mhurhangee/patent-ind-claim-en huggingface dataset:
A closed intubation system comprising at least an endotracheal tube suitable for insertion into the trachea of a patient, a tubular connection to a breathing device and an adapter arrangement with at least three cylindrically designed receptacles for establishing a gas-tight coupling between the endotracheal tube , the connection of the breathing device and at least one further receptacle , wherein the adapter arrangement comprises at least: a) an adapter base body with at least one shut-off device , which is configured in a T-shape via the arrangement of the receptacles , the shut-off device being designed to open or close the airway between the further receptacle and the two receptacles for the breathing device and the endotracheal tube in a gas-tight manner, b) an adapter attachment that can be coupled to the further receptacle , wherein the adapter attachment can be connected in a gas-tight manner to the adapter base body via a seal and is designed to be mechanically fixed to the latter by holding means; c) an elastic, tubular sheath that is arranged in a gas-tight manner at one end on the adapter attachment ; d) an attachment connected in a gas-tight manner to the other end of the elastic, tubular sheath , characterised in that the attachment comprises a passage to the tubular sheath with a sealing device arranged therein, wherein the sealing device is configured to receive cylindrically configured devices and to guide them in a displaceable and gas-tight manner through the attachment , the tubular sheath , the adapter attachment , the adapter base body and the endotracheal tube . a) an adapter base body with at least one shut-off device , which is configured in a T-shape via the arrangement of the receptacles , the shut-off device being designed to open or close the airway between the further receptacle and the two receptacles for the breathing device and the endotracheal tube in a gas-tight manner, b) an adapter attachment that can be coupled to the further receptacle , wherein the adapter attachment can be connected in a gas-tight manner to the adapter base body via a seal and is designed to be mechanically fixed to the latter by holding means; c) an elastic, tubular sheath that is arranged in a gas-tight manner at one end on the adapter attachment ; d) an attachment connected in a gas-tight manner to the other end of the elastic, tubular sheath , characterised in that the attachment comprises a passage to the tubular sheath with a sealing device arranged therein, wherein the sealing device is configured to receive cylindrically configured devices and to guide them in a displaceable and gas-tight manner through the attachment , the tubular sheath , the adapter attachment , the adapter base body and the endotracheal tube .
A wireless device comprising: a transmitter including a plurality of antennas; and a communication processor configured to calculate a total exposure ratio (TER) value of each of the plurality of antennas, wherein the communication processor includes: an antenna index buffer configured to store a used antenna index, which is an index of one or more used antennas from among the plurality of antennas used in each window of a plurality of windows in a TER measurement interval; a used power buffer configured to store used power of an antenna corresponding to the used antenna index; and a controller configured to calculate the TER value based on the used antenna index, the used power, and an influence matrix, wherein the influence matrix includes a plurality of influence coefficients R (i, j), each of which represents a degree of influence of exposure caused by a radio frequency (RF) signal transmission of an ith antenna on a jth antenna, and wherein i and j are integer numbers equal to a number of the plurality of antennas. a transmitter including a plurality of antennas; and a communication processor configured to calculate a total exposure ratio (TER) value of each of the plurality of antennas, wherein the communication processor includes: an antenna index buffer configured to store a used antenna index, which is an index of one or more used antennas from among the plurality of antennas used in each window of a plurality of windows in a TER measurement interval; a used power buffer configured to store used power of an antenna corresponding to the used antenna index; and a controller configured to calculate the TER value based on the used antenna index, the used power, and an influence matrix, wherein the influence matrix includes a plurality of influence coefficients R (i, j), each of which represents a degree of influence of exposure caused by a radio frequency (RF) signal transmission of an ith antenna on a jth antenna, and wherein i and j are integer numbers equal to a number of the plurality of antennas. an antenna index buffer configured to store a used antenna index, which is an index of one or more used antennas from among the plurality of antennas used in each window of a plurality of windows in a TER measurement interval; a used power buffer configured to store used power of an antenna corresponding to the used antenna index; and a controller configured to calculate the TER value based on the used antenna index, the used power, and an influence matrix, wherein the influence matrix includes a plurality of influence coefficients R (i, j), each of which represents a degree of influence of exposure caused by a radio frequency (RF) signal transmission of an ith antenna on a jth antenna, and wherein i and j are integer numbers equal to a number of the plurality of antennas.
Transparent support for a semi-conducting thin layer structure with a superstrate with an upper side intended for incidence of light and an underside on which is arranged a light trapping structure which improves the optical properties of the superstrate and to which the thin layer structure is connectable, wherein the light trapping structure comprises at least one three-dimensional structural layer in the sub-micrometre range made of silicon oxide on the superstrate , characterised in that the three-dimensional structural layer is designed with a periodic nanostructure with a period P between 200 nm and 1000 mm and a first anti-reflection layer following the structural layer designed as a nanocrystalline titanium oxide layer or as a tin oxide layer, wherein the first anti-reflection layer reduces the relative height HN of the nanostructure of the structure layer by at least 30% so that the residual height HL of the light trapping structure is levelled and wherein the height HL of the light trapping structure is between 20 nm and 200 nm and the angles W between the surfaces of the light trapping structure and the underside of the superstrate are no greater than 60°, and in that a passivisation layer is arranged on the light trapping structure , ensuring temperature stability of the support for liquid phase crystallisation.
A method for manufacturing a scintillator, the method comprises the steps of: - providing (S1) a basic scintillator structure in the form of a silicon (Si) substrate having micromechanical features formed in the substrate, said basic scintillator structure having a front and a back , wherein the step (S1) of providing a basic scintillator structure further comprises filling (S12) said micromechanical features with scintillating material; - applying (S2) a reflector on the front of the basic scintillator structure ; said method being characterized in the steps of - opening (S3) the back of said basic scintillator structure to create a scintillator having open ended micromechanical features formed in the substrate and filled with scintillating material, wherein the reflector is applied on the front side of the basic scintillator structure , where openings of the micromechanical features are initially located, to close the openings, and then the back side of the basic scintillator structure is opened to provide the open-ended micromechanical features . - providing (S1) a basic scintillator structure in the form of a silicon (Si) substrate having micromechanical features formed in the substrate, said basic scintillator structure having a front and a back , wherein the step (S1) of providing a basic scintillator structure further comprises filling (S12) said micromechanical features with scintillating material; - applying (S2) a reflector on the front of the basic scintillator structure ; said method being characterized in the steps of - opening (S3) the back of said basic scintillator structure to create a scintillator having open ended micromechanical features formed in the substrate and filled with scintillating material,
Headrest having a head support part that can be mounted on a structure of a vehicle, in particular on a vehicle seat, by means of a fixing device , wherein the head support part can be moved forwards towards the head of a user and back in the opposite direction relative to the fixing device by means of a displacement device , wherein the displacement device comprises at least one first control link and one second control link , wherein each control link forms at least one joint with a head support device comprising the head support part and with the fixing device , and wherein a relative movement between the fixing device and the head support part can be releasably blocked by means of a locking device , wherein the locking device has first locking means that are formed on at least one control link and second locking means that are assigned to the head support part or the fixing device , wherein the first locking means and the second locking means are releasably engageable, characterised in that the first control link and the second control link respectively have two arms that are arranged in parallel with each other in the displacement direction (x1, x2), and in that a spacing is formed between the parallel arms.
A system that facilitates secure scanning of a computer, comprising: a processor coupled to a memory , the processor configured to execute the following computer executable components stored in the memory: a data acquisition component configured to receive state data of a target computer; a virtualization component configured to generate a virtual replica of the target computer from the state data on a second computer isolated from the target computer; and an interface component configured to intercept a request by a computer scanner for the state data from the target computer, to retrieve the state data that satisfies the request from the virtual replica of the target computer and to provide the retrieved state data to the computer scanner in response to the request. a data acquisition component configured to receive state data of a target computer; a virtualization component configured to generate a virtual replica of the target computer from the state data on a second computer isolated from the target computer; and an interface component configured to intercept a request by a computer scanner for the state data from the target computer, to retrieve the state data that satisfies the request from the virtual replica of the target computer and to provide the retrieved state data to the computer scanner in response to the request.
An engine system for an aircraft , the engine system comprising: a first gas turbine engine ; a second gas turbine engine ; a control system configured to: operate the first gas turbine engine with an idle fuel burn schedule in a taxi mode of the aircraft; operate the second gas turbine engine with a sub-idle fuel burn schedule in the taxi mode of the aircraft, the sub-idle fuel burn schedule comprising a reduction of the idle fuel burn schedule; and increase a fuel flow of the first gas turbine engine and the second gas turbine engine above the idle fuel burn schedule prior to takeoff of the aircraft; characterized in that : the control system is further configured to alternate a designation of the first gas turbine engine and the second gas turbine engine between two or more gas turbine engines of the aircraft . a first gas turbine engine ; a second gas turbine engine ; a control system configured to: operate the first gas turbine engine with an idle fuel burn schedule in a taxi mode of the aircraft; operate the second gas turbine engine with a sub-idle fuel burn schedule in the taxi mode of the aircraft, the sub-idle fuel burn schedule comprising a reduction of the idle fuel burn schedule; and increase a fuel flow of the first gas turbine engine and the second gas turbine engine above the idle fuel burn schedule prior to takeoff of the aircraft; operate the first gas turbine engine with an idle fuel burn schedule in a taxi mode of the aircraft; operate the second gas turbine engine with a sub-idle fuel burn schedule in the taxi mode of the aircraft, the sub-idle fuel burn schedule comprising a reduction of the idle fuel burn schedule; and increase a fuel flow of the first gas turbine engine and the second gas turbine engine above the idle fuel burn schedule prior to takeoff of the aircraft; characterized in that : the control system is further configured to alternate a designation of the first gas turbine engine and the second gas turbine engine between two or more gas turbine engines of the aircraft .
Support part and sewn covering (30, 30.2, 30.3, 30.4, 30.5) for laminating the support part , wherein the sewn covering (30, 30.2, 30.3, 30.4 30.5) has at least one first and at least one second cover element which are interconnected by way of a functional seam , so that on the underside of the sewn covering (30, 30.2, 30.3, 30.4, 30.5) a seam stump is formed, wherein in the case of the sewn covering (30, 30.2, 30.3, 30.4, 30.5) at least in portions at least one soft insert (14, 14.3, 20, 22, 70) is present which runs along the functional seam and is sewn into the functional seam ; wherein the support part has a seam trench , characterized in that the maximum width of the seam stump enveloped by the soft insert (14, 14.3, 20, 22, 70) is larger than the width of the seam trench of the support part . wherein the support part has a seam trench , characterized in that the maximum width of the seam stump enveloped by the soft insert (14, 14.3, 20, 22, 70) is larger than the width of the seam trench of the support part .
A system comprising: a cannula comprising a side wall defining a lumen (138; 187), an opening in fluid communication with the lumen (138; 187) and extending through the side wall and a tapered distal tip (134; 190) of the cannula to define a trough having a depth, a curved distal portion , and a distal opening surface (142; 188A, 188B, 192A, 192B) surrounding the opening , the tapered distal tip (134; 190) of the cannula being shaped and configured to stretch Schlemm's canal tissues over a portion of the trough as the tapered distal tip (134; 190) is advanced into Schlemm's canal; an ocular implant disposed inside the cannula lumen (138; 187); and a delivery tool coupled to the ocular implant within the lumen (138; 187) and adapted to move the implant distally into the trough and through the cannula opening into Schlemm's canal of a patient's eye when the cannula opening is in fluid communication with Schlemm's canal; characterized in that the ocular implant has a height less than the depth of the trough so that a distal end of the ocular implant can travel between an inner surface of the trough and the Schlemm's canal tissue stretched over the trough after the tapered distal tip (134; 190) of the cannula is inserted into Schlemm's canal. a cannula comprising a side wall defining a lumen (138; 187), an opening in fluid communication with the lumen (138; 187) and extending through the side wall and a tapered distal tip (134; 190) of the cannula to define a trough having a depth, a curved distal portion , and a distal opening surface (142; 188A, 188B, 192A, 192B) surrounding the opening , the tapered distal tip (134; 190) of the cannula being shaped and configured to stretch Schlemm's canal tissues over a portion of the trough as the tapered distal tip (134; 190) is advanced into Schlemm's canal; an ocular implant disposed inside the cannula lumen (138; 187); and a delivery tool coupled to the ocular implant within the lumen (138; 187) and adapted to move the implant distally into the trough and through the cannula opening into Schlemm's canal of a patient's eye when the cannula opening is in fluid communication with Schlemm's canal; characterized in that the ocular implant has a height less than the depth of the trough so that a distal end of the ocular implant can travel between an inner surface of the trough and the Schlemm's canal tissue stretched over the trough after the tapered distal tip (134; 190) of the cannula is inserted into Schlemm's canal.
Cutting tool for machining a bore in a workpiece, in particular for simultaneously machining a plurality of bores spaced apart from one another by a pre-determined distance, comprising a cutting body extending in the direction of a tool longitudinal axis having at least one cutting element arranged circumferentially and a guide body attached to the cutting body , which is free of cutting elements , wherein the guide body comprises a body longitudinal axis , which is arranged offset from the tool longitudinal axis during use, wherein the guide body can radially move by means of an adjustment mechanism relative to the tool longitudinal axis , wherein the guide body adjoins the cutting body in the direction of the tool longitudinal axis , characterized in that the guide body comprises two guide elements which are arranged on the circumferential side at two angular positions , wherein the guide body is configured to exert a preload force such that, when used, the two guide elements are loaded against a bearing for the guide body , wherein the two angular positions are associated with an angular bisector and the preload force extends in the direction of the angular bisector .
A dental device for removing a dental implant which is at least partially or fully osseointegrated with a patient's jaw , comprising: a head portion for rotatingly holding a dental tool for unscrewing the dental implant ; and a driving means for applying a torque to the dental tool for unscrewing the dental implant ; characterized in that the driving means is specifically adapted to apply pulsed torques ( τ; τ 1 , τ 2 , τ 3 ) to the dental tool to unscrew the dental implant . a head portion for rotatingly holding a dental tool for unscrewing the dental implant ; and a driving means for applying a torque to the dental tool for unscrewing the dental implant ; characterized in that the driving means is specifically adapted to apply pulsed torques ( τ; τ 1 , τ 2 , τ 3 ) to the dental tool to unscrew the dental implant .
Method for the self-diagnosis of an ultrasonic sensor for a vehicle assistance system, wherein the ultrasonic sensor is configured to capture the environment around a motor vehicle, wherein an acceleration of a diaphragm of the ultrasonic sensor is measured using an acceleration sensor and a variable which can be compared with a corresponding reference value is determined from acceleration, wherein the acceleration sensor is arranged on a sensor element of the ultrasonic sensor , and wherein the sensor element is a piezo element.
A laser assisted eye treatment system for carrying out an eye treatment workflow, comprising: - a laser treatment unit with a laser source generating a pulsed laser beam, - a characterization unit , - a system controller , configured to control the laser assisted eye treatment system , - a first control panel arranged to display a first graphical user interface provided by the system controller and configured to communicate information required for the eye treatment workflow, - a second control panel arranged to display a second graphical user interface provided by the system controller and - wherein the second control panel is configured to communicate a subset of information, being a restricted selection of information, directly available to a surgeon and used during the laser treatment by the surgeon, out of an entire set of information required for the eye treatment workflow. - a laser treatment unit with a laser source generating a pulsed laser beam, - a characterization unit , - a system controller , configured to control the laser assisted eye treatment system , - a first control panel arranged to display a first graphical user interface provided by the system controller and configured to communicate information required for the eye treatment workflow, - a second control panel arranged to display a second graphical user interface provided by the system controller and - wherein the second control panel is configured to communicate a subset of information, being a restricted selection of information, directly available to a surgeon and used during the laser treatment by the surgeon, out of an entire set of information required for the eye treatment workflow.
Filter system , comprising - a housing with housing wall and at least one cover , - an inlet port disposed on the housing for supplying a fluid to be filtered, in particular air, - an outlet port disposed on the housing for discharging the filtered fluid, - a support tube disposed inside the housing for accommodating a filter element, wherein the support tube extends along a housing axis (L) and is connected to the housing via a latching connection on a receiving side so as to be angularly mountable only in one angular direction relative to the housing axis, wherein the latching connection is formed from corresponding latching elements on the housing and on the support tube , and the latching elements are designed in such a way that corresponding latching elements can only be latched to one another in a fixed manner. - a housing with housing wall and at least one cover , - an inlet port disposed on the housing for supplying a fluid to be filtered, in particular air, - an outlet port disposed on the housing for discharging the filtered fluid, - a support tube disposed inside the housing for accommodating a filter element, wherein the support tube extends along a housing axis (L) and is connected to the housing via a latching connection on a receiving side so as to be angularly mountable only in one angular direction relative to the housing axis, wherein the latching connection is formed from corresponding latching elements on the housing and on the support tube , and the latching elements are designed in such a way that corresponding latching elements can only be latched to one another in a fixed manner.