mhurhangee/patent-ind-claim-en huggingface dataset:
A landing gear lifting/lowering Electro Hydrostatic Actuator (EHA) system , comprising: a hydraulic actuator configured to be attached to a leg of an aircraft and configured to lift and lower the leg; at least one electrically operated hydraulic pump , comprising at least one hydraulic pump driven by an electric motor , configured to supply a hydraulic fluid to the hydraulic actuator at a time of lifting or lowering the leg; a hydraulic path connecting the hydraulic actuator and the electrically operated hydraulic pump ; a pressure sensor attached to the hydraulic actuator or the hydraulic path and configured to output a measurement signal corresponding to a hydraulic pressure; and a sensor configured to output a measurement signal corresponding to a revolution speed of the at least one hydraulic pump and/or the electric motor , and; a control unit configured to receive the measurement signals and characterized in that it is further configured to output to the electrically operated hydraulic pump , a control signal based on the hydraulic pressure and the revolution speed, wherein, when a state in which the revolution speed of the electrically operated hydraulic pump is not more than a set revolution speed and the hydraulic pressure exceeds a set pressure continues for a set time while the leg is being lifted, the control unit stops the electrically operated hydraulic pump in operation and resumes the operation of the electrically operated hydraulic pump after the hydraulic pressure drops to or below a second set pressure after the electrically operated hydraulic pump is stopped. a hydraulic actuator configured to be attached to a leg of an aircraft and configured to lift and lower the leg; at least one electrically operated hydraulic pump , comprising at least one hydraulic pump driven by an electric motor , configured to supply a hydraulic fluid to the hydraulic actuator at a time of lifting or lowering the leg; a hydraulic path connecting the hydraulic actuator and the electrically operated hydraulic pump ; a pressure sensor attached to the hydraulic actuator or the hydraulic path and configured to output a measurement signal corresponding to a hydraulic pressure; and a sensor configured to output a measurement signal corresponding to a revolution speed of the at least one hydraulic pump and/or the electric motor , and; a control unit configured to receive the measurement signals and characterized in that it is further configured to output to the electrically operated hydraulic pump , a control signal based on the hydraulic pressure and the revolution speed, wherein, when a state in which the revolution speed of the electrically operated hydraulic pump is not more than a set revolution speed and the hydraulic pressure exceeds a set pressure continues for a set time while the leg is being lifted, the control unit stops the electrically operated hydraulic pump in operation and resumes the operation of the electrically operated hydraulic pump after the hydraulic pressure drops to or below a second set pressure after the electrically operated hydraulic pump is stopped.
A method for regulating at least one fluidic parameter P i, actual to a predetermined target value P i, target by at least one motor parameter M i of a ventilator in a system, wherein the ventilator is operated with the at least one motor parameter M i regulated to a constant value, wherein first, actual values of the at least one motor parameter M i are acquired and actual values of the at least one fluidic parameter P i,actual are determined, and a comparison of the actual values and the target value P i,tagert values of the at least one fluidic parameter P i,actual is carried out, wherein, in the case of a deviation of the actual-target comparison of the at least one fluidic parameter P i,actual , an adjustment of the rotational speed occurs, in order to reach the predetermined target value, characterized in that , for the case in which the at least one fluidic parameter P i,actual does not exceed the inflection operating point, the constant value of the at least one motor parameter M i is changed via a rotational speed change so that the actual value of at least one fluidic parameter P i,actual is regulated to its target value P i, target , without a change of the at least one motor parameter M i occurring.
A brewing unit for the preparation of a beverage, comprising a support structure which is stationary in operation and in which a brewing zone is defined where a hydraulically operated piercing and liquid-supplying device is mounted movable between a retracted rest position and an extracted working position, and an associated movable drawer which forms a receptacle adapted to receive a capsule (C) containing a substance for the preparation of a beverage and is insertable into and extractable from said support structure to place a capsule (C) in the brewing zone with a top wall of the capsule (C) facing said piercing and liquid-supplying device and to allow an exhausted capsule (C) to be ejected after the beverage has been dispensed and a new capsule (C) has been loaded; wherein the piercing and liquid-supplying device comprises a plurality of points for piercing said top wall of a capsule (C) placed in the brewing zone and a conduit for supplying a flow of pressurized liquid to a brewing chamber adjacent and above the top wall of the capsule (C) and thereafter inside the capsule (C) through holes pierced by the points in the top wall of the capsule (C); wherein the brewing unit is configured in such a manner that when the drawer is inserted into the support structure with a capsule (C) positioned in the receptacle , the top wall of the capsule (C) lies essentially in a plane inclined to the horizontal plane, and wherein in the drawer there is defined a discharge channel adapted to be put into fluid communication with the region above the top wall of the capsule (C) when, after the beverage has been prepared and dispensed, the piercing and liquid-supplying device moves from the extracted work position to the retracted rest position, to allow pouring of the remaining liquid from said region to the discharge channel , characterized in that the discharge channel of the drawer has an outlet passage which, when the drawer is inserted in the work position into the support structure , is adapted to be put into fluid communication with a discharge conduit arranged in said support structure by the return of the piercing and liquid-supplying device to the retracted rest position.
A headrest comprising: a plurality of speakers ; fiber pads provided to the front surfaces of each of the speakers ; a median sound-insulating pad provided between the fiber pads; outside sound-insulating pads provided on the outer sides of the fiber pads ; and a surface skin for covering the speakers, the fiber pads , and the sound-insulating pads , wherein: the fiber pads are formed from an elastic material that has a three-dimensional-mesh structure therein; the sound-insulating pads are formed from an elastic material for minimizing the transmission of sound; the fiber pads are filled into spaces formed by the median sound-insulating pad and the outside sound-insulating pads ; and the spaces formed by the median sound-insulating pad and the outside sound-insulating pads have shapes extending laterally in a direction from a location near the plurality of speakers toward a location away from the plurality of speakers. a plurality of speakers ; fiber pads provided to the front surfaces of each of the speakers ; a median sound-insulating pad provided between the fiber pads; outside sound-insulating pads provided on the outer sides of the fiber pads ; and a surface skin for covering the speakers, the fiber pads , and the sound-insulating pads , wherein: the fiber pads are formed from an elastic material that has a three-dimensional-mesh structure therein; the sound-insulating pads are formed from an elastic material for minimizing the transmission of sound; the fiber pads are filled into spaces formed by the median sound-insulating pad and the outside sound-insulating pads ; and the spaces formed by the median sound-insulating pad and the outside sound-insulating pads have shapes extending laterally in a direction from a location near the plurality of speakers toward a location away from the plurality of speakers. the fiber pads are formed from an elastic material that has a three-dimensional-mesh structure therein; the sound-insulating pads are formed from an elastic material for minimizing the transmission of sound; the fiber pads are filled into spaces formed by the median sound-insulating pad and the outside sound-insulating pads ; and the spaces formed by the median sound-insulating pad and the outside sound-insulating pads have shapes extending laterally in a direction from a location near the plurality of speakers toward a location away from the plurality of speakers.
A composition comprising at least about 98 wt% C 7 -C 12 n-paraffins, wherein at least about 10 wt% of composition comprises n-decane, at least about 20 wt% of the composition comprises n-dodecane, and at least about 75 wt% of the composition comprises even carbon number paraffins, and the composition comprises a weight ratio of C 12 paraffins to C 11 paraffins from 3.0:1 to 1.2:1; less than about 0.1 wt% oxygenates; and less than about 0.1 wt % aromatics; wherein the composition is suitable as a diesel fuel, a turbine fuel, an aviation fuel, a charcoal lighter fluid, or a combination of any two or more thereof. at least about 98 wt% C 7 -C 12 n-paraffins, wherein at least about 10 wt% of composition comprises n-decane, at least about 20 wt% of the composition comprises n-dodecane, and at least about 75 wt% of the composition comprises even carbon number paraffins, and the composition comprises a weight ratio of C 12 paraffins to C 11 paraffins from 3.0:1 to 1.2:1; less than about 0.1 wt% oxygenates; and less than about 0.1 wt % aromatics; wherein the composition is suitable as a diesel fuel, a turbine fuel, an aviation fuel, a charcoal lighter fluid, or a combination of any two or more thereof.
A computer-implemented method of presenting user-specific advertising material in a virtual environment , comprising: presenting, by a presenting module, a virtual environment to a user, wherein the user has a presence in the virtual environment as an avatar ; embedding, by an advertising module, an object in said virtual environment , the object is communicatively connected to a server, wherein the object is capable of presenting the user-specific advertising material when one or more digital trigger is activated; determining, by the advertising module, if there is a digital trigger activated in the virtual environment ; presenting, by the presenting module, at least one advertising material via the object based on the digital trigger, wherein said advertising material is visible to or heard by the user when said digital trigger is activated; identifying, by the presenting module, a percentage of at least one original ad of the advertising material that is visible as on-screen ads within a field of view of the user when the visible advertising material is presented to the user via the object , wherein identifying the percentage comprises performing a pixel sampling operation on the advertising material rendered from the virtual environment ; and tracking and recording, by the advertising module, one or more interactions of the user with at least one of the displayed object and the displayed advertising material . presenting, by a presenting module, a virtual environment to a user, wherein the user has a presence in the virtual environment as an avatar ; embedding, by an advertising module, an object in said virtual environment , the object is communicatively connected to a server, wherein the object is capable of presenting the user-specific advertising material when one or more digital trigger is activated; determining, by the advertising module, if there is a digital trigger activated in the virtual environment ; presenting, by the presenting module, at least one advertising material via the object based on the digital trigger, wherein said advertising material is visible to or heard by the user when said digital trigger is activated; identifying, by the presenting module, a percentage of at least one original ad of the advertising material that is visible as on-screen ads within a field of view of the user when the visible advertising material is presented to the user via the object , wherein identifying the percentage comprises performing a pixel sampling operation on the advertising material rendered from the virtual environment ; and tracking and recording, by the advertising module, one or more interactions of the user with at least one of the displayed object and the displayed advertising material .
A turning control device comprising: a command value calculation unit configured to calculate, based on an operation acting on a steering operation unit of a vehicle, a current command value for an actuator providing a turning mechanism with steering assist force; a position detection unit configured to detect a steered position of the turning mechanism; a terminal position learning unit configured to learn a terminal position of the turning mechanism, based on the steered position detected by the position detection unit ; a command value correction unit configured to, when a steered position detected by the position detection unit is in a vicinity of the terminal position learned by the terminal position learning unit , correct the current command value calculated by the command value calculation unit ; characterized by a correction amount limiting unit configured to limit a correction amount of the current command value by the command value correction unit , based on a comparison result between the learned terminal position and a predetermined position and a comparison result between stroke length of the turning mechanism calculated from the learned terminal positions and a predetermined length. a command value calculation unit configured to calculate, based on an operation acting on a steering operation unit of a vehicle, a current command value for an actuator providing a turning mechanism with steering assist force; a position detection unit configured to detect a steered position of the turning mechanism; a terminal position learning unit configured to learn a terminal position of the turning mechanism, based on the steered position detected by the position detection unit ; a command value correction unit configured to, when a steered position detected by the position detection unit is in a vicinity of the terminal position learned by the terminal position learning unit , correct the current command value calculated by the command value calculation unit ; characterized by a correction amount limiting unit configured to limit a correction amount of the current command value by the command value correction unit , based on a comparison result between the learned terminal position and a predetermined position and a comparison result between stroke length of the turning mechanism calculated from the learned terminal positions and a predetermined length.
Device for capping a bottle of substantially cylindrical internally hollow shape, comprising • an upper portion , which forms a tank therein for a first substance to be mixed with a second substance present in the bottle, • a lower portion provided with means for securing to the bottle, • the base of the tank having a film welded on an edge located in the vicinity of the junction of the upper portion with the lower portion, • means for breaking the base of the tank that can be operated by pressure and manually from the top of said device comprising a piston able to slide downwardly inside the hollow upper portion provided with at least one fracture tip on its lower end, which during the descent of the piston pierces the aforementioned film releasing the contents of the tank into the bottle, • the top of the piston comprises a membrane that can be pierced by a syringe needle that when the piston itself has pierced the tank itself allows such needle to take the contents of the mixture in the bottle, characterised in that said membrane is of a discoid shape and is recessed in a seat obtained on the top of the piston so as not to protrude with respect to a circular crown which delimits such seat, wherein the membrane is co-moulded together with the piston or the device when the latter is made in one piece. • an upper portion , which forms a tank therein for a first substance to be mixed with a second substance present in the bottle, • a lower portion provided with means for securing to the bottle, • the base of the tank having a film welded on an edge located in the vicinity of the junction of the upper portion with the lower portion, • means for breaking the base of the tank that can be operated by pressure and manually from the top of said device comprising a piston able to slide downwardly inside the hollow upper portion provided with at least one fracture tip on its lower end, which during the descent of the piston pierces the aforementioned film releasing the contents of the tank into the bottle, • the top of the piston comprises a membrane that can be pierced by a syringe needle that when the piston itself has pierced the tank itself allows such needle to take the contents of the mixture in the bottle,
A fabric care formulation comprising: a liquid carrier; and a plurality of composite opacifier particles, wherein the composite opacifier particles comprise metal oxide particles that are partially or completely encapsulated by a wax; wherein the metal oxide particles are selected from the group consisting of zinc oxide, titanium oxide and mixtures thereof; wherein the metal oxide particles have a z average particle size of > 100 nm as measured by dynamic light scattering; wherein the wax has a melting point temperature of 45 to 110 °C; and wherein the composite opacifier particles have a z average particle size of > 100 nm to 2,000 nm as measured by dynamic light scattering. a liquid carrier; and a plurality of composite opacifier particles, wherein the composite opacifier particles comprise metal oxide particles that are partially or completely encapsulated by a wax; wherein the metal oxide particles are selected from the group consisting of zinc oxide, titanium oxide and mixtures thereof; wherein the metal oxide particles have a z average particle size of > 100 nm as measured by dynamic light scattering; wherein the wax has a melting point temperature of 45 to 110 °C; and wherein the composite opacifier particles have a z average particle size of > 100 nm to 2,000 nm as measured by dynamic light scattering.
An anti-huLRRC15 antibody drug conjugate ("ADC") comprising an antimitotic agent linked to an anti-huLRRC15 antibody by way of a linker, wherein the ADC has a structure of formula (IIIa): wherein: n is an integer ranging from 2 to 8; Ab is an anti-huLRRC15 antibody comprising a V H chain comprising the sequence of SEQ ID NO:16; and a V L chain comprising the sequence of SEQ ID NO:17. n is an integer ranging from 2 to 8; Ab is an anti-huLRRC15 antibody comprising a V H chain comprising the sequence of SEQ ID NO:16; and a V L chain comprising the sequence of SEQ ID NO:17. a V H chain comprising the sequence of SEQ ID NO:16; and a V L chain comprising the sequence of SEQ ID NO:17.
An aircraft seat frame with enhanced dynamic response, comprising: a frame beam member , the frame beam member comprising: a tubular volume including at least one wall with a first plurality of undulations and a second plurality of undulations alternatingly arranged and extending radially outward along a length of the tubular volume, the first plurality of undulations and the second plurality of undulations being configured to allow the tubular volume to absorb energy of a compressive load applied during a flight scenario through local bending of the first plurality of undulations and the second plurality of undulations, the first plurality of undulations being configured to have a first curvature when unloaded, the first plurality of undulations being configured to have a second curvature when the compressive load is applied, the second curvature being greater than the first curvature, the second plurality of undulations being configured to have a third curvature when unloaded, the first curvature being greater than the third curvature by which the first plurality of undulations are configured to deform prior to the second plurality of undulations, the frame beam member being one of a plurality of frame beam members of the aircraft seat frame, the plurality of frame beam members being configured to couple to a plurality of joints of the aircraft seat frame, at least one joint of the plurality of joints or at least one frame beam member of the plurality of frame beam members being configured to couple to an aircraft body. a tubular volume including at least one wall with a first plurality of undulations and a second plurality of undulations alternatingly arranged and extending radially outward along a length of the tubular volume, the first plurality of undulations and the second plurality of undulations being configured to allow the tubular volume to absorb energy of a compressive load applied during a flight scenario through local bending of the first plurality of undulations and the second plurality of undulations, the first plurality of undulations being configured to have a first curvature when unloaded, the first plurality of undulations being configured to have a second curvature when the compressive load is applied, the second curvature being greater than the first curvature, the second plurality of undulations being configured to have a third curvature when unloaded, the first curvature being greater than the third curvature by which the first plurality of undulations are configured to deform prior to the second plurality of undulations, the frame beam member being one of a plurality of frame beam members of the aircraft seat frame, the plurality of frame beam members being configured to couple to a plurality of joints of the aircraft seat frame, at least one joint of the plurality of joints or at least one frame beam member of the plurality of frame beam members being configured to couple to an aircraft body.