mhurhangee/patent-ind-claim-en huggingface dataset:
An endoscopic treatment tool comprising: a sheath ; an operating wire inserted into the sheath to be capable of advancing and retracting; a basket part positioned at a distal side of the operating wire and formed by binding a plurality of elastic basket wires having helical shapes in a natural state; a distal end tip which binds and fixes distal ends of the plurality of basket wires at a distal end of the basket part ; a binding part in which proximal end portions of the plurality of basket wires are bound together and fixed; and a support member disposed through the basket part along a central axis of the basket part , a proximal end portion of the support member being positioned inside the sheath , and a distal end portion of the support member being fixed to the distal end tip ; characterised by ; a connecting member positioned at a more proximal side than the binding part , and in that the connecting member is fixed to the operating wire or the proximal end portion of the support member , and the connecting member is configured to be slidable with respect to the other one of the operating wire or the proximal end portion of the support member inside the sheath along a longitudinal axis of the operating wire . a sheath ; an operating wire inserted into the sheath to be capable of advancing and retracting; a basket part positioned at a distal side of the operating wire and formed by binding a plurality of elastic basket wires having helical shapes in a natural state; a distal end tip which binds and fixes distal ends of the plurality of basket wires at a distal end of the basket part ; a binding part in which proximal end portions of the plurality of basket wires are bound together and fixed; and a support member disposed through the basket part along a central axis of the basket part , a proximal end portion of the support member being positioned inside the sheath , and a distal end portion of the support member being fixed to the distal end tip ; characterised by ; a connecting member positioned at a more proximal side than the binding part , and in that the connecting member is fixed to the operating wire or the proximal end portion of the support member , and the connecting member is configured to be slidable with respect to the other one of the operating wire or the proximal end portion of the support member inside the sheath along a longitudinal axis of the operating wire .
A decorative sheet comprising a release layer, a pressure-sensitive adhesive layer disposed on a surface of the release layer, and a skin layer disposed on a surface of the pressure-sensitive adhesive layer, wherein: the release layer includes a shape retention layer, and an easy release layer interposed between the pressure-sensitive adhesive layer and the shape retention layer; the shape retention layer is a resin sheet made from an acrylonitrile-butadiene-styrene copolymer being obtained by copolymerizing acrylonitrile, butadiene, and styrene by a polymerization method, such as a blend polymerization method or a graft polymerization method, wherein polymerization ratios of the acrylonitrile, butadiene, and styrene in the ABS resin are adjusted so that the shape retention layer has a softening start temperature and a rate of elongation in predetermined ranges; and the shape retention layer has a thickness of not less than 100 μm and not more than 700 μm, wherein the shape retention layer has a softening start temperature of not less than 80°C and not more than 150°C, wherein the softening start temperature is a temperature at which deformation begins when the object of measurement is heated in a no-load state, and is measured according to JIS K 7196 ,wherein the shape retention layer has a rate of elongation at 120°C of not less than 200%, wherein the rate of elongation is measured according to JIS K 6734 . the release layer includes a shape retention layer, and an easy release layer interposed between the pressure-sensitive adhesive layer and the shape retention layer; the shape retention layer is a resin sheet made from an acrylonitrile-butadiene-styrene copolymer being obtained by copolymerizing acrylonitrile, butadiene, and styrene by a polymerization method, such as a blend polymerization method or a graft polymerization method, wherein polymerization ratios of the acrylonitrile, butadiene, and styrene in the ABS resin are adjusted so that the shape retention layer has a softening start temperature and a rate of elongation in predetermined ranges; and the shape retention layer has a thickness of not less than 100 μm and not more than 700 μm, wherein the shape retention layer has a softening start temperature of not less than 80°C and not more than 150°C, wherein the softening start temperature is a temperature at which deformation begins when the object of measurement is heated in a no-load state, and is measured according to JIS K 7196 ,wherein the shape retention layer has a rate of elongation at 120°C of not less than 200%, wherein the rate of elongation is measured according to JIS K 6734 .
An anti-NMDA receptor monoclonal antibody or a fragment thereof, wherein said antibody or fragment thereof inhibits the interaction between the NMDA receptor and t-PA, and wherein said antibody or fragment thereof is capable of binding an epitope consisting in an amino acid sequence selected from the group consisting of SEQ ID NOs:15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28 and the peptide fragments: - LVSDDHEGRAAQKRL, - DDHEGRAAQKRLETL, - EGRAAQKRLETLLEE, and - AAQKRLETLLEERES - LVSDDHEGRAAQKRL, - DDHEGRAAQKRLETL, - EGRAAQKRLETLLEE, and - AAQKRLETLLEERES
A surface cooler assembly for a gas turbine engine comprising: at least one surface cooler , the at least one surface cooler comprising at least two surface cooler hook rails , the at least two surface cooler hook rails extending the length of the surface cooler in a circumferential direction, each of the at least two surface cooler hook rails comprising at least one axially extending portion and at least one radially extending portion , and the axially extending portions of the at least two hook rails extend axially opposite each other; at least one support bracket , the at least one support bracket comprising at least two bracket hook rails , the at least two bracket hook rails extending the length of the support bracket in a circumferential direction, each of the at least two bracket hook rails comprising at least one axially extending portion and at least one radially extending portion ; wherein the at least one support bracket and the at least one surface cooler are contoured in a circumferential direction, and wherein a portion of each of the at least two surface cooler hook rails contacts a portion of each of the at least two bracket hook rails ; the surface cooler assembly being further characterized in that it further comprises at least one linear wave spring , the at least one linear wave spring disposed radially between the at least two surface cooler hook rails and the at least two bracket hook rails , wherein a successive peak and a successive nadir of the at least one linear wave spring are arranged in the circumferential direction. at least one surface cooler , the at least one surface cooler comprising at least two surface cooler hook rails , the at least two surface cooler hook rails extending the length of the surface cooler in a circumferential direction, each of the at least two surface cooler hook rails comprising at least one axially extending portion and at least one radially extending portion , and the axially extending portions of the at least two hook rails extend axially opposite each other; at least one support bracket , the at least one support bracket comprising at least two bracket hook rails , the at least two bracket hook rails extending the length of the support bracket in a circumferential direction, each of the at least two bracket hook rails comprising at least one axially extending portion and at least one radially extending portion ; wherein the at least one support bracket and the at least one surface cooler are contoured in a circumferential direction, and wherein a portion of each of the at least two surface cooler hook rails contacts a portion of each of the at least two bracket hook rails ; the surface cooler assembly being further characterized in that it further comprises at least one linear wave spring , the at least one linear wave spring disposed radially between the at least two surface cooler hook rails and the at least two bracket hook rails , wherein a successive peak and a successive nadir of the at least one linear wave spring are arranged in the circumferential direction.
Method for cutting a laminate composed of at least one glass layer with a thickness less than or equal to 0.3 mm and at least one polymeric layer , comprising at least: a) generating a surface scratch on a first surface (I) of the glass layer , wherein the scratch , starting from a lateral edge, extends along a cutting line (L); b) subsequently moving a first laser beam , starting from the scratch , across the first surface (I) along the cutting line (L); c) subsequently cooling the glass layer along the cutting line (L), wherein the glass layer breaks along the cutting line (L); and wherein the polymeric layer is severed by moving a second laser beam along the cutting line (L). a) generating a surface scratch on a first surface (I) of the glass layer , wherein the scratch , starting from a lateral edge, extends along a cutting line (L); b) subsequently moving a first laser beam , starting from the scratch , across the first surface (I) along the cutting line (L); c) subsequently cooling the glass layer along the cutting line (L), wherein the glass layer breaks along the cutting line (L);
A message processing method, wherein the method comprises: calculating, by a calling party, a sending time length for sending a service message; requesting an occupation time period from a control node according to the sending time length (S1); upon reception of an application message for the occupation time period from the calling party, determining, by the control node, an application result of the occupation time period of the calling party according to a predetermined rule; feeding the application result back to the corresponding calling party (S2); calculating, by the calling party, a sending time of the service message when a received application result of the occupation time period is success (S3); applying, by the calling party, for a sending token of the service message from the control node when the calling party monitors that the sending time of the service message is exceeded (S4); upon reception of an application message for the sending token from the calling party, determining, by the control node, an application result of the sending token of the calling party according to whether the maximum service processing capability of a called party is reached; feeding the application result back to the corresponding calling party (S5); and sending, by the calling party, the service message of which the sending token is successfully applied for when the received application result of the sending token of the service message is success (S6). calculating, by a calling party, a sending time length for sending a service message; requesting an occupation time period from a control node according to the sending time length (S1); upon reception of an application message for the occupation time period from the calling party, determining, by the control node, an application result of the occupation time period of the calling party according to a predetermined rule; feeding the application result back to the corresponding calling party (S2); calculating, by the calling party, a sending time of the service message when a received application result of the occupation time period is success (S3); applying, by the calling party, for a sending token of the service message from the control node when the calling party monitors that the sending time of the service message is exceeded (S4); upon reception of an application message for the sending token from the calling party, determining, by the control node, an application result of the sending token of the calling party according to whether the maximum service processing capability of a called party is reached; feeding the application result back to the corresponding calling party (S5); and sending, by the calling party, the service message of which the sending token is successfully applied for when the received application result of the sending token of the service message is success (S6).
Testing device for detecting defects of transparent test specimens , in particular of ophthalmological lenses, with an illumination device for transilluminating test specimens to be examined and with an image acquisition device for imaging the test specimen transilluminated by the illumination device , characterized in that the illumination device comprises a plurality of light sources , which are linearly moveable by a first drive in a first direction for generating a stripe pattern , and in that , in order to capture the stripe pattern , the acquisition duration of the image acquisition device can be adjusted in such a way that the light emitted by each of the light sources , moved linearly by the first drive in the first directions , is detected as a light stripe (19.1).
A radiative fin for a spacecraft (S), comprising : - an end fitting of heat conductive material, adapted to be mounted on the spacecraft (S), - a flexible radiative laminate , connected to the end fitting at one end and having an opposite free end , and comprising : ∘ at least one pyrolytic graphite sheet , and ∘ at least one heat emission layer in contact with the pyrolythic graphite sheet on at least part of the surface of the pyrolythic graphite sheet, and - a flexible rod , extending from the end fitting along at least part of a side of the flexible radiative laminate and being affixed to the latter, wherein the flexible rod is adapted to occupy a folded position and a deployed position and to exert, while in the folded position, a deployment torque adapted to bring the flexible rod back to the deployed position, characterized in that the flexible rod is a pinless hinge being a strip comprising a portion of reduced width dimensioned to exhibit an elastic behavior in the folded and deployed positions. - an end fitting of heat conductive material, adapted to be mounted on the spacecraft (S), - a flexible radiative laminate , connected to the end fitting at one end and having an opposite free end , and comprising : ∘ at least one pyrolytic graphite sheet , and ∘ at least one heat emission layer in contact with the pyrolythic graphite sheet on at least part of the surface of the pyrolythic graphite sheet, and ∘ at least one pyrolytic graphite sheet , and ∘ at least one heat emission layer in contact with the pyrolythic graphite sheet on at least part of the surface of the pyrolythic graphite sheet, and - a flexible rod , extending from the end fitting along at least part of a side of the flexible radiative laminate and being affixed to the latter, wherein the flexible rod is adapted to occupy a folded position and a deployed position and to exert, while in the folded position, a deployment torque adapted to bring the flexible rod back to the deployed position,
A baffle plate element having a connection end (10; 10'; 10A; 10B), which has a first connection region for connection to a vessel wall and a relief edge , which connects one end of a free baffle plate edge to the first connection region , the relief edge having a first portion that extends along the first connection region and forms a rib portion therewith, a second portion , which connects the first portion to the free edge of the baffle plate element , characterized in that the relief edge extends smoothly between the first connection region and the free edge .
Proto-device for implantation into soft tissue, in particular nervous or endocrine tissue, selected from the group consisting of proto-microelectrode, proto-optical fibre, proto-polymer tube for drug delivery, proto-electrical lead, proto-encapsulated electronics, comprising an oblong device body having a proximal end, a distal end, and a central axis; characterized in that the proto-device further comprises: (i) biodegradable microfibres adhesively attached to the device body, wherein a microfibre is biodegradable in the tissue within a period of one or two weeks or one month or two months from implantation; (ii) a rigid matrix of biocompatible material having an outer face and enclosing the device body and the microfibres, wherein the rigid matrix of biocompatible material is dissolvable and/or degradable in aqueous body fluid at a rate superior to the rate of microfibre degradation by a factor of 2 or 5 or 10 or 20 or, in particular, 100 or more; and (iii) a means for supporting permanent positional stabilization upon biodegradation of the microfibres comprised by the device body or attached to an outer face thereof, wherein the means is selected from the group consisting of: rugged surface of the device body, knobby retainer optionally comprising a rugged surface attached to device body, eye, loop or bent section of the device body, wherein the bending section is bent away from the central axis by an angle of 15 ° or more, in particular by an angle of 30° or more. (i) biodegradable microfibres adhesively attached to the device body, wherein a microfibre is biodegradable in the tissue within a period of one or two weeks or one month or two months from implantation; (ii) a rigid matrix of biocompatible material having an outer face and enclosing the device body and the microfibres, wherein the rigid matrix of biocompatible material is dissolvable and/or degradable in aqueous body fluid at a rate superior to the rate of microfibre degradation by a factor of 2 or 5 or 10 or 20 or, in particular, 100 or more; and (iii) a means for supporting permanent positional stabilization upon biodegradation of the microfibres comprised by the device body or attached to an outer face thereof, wherein the means is selected from the group consisting of: rugged surface of the device body, knobby retainer optionally comprising a rugged surface attached to device body, eye, loop or bent section of the device body, wherein the bending section is bent away from the central axis by an angle of 15 ° or more, in particular by an angle of 30° or more.
An assay monitoring system for monitoring the staining process of an assay, comprising: a sample processing system comprising at least one sample having at least one specimen undergoing a staining process in the course of an assay; an imaging system positioned adjacent the sample processing system , a controller configured to control the imaging system and the sample processing system ; the imaging system configured to capture an image of the at least one sample during the staining process of the specimen ; wherein the controller is communicatively coupled to the imaging system to receive the captured image of the at least one sample from the imaging system , wherein the controller is configured to process the captured image to determine at least one attribute associated with the staining process based on the processed image and to control the sample processing system in response to the determined at least one attribute. a sample processing system comprising at least one sample having at least one specimen undergoing a staining process in the course of an assay; an imaging system positioned adjacent the sample processing system , a controller configured to control the imaging system and the sample processing system ; the imaging system configured to capture an image of the at least one sample during the staining process of the specimen ; wherein the controller is communicatively coupled to the imaging system to receive the captured image of the at least one sample from the imaging system , wherein the controller is configured to process the captured image to determine at least one attribute associated with the staining process based on the processed image and to control the sample processing system in response to the determined at least one attribute.
Method for manufacturing a cladding component, in particular an exterior cladding component, for mounting onto the chassis of a motor vehicle, comprised of a main body which, in a first method step, is manufactured in a mold cavity in a foam injection molding process, and of a coating of at least partial surfaces of the main body , wherein the coating is applied to the main body , following the foam injection molding process, in the mold cavity in which the main body itself was produced, wherein the coating is a hard component with a hardness of at least 68 Shore D, wherein a female and a male are used to delimit the, apart from that, same mold cavity before the coating is applied, wherein, during the process, the mold cavity is altered in at least one dimension at least once, characterized in that , after the injection molding of the main body , instead of the first female , a second female is placed onto the male , almost to the main body , with no gap to the male , in order to enlarge the mold cavity. wherein the coating is a hard component with a hardness of at least 68 Shore D, wherein a female and a male are used to delimit the, apart from that, same mold cavity before the coating is applied, wherein, during the process, the mold cavity is altered in at least one dimension at least once, characterized in that , after the injection molding of the main body , instead of the first female , a second female is placed onto the male , almost to the main body , with no gap to the male , in order to enlarge the mold cavity.
A combustor wall assembly for a combustor of a gas turbine engine , the combustor wall assembly comprising: a support shell with a multiple of impingement holes ; a liner panel with a multiple of film holes , the liner panel mounted to the support shell via a multiple of studs that extend from a cold side of the liner panel , the liner panel including a periphery rail that extends from the cold side of the liner panel to interface with the support shell ; and a gasket between the support shell and the liner panel , characterised in that : the gasket includes a lattice structure that forms a multiple of cells between the support shell and the liner panel . a support shell with a multiple of impingement holes ; a liner panel with a multiple of film holes , the liner panel mounted to the support shell via a multiple of studs that extend from a cold side of the liner panel , the liner panel including a periphery rail that extends from the cold side of the liner panel to interface with the support shell ; and a gasket between the support shell and the liner panel , characterised in that : the gasket includes a lattice structure that forms a multiple of cells between the support shell and the liner panel .