mhurhangee/ep-ind-claims huggingface dataset:
An antibody or a fragment thereof that binds to an SRPX2 amino acid sequence selected from SEQ ID NOs: 14-23 and inhibits the activity of SRPX2 in angiogenesis.
An aircraft comprising: a cabin having a floor, side walls, a ceiling and an interior, a first class section positioned in the interior that includes a longitudinally extending first aisle extending therethrough, a first door positioned fore of the first class section, an other class section (16, 18) positioned in the interior, and a longitudinally extending second aisle that extends parallel to the first aisle and that does not extend through the first class section, wherein an other class passenger that enters through the first door travels down the second aisle to enter the other class section (16, 18). a cabin having a floor, side walls, a ceiling and an interior, a first class section positioned in the interior that includes a longitudinally extending first aisle extending therethrough, a first door positioned fore of the first class section, an other class section (16, 18) positioned in the interior, and a longitudinally extending second aisle that extends parallel to the first aisle and that does not extend through the first class section, wherein an other class passenger that enters through the first door travels down the second aisle to enter the other class section (16, 18).
A cryoablation catheter comprising: a catheter body comprising a cold-source fluid input lumen and a cold-source fluid output lumen both extending in an axial direction of the catheter body; and a freezing unit arranged at a distal portion of the catheter body, the freezing unit comprises a first balloon in fluid communication with the cold-source fluid input lumen and the cold-source fluid output lumen, and a second balloon arranged external to the first balloon, with the length of the first balloon being less than the length of the second balloon, an area between the first balloon and the second balloon is a sealed space, and the sealed space is configured to be pumped to a vacuum state in advance, a part of wall of the first balloon and a part of wall of the second balloon are fitted to each other, and the joint portion of the walls of the first balloon and of the second balloon is a channel for transferring freezing energy to a treatment position, when the first balloon and the second balloon are dilated, a cavity for avoiding energy transfer is formed between the first balloon and the second balloon, to prevent energy transfer in the space of the freezing unit corresponding to the cavity.
A complex in which an anti-cotinine antibody is bound to a conjugate of cotinine and a binding material, wherein the binding material is selected from the group consisting of a peptide, an aptamer, a hormone and a protein, wherein the binding material is linked to the cotinine via a PEG linker or an amino C6 linker.
A method of producing a fertilizer comprising: feeding synthetic gypsum to a drying device; drying the synthetic gypsum at a temperature below 128°C (262°F), wherein the synthetic gypsum is dried to less than 3% moisture; calcining the dried synthetic gypsum to convert the synthetic gypsum into either alpha-hemihydrate or beta-hemihydrate; feeding the calcined synthetic gypsum to a mixing device; feeding a binder composition to the mixing device; mixing the calcined synthetic gypsum and binder composition to form a mixture; feeding the mixture to a forming device, wherein the forming device comprises an extruder; and forming the material fed to the forming device to a mean pellet size guide number from 100 to 500, wherein the resulting pelletized synthetic gypsum has a crush strength from 0.91 kilograms (2 lbf) -force to 5.44 kilograms (12 lbf) -force. feeding synthetic gypsum to a drying device; drying the synthetic gypsum at a temperature below 128°C (262°F), wherein the synthetic gypsum is dried to less than 3% moisture; calcining the dried synthetic gypsum to convert the synthetic gypsum into either alpha-hemihydrate or beta-hemihydrate; feeding the calcined synthetic gypsum to a mixing device; feeding a binder composition to the mixing device; mixing the calcined synthetic gypsum and binder composition to form a mixture; feeding the mixture to a forming device, wherein the forming device comprises an extruder; and forming the material fed to the forming device to a mean pellet size guide number from 100 to 500, wherein the resulting pelletized synthetic gypsum has a crush strength from 0.91 kilograms (2 lbf) -force to 5.44 kilograms (12 lbf) -force.
A head (14, 15) for an oral care implement (10, 54) comprising: at least two tufts (18, 50, 56) extending from a mounting surface of the head (14, 15), the tufts (18, 50, 56) being inclined with respect to the mounting surface in at least two different directions, wherein each of the tufts (18, 50, 56) comprises a first group of filaments (34, 66) having a first length and at least a second group of filaments (36, 68) having a second length, the first length being different from the second length, characterized in that at least one tuft (18, 50, 56) is inclined in a direction being substantially parallel to the longitudinal extension of the head (14, 15), and the at least one tuft (18, 50, 56) further comprises at least a third group of filaments, and the first group of filaments is sandwiched between the second and the third group of filaments (68, 70), and the first group of filaments has the greater length, and wherein higher bending stiffness is provided in a brushing direction along the longitudinal extension of the head, and a lower bending stiffness in an orthogonal direction thereto. at least two tufts (18, 50, 56) extending from a mounting surface of the head (14, 15), the tufts (18, 50, 56) being inclined with respect to the mounting surface in at least two different directions, wherein each of the tufts (18, 50, 56) comprises a first group of filaments (34, 66) having a first length and at least a second group of filaments (36, 68) having a second length, the first length being different from the second length, characterized in that at least one tuft (18, 50, 56) is inclined in a direction being substantially parallel to the longitudinal extension of the head (14, 15), and the at least one tuft (18, 50, 56) further comprises at least a third group of filaments, and the first group of filaments is sandwiched between the second and the third group of filaments (68, 70), and the first group of filaments has the greater length, and wherein higher bending stiffness is provided in a brushing direction along the longitudinal extension of the head, and a lower bending stiffness in an orthogonal direction thereto.
A method for converting call mode, characterized in that said method comprises: establishing, by a mobile switching center, circuits of port A for both parties of a call of a local switch and sending a conversion notification message; and establishing, by a base station controller, circuits of port A for both parties of a call of the local switch according to the conversion notification message received by the base station controller from the mobile switching center. establishing, by a mobile switching center, circuits of port A for both parties of a call of a local switch and sending a conversion notification message; and establishing, by a base station controller, circuits of port A for both parties of a call of the local switch according to the conversion notification message received by the base station controller from the mobile switching center.
An adjustable seat comprising: an upper frame comprising a pair of support arms, a seat pan, a back rest pivotally coupled to the upper frame; a lower frame comprising a pair of support legs; and a coupling system comprising an upper rod and a lower rod; wherein the upper rod and the lower rod are pivotally coupled to the pair of support arms and the pair of support legs, and the upper rod and the lower rod have substantially similar lengths, the position of the pivotal coupling between the upper rod and the pair of support arms being substantially vertically aligned with the position of the pivotal coupling between the lower rod and the pair of support arms, the position of the pivotal coupling between the upper rod and the pair of support legs being substantially vertically aligned with the position of the pivotal coupling between the lower rod and the pair of support legs, characterized in that the support legs are positioned at an angle toward a central location, such that a distance between lower portions of the support legs is greater than a distance between upper portions of the support legs. an upper frame comprising a pair of support arms, a seat pan, a back rest pivotally coupled to the upper frame; a lower frame comprising a pair of support legs; and a coupling system comprising an upper rod and a lower rod; wherein the upper rod and the lower rod are pivotally coupled to the pair of support arms and the pair of support legs, and the upper rod and the lower rod have substantially similar lengths, the position of the pivotal coupling between the upper rod and the pair of support arms being substantially vertically aligned with the position of the pivotal coupling between the lower rod and the pair of support arms, the position of the pivotal coupling between the upper rod and the pair of support legs being substantially vertically aligned with the position of the pivotal coupling between the lower rod and the pair of support legs, characterized in that the support legs are positioned at an angle toward a central location, such that a distance between lower portions of the support legs is greater than a distance between upper portions of the support legs.
A sensor device (10E, 10F, 10G, 10H), comprising: a plurality of sensor units, comprising: a plurality of sensor elements; an interlayer disposed on the plurality of sensor elements; a passivation layer disposed on the interlayer; a micro-lens structure comprising an array of micro-lenses disposed on the passivation layer; a plurality of openings each disposed in a respective micro-lens of the micro-lens structure; a first reflecting layer disposed on the micro-lens structure, wherein the first reflecting layer extends from the openings to the passivation layer; and a second reflecting layer disposed between the interlayer and the micro-lens structure provided as a plurality of portions laterally spaced apart from each other with each portion of the second reflecting layer being located in alignment with a respective opening. a plurality of sensor elements; an interlayer disposed on the plurality of sensor elements; a passivation layer disposed on the interlayer; a micro-lens structure comprising an array of micro-lenses disposed on the passivation layer; a plurality of openings each disposed in a respective micro-lens of the micro-lens structure; a first reflecting layer disposed on the micro-lens structure, wherein the first reflecting layer extends from the openings to the passivation layer; and a second reflecting layer disposed between the interlayer and the micro-lens structure provided as a plurality of portions laterally spaced apart from each other with each portion of the second reflecting layer being located in alignment with a respective opening.
A T cell activating bispecific antigen binding molecule comprising a first and a second antigen binding moiety, one of which is a Fab molecule capable of specific binding to an activating T cell antigen and the other one of which is a Fab molecule capable of specific binding to a target cell antigen, and an Fc domain composed of a first and a second subunit capable of stable association; wherein the first antigen binding moiety is a crossover Fab molecule wherein either the variable or the constant regions of the Fab light chain and the Fab heavy chain are exchanged; wherein the first and the second antigen binding moiety are fused to each other, optionally via a peptide linker; and wherein the T cell activating bispecific antigen binding molecule comprises not more than one antigen binding moiety capable of specific binding to an activating T cell antigen.
A system for routing a message to a first network server in a server pool (CNSP) of a mobile communication system, the mobile communication system comprising a controller of an access network connectable to the first network server and at least one further network server in the server pool (CNSP), wherein service points are defined and one or more of the service points are allocated uniquely to each of the network servers (MSC1, MSC2) in the server pool (CNSP), at least the first network server having allocated at least two of the service points, wherein the first network server is adapted to assign a temporary identity to a mobile device, the temporary identity including a selected service point which is selected from the service points allocated to the first network server, the first network server is adapted to send the temporary identity to the mobile device, the controller is adapted to route a message comprising the selected service point from the mobile device to the first network server by applying a routing algorithm to the selected service point, the routing algorithm revealing the first network server from an analysis of the selected service point.
A computer-implemented method comprising: defining, in a buffer, a plurality of particles having a plurality of initial positions in an absolute coordinate system independent of a graphical user interface, GUI, in which the plurality of particles are renderable; assigning a plurality of memory ranges within the buffer to corresponding ones of the plurality of particles; generating, in the plurality of memory ranges, a plurality of updated positions for the plurality of particles; determining, in the plurality of memory ranges and from a combination of the plurality of initial positions and the plurality of updated positions, a corresponding plurality of vertices for each of the plurality of particles; creating, from the corresponding plurality of vertices, a plurality of corresponding particle trails for the plurality of particles; and storing the plurality of corresponding particle trails in the plurality of memory ranges associated with the plurality of particles. defining, in a buffer, a plurality of particles having a plurality of initial positions in an absolute coordinate system independent of a graphical user interface, GUI, in which the plurality of particles are renderable; assigning a plurality of memory ranges within the buffer to corresponding ones of the plurality of particles; generating, in the plurality of memory ranges, a plurality of updated positions for the plurality of particles; determining, in the plurality of memory ranges and from a combination of the plurality of initial positions and the plurality of updated positions, a corresponding plurality of vertices for each of the plurality of particles; creating, from the corresponding plurality of vertices, a plurality of corresponding particle trails for the plurality of particles; and storing the plurality of corresponding particle trails in the plurality of memory ranges associated with the plurality of particles.
A thrust reverser cascade comprising: a plurality of cascade vanes (420A-C) arranged in a ramp shaped cross-section and configured to couple to a portion of an aircraft propulsor nacelle and permit airflow through the cascade vanes (420A-C), wherein the ramp shaped cross-section comprises: a first portion configured to be disposed at a first angle to at least a portion of a surface of the aircraft propulsor nacelle, a second portion disposed at a second angle to the first portion, wherein the first portion is configured to raise the second portion as compared to a linear thrust reverser, and a third portion disposed at a third angle to the second portion, and being configured to be coupled to a cascade support ring, wherein the thrust reverser cascade defines a bridge shape; and a connecting structure coupled to at least two of the plurality of cascade vanes (420A-C). a plurality of cascade vanes (420A-C) arranged in a ramp shaped cross-section and configured to couple to a portion of an aircraft propulsor nacelle and permit airflow through the cascade vanes (420A-C), wherein the ramp shaped cross-section comprises: a first portion configured to be disposed at a first angle to at least a portion of a surface of the aircraft propulsor nacelle, a second portion disposed at a second angle to the first portion, wherein the first portion is configured to raise the second portion as compared to a linear thrust reverser, and a third portion disposed at a third angle to the second portion, and being configured to be coupled to a cascade support ring, a first portion configured to be disposed at a first angle to at least a portion of a surface of the aircraft propulsor nacelle, a second portion disposed at a second angle to the first portion, wherein the first portion is configured to raise the second portion as compared to a linear thrust reverser, and a third portion disposed at a third angle to the second portion, and being configured to be coupled to a cascade support ring, wherein the thrust reverser cascade defines a bridge shape; and a connecting structure coupled to at least two of the plurality of cascade vanes (420A-C).
An element (10; 50) comprising: a core structure (11; 51) which has a root portion (18; 54) and is formed from a high thermal conductivity ceramic matrix composite material; and a low thermal conductivity layer (14; 52) co-formed with said core structure (11; 51) and surrounding said root portion (18; 54) of said core structure (11; 51); characterized in that said low thermal conductivity layer (14; 52) is formed from a three dimensional woven material infiltrated by a matrix material. a core structure (11; 51) which has a root portion (18; 54) and is formed from a high thermal conductivity ceramic matrix composite material; and a low thermal conductivity layer (14; 52) co-formed with said core structure (11; 51) and surrounding said root portion (18; 54) of said core structure (11; 51); characterized in that said low thermal conductivity layer (14; 52) is formed from a three dimensional woven material infiltrated by a matrix material.
An image display device, comprising: an image forming unit (111, 211); an optical unit configured to input and output light that is output from the image forming unit; a temperature measuring unit configured to measure a temperature of the image forming unit; and a control unit configured to control an operation of the image forming unit based on a result of a temperature measurement by the temperature measuring unit, wherein the image forming unit includes a light source including a GaN-based semiconductor laser element, the temperature measuring unit is configured to measure a temperature of the semiconductor laser element, and the control unit is configured to control a wavelength of the semiconductor laser element, wherein the control unit is configured to control a current supplied to the semiconductor laser element to thus control the wavelength of the semiconductor laser element. an image forming unit (111, 211); an optical unit configured to input and output light that is output from the image forming unit; a temperature measuring unit configured to measure a temperature of the image forming unit; and a control unit configured to control an operation of the image forming unit based on a result of a temperature measurement by the temperature measuring unit, wherein
A method for measuring a wireless link quality by a user equipment, UE (1a-1j), in a communication system, the method comprising: receiving a message including candidate transmission gap configurations and a serving cell quality threshold from a wireless access network; selecting a transmission gap configuration from the candidate transmission gap configurations; transmitting information indicating the selected transmission gap configuration to the network; performing quality measurement for wireless links of neighboring cells during a period according to the transmission gap configuration, based on a result of a comparison between a wireless link quality of a serving cell and the serving cell quality threshold. receiving a message including candidate transmission gap configurations and a serving cell quality threshold from a wireless access network; selecting a transmission gap configuration from the candidate transmission gap configurations; transmitting information indicating the selected transmission gap configuration to the network; performing quality measurement for wireless links of neighboring cells during a period according to the transmission gap configuration, based on a result of a comparison between a wireless link quality of a serving cell and the serving cell quality threshold.
An earth boring drill bit (10, 11) comprising: a bit body having a longitudinal axis along a path of the bit (10, 11); a first plurality of cutters mounted to the body; a second plurality of cutters rotatably mounted to the body;wherein a longitudinal axial relationship between the first plurality of cutters and the second plurality of cutters is adjustable; a sensor providing an indication of a formation type being excavated by the bit (10, 11); and a processor controlling the longitudinal axial relationship based on the indication. a bit body having a longitudinal axis along a path of the bit (10, 11); a first plurality of cutters mounted to the body; a second plurality of cutters rotatably mounted to the body;wherein a longitudinal axial relationship between the first plurality of cutters and the second plurality of cutters is adjustable; a sensor providing an indication of a formation type being excavated by the bit (10, 11); and a processor controlling the longitudinal axial relationship based on the indication.
An aircraft engine system (50, 150, 180, 250) comprising: a high pressure stage turbocharger assembly (52, 252) comprising a high pressure stage wastegate (88, 288) and a turbocharger control unit (80, 280) configured for controlling pressure input to the engine by controlling the extent to which the high pressure stage wastegate opens and closes; and a supplemental stage turbocharger assembly (56, 256) disposed in series with respect to said high pressure stage turbocharger assembly comprising a supplemental wastegate (132, 332, 349) and a supplemental turbocharger control unit (120, 320) configured for controlling pressure input to the high pressure stage turbocharger assembly by controlling the extent to which the supplemental wastegate opens and closes, characterised in that the supplemental stage turbocharger assembly is configured to provide a compressor unit (62, 262) of the high pressure stage turbocharger assembly with substantially constant original critical altitude pressure input when the aircraft engine system is located above an original critical altitude of the aircraft engine system and below a new critical altitude (CR2, CR3) of the aircraft engine system. a high pressure stage turbocharger assembly (52, 252) comprising a high pressure stage wastegate (88, 288) and a turbocharger control unit (80, 280) configured for controlling pressure input to the engine by controlling the extent to which the high pressure stage wastegate opens and closes; and a supplemental stage turbocharger assembly (56, 256) disposed in series with respect to said high pressure stage turbocharger assembly comprising a supplemental wastegate (132, 332, 349) and a supplemental turbocharger control unit (120, 320) configured for controlling pressure input to the high pressure stage turbocharger assembly by controlling the extent to which the supplemental wastegate opens and closes, characterised in that the supplemental stage turbocharger assembly is configured to provide a compressor unit (62, 262) of the high pressure stage turbocharger assembly with substantially constant original critical altitude pressure input when the aircraft engine system is located above an original critical altitude of the aircraft engine system and below a new critical altitude (CR2, CR3) of the aircraft engine system.