mhurhangee/ep-ind-claims huggingface dataset:
An acoustic panel for an aircraft comprising: a sound attenuating sheet comprising two layers of sound attenuating sheets (121, 122), each comprising a plurality of cavities, the two sound attenuating sheets being separated by a septum, the sound attenuating sheet having a first surface, a second surface opposite to the first surface and an end surface connecting the first and second surfaces, a first sheet portion extending over and abutting both at least a portion of the first surface and at least a portion of the end surface, a second sheet portion extending over and abutting both at least a portion of the second surface and at least a portion of the end surface, and a third sheet, separate from the first and second sheet portions, wherein the first and the second sheet portions form a single continuous sheet such that a tensile force can be transferred there between, and wherein the panel is curved, such that the first surface is a radially outer surface and the second surface is a radially inner surface, the end surface having an annular or arcuate shape, characterised in that the third sheet includes a stepped portion extending over and directly abutting a part of the first sheet portion that extends over at least a portion of the first surface of the sound attenuating sheet, the third sheet further including a planar portion extending over and directly abutting the first surface of the sound attenuating sheet, the planar portion of the third sheet being coplanar with said part of the first sheet portion. a sound attenuating sheet comprising two layers of sound attenuating sheets (121, 122), each comprising a plurality of cavities, the two sound attenuating sheets being separated by a septum, the sound attenuating sheet having a first surface, a second surface opposite to the first surface and an end surface connecting the first and second surfaces, a first sheet portion extending over and abutting both at least a portion of the first surface and at least a portion of the end surface, a second sheet portion extending over and abutting both at least a portion of the second surface and at least a portion of the end surface, and a third sheet, separate from the first and second sheet portions, wherein the first and the second sheet portions form a single continuous sheet such that a tensile force can be transferred there between, and wherein the panel is curved, such that the first surface is a radially outer surface and the second surface is a radially inner surface, the end surface having an annular or arcuate shape, characterised in that the third sheet includes a stepped portion extending over and directly abutting a part of the first sheet portion that extends over at least a portion of the first surface of the sound attenuating sheet, the third sheet further including a planar portion extending over and directly abutting the first surface of the sound attenuating sheet, the planar portion of the third sheet being coplanar with said part of the first sheet portion.
Catheter device comprising a drive shaft, a rotor (3.2) for conveying blood, which is connected to the drive shaft, characterized in that a guide spiral is arranged around the drive shaft. a drive shaft, a rotor (3.2) for conveying blood, which is connected to the drive shaft, characterized in that a guide spiral is arranged around the drive shaft.
A vehicle comprising: a vehicle cabin; a storage chamber (5, 6, 7) arranged on at least one side of the vehicle cabin in a vehicle front-rear direction; and a partition wall separating the storage chamber (5, 6, 7) from the vehicle cabin, wherein a first brake fluid pressure generation device (20, 30, 40) included in a braking device for wheel braking is stored in the storage chamber (5, 6, 7), and the first brake fluid pressure generation device (20, 30, 40) includes a reservoir tank (25, 35) in which hydraulic fluid is accumulated; characterized in that the partition wall has an opening, via which the storage chamber (5, 6, 7) communicates with the vehicle cabin, such that maintenance of the first brake fluid pressure generation device (20, 30, 40) is performable from the vehicle cabin side through the opening, a cover configured to open and close the opening is provided over the opening, and the first brake fluid pressure generation device (20, 30, 40) including the reservoir tank (25, 35) is arranged at a position facing the opening. a vehicle cabin; a storage chamber (5, 6, 7) arranged on at least one side of the vehicle cabin in a vehicle front-rear direction; and a partition wall separating the storage chamber (5, 6, 7) from the vehicle cabin, wherein a first brake fluid pressure generation device (20, 30, 40) included in a braking device for wheel braking is stored in the storage chamber (5, 6, 7), and the first brake fluid pressure generation device (20, 30, 40) includes a reservoir tank (25, 35) in which hydraulic fluid is accumulated; characterized in that the partition wall has an opening, via which the storage chamber (5, 6, 7) communicates with the vehicle cabin, such that maintenance of the first brake fluid pressure generation device (20, 30, 40) is performable from the vehicle cabin side through the opening, a cover configured to open and close the opening is provided over the opening, and the first brake fluid pressure generation device (20, 30, 40) including the reservoir tank (25, 35) is arranged at a position facing the opening.
Dosing device, comprising a rod element having a stem with a longitudinal axis and a first thread arrangement (35, 36), and a shell having a second thread arrangement, wherein, the first thread arrangement (35, 36) of the rod element or the second thread arrangement of the shell comprises a thread, the first thread arrangement (35, 36) of the rod element and the second thread arrangement of the shell engage, the rod element is movable along the longitudinal axis of its stem by rotating the shell and the rod element relative to each other causing the first thread arrangement (35, 36) of the rod element and the second thread arrangement of the shell to travel along each other, a dosage chamber is formed by moving the rod element along the longitudinal axis of its stem, and the volume of the dosage chamber is adapted by moving the rod element along the longitudinal axis of its stem, characterized in that an inclination angle (α, β) of the thread of the first thread arrangement (35, 36) of the rod element or the second thread arrangement of the shell varies along the thread of the first thread arrangement (35, 36) of the rod element or the second thread arrangement of the shell. a rod element having a stem with a longitudinal axis and a first thread arrangement (35, 36), and a shell having a second thread arrangement, wherein, the first thread arrangement (35, 36) of the rod element or the second thread arrangement of the shell comprises a thread, the first thread arrangement (35, 36) of the rod element and the second thread arrangement of the shell engage, the rod element is movable along the longitudinal axis of its stem by rotating the shell and the rod element relative to each other causing the first thread arrangement (35, 36) of the rod element and the second thread arrangement of the shell to travel along each other, a dosage chamber is formed by moving the rod element along the longitudinal axis of its stem, and the volume of the dosage chamber is adapted by moving the rod element along the longitudinal axis of its stem, characterized in that the first thread arrangement (35, 36) of the rod element or the second thread arrangement of the shell comprises a thread, the first thread arrangement (35, 36) of the rod element and the second thread arrangement of the shell engage, the rod element is movable along the longitudinal axis of its stem by rotating the shell and the rod element relative to each other causing the first thread arrangement (35, 36) of the rod element and the second thread arrangement of the shell to travel along each other, a dosage chamber is formed by moving the rod element along the longitudinal axis of its stem, and the volume of the dosage chamber is adapted by moving the rod element along the longitudinal axis of its stem, an inclination angle (α, β) of the thread of the first thread arrangement (35, 36) of the rod element or the second thread arrangement of the shell varies along the thread of the first thread arrangement (35, 36) of the rod element or the second thread arrangement of the shell.
A method of securing a computing device, wherein the computing device is configured to store an access key in a storage location in order for the computing device to operate in an operational mode and the computing device is configured to prevent operation in the operational mode without the access key, the method comprising: the computing device retrieving the access key from an external computing device in response to provision of identification data by a user and storing the access key in the storage location; the computing device operating in said operational mode in response to receipt and storage of the access key; the computing device removing the access key from the storage location in response to an event indicative of the end of the operational mode, wherein removing the access key from the storage location comprises deleting the access key, and characterised in that: removing the access key from the storage location further comprises storing the access key on a further computing device in data communication with the first computing device. the computing device retrieving the access key from an external computing device in response to provision of identification data by a user and storing the access key in the storage location; the computing device operating in said operational mode in response to receipt and storage of the access key; the computing device removing the access key from the storage location in response to an event indicative of the end of the operational mode, wherein removing the access key from the storage location comprises deleting the access key, and characterised in that: removing the access key from the storage location further comprises storing the access key on a further computing device in data communication with the first computing device.
Apparatus for forming plastic preforms into plastic containers, having a transport device which transports the plastic preforms along a predetermined transport path, wherein the transport device having a rotatable transport carrier on which a plurality of forming stations for forming the plastic preforms into the plastic containers is arranged, wherein the forming stations each have application devices, in order to pressurize the plastic preforms with a flowable and in particular gaseous medium, and wherein the apparatus has at least one rotatable annular channel coupled to the rotational movement of the transport carrier for storing the flowable and in particular gaseous medium, and this annular channel is in flow connection with the individual forming stations via connecting lines, characterized in that the annular channel extends in a predetermined plane and in particular a horizontal plane and a plurality of connections are provided on the annular channel for arranging the connecting lines and at least one of these connections extends from the annular channel in a direction which extends at an angle a of at least 20° relative to the plane of the annular channel.
A dry gas sealing system for a turbo machine, in particular for a turbo compressor, having at least one dry gas seal for sealing a rotor-side component against a stator-side component of the the turbo machine, having a shaft of a turbo machine, and having a cleaning device for cleaning process gas removed from the turbo machine, which after the cleaning is suppliable to the or each dry gas seal as cleaned sealing gas, characterized in that the cleaning device is embodied as centrifugal device that is integrated in the rotor-side component of the turbo machine, wherein the centrifugal device is integrated in the shaft and the shaft has at least one radial inlet bore for the process gas and for each dry gas seal has at least one radial outlet bore for the sealing gas.
An assembly of molding materials, each of which comprising: a carbon fiber bundle containing an impregnation aid; and a thermoplastic resin covering the carbon fiber bundle, wherein each molding material has a core-sheath structure in which the carbon fiber bundle is covered with the thermoplastic resin; characterized in that 30% or more of the molding materials in the assembly satisfy 100 ≤ F/L < 10000, wherein F/L is in units of N/m, wherein L represents a length of each molding material in an axial direction of the carbon fiber bundle, and F represents a grip force of the carbon fiber bundle to the molding material, wherein F is measured by: randomly taking 100 molding materials out from the assembly of molding materials; using a force gauge equipped with a pin having φ0.8 mm at the tip thereof, pushing the pin into the carbon fiber bundle of the core portion of the molding material; and measuring the maximum load when the carbon fibers fall off; wherein each of the molding materials satisfies the following Formula when the molding material cut in an axial center direction thereof is observed: 0.4 ≤ area of carbon single fiber × number of single fibers in carbon fiber bundle / area surrounded by inner periphery of thermoplastic resin; wherein, the area surrounded by the inner periphery of the thermoplastic resin is an average value of the molding materials in the assembly. a carbon fiber bundle containing an impregnation aid; and a thermoplastic resin covering the carbon fiber bundle, wherein each molding material has a core-sheath structure in which the carbon fiber bundle is covered with the thermoplastic resin; characterized in that 30% or more of the molding materials in the assembly satisfy 100 ≤ F/L < 10000, wherein F/L is in units of N/m, wherein L represents a length of each molding material in an axial direction of the carbon fiber bundle, and F represents a grip force of the carbon fiber bundle to the molding material, wherein F is measured by: randomly taking 100 molding materials out from the assembly of molding materials; using a force gauge equipped with a pin having φ0.8 mm at the tip thereof, pushing the pin into the carbon fiber bundle of the core portion of the molding material; and measuring the maximum load when the carbon fibers fall off; randomly taking 100 molding materials out from the assembly of molding materials; using a force gauge equipped with a pin having φ0.8 mm at the tip thereof, pushing the pin into the carbon fiber bundle of the core portion of the molding material; and measuring the maximum load when the carbon fibers fall off; wherein each of the molding materials satisfies the following Formula when the molding material cut in an axial center direction thereof is observed: 0.4 ≤ area of carbon single fiber × number of single fibers in carbon fiber bundle / area surrounded by inner periphery of thermoplastic resin;
A holographic imaging system comprising: an antenna having a transmission line coupled thereto, said transmission line coupled to the antenna at one end and coupled to a signal source at another end, said antenna defining an aperture through which a signal generated by the signal source is transmitted incident to an object located remotely from the aperture and through which a signal reflected from the object is received by the antenna aperture; a standing wave probe located at a distance from the antenna aperture, wherein the distance of the standing wave probe from the antenna aperture is a fraction of a wavelength of the signal generated by the signal source such that the standing wave probe is phase-referenced to the antenna aperture for sampling the reflected signal; a detector connected to the standing wave probe and configured to receive the sampled reflected signal, the detector providing an output signal that represents a real-valued signal proportional to an in-phase component of the reflected signal from the object and determining a reflection coefficient from the remote object measured at the aperture of the antenna; and a processor configured to execute an imaging algorithm for generating a multi-dimensional profile representative of the object based on the output signal from the detector. an antenna having a transmission line coupled thereto, said transmission line coupled to the antenna at one end and coupled to a signal source at another end, said antenna defining an aperture through which a signal generated by the signal source is transmitted incident to an object located remotely from the aperture and through which a signal reflected from the object is received by the antenna aperture; a standing wave probe located at a distance from the antenna aperture, wherein the distance of the standing wave probe from the antenna aperture is a fraction of a wavelength of the signal generated by the signal source such that the standing wave probe is phase-referenced to the antenna aperture for sampling the reflected signal; a detector connected to the standing wave probe and configured to receive the sampled reflected signal, the detector providing an output signal that represents a real-valued signal proportional to an in-phase component of the reflected signal from the object and determining a reflection coefficient from the remote object measured at the aperture of the antenna; and a processor configured to execute an imaging algorithm for generating a multi-dimensional profile representative of the object based on the output signal from the detector.
A method for determination of a payload parameter of a device under test, wherein the payload parameter to be determined is dependent from a frequency band or is dependent from a noise temperature, comprising the steps of: a) conducting a plurality of near field payload measurements of the device under test; b) determining a respective near-field correction factor (v) for each measurement of the payload parameter; c) determining the payload parameter for the frequency band or the noise temperature by calculating it from the measured plurality of payload parameters and the respective near-field correction factors (v). a) conducting a plurality of near field payload measurements of the device under test; b) determining a respective near-field correction factor (v) for each measurement of the payload parameter; c) determining the payload parameter for the frequency band or the noise temperature by calculating it from the measured plurality of payload parameters and the respective near-field correction factors (v).
A delivery control system for a radiotherapy apparatus, arranged to transmit a treatment plan for delivering a dose distribution to delivery elements of the radiotherapy apparatus, the delivery control system comprising a processor, at least one data store, and a program stored in the data store, the program being adapted to cause the processor to: i. receive the treatment plan ii. receive inertial characteristics of the delivery elements iii. perform a process on the treatment plan in order to produce a delivery plan which corresponds to the treatment plan in the light of the inertial characteristics and which matches the acceleration and deceleration phases of all the delivery elements so that the delivery elements are adjusted in synchrony iv. transmit at least part of the delivery plan to the delivery elements. the program being adapted to cause the processor to: i. receive the treatment plan ii. receive inertial characteristics of the delivery elements iii. perform a process on the treatment plan in order to produce a delivery plan which corresponds to the treatment plan in the light of the inertial characteristics and which matches the acceleration and deceleration phases of all the delivery elements so that the delivery elements are adjusted in synchrony iv. transmit at least part of the delivery plan to the delivery elements. i. receive the treatment plan ii. receive inertial characteristics of the delivery elements iii. perform a process on the treatment plan in order to produce a delivery plan which corresponds to the treatment plan in the light of the inertial characteristics and which matches the acceleration and deceleration phases of all the delivery elements so that the delivery elements are adjusted in synchrony iv. transmit at least part of the delivery plan to the delivery elements.
A spinal stabilization system, comprising: first and second anchor members (12, 14, 10) configured to be secured to first and second vertebrae (18, 20, 22), respectively, within a patient's body; a flexible element (140, 190, 214) secured to the first anchor member and having an end portion (144, 192, 212); a rigid element (142, 172, 218) secured to the second anchor member and having an end portion (150, 174, 220) including an axial bore (158, 178, 216) extending therein and an outer surface (152, 180, 226) surrounding the axial bore, wherein the end portion of the flexible element is received in the axial bore; characterized in that an opening (160, 162, 182, 184, 224) on the outer surface extends into the axial bore and in that the system further comprises a fastener (164, 166, 186, 188, 210) secured in the opening and extending into the axial bore to retain the flexible element therein.