mhurhangee/patent-ind-claim-en huggingface dataset:
A system for transferring graphical representations on an object by sublimation, said system comprising: - a first loading device configured to load on a work plane a support comprising at least one graphical representation to be transferred, - a second loading device configured to load, in use, the object over said support on said work plane , - a sublimation apparatus comprising - a catenary , and - a plurality of pendulum components hooked to the catenary , each component comprising ends and jaws (10A-10B) configured to cooperate with the work plane so that, by suction, said support wraps said object , is made to adhere to said object and is moved together with the object by way of the catenary in an oven arranged for transferring the support graphical representation from the support to the object , characterized in that said work plane comprises - a plurality of pliers comprising suction type ends arranged longitudinally to the work plane and configured to wrap the object by way of the support and make the support adhere to said ends of said pendulum component . - a first loading device configured to load on a work plane a support comprising at least one graphical representation to be transferred, - a second loading device configured to load, in use, the object over said support on said work plane , - a sublimation apparatus comprising - a catenary , and - a plurality of pendulum components hooked to the catenary , each component comprising ends and jaws (10A-10B) configured to cooperate with the work plane so that, by suction, said support wraps said object , is made to adhere to said object and is moved together with the object by way of the catenary in an oven arranged for transferring the support graphical representation from the support to the object , characterized in that said work plane comprises - a catenary , and - a plurality of pendulum components hooked to the catenary , each component comprising ends and jaws (10A-10B) configured to cooperate with the work plane so that, by suction, said support wraps said object , is made to adhere to said object and is moved together with the object by way of the catenary in an oven arranged for transferring the support graphical representation from the support to the object , characterized in that said work plane comprises - a plurality of pliers comprising suction type ends arranged longitudinally to the work plane and configured to wrap the object by way of the support and make the support adhere to said ends of said pendulum component .
A turning air mattress , comprising at least one turning air cell , characterized in that the turning air cell comprising: a left air chamber and a right air chamber ; an upper portion defined by an upper side of the left air chamber and an upper side of the right air chamber ; and a lower portion defined by a lower side of the left air chamber and a lower side of the right air chamber , located on a side opposite to the upper portion , a width of the lower portion being smaller than a width of the upper portion ; wherein, the left air chamber and the right air chamber of the turning air cell are configured to be inflated and deflated correspondingly to achieve the effect of body turning. a left air chamber and a right air chamber ; an upper portion defined by an upper side of the left air chamber and an upper side of the right air chamber ; and a lower portion defined by a lower side of the left air chamber and a lower side of the right air chamber , located on a side opposite to the upper portion , a width of the lower portion being smaller than a width of the upper portion ; wherein, the left air chamber and the right air chamber of the turning air cell are configured to be inflated and deflated correspondingly to achieve the effect of body turning.
Waveguide (MS1) for radio frequency, RF, signals (RFS) having a signal frequency, comprising a composite substrate (100; 100a), a first conductor arranged on a first surface of said composite substrate (100; 100a), and a second conductor arranged on a second surface of said composite substrate (100; 100a), wherein said composite substrate (100; 100a) comprises at least three layers of dielectric material, said at least three layers of dielectric material comprising a first layer of dielectric material, a second layer of dielectric material, and at least one further layer of dielectric material, and at least two conductor layers of an electrically conductive material arranged between said first layer and said second layer , wherein the at least one further layer of dielectric material is provided between said at least two conductor layers , wherein a layer thickness (h21, h22) of said at least two conductor layers is smaller than about 120 percent of a skin depth of said RF signals (RFS) within said electrically conductive material of said conductor layers , wherein an aggregated conductor layer thickness of said at least two conductor layers is greater than about 2 percent of an aggregated layer thickness of said at least three layers of dielectric material.
A method comprising: extracting a sound originating from a premises, wherein the sound is detected by microphones of a microphone array; performing pattern matching to identify an alarm event associated with the extracted sound; determining a location of the alarm event within the premises based on information obtained individually by the microphones of the microphone array; and communicating the alarm event and the location of the alarm event to one or some of a plurality of client devices remotely located with respect to the premises, said one or some of the plurality of client devices chosen based on the location of the alarm event. extracting a sound originating from a premises, wherein the sound is detected by microphones of a microphone array; performing pattern matching to identify an alarm event associated with the extracted sound; determining a location of the alarm event within the premises based on information obtained individually by the microphones of the microphone array; and communicating the alarm event and the location of the alarm event to one or some of a plurality of client devices remotely located with respect to the premises, said one or some of the plurality of client devices chosen based on the location of the alarm event.
A composite graphite material, comprising a bulk particle and a cladding layer located on at least a partial surface of the bulk particle, wherein the bulk particle is a secondary particle formed by aggregation of more than two primary particles , the bulk particle comprises artificial graphite, and the cladding layer comprises amorphous carbon, wherein, an air oxidation temperature T 0 of the composite graphite material is from 630°C to 730°C, and is optionally from 660°C to 710°C, and the air oxidation temperature T 0 is a temperature corresponding to an intersection of two tangents at two points corresponding to 500°C and a temperature T 1 respectively on a thermogravimetric curve of the composite graphite material, the temperature T 1 is a peak temperature of a peak with a largest area in a differential thermogravimetric curve of the composite graphite material, and the thermogravimetric curve and the differential thermogravimetric curve may be obtained by thermogravimetric analysis under following conditions: sample mass: 10±0.05mg, purge gas: air at a gas flow rate of 60mL/min, heating rate: 5°C/min, and a test temperature ranging from 35°C to 950°C, characterized in that the composite graphite material further comprises a kinetic carbon material and that a raw material of the kinetic carbon material is selected from one or more of hard carbon, micro-expanded graphite, expanded graphite, or graphene. an air oxidation temperature T 0 of the composite graphite material is from 630°C to 730°C, and is optionally from 660°C to 710°C, and the air oxidation temperature T 0 is a temperature corresponding to an intersection of two tangents at two points corresponding to 500°C and a temperature T 1 respectively on a thermogravimetric curve of the composite graphite material, the temperature T 1 is a peak temperature of a peak with a largest area in a differential thermogravimetric curve of the composite graphite material, and the thermogravimetric curve and the differential thermogravimetric curve may be obtained by thermogravimetric analysis under following conditions: sample mass: 10±0.05mg, purge gas: air at a gas flow rate of 60mL/min, heating rate: 5°C/min, and a test temperature ranging from 35°C to 950°C, characterized in that the composite graphite material further comprises a kinetic carbon material and that a raw material of the kinetic carbon material is selected from one or more of hard carbon, micro-expanded graphite, expanded graphite, or graphene.
A lithographic apparatus comprising: a base frame (BF) constructed to form a supporting structure of the lithographic apparatus, an active base frame support (ABS) configured to support the base frame on a ground plane (GF) the active base frame support comprising a horizontal piezo actuator (HBSA) configured to exert a force in a horizontal direction on the base frame and a horizontal piezo force sensor (HBSS) configured to measure a horizontal force on the base frame, a control device (C) configured to drive the horizontal piezo actuator, a signal (FSI) representing a force (F) on the base frame being provided to the control device, the control device being configured to drive the horizontal piezo actuator based on the signal representing the force on the base frame, wherein the signal representing the force on the base frame comprises a horizontal force sensor signal of the horizontal piezo force sensor, and wherein the horizontal piezo actuator and the horizontal piezo force sensor are vertically stacked. a base frame (BF) constructed to form a supporting structure of the lithographic apparatus, an active base frame support (ABS) configured to support the base frame on a ground plane (GF) the active base frame support comprising a horizontal piezo actuator (HBSA) configured to exert a force in a horizontal direction on the base frame and a horizontal piezo force sensor (HBSS) configured to measure a horizontal force on the base frame, a control device (C) configured to drive the horizontal piezo actuator, a signal (FSI) representing a force (F) on the base frame being provided to the control device, the control device being configured to drive the horizontal piezo actuator based on the signal representing the force on the base frame, wherein the signal representing the force on the base frame comprises a horizontal force sensor signal of the horizontal piezo force sensor, and wherein the horizontal piezo actuator and the horizontal piezo force sensor are vertically stacked.
A hair care composition for improving curl retention of hair, comprising: a carrier; and a quaternary ammonium compound configured to improve curl retention of hair, wherein the quaternary ammonium compound is represented by chemical formula (I): wherein: R 1 is independently selected from: a C 10 -C 22 alkyl group, a C 10 -C 22 ester group, an R 5 -C(=O)NH(CH 2 ) m group, where R 5 is a C 10 -C 22 alkyl and m is an integer from 1 to 3, and mixtures thereof; R 2 and R 4 are each independently selected from: H, C 1 -C 5 alkyl and polyoxyalkylene groups having polyalkylene repeating units containing from 1 to 4 carbon atoms; R 3 is independently selected from R 1 , R 2 , and R 4 ; and X - is a counterion, wherein the quaternary ammonium compound of formula (I) is present in an amount of from 0.2 weight % to 0.3 weight %, based on a total weight of the hair care composition. a carrier; and a quaternary ammonium compound configured to improve curl retention of hair, wherein the quaternary ammonium compound is represented by chemical formula (I): wherein: R 1 is independently selected from: a C 10 -C 22 alkyl group, a C 10 -C 22 ester group, an R 5 -C(=O)NH(CH 2 ) m group, where R 5 is a C 10 -C 22 alkyl and m is an integer from 1 to 3, and mixtures thereof; R 2 and R 4 are each independently selected from: H, C 1 -C 5 alkyl and polyoxyalkylene groups having polyalkylene repeating units containing from 1 to 4 carbon atoms; R 3 is independently selected from R 1 , R 2 , and R 4 ; and X - is a counterion, wherein the quaternary ammonium compound of formula (I) is present in an amount of from 0.2 weight % to 0.3 weight %, based on a total weight of the hair care composition. R 1 is independently selected from: a C 10 -C 22 alkyl group, a C 10 -C 22 ester group, an R 5 -C(=O)NH(CH 2 ) m group, where R 5 is a C 10 -C 22 alkyl and m is an integer from 1 to 3, and mixtures thereof; R 2 and R 4 are each independently selected from: H, C 1 -C 5 alkyl and polyoxyalkylene groups having polyalkylene repeating units containing from 1 to 4 carbon atoms; R 3 is independently selected from R 1 , R 2 , and R 4 ; and X - is a counterion, wherein the quaternary ammonium compound of formula (I) is present in an amount of from 0.2 weight % to 0.3 weight %, based on a total weight of the hair care composition.
Hydropneumatic piston-cylinder arrangement, particularly for use as a suspension strut in vehicle suspension systems, with a cylinder housing and a piston that is guided such that it can be moved axially in the cylinder chamber , which is filled with a hydraulic fluid, of said cylinder housing, said piston comprising a piston rod on one side of the piston, said rod leading out of one end of the cylinder chamber in a sealed manner, the hydraulic fluid, which is contained in the cylinder chamber on the side of the piston base facing away from the piston rod , being able to be brought into operative connection with a pneumatic spring accumulator , wherein the pneumatic spring accumulator is a piston accumulator , which is arranged in the cylinder housing , and wherein the piston accumulator is received in the cylinder housing with its accumulator housing on the outer circumference, characterised in that the cylinder chamber comprises a fluid connection point on each end region, said connection points serving to extend the piston rod unit when pressure is applied; in that one of the connection points emerges into a fluid chamber forming part of the cylinder chamber , said fluid chamber being released in the original position of the two pistons which are adjacent to and opposite one another; and in that , in its installed position, the accumulator housing of the piston accumulator protrudes into a hole in the housing of one fluid connection point with a small overhang . pneumatic spring accumulator , wherein the pneumatic spring accumulator is a piston accumulator , which is arranged in the cylinder housing , and wherein the piston accumulator is received in the cylinder housing with its accumulator housing on the outer circumference, characterised in that the cylinder chamber comprises a fluid connection point on each end region, said connection points serving to extend the piston rod unit when pressure is applied; in that one of the connection points emerges into a fluid chamber forming part of the cylinder chamber , said fluid chamber being released in the original position of the two pistons which are adjacent to and opposite one another; and in that , in its installed position, the accumulator housing of the piston accumulator protrudes into a hole in the housing of one fluid connection point with a small overhang .
A rotorcraft comprising: a tail rotor assembly , the tail rotor assembly comprising: a yoke , the yoke comprising a yoke arm ; a rotor blade (302a-d); and at least three spherical bearings (406a-c, 406d-f), each of the at least three spherical bearings (406a-c, 406d-f) carried by the yoke arm and configured to pivotally secure the rotor blade (302a-d) to the yoke arm and to allow feathering movement of the rotor blade (302a-d) relative to the yoke arm during flight; characterised in that the at least three spherical bearings (406a-c, 406d-f) are evenly spaced from each other on the yoke arm ; and the yoke comprises a length in the range of 0.699 m (27.5 inches) and 0.724 m (28.5 inches). a tail rotor assembly , the tail rotor assembly comprising: a yoke , the yoke comprising a yoke arm ; a rotor blade (302a-d); and at least three spherical bearings (406a-c, 406d-f), each of the at least three spherical bearings (406a-c, 406d-f) carried by the yoke arm and configured to pivotally secure the rotor blade (302a-d) to the yoke arm and to allow feathering movement of the rotor blade (302a-d) relative to the yoke arm during flight; a yoke , the yoke comprising a yoke arm ; a rotor blade (302a-d); and at least three spherical bearings (406a-c, 406d-f), each of the at least three spherical bearings (406a-c, 406d-f) carried by the yoke arm and configured to pivotally secure the rotor blade (302a-d) to the yoke arm and to allow feathering movement of the rotor blade (302a-d) relative to the yoke arm during flight; characterised in that the at least three spherical bearings (406a-c, 406d-f) are evenly spaced from each other on the yoke arm ; and the yoke comprises a length in the range of 0.699 m (27.5 inches) and 0.724 m (28.5 inches).
Method for controlling a mobile working machine, wherein the working machine is provided with at least two power participants that are each configured to receive energy from a motor and convert it into a work task and/or into a driving task of the working machine, characterized in that the method comprises the following steps: a. ascertaining a load on the motor in the form of a load factor ( fac LLC ); b. calculating a power factor ( facV_x ) for each power participant , wherein the power factor ( facV_x ) is calculated by means of a prioritization function assigned to the respective power participant , wherein the respective prioritization function can ascertain a value for the power factor (facV_x) based on the ascertained load factor ( fac LLC ) and a prioritization factor (Pr_x) assigned to the respective power participant; c. calculating a target power for each power participant on the basis of the respective power factor ( facV_x ) and a respective requested power. a. ascertaining a load on the motor in the form of a load factor ( fac LLC ); b. calculating a power factor ( facV_x ) for each power participant , wherein the power factor ( facV_x ) is calculated by means of a prioritization function assigned to the respective power participant , wherein the respective prioritization function can ascertain a value for the power factor (facV_x) based on the ascertained load factor ( fac LLC ) and a prioritization factor (Pr_x) assigned to the respective power participant; c. calculating a target power for each power participant on the basis of the respective power factor ( facV_x ) and a respective requested power.
An optical device , comprising: a) a first optical coupler configured to receive a light signal and provide a first output and a second output; b) a first optical waveguide in optical communication with the first output and configured to provide a first optical path for a first portion of the light signal; and c) a second optical waveguide in optical communication with the second output and configured to provide a second optical path for a second portion of the light signal, d) wherein at least the first optical waveguide is configured to provide a phase differential between the first optical path and the second optical path, e) wherein the second optical waveguide is positioned within a lateral thermal diffusion length associated with the first optical waveguide , and f) wherein the lateral thermal diffusion length is a spreading distance of a thermal effect in a direction about perpendicular to the first optical path; g) wherein the first optical waveguide is constructed from a silicon material, wherein to provide the phase differential, the first optical waveguide is doped with dopants to cause injection of free carriers into the silicon material, and wherein the injection of the free carriers causes the thermal effect; and h) wherein the first optical waveguide is disposed on a silicon substrate layer , and a part of the silicon substrate layer is removed such that air cavities are formed between the first optical waveguide and the silicon substrate layer to thermally insulate the waveguides from the silicon substrate layer . a) a first optical coupler configured to receive a light signal and provide a first output and a second output; b) a first optical waveguide in optical communication with the first output and configured to provide a first optical path for a first portion of the light signal; and c) a second optical waveguide in optical communication with the second output and configured to provide a second optical path for a second portion of the light signal, d) wherein at least the first optical waveguide is configured to provide a phase differential between the first optical path and the second optical path, e) wherein the second optical waveguide is positioned within a lateral thermal diffusion length associated with the first optical waveguide , and f) wherein the lateral thermal diffusion length is a spreading distance of a thermal effect in a direction about perpendicular to the first optical path; g) wherein the first optical waveguide is constructed from a silicon material, wherein to provide the phase differential, the first optical waveguide is doped with dopants to cause injection of free carriers into the silicon material, and wherein the injection of the free carriers causes the thermal effect; and h) wherein the first optical waveguide is disposed on a silicon substrate layer , and a part of the silicon substrate layer is removed such that air cavities are formed between the first optical waveguide and the silicon substrate layer to thermally insulate the waveguides from the silicon substrate layer .