, 310, 410, 510), which car is moved at a nominal speed within the travelway in normal operation of the elevator system (10, 310, 410, 510), and the method has the following method steps: - placing multiple base modules (14, 16, 18, 518) on each other, - closing the elevator shaft upwards by mounting a top module (21, 521), - providing an intermediate element (19, 119, 219, 319, 419, 519), and - arranging the selected intermediate element (19, 119, 219, 319, 419, 519), between an uppermost base module (18, 518) and the top module (21, 521), characterized in that, the intermediate element (19, 119, 219, 319, 419, 519) comprising an intermediate element height (h1, h3, h4, h5) dependent on the mentioned nominal speed of the car. wherein the elevator shaft is mainly vertically aligned and forms a travelway for a car of the elevator system (10, 310, 410, 510), which car is moved at a nominal speed within the travelway in normal operation of the elevator system (10, 310, 410, 510), and the method has the following method steps: - placing multiple base modules (14, 16, 18, 518) on each other, - closing the elevator shaft upwards by mounting a top module (21, 521), - providing an intermediate element (19, 119, 219, 319, 419, 519), and - arranging the selected intermediate element (19, 119, 219, 319, 419, 519), between an uppermost base module (18, 518) and the top module (21, 521), - placing multiple base modules (14, 16, 18, 518) on each other, - closing the elevator shaft upwards by mounting a top module (21, 521), - providing an intermediate element (19, 119, 219, 319, 419, 519), and - arranging the selected intermediate element (19, 119, 219, 319, 419, 519), between an uppermost base module (18, 518) and the top module (21, 521), characterized in that, the intermediate element (19, 119, 219, 319, 419, 519) comprising an intermediate element height (h1, h3, h4, h5) dependent on the mentioned nominal speed of the car.
Device for performing a bending test - having a base plate, - having counter bearings (6a, 6b) connected via the base plate - having bearing blocks (8a, 8b), which in each case comprise a support (10a, 10b) for applying a bending sample and - having a bending punch or a bending rail for exerting a force on a bending sample, characterised in that - the counter bearings (6a, 6b) and the bearing blocks (8a, 8b) abut against each other via contact surfaces (14a, 14b; 16a, 16b) inclined to the base plate. - having a base plate, - having counter bearings (6a, 6b) connected via the base plate - having bearing blocks (8a, 8b), which in each case comprise a support (10a, 10b) for applying a bending sample and - having a bending punch or a bending rail for exerting a force on a bending sample, characterised in that - the counter bearings (6a, 6b) and the bearing blocks (8a, 8b) abut against each other via contact surfaces (14a, 14b; 16a, 16b) inclined to the base plate.
Turbomachine part comprising: - a substrate of metallic or composite material, - a coating layer to protect against the infiltration of compounds such as calcium, magnesium, aluminium or silicon oxides, or CMAS, the coating layer at least partially covering the surface of the substrate, the coating layer comprising a plurality of elementary layers, each elementary layer having a substantially homogeneous chemical composition and substantially homogeneous physicochemical characteristics, elemental layers of a first set of elemental layers being sandwiched between elemental layers of a second set of elemental layers, each elemental layer of the first set and each elemental layer of the second set comprising an anti-CMAS compound, the part being characterised in that each elementary layer of the first assembly has a tenacity which differs by at least 0.7 Mpa.m 1/2, or a coefficient of thermal expansion which differs by at least 3.5 10 -6 K -1, respectively with respect to the tenacities or the coefficients of thermal expansion of all the elementary layers of the second assembly, each zone of contact between an elementary layer of the first assembly and an elementary layer of the second assembly forming an interface which encourages the propagation of cracks along said interface. - a substrate of metallic or composite material, - a coating layer to protect against the infiltration of compounds such as calcium, magnesium, aluminium or silicon oxides, or CMAS, the coating layer at least partially covering the surface of the substrate, the coating layer comprising a plurality of elementary layers, each elementary layer having a substantially homogeneous chemical composition and substantially homogeneous physicochemical characteristics, elemental layers of a first set of elemental layers being sandwiched between elemental layers of a second set of elemental layers, each elemental layer of the first set and each elemental layer of the second set comprising an anti-CMAS compound, the part being characterised in that each elementary layer of the first assembly has a tenacity which differs by at least 0.7 Mpa.m 1/2, or a coefficient of thermal expansion which differs by at least 3.5 10 -6 K -1, respectively with respect to the tenacities or the coefficients of thermal expansion of all the elementary layers of the second assembly, each zone of contact between an elementary layer of the first assembly and an elementary layer of the second assembly forming an interface which encourages the propagation of cracks along said interface.
A computer implemented method for generating a geometric pattern on a piece of sports and leisure clothing and a computer comprising the steps of: loading surface data of the piece of sports and leisure clothing into the computer, loading a base boundary into the computer, wherein the base boundary forms the contour of a base item that is to be visualized on the piece of sports and leisure clothing, dividing the surrounding area of the piece of sports and leisure clothing outside the base item into a plurality of subareas, loading a plurality of images into the computer, distributing the plurality of images over the plurality of subareas, so that each subarea contains at least one image, thereby visually defining the base boundary by means of the arrangement of the plurality of images, generating the geometric pattern on the piece of sports and leisure clothing, characterized in that, the base boundary creates an abrupt transition from the base item to the surrounding area, wherein the base boundary is visible due to the color and/or brightness of the plurality of images that differ from the color and brightness of the area inside of the base boundary. loading surface data of the piece of sports and leisure clothing into the computer, loading a base boundary into the computer, wherein the base boundary forms the contour of a base item that is to be visualized on the piece of sports and leisure clothing, dividing the surrounding area of the piece of sports and leisure clothing outside the base item into a plurality of subareas, loading a plurality of images into the computer, distributing the plurality of images over the plurality of subareas, so that each subarea contains at least one image, thereby visually defining the base boundary by means of the arrangement of the plurality of images, generating the geometric pattern on the piece of sports and leisure clothing, characterized in that, the base boundary creates an abrupt transition from the base item to the surrounding area, wherein the base boundary is visible due to the color and/or brightness of the plurality of images that differ from the color and brightness of the area inside of the base boundary.
Method for manufacturing a foldable building plate element, comprising the steps of: - providing a flat plate; - providing at least one folding groove in the flat plate; - providing a folding profile, comprising two side wings and, in cross-sectional view, a folded portion interposed between the side wings; - fitting the folding profile into the folding groove in such a way, that the side wings thereof form a strong connection with both side faces of the folding groove and/or with the zones of the flat plate, located adjacently to the folding groove; wherein the side wings of the folding profile are provided with connecting means, which are arranged to detachably interconnect with each other, when the side wings are folded towards each another, - folding the side wings towards each other and locking the side wings in the folded position by means of the connecting means on the side wings; - providing a removable bridging strip during transport or storage of the flat plate, the bridging strip detachably interconnecting and locking the side wings of the profile; characterized, in that the connecting means on the side wings are mutually snap-connectable, and in that the bridging strip comprises connecting means, the connecting means on the bridging strip are snap-connectable and snap-detachable, wherein the connecting means upon the bridging strip are the same as the connecting means on the side wings of the folding profile, so that in the open position of the side wings, the snap-connectable means of the bridging strip are snap-connected to the snap-connectable means on both side wings of the profile. - providing a flat plate; - providing at least one folding groove in the flat plate; - providing a folding profile, comprising two side wings and, in cross-sectional view, a folded portion interposed between the side wings; - fitting the folding profile into the folding groove in such a way, that the side wings thereof form a strong connection with both side faces of the folding groove and/or with the zones of the flat plate, located adjacently to the folding groove; - folding the side wings towards each other and locking the side wings in the folded position by means of the connecting means on the side wings; - providing a removable bridging strip during transport or storage of the flat plate, the bridging strip detachably interconnecting and locking the side wings of the profile;