mhurhangee/ep-ind-claims huggingface dataset:
Use of a carbon molecular sieve membrane in a process for separating acid gas components from a natural gas stream, wherein a natural gas stream having a CO 2 partial pressure of at least 50 bar contacts with the carbon molecular sieve membrane to produce i. a retentate stream having a reduced concentration of acid gas components, and ii. a permeate stream having an increased concentration of acid gas components; the carbon molecular sieve membrane is produced by contacting one from unreinforced amorphous polyetherimide having the following chemical formula (Ultem ® 1000), 5 -amino-1-(4'aminophenyl)-1,3,-trimethylindane (Matrimid ® 5218), 5,5-[2,2,2-trifluoro-1-(trifluoromethyl)ethylidene]bis-1,3-isobenzofurandione/3,3,4,4-biphenyl tetracarboxylic dianhydride-2,4,6-Trimethyl-1,3-phenylene diamine (6FDA/BPDA-DAM), 5,5-[2,2,2-trifluoro-1-(trifluoromethyl)ethylidene]bis-1,3-isobenzofurandione-4,4'-(hexafluoroisopropylidene)-dianiline (6FDA-6FpDA), or 5,5-[2,2,2-trifluoro-1-(trifluoromethyl)ethylidene]bis-1,3-isobenzofurandione-4,4'-(isopropylidene)-dianiline (6FDA-IPDA) with a modifying agent and pyrolyzing at a pyrolysis temperature between 500 °C and 900 °C; and the CO 2 /CH 4 selectivity of the carbon molecular sieve membrane during the contacting step is at least 80% of the CO 2 /CH 4 selectivity of the carbon molecular sieve membrane when contacted with a natural gas stream having at a CO 2 partial pressure of 10 bar or less under the same temperature. a natural gas stream having a CO 2 partial pressure of at least 50 bar contacts with the carbon molecular sieve membrane to produce i. a retentate stream having a reduced concentration of acid gas components, and ii. a permeate stream having an increased concentration of acid gas components; i. a retentate stream having a reduced concentration of acid gas components, and ii. a permeate stream having an increased concentration of acid gas components; the carbon molecular sieve membrane is produced by contacting one from unreinforced amorphous polyetherimide having the following chemical formula (Ultem ® 1000), 5 -amino-1-(4'aminophenyl)-1,3,-trimethylindane (Matrimid ® 5218), 5,5-[2,2,2-trifluoro-1-(trifluoromethyl)ethylidene]bis-1,3-isobenzofurandione/3,3,4,4-biphenyl tetracarboxylic dianhydride-2,4,6-Trimethyl-1,3-phenylene diamine (6FDA/BPDA-DAM), 5,5-[2,2,2-trifluoro-1-(trifluoromethyl)ethylidene]bis-1,3-isobenzofurandione-4,4'-(hexafluoroisopropylidene)-dianiline (6FDA-6FpDA), or 5,5-[2,2,2-trifluoro-1-(trifluoromethyl)ethylidene]bis-1,3-isobenzofurandione-4,4'-(isopropylidene)-dianiline (6FDA-IPDA) with a modifying agent and pyrolyzing at a pyrolysis temperature between 500 °C and 900 °C; and the CO 2 /CH 4 selectivity of the carbon molecular sieve membrane during the contacting step is at least 80% of the CO 2 /CH 4 selectivity of the carbon molecular sieve membrane when contacted with a natural gas stream having at a CO 2 partial pressure of 10 bar or less under the same temperature.
An assembly of a drug delivery device with a longitudinal axis, comprising: - a body comprising a proximal end and a distal end, - a drive assembly being at least partially arranged within the body and being adapted to dispense a medicinal product contained in a cartridge, wherein the drive assembly comprises a piston rod which pushes a bung of the cartridge along an inside wall of the cartridge thereby dispensing the medicinal product, - a first button member acting on the drive assembly to prepare the drug delivery device in the form of compensating for any backlashes and tolerances of mechanical parts of the drive assembly and the drug delivery device and/or closing a gap between the bung and the drive assembly and/or mixing powder with a fluid and/or expelling a priming portion of the medicinal product or air during a pre-ready state and a transient state of the assembly for dispensing the medicinal product during a ready state of the assembly, wherein the ready state chronological follows the preparation during the pre-ready state and the transient state of the assembly, characterized in that the first button member is adapted to be detachable from the body after the preparation of the drug delivery device is completed. - a body comprising a proximal end and a distal end, - a drive assembly being at least partially arranged within the body and being adapted to dispense a medicinal product contained in a cartridge, wherein the drive assembly comprises a piston rod which pushes a bung of the cartridge along an inside wall of the cartridge thereby dispensing the medicinal product, - a first button member acting on the drive assembly to prepare the drug delivery device in the form of compensating for any backlashes and tolerances of mechanical parts of the drive assembly and the drug delivery device and/or closing a gap between the bung and the drive assembly and/or mixing powder with a fluid and/or expelling a priming portion of the medicinal product or air during a pre-ready state and a transient state of the assembly for dispensing the medicinal product during a ready state of the assembly, wherein the ready state chronological follows the preparation during the pre-ready state and the transient state of the assembly, characterized in that the first button member is adapted to be detachable from the body after the preparation of the drug delivery device is completed. compensating for any backlashes and tolerances of mechanical parts of the drive assembly and the drug delivery device and/or closing a gap between the bung and the drive assembly and/or mixing powder with a fluid and/or expelling a priming portion of the medicinal product or air during a pre-ready state and a transient state of the assembly for dispensing the medicinal product during a ready state of the assembly,
An engine system for an aircraft, the engine system comprising: a first gas turbine engine; a first core turning system operably coupled to the first gas turbine engine; a second gas turbine engine; a second core turning system operably coupled to the second gas turbine engine; and a controller, characterized in that the controller is operable to: shut down the first gas turbine engine responsive to determining that the aircraft has landed; operate the second gas turbine engine in a taxi mode while using the first core turning system to cool the first gas turbine engine; shut down the second gas turbine engine and disable the first core turning system based on a power-down condition; restart the first gas turbine engine and use the second core turning system to cool the second gas turbine engine based on a restart condition; and complete cooling of the second gas turbine prior to restarting the second gas turbine engine. a first gas turbine engine; a first core turning system operably coupled to the first gas turbine engine; a second gas turbine engine; a second core turning system operably coupled to the second gas turbine engine; and a controller, characterized in that the controller is operable to: shut down the first gas turbine engine responsive to determining that the aircraft has landed; operate the second gas turbine engine in a taxi mode while using the first core turning system to cool the first gas turbine engine; shut down the second gas turbine engine and disable the first core turning system based on a power-down condition; restart the first gas turbine engine and use the second core turning system to cool the second gas turbine engine based on a restart condition; and complete cooling of the second gas turbine prior to restarting the second gas turbine engine. shut down the first gas turbine engine responsive to determining that the aircraft has landed; operate the second gas turbine engine in a taxi mode while using the first core turning system to cool the first gas turbine engine; shut down the second gas turbine engine and disable the first core turning system based on a power-down condition; restart the first gas turbine engine and use the second core turning system to cool the second gas turbine engine based on a restart condition; and complete cooling of the second gas turbine prior to restarting the second gas turbine engine.
Industrial truck having at least one vertically movable fork carrier which comprises at least two transverse carriers (12, 13), and at least one device which is arranged in the region of the fork carrier and has the purpose of carrying out wireless communication with an RFID transponder mounted on a pallet, characterized in that at least one device for carrying out wireless communication is arranged on the fork carrier behind the side, facing away from the load, of the plane defined by the centre line of at least two transverse carriers (12, 13) of the vertically movable fork carrier.
A printing system for printing on a substantially planar surface of a 3D-object, the printing system comprising: a) printing means for printing on the planar surface of the 3D-object; and b) control means configured to control printing of the printing means; wherein the printing system further comprises a mask generation module configured to generate a mask having the shape of the planar surface from a 3D-model of the 3D-object and to provide the control means with the mask to prevent printing outside said planar surface according to the mask, characterized in that the mask generation module is configured to generate the shape of the mask from a mesh model defined by a plurality of 2D-faces by selection of 2D-faces of the plurality having a corresponding normal with respect to a reference normal of a reference 2D-face arranged in an area of the mesh model corresponding to the planar surface of the 3D-object. a) printing means for printing on the planar surface of the 3D-object; and b) control means configured to control printing of the printing means; wherein the printing system further comprises a mask generation module configured to generate a mask having the shape of the planar surface from a 3D-model of the 3D-object and to provide the control means with the mask to prevent printing outside said planar surface according to the mask, characterized in that the mask generation module is configured to generate the shape of the mask from a mesh model defined by a plurality of 2D-faces by selection of 2D-faces of the plurality having a corresponding normal with respect to a reference normal of a reference 2D-face arranged in an area of the mesh model corresponding to the planar surface of the 3D-object.
Aircraft comprising a fuselage, a propulsion system, a first pair of swept-back airfoils, connected to the top forward portion of the fuselage, a second pair of swept-forward airfoils, connected to the lower rear portion of the fuselage at a point of the said fuselage aft of the connection of the swept-back airfoils, and a third pair of substantially vertical airfoils, wherein the swept-forward airfoils are connected to the lower side of the swept-back airfoils at an intermediate point of the span of the said swept-back airfoils, by means of the substantially vertical airfoils, the swept-back airfoils having a higher aspect ratio than that of the swept-forward airfoils, which makes the swept-back airfoils have a reduced induced drag without penalizing their weight, as their maximum bending moment is reduced because of the structural support that the swept-forward airfoils provide to the swept-back airfoils through the vertical airfoils, and wherein the aircraft also comprises a landing gear system comprising at least one leg connected to the lower portion of the forward fuselage, characterized in that the tips of the swept-forward airfoils are connected to the lower side of the swept-back airfoils at said intermediate point by means of said substantially vertical airfoils, and in that the landing gear system further comprises two legs connected to the lower side of the swept-forward airfoils, the at least two legs of the lower side of the swept-forward airfoils and the propulsion system being connected to the same structural spar of the swept-forward airfoils, so that the inertial loads introduced by the propulsion system in cases of landing with high vertical accelerations are transmitted to the landing gear legs through the shortest possible load path within the airframe as it is allowed by landing gear legs separation and engine installation requirements.
A photovoltaic device (100, 210) comprising: a plurality of electrically connected photovoltaic cells, wherein the photovoltaic cells comprise a conducting layer having a first surface and a second surface, the first surface facing an absorber layer; an insulating material disposed on the second surface over at least one of the photovoltaic cells; a conductive member on the insulating material, wherein the insulating material is configured to electrically insulate the conductive member from the second surface; a bus member, wherein the bus member is electrically coupled to the one of the plurality of photovoltaic cells; and an edge seal comprising a sealant material extending over at least a portion of the one of the plurality of photovoltaic cells; characterized in that: the photovoltaic device (100, 210) further comprises a patch comprising a conductive material on a peripheral edge of the conductive member and a peripheral edge of the insulating material; wherein the bus member is over the one of the plurality of photovoltaic cells and the patch, and is disposed between the edge seal and the patch; and wherein the patch electrically couples the bus member to the conductive member. a plurality of electrically connected photovoltaic cells, wherein the photovoltaic cells comprise a conducting layer having a first surface and a second surface, the first surface facing an absorber layer; an insulating material disposed on the second surface over at least one of the photovoltaic cells; a conductive member on the insulating material, wherein the insulating material is configured to electrically insulate the conductive member from the second surface; a bus member, wherein the bus member is electrically coupled to the one of the plurality of photovoltaic cells; and an edge seal comprising a sealant material extending over at least a portion of the one of the plurality of photovoltaic cells; characterized in that: the photovoltaic device (100, 210) further comprises a patch comprising a conductive material on a peripheral edge of the conductive member and a peripheral edge of the insulating material; wherein the bus member is over the one of the plurality of photovoltaic cells and the patch, and is disposed between the edge seal and the patch; and wherein the patch electrically couples the bus member to the conductive member. the photovoltaic device (100, 210) further comprises a patch comprising a conductive material on a peripheral edge of the conductive member and a peripheral edge of the insulating material; wherein the bus member is over the one of the plurality of photovoltaic cells and the patch, and is disposed between the edge seal and the patch; and wherein the patch electrically couples the bus member to the conductive member.
An orientation device for objects provided with a stem and with a head that has a minimum width, comprising: a slot which has two edges (31,32) separated by a predetermined distance, less than the maximum width of the head and greater than the maximum width of the stem; an uncoupling device, movable between an active configuration, in which it is able to retain an object with respect to lifting, and an inactive configuration, in which it is not able to interact with an object; a magnetic gripping element, capable of collecting an object and positioning the object above the slot, which magnetic gripping element is movable along at least a vertical direction between an upper position and a lower position, in which an object associated with the gripping element is in a position such as to be retained by the uncoupling device so as to be detached from the gripping element and resting on the slot.
A microphone array comprising: a sound-diffracting structure that has a closed three-dimensional shape with an indentation in a perimeter of the sound-diffracting structure and with a surface surrounding the shape, wherein the sound-diffracting structure is a rigid sphere; and a differential microphone comprising two omnidirectional microphones (601, 604) and a beamforming circuit (1100, 1203-1206); wherein the two omnidirectional microphones (601, 604) are mounted flush on the surface in the indentation of the sound-diffracting structure; and the two omnidirectional microphones (601, 604) and the beamforming circuit (1100, 1203-1206) are configured to provide a differential microphone output signal (1107, 1205, 1206). a sound-diffracting structure that has a closed three-dimensional shape with an indentation in a perimeter of the sound-diffracting structure and with a surface surrounding the shape, wherein the sound-diffracting structure is a rigid sphere; and a differential microphone comprising two omnidirectional microphones (601, 604) and a beamforming circuit (1100, 1203-1206); wherein the two omnidirectional microphones (601, 604) are mounted flush on the surface in the indentation of the sound-diffracting structure; and the two omnidirectional microphones (601, 604) and the beamforming circuit (1100, 1203-1206) are configured to provide a differential microphone output signal (1107, 1205, 1206).
Laminoplasty implant, in particular for cervical laminoplasty, adapted to connect the two portions of the lamina of a vertebra resulting from an ablation of the central zone of said lamina, comprising: - a body having a first end and a second end, said body having an outer side, an inner side, an upper side and a lower side; a first direction extends from the outer side toward the inner side of said body; and - two anchoring portions, one of which is connected to said first end and the other of which is connected to said second end, each anchoring portion being in the shape of a U, i.e. comprising an inner side wall, an outer side wall, and an intermediate wall connecting said inner side wall to said outer side wall; a second directibn extends from said intermediate wall, perpendicularly thereto, toward the opening of the U defined between the free end edges of said inner side wall and said outer side wall; - said body comprises mounting means; characterized in that said intermediate wall of each anchor portion is situated at the upper side of the body of the implant, and said second direction is perpendicular to said first direction. - a body having a first end and a second end, said body having an outer side, an inner side, an upper side and a lower side; a first direction extends from the outer side toward the inner side of said body; and - two anchoring portions, one of which is connected to said first end and the other of which is connected to said second end, each anchoring portion being in the shape of a U, i.e. comprising an inner side wall, an outer side wall, and an intermediate wall connecting said inner side wall to said outer side wall; a second directibn extends from said intermediate wall, perpendicularly thereto, toward the opening of the U defined between the free end edges of said inner side wall and said outer side wall; - said body comprises mounting means;
A refrigeration system comprising: (a) a compressor arrangement for compressing gaseous refrigerant from a first pressure to a second pressure, wherein the second pressure comprises a condensing pressure; (b) a plurality of condenser evaporator systems, wherein each condenser evaporator system comprises: a condenser for receiving gaseous refrigerant at a condensing pressure and condensing the refrigerant to a liquid refrigerant; a controlled pressure receiver for holding the liquid refrigerant from the condenser; and an evaporator for evaporating liquid refrigerant from the controlled pressure receiver to form gaseous refrigerant; (c) a first gaseous refrigerant feed line for feeding the gaseous refrigerant at the second pressure from the compressor arrangement to the plurality of condenser evaporator systems; and (d) a second gaseous refrigerant feed line (120, 124) for feeding gaseous refrigerant from the plurality of condenser evaporator systems to the compressor arrangement. (a) a compressor arrangement for compressing gaseous refrigerant from a first pressure to a second pressure, wherein the second pressure comprises a condensing pressure; (b) a plurality of condenser evaporator systems, wherein each condenser evaporator system comprises: a condenser for receiving gaseous refrigerant at a condensing pressure and condensing the refrigerant to a liquid refrigerant; a controlled pressure receiver for holding the liquid refrigerant from the condenser; and an evaporator for evaporating liquid refrigerant from the controlled pressure receiver to form gaseous refrigerant; a condenser for receiving gaseous refrigerant at a condensing pressure and condensing the refrigerant to a liquid refrigerant; a controlled pressure receiver for holding the liquid refrigerant from the condenser; and an evaporator for evaporating liquid refrigerant from the controlled pressure receiver to form gaseous refrigerant; (c) a first gaseous refrigerant feed line for feeding the gaseous refrigerant at the second pressure from the compressor arrangement to the plurality of condenser evaporator systems; and (d) a second gaseous refrigerant feed line (120, 124) for feeding gaseous refrigerant from the plurality of condenser evaporator systems to the compressor arrangement.
A bending machine press group having at least one press element for bending a work piece and at least one guide whereon said press element is positioned, wherein the guide comprises a housing and the press element comprises two protrusion which extends in the direction of the axis of said guide, one of the protrusion is positioned on the housing provided on the guide and the bending machine press group comprises at least one first wedge which extends in the direction of the axis of said guide and which has a form narrowing at a predetermined angle which rests on the other protrusion, at least one second wedge provided between the first wedge and the guide which has a form widening at an angle which is essentially equal to the narrowing angle of the first wedge, and the bending machine press group comprises at least one drive unit which is connected to and which moves said second wedge essentially in the direction of the axis of the guide, the bending machine being characterized in that the first wedge comprises at least one recess which is positioned in order to provide bending of the first wedge during the contact of the first wedge to the press element.