mhurhangee/patent-ind-claim-en huggingface dataset:
An endorectal coil comprising: a tube configured for insertion into a rectum ; a spreader configured to be positioned at a distal end of the tube and mechanically spread to compress surrounding tissue after the tube is inserted; and one or more electrically conductive elements tuned to receive magnetic resonance data disposed on at least one of the tube and the spreader , characterized in that the spreader includes a rolled strip of material formed as a roll spring, wherein a stub is attached to a center edge of the spreader , and the diameter of the spreader can be increased and/or decreased by rotating the stub . a tube configured for insertion into a rectum ; a spreader configured to be positioned at a distal end of the tube and mechanically spread to compress surrounding tissue after the tube is inserted; and one or more electrically conductive elements tuned to receive magnetic resonance data disposed on at least one of the tube and the spreader , characterized in that the spreader includes a rolled strip of material formed as a roll spring, wherein a stub is attached to a center edge of the spreader , and the diameter of the spreader can be increased and/or decreased by rotating the stub .
An analysis device comprising: a specifying unit that specifies an implementation portion of a first code in a cooperation mechanism that sends and receives data between an application implemented by the first code and an application implemented by a second code different from the first code and that specifies a method in which a return value that can be called by the second code is set in the cooperation mechanism; an inserting unit that inserts, into the first code, a call code of a simulation function in which the return value of the specified method is inserted into an argument; and an analysis unit that analyzes a data flow by observing, by using the argument and the return value of the simulation function and the specified method, the data that is sent and received between the application implemented by the first code and the application implemented by the second code. a specifying unit that specifies an implementation portion of a first code in a cooperation mechanism that sends and receives data between an application implemented by the first code and an application implemented by a second code different from the first code and that specifies a method in which a return value that can be called by the second code is set in the cooperation mechanism; an inserting unit that inserts, into the first code, a call code of a simulation function in which the return value of the specified method is inserted into an argument; and an analysis unit that analyzes a data flow by observing, by using the argument and the return value of the simulation function and the specified method, the data that is sent and received between the application implemented by the first code and the application implemented by the second code.
A passenger service unit for an aircraft cabin, comprising: a mounting mechanism for mounting the passenger service unit above at least one seat; a dynamic seat row marker that is adapted to provide an indication of a seat position and a status portion indicating a status of a passenger or trip aspect that is readily viewable from an aircraft aisle and is changeable during a trip; a programmable active display that is readily viewable from the seat and provides trip changeable information about the trip to the passenger; an oxygen supply module comprising an oxygen canister (24.2a) and a plurality of oxygen masks (24.2b); a lighting module comprising a plurality of LED reading lights; at least one speaker comprising a horn having a circular cross section; and a power/logic module (20.1) for controlling the lighting module , and the at least one speaker , wherein the power/logic module (20.1) comprises a power supply adapted to convert supplied AC oder DC power into DC voltage usable by the power/logic module (20.1), and a common data communications interface for communicating with a cabin management system; and wherein a first speaker of the at least one speaker is vertically integrated into a first LED reading light of the plurality of LED reading lights, wherein an LED for illuminating the first LED reading light is at least partially surrounded by the horn of the first speaker, and wherein the first speaker and the first LED reading light share a common housing. a mounting mechanism for mounting the passenger service unit above at least one seat; a dynamic seat row marker that is adapted to provide an indication of a seat position and a status portion indicating a status of a passenger or trip aspect that is readily viewable from an aircraft aisle and is changeable during a trip; a programmable active display that is readily viewable from the seat and provides trip changeable information about the trip to the passenger; an oxygen supply module comprising an oxygen canister (24.2a) and a plurality of oxygen masks (24.2b); a lighting module comprising a plurality of LED reading lights; at least one speaker comprising a horn having a circular cross section; and a power/logic module (20.1) for controlling the lighting module , and the at least one speaker , wherein the power/logic module (20.1) comprises a power supply adapted to convert supplied AC oder DC power into DC voltage usable by the power/logic module (20.1), and a common data communications interface for communicating with a cabin management system; and a power supply adapted to convert supplied AC oder DC power into DC voltage usable by the power/logic module (20.1), and a common data communications interface for communicating with a cabin management system; and wherein a first speaker of the at least one speaker is vertically integrated into a first LED reading light of the plurality of LED reading lights, wherein an LED for illuminating the first LED reading light is at least partially surrounded by the horn of the first speaker, and wherein the first speaker and the first LED reading light share a common housing.
An image display program for stereoscopically displaying a virtual object , which is disposed in a virtual space, on a screen of a stereoscopic-viewing-enabling stereoscopic display device via a rendition of the virtual object with a usage of one pair of virtual cameras , the image display program causing a computer to operate as: stereoscopic vision reference distance determination means (31, S15) for determining a stereoscopic vision reference distance (F), which is a distance in an imaging direction from the one pair of virtual cameras and which is used as a reference for a sense of depth of stereoscopic vision, so as to change in accordance with an imaging distance (Do) which is a distance from the virtual cameras to the virtual object in the imaging direction; virtual camera setting means (31, S16) for setting the one pair of virtual cameras such that each of which obtains a view volume providing a predetermined sense of depth for the stereoscopic vision reference distance determined by the stereoscopic vision reference distance determination means; and stereoscopic display control means (31, S16) for stereoscopically displaying the virtual object on the screen of the stereoscopic display device by using one pair of virtual images generated by imaging the virtual object with the one pair of virtual cameras set by the virtual camera setting means. stereoscopic vision reference distance determination means (31, S15) for determining a stereoscopic vision reference distance (F), which is a distance in an imaging direction from the one pair of virtual cameras and which is used as a reference for a sense of depth of stereoscopic vision, so as to change in accordance with an imaging distance (Do) which is a distance from the virtual cameras to the virtual object in the imaging direction; virtual camera setting means (31, S16) for setting the one pair of virtual cameras such that each of which obtains a view volume providing a predetermined sense of depth for the stereoscopic vision reference distance determined by the stereoscopic vision reference distance determination means; and stereoscopic display control means (31, S16) for stereoscopically displaying the virtual object on the screen of the stereoscopic display device by using one pair of virtual images generated by imaging the virtual object with the one pair of virtual cameras set by the virtual camera setting means.
A vibration actuator comprising: a vibrator including a shaft, an electro-mechanical energy conversion element , and an elastic body that are penetrated by the shaft; a rotating body penetrated by the shaft, in contact with the vibrator , and for rotating about an axis of the shaft by a vibration of the elastic body ; an output transmission member penetrated by the shaft, engaged with the rotating body , and for rotating about the axis of the shaft by the rotation of the rotating body ; a fixed member not moving relative to the shaft and allowing the output transmission member to move relative to the fixed member ; and a pressure member for pressing the output transmission member toward the fixed member and pressing the rotating body toward the vibrator ; wherein the fixed member includes a base portion and a projection portion protruding from the base portion along the output transmission member , wherein the vibration actuator includes a pressure reception member between the base portion and the output transmission member in an axial direction of the shaft , and the base portion is pressed indirectly by the pressure member , with the output transmission member and the pressure reception member disposed therebetween, characterised in that the projection portion and the output transmission member are in contact with each other in a direction orthogonal to the axial direction of the shaft . a vibrator including a shaft, an electro-mechanical energy conversion element , and an elastic body that are penetrated by the shaft; a rotating body penetrated by the shaft, in contact with the vibrator , and for rotating about an axis of the shaft by a vibration of the elastic body ; an output transmission member penetrated by the shaft, engaged with the rotating body , and for rotating about the axis of the shaft by the rotation of the rotating body ; a fixed member not moving relative to the shaft and allowing the output transmission member to move relative to the fixed member ; and a pressure member for pressing the output transmission member toward the fixed member and pressing the rotating body toward the vibrator ; wherein the fixed member includes a base portion and a projection portion protruding from the base portion along the output transmission member , wherein the vibration actuator includes a pressure reception member between the base portion and the output transmission member in an axial direction of the shaft , and the base portion is pressed indirectly by the pressure member , with the output transmission member and the pressure reception member disposed therebetween, characterised in that the projection portion and the output transmission member are in contact with each other in a direction orthogonal to the axial direction of the shaft .
An acoustic attenuation panel comprising: - an alveolar structure including a plurality of acoustic cells separated from each other by peripheral partitions , - a perforated acoustic structure , the perforated acoustic structure and the alveolar structure being formed in a single piece in a first material, and - a porous acoustic layer formed of a second material, fastened to a surface of the perforated acoustic structure by entanglement of the first material in the second material and/or the second material in the first material, characterized in that - each perforation of the perforated acoustic structure has a substantially rectangular shape with rounded tops, or - the shape of the perforations corresponds to fractal shapes, or - at least one perforation is circular in shape and at least one perforation is trapezoidal in shape. - an alveolar structure including a plurality of acoustic cells separated from each other by peripheral partitions , - a perforated acoustic structure , - a porous acoustic layer formed of a second material, fastened to a surface of the perforated acoustic structure by entanglement of the first material in the second material and/or the second material in the first material, - each perforation of the perforated acoustic structure has a substantially rectangular shape with rounded tops, or - the shape of the perforations corresponds to fractal shapes, or - at least one perforation is circular in shape and at least one perforation is trapezoidal in shape.
Isolated peptide derived from the human cyclin B1 sequence of SEQ ID NO. 1 and which comprises at least one human cyclin B1 CD4 + T epitope which is immunodominant in vitro, said peptide being selected from the group consisting of: a) the sequences of up to 30 consecutive amino acids of the human cyclin B1 sequence of SEQ ID NO. 1 comprising one of the sequences of SEQ ID NO: 10, 57, 58, 61, 76, 77, 83, 84, 87, 88 and 91, and b) the sequences of 15 to 25 amino acids having at least 85 % identity with a sequence in a), with the exclusion of the sequence of 15 amino acids consisting of residues 279 to 293 of said sequence SEQ ID NO. 1, and said peptide in a) and b) being capable of stimulating a specific human CD4 + T lymphocyte response wherein the average strength of the in vitro response of human CD4 + T lymphocytes specific for said peptide is at least 2.8% in a group of human individuals expressing varied HLA II molecules including at least the HLA-DR1, HLA-DR3, HLA-DR4, HLA-DR7, HLA-DR11, HLA-DR13 and HLA-DR15 molecules, and the frequency of responders in vitro to said peptide is at least 65% in said group of human individuals. a) the sequences of up to 30 consecutive amino acids of the human cyclin B1 sequence of SEQ ID NO. 1 comprising one of the sequences of SEQ ID NO: 10, 57, 58, 61, 76, 77, 83, 84, 87, 88 and 91, and b) the sequences of 15 to 25 amino acids having at least 85 % identity with a sequence in a), with the exclusion of the sequence of 15 amino acids consisting of residues 279 to 293 of said sequence SEQ ID NO. 1, and said peptide in a) and b) being capable of stimulating a specific human CD4 + T lymphocyte response wherein the average strength of the in vitro response of human CD4 + T lymphocytes specific for said peptide is at least 2.8% in a group of human individuals expressing varied HLA II molecules including at least the HLA-DR1, HLA-DR3, HLA-DR4, HLA-DR7, HLA-DR11, HLA-DR13 and HLA-DR15 molecules, and the frequency of responders in vitro to said peptide is at least 65% in said group of human individuals.
Electronic weighing device comprising: - a reception tray to hold a load to be weighed, - at least one weight sensor designed to output at least one signal representative of the load applied on the reception tray , and - a user control interface designed to receive instructions from a user, characterised in that the user control interface comprises a touch interface comprising means of recognition of touch commands (MRC) arranged to determine at least one displacement of a contact between two points on the surface of the touch interface so as to control a function of the apparatus, and in that said at least one weight sensor is designed to output at least one signal representative of the applied load and of the load application position on the reception tray , and in that the touch command recognition means (MRC) are capable of determining at least the displacement of the contact between the two points on the surface of the touch interface as a function of data supplied by said at least one weight sensor . - a reception tray to hold a load to be weighed, - at least one weight sensor designed to output at least one signal representative of the load applied on the reception tray , and - a user control interface designed to receive instructions from a user,
A communication hub for a communication system, with at least an audio I/O interface for connection with one or more audio sources to at least receive an input audio signal and to transmit an output audio signal; a user device interface for connection with at least one user audio device ; a processor to provide a user input audio signal to the user device interface from the input audio signal and to receive a user output audio signal from the user device interface and to provide the output audio signal to the audio I/O interface ; characterized in that the communication hub further comprises a reporting module , configured to generate metadata comprising a sound pressure level of the input audio signal and to provide the metadata to a monitoring device of the communication system; wherein the reporting module is configured to determine a sound pressure level by analyzing the input audio signal together with settings of the communication hub; and wherein the communication hub is an intermediate device, connectable between the one or more audio sources and the at least one user audio device. an audio I/O interface for connection with one or more audio sources to at least receive an input audio signal and to transmit an output audio signal; a user device interface for connection with at least one user audio device ; a processor to provide a user input audio signal to the user device interface from the input audio signal and to receive a user output audio signal from the user device interface and to provide the output audio signal to the audio I/O interface ; characterized in that the communication hub further comprises a reporting module , configured to generate metadata comprising a sound pressure level of the input audio signal and to provide the metadata to a monitoring device of the communication system; wherein the reporting module is configured to determine a sound pressure level by analyzing the input audio signal together with settings of the communication hub; and wherein the communication hub is an intermediate device, connectable between the one or more audio sources and the at least one user audio device.
A composite positive active material comprising a composite represented by Formula 1: Formula 1 δLi 2 MO 3 ·(1-δ)[xLi 2 MnO 3 ·(1-x)Li d Ni a CO b M' c O 2 ] wherein, in Formula 1, M is Ti or Zr; M' is Mn, V, Mg, Ga, Si, W, Mo, Fe, Cr, Cu, Zn, Ti, Al, B, or a combination thereof; 0<x<0.3; a+b+c≤1; wherein the compound represented by Formula 1 is a compound represented by Formula 2, a compound represented by Formula 3, a compound represented by Formula 4, or a compound represented by Formula 5: Formula 2 δLi 2 TiO 3 ·(1-δ)[xLi 2 MnO 3 ·(1-x)Li d Ni a CO b Mn c O 2 ] wherein, in Formula 2, 0<δ<0.1, 0<x<0.1, a+b+c≤1, 0<a<1, 0<b<1, 0<c<1, and 0.95≤d≤1.05, Formula 3 δLi 2 ZrO 3 ·(1-δ)[xLi 2 MnO 3 ·(1-x)Li d Ni a CO b Mn c O 2 ] wherein, in Formula 3, 0<δ<0.1, 0<x<0.1, a+b+c≤1, 0<a<1, 0<b<1, 0<c<1, and 0.95≤d≤1.05, Formula 4 δLi 2 TiO 3 ·(1-δ)[xLi 2 MnO 3 ·(1-x)Li d Ni a Co b Al c O 2 ] wherein, in Formula 4, 0<δ<0.1, 0<x<0.1, a+b+c≤1, 0<a<1, 0<b<1, 0<c<1, and 0.95≤d≤1.05, and Formula 5 δLi 2 ZrO 3 ·(1-δ)[xLi 2 MnO 3 ·(1-x)Li d Ni a Co b Al c O 2 ] wherein, in Formula 5, 0<δ<0.1, 0<x<0.1, a+b+c≤1, 0<a<1, 0<b<1, 0<c<1, and 0.95≤d≤1.05 M is Ti or Zr; M' is Mn, V, Mg, Ga, Si, W, Mo, Fe, Cr, Cu, Zn, Ti, Al, B, or a combination thereof; 0<x<0.3; a+b+c≤1; wherein the compound represented by Formula 1 is a compound represented by Formula 2, a compound represented by Formula 3, a compound represented by Formula 4, or a compound represented by Formula 5:
An adaptive aircraft electrical power distribution system , comprising: an aircraft power source configured to be disposed within an aircraft, the aircraft power source operable to generate and supply electrical power; a power connector configured to be mounted on a fuselage of the aircraft and adapted to connect to an external power cable to receive power from an external power source and to supply power to an external power load ; an aircraft power distribution bus configured to be disposed within the aircraft and operable to distribute electrical power to an aircraft electrical load; and a bidirectional power controller configured to be mounted in the aircraft and electrically coupled to the aircraft power source, the aircraft power connector, and the aircraft power distribution bus, the bidirectional power controller configured to: sense when the aircraft power source is generating and supplying electrical power, sense when electrical power is being supplied to the power connector from the external power source, and selectively couple at least one of the aircraft power source or the power connector to the aircraft power distribution system. an aircraft power source configured to be disposed within an aircraft, the aircraft power source operable to generate and supply electrical power; a power connector configured to be mounted on a fuselage of the aircraft and adapted to connect to an external power cable to receive power from an external power source and to supply power to an external power load ; an aircraft power distribution bus configured to be disposed within the aircraft and operable to distribute electrical power to an aircraft electrical load; and a bidirectional power controller configured to be mounted in the aircraft and electrically coupled to the aircraft power source, the aircraft power connector, and the aircraft power distribution bus, the bidirectional power controller configured to: sense when the aircraft power source is generating and supplying electrical power, sense when electrical power is being supplied to the power connector from the external power source, and selectively couple at least one of the aircraft power source or the power connector to the aircraft power distribution system.
A network for maintaining communication, comprising: a plurality of nodes, each node being one of a base transceiver station (fig. 8B: 1-8) and a mobile station and being configured to communicate with other nodes of the plurality of nodes; a plurality of radio modules associated with each node, each radio module being configured to establish a link with a radio module associated with another one of the plurality of nodes; a mobility controller associated with each node, each mobility controller being configured to control the radio modules associated with that node; and a plurality of directional antennas (fig. 4A: 1-8) associated with each node, each directional antenna being configured to maintain one of the links concurrent to another of the antennas to maintain another link, wherein the links are between any combination of base transceiver stations and mobile stations. a plurality of nodes, each node being one of a base transceiver station (fig. 8B: 1-8) and a mobile station and being configured to communicate with other nodes of the plurality of nodes; a plurality of radio modules associated with each node, each radio module being configured to establish a link with a radio module associated with another one of the plurality of nodes; a mobility controller associated with each node, each mobility controller being configured to control the radio modules associated with that node; and a plurality of directional antennas (fig. 4A: 1-8) associated with each node, each directional antenna being configured to maintain one of the links concurrent to another of the antennas to maintain another link, wherein the links are between any combination of base transceiver stations and mobile stations.
A composition comprising a molecularly imprinted polymer synthesized using an ochratoxin mycotoxin template, wherein said ochratoxin mycotoxin template is N-(2-hydroxy-3,5-dichlorobenzoyl)-L-phenylalanine.