mhurhangee/patent-ind-claim-en huggingface dataset:
A device for measuring the geometry of a sample and the spatially varying surface reflectance of the sample surface, comprising a basic dome-like three-dimensional structure to be placed over the surface (1.1) of the sample to be measured, wherein the basic dome-like three-dimensional structure has at least one concave wall concavely curved on the side facing the sample , wherein the device further comprises at least two first illumination units whose outputs direct light via respective apertures onto the sample surface to be measured, said apertures being rigidly or movably connected to the dome-like three-dimensional structure , and an optical acquisition system including at least two devices selected from the group consisting of cameras and optical detectors, wherein the sample is in a stationary position and the device further comprises a frame and a first motor for-rotationally driving the basic dome-like three-dimensional structure , the motor being attached to said frame , wherein the basic dome-like three-dimensional structure is mechanically connected to a rotating part having an axis of rotation, wherein said rotating part is the shaft of the first motor oriented in such way that its axis of rotation passes through the concave wall of the basic dome-like three-dimensional structure or through an opening created in the concave wall or wherein said rotating part is an element connected to the shaft of the first motor by means of motion transmission means and the orientation of the shaft of the first motor and the motion transmission means are such that the axis of rotation of the rotating part passes through the concave wall of the basic dome-like three-dimensional structure or through an opening created in the concave wall , and wherein at least one first arm , which carries a set of at least two optical elements mediating the imaging onto the acquisition system, the optical elements consisting of mirrors and/or lenses and/or imaging bundles and/or prisms, is attached to the basic dome-like three-dimensional structure or to other parts mechanically fixed to the basic dome-like three-dimensional structure so that-the first arm can rotate together with the basic dome-like three-dimensional structure , wherein this first arm is also mechanically connected to at least one second motor , said second motor being attached to the basic dome-like three-dimensional structure or to other parts mechanically fixed to the basic dome-like three-dimensional structure for independently driving the movement of the first arm with respect to a reference coordinate system associated with the basic dome-like three-dimensional structure .
A method of communication of a network, comprising: receiving a failure indication from a system if the system determines that a request of a mobile device to obtain an unmanned aerial system (UAS) service has failed at an authentication or an authorization, wherein the system comprises a UAS service supplier (USS) and/or a UAS traffic management system, the USS/UTM decides that the mobile device request to obtain unmanned aerial system (UAS) service has failed at authentication/authorization, and the network comprises a 3rd Generation Partnership Project network; wherein the method further comprises transmitting the failure indication to the mobile device if the authentication or the authorization is a follow on or a concatenation of a 3GPP registration; wherein when the 3GPP registration completes successfully but the authentication or the authorization fails, the network decides whether to allow or not allow the mobile device to continue to access the network; wherein the network decides whether to allow or not allow the mobile device to continue to access the network based on an operator policy. receiving a failure indication from a system if the system determines that a request of a mobile device to obtain an unmanned aerial system (UAS) service has failed at an authentication or an authorization, wherein the system comprises a UAS service supplier (USS) and/or a UAS traffic management system, the USS/UTM decides that the mobile device request to obtain unmanned aerial system (UAS) service has failed at authentication/authorization, and the network comprises a 3rd Generation Partnership Project network; wherein the method further comprises transmitting the failure indication to the mobile device if the authentication or the authorization is a follow on or a concatenation of a 3GPP registration; wherein when the 3GPP registration completes successfully but the authentication or the authorization fails, the network decides whether to allow or not allow the mobile device to continue to access the network; wherein the network decides whether to allow or not allow the mobile device to continue to access the network based on an operator policy.
A gas turbine engine sealing air system comprising: a compressor and a starter air system of the gas turbine engine ; a bearing chamber seal to prevent lubricant fluid loss from a fluid chamber , the sealing effected by ingress of sealing air; a sealing air supply duct coupled between the compressor and the bearing chamber seal during normal operation of the gas turbine engine ; an air vent duct coupled to the bearing chamber seal ; an ejector located within the air vent duct to pump sealing air from the bearing chamber seal and through the air vent duct ; a switching mechanism connected with the ejector ; and a first duct coupled between the starter air system and the switching mechanism ; characterized by a second duct coupled between the compressor and the switching mechanism ; wherein the switching mechanism is configured to switch the supply of motive fluid to the ejector to the starter air system via the first duct during at least gas turbine engine starting, to the compressor via the second duct during other periods operation of the gas turbine engine , or to stop the supply of motive fluid. a compressor and a starter air system of the gas turbine engine ; a bearing chamber seal to prevent lubricant fluid loss from a fluid chamber , the sealing effected by ingress of sealing air; a sealing air supply duct coupled between the compressor and the bearing chamber seal during normal operation of the gas turbine engine ; an air vent duct coupled to the bearing chamber seal ; an ejector located within the air vent duct to pump sealing air from the bearing chamber seal and through the air vent duct ; a switching mechanism connected with the ejector ; and a first duct coupled between the starter air system and the switching mechanism ; characterized by a second duct coupled between the compressor and the switching mechanism ; wherein the switching mechanism is configured to switch the supply of motive fluid to the ejector to the starter air system via the first duct during at least gas turbine engine starting, to the compressor via the second duct during other periods operation of the gas turbine engine , or to stop the supply of motive fluid.
Sulfur-crosslinkable rubber mixture, in particular for two-wheeler tyre treads, containing at least the following constituents: - 10 to 100 phr of natural polyisoprene from dandelions and - 15 to 75 phr of at least one first carbon black A having an iodine adsorption number according to ASTM D 1510 of 40 to 75 g/kg and a DBP number according to ASTM D 2414 of 130 to 200 ml/100 g and - 15 to 75 phr of at least one second carbon black B having an iodine adsorption number according to ASTM D 1510 of 100 to 140 g/kg and a DBP number according to ASTM D 2414 of 100 to 170 ml/100 g, wherein the weight ratio of carbon black A to carbon black B is between 5:1 and 1:5 and wherein the total amount of carbon black in the rubber mixture is 30 bis 150 phr. - 10 to 100 phr of natural polyisoprene from dandelions and - 15 to 75 phr of at least one first carbon black A having an iodine adsorption number according to ASTM D 1510 of 40 to 75 g/kg and a DBP number according to ASTM D 2414 of 130 to 200 ml/100 g and - 15 to 75 phr of at least one second carbon black B having an iodine adsorption number according to ASTM D 1510 of 100 to 140 g/kg and a DBP number according to ASTM D 2414 of 100 to 170 ml/100 g, wherein the weight ratio of carbon black A to carbon black B is between 5:1 and 1:5 and wherein the total amount of carbon black in the rubber mixture is 30 bis 150 phr.
A transceiver, comprising: a substrate ; a membrane suspending from the substrate; a bottom electrode disposed on the membrane ; a piezoelectric layer disposed on the bottom electrode; and first and second top electrodes disposed on the piezoelectric layer , the first top electrode being electrically separated from the second top electrode; the piezoelectric layer including a first portion located under the first top electrode and poled in a first direction and a second portion located under the second top electrode and poled in a second direction, the transceiver being configured to operate in a flexural mode of operation causing a flex tensional motion of the membrane, characterized in that the direction of the second top electrode is poled in a direction opposite to the direction of the first electrode; and wherein the first top electrode is responsive to at least a first frequency and the second top electrode is responsive to at least a second frequency different from the first and the bottom electrode is responsive to both frequencies, a substrate ; a membrane suspending from the substrate; a bottom electrode disposed on the membrane ; a piezoelectric layer disposed on the bottom electrode; and first and second top electrodes disposed on the piezoelectric layer , the first top electrode being electrically separated from the second top electrode; the piezoelectric layer including a first portion located under the first top electrode and poled in a first direction and a second portion located under the second top electrode and poled in a second direction, the transceiver being configured to operate in a flexural mode of operation causing a flex tensional motion of the membrane, characterized in that the direction of the second top electrode is poled in a direction opposite to the direction of the first electrode; and wherein the first top electrode is responsive to at least a first frequency and the second top electrode is responsive to at least a second frequency different from the first and the bottom electrode is responsive to both frequencies,
A wearable computing device designed to be worn by a user, comprising: a directional antenna; a signal capturing module configured to capture one or more signals through the directional antenna, the one or more signals having been transmitted by one or more electronic devices; a nearby ascertaining module configured to ascertain that the one or more electronic devices that transmitted the one or more signals are within a spatial pod of the wearable computing device based, at least in part, on the one or more signals captured through the directional antenna, the spatial pod of the wearable computing device being a spatial volume that includes the wearable computing device and being defined by an enveloping boundary, where low-power signals transmitted via the directional antenna being discernible over background noise within the enveloping boundary and not discernible over background noise outside the enveloping boundary; and a functionality acquiring module configured to acquire, via the directional antenna, at least access to one or more functionalities from the one or more electronic devices that were ascertained to be within the spatial pod of the wearable computing device. a directional antenna; a signal capturing module configured to capture one or more signals through the directional antenna, the one or more signals having been transmitted by one or more electronic devices; a nearby ascertaining module configured to ascertain that the one or more electronic devices that transmitted the one or more signals are within a spatial pod of the wearable computing device based, at least in part, on the one or more signals captured through the directional antenna, the spatial pod of the wearable computing device being a spatial volume that includes the wearable computing device and being defined by an enveloping boundary, where low-power signals transmitted via the directional antenna being discernible over background noise within the enveloping boundary and not discernible over background noise outside the enveloping boundary; and a functionality acquiring module configured to acquire, via the directional antenna, at least access to one or more functionalities from the one or more electronic devices that were ascertained to be within the spatial pod of the wearable computing device.
A method of producing porous silica-carbon composites, the method comprising steps of: mixing fine particulate carbon dispersed in water by a surfactant, alkali metal silicate aqueous solution, and mineral acid so as to produce a co-dispersion in which silica hydrosol, produced by reaction of the alkali metal silicate and the mineral acid, and the fine particulate carbon are uniformly dispersed: and gelling the silica hydrosol, contained in the co-dispersion, and making the co-dispersion into porous bodies having specific surface area from 20 to 1000 m2/g, pore volume from 0.3 to 2.0 ml/g, and average pore diameter from 2 to 100 nm, wherein the porous silica-carbon composites have a carbon content of 1 to 50%. mixing fine particulate carbon dispersed in water by a surfactant, alkali metal silicate aqueous solution, and mineral acid so as to produce a co-dispersion in which silica hydrosol, produced by reaction of the alkali metal silicate and the mineral acid, and the fine particulate carbon are uniformly dispersed: and gelling the silica hydrosol, contained in the co-dispersion, and making the co-dispersion into porous bodies having specific surface area from 20 to 1000 m2/g, pore volume from 0.3 to 2.0 ml/g, and average pore diameter from 2 to 100 nm, wherein the porous silica-carbon composites have a carbon content of 1 to 50%.
A clothing treating device, comprising a first clothing treating bucket , a second clothing treating bucket and an air duct , wherein an air inlet end of the air duct is respectively communicated with a first air inlet of the first clothing treating bucket and a second air inlet of the second clothing treating bucket through a first air duct conversion device at the air inlet end, and an air outlet end of the air duct is respectively communicated with a first air outlet of the first clothing treating bucket and a second air outlet of the second clothing treating bucket through a second air duct conversion device at the air outlet end of the air duct . an air inlet end of the air duct is respectively communicated with a first air inlet of the first clothing treating bucket and a second air inlet of the second clothing treating bucket through a first air duct conversion device at the air inlet end, and an air outlet end of the air duct is respectively communicated with a first air outlet of the first clothing treating bucket and a second air outlet of the second clothing treating bucket through a second air duct conversion device at the air outlet end of the air duct .
Cap anchoring element arrangement comprising - an anchoring element (VE) on which there is a circumferential groove (NU), - a cap (KA) for fastening dentures on the anchoring element (VE), which cap has a projection (VO) facing radially inwards and a conical end (AB), and - a die (MA) which is made of a resiliently elastic deformable material and is arranged in the cap (KA) only above the conical end (AB), - wherein the projection (VO) interacts with the circumferential groove (NU) on the anchoring element (VE) as a retention element (RE) so that the cap (KA) can be or is releasably fastened to the anchoring element (VE) by means of the die (MA), and wherein, in the fastened state, the conical end (AB) arranged below the retention element (RE) at least partially encloses a corresponding outer surface (AF) of the anchoring element (VE). - an anchoring element (VE) on which there is a circumferential groove (NU), - a cap (KA) for fastening dentures on the anchoring element (VE), which cap has a projection (VO) facing radially inwards and a conical end (AB), and - a die (MA) which is made of a resiliently elastic deformable material and is arranged in the cap (KA) only above the conical end (AB), - wherein the projection (VO) interacts with the circumferential groove (NU) on the anchoring element (VE) as a retention element (RE) so that the cap (KA) can be or is releasably fastened to the anchoring element (VE) by means of the die (MA), and wherein, in the fastened state, the conical end (AB) arranged below the retention element (RE) at least partially encloses a corresponding outer surface (AF) of the anchoring element (VE).
An apparatus comprising: a substrate defining a bacteria binding volume thereon; a light source arranged to cast light toward the substrate, such that the light is totally internally reflected on the surface of the substrate to thereby create an evanescent field , such that the bacteria binding volume is within the evanescent field; a detector arranged to receive scattered light from the bacteria binding volume and output first data ; a second detector , arranged to receive light from the light source having undergone total internal reflection within the substrate, which is not scattered by the bacteria and output second data ; and a computer system arranged to gather the first and second data , the computer system comprising a processor, the processor being configured to determine a level of vibration of bacteria within the bacteria binding volume in three-dimensions from the first data and to determine whether the first data received from the first detector is correct based on the second data . a substrate defining a bacteria binding volume thereon; a light source arranged to cast light toward the substrate, such that the light is totally internally reflected on the surface of the substrate to thereby create an evanescent field , such that the bacteria binding volume is within the evanescent field; a detector arranged to receive scattered light from the bacteria binding volume and output first data ; a second detector , arranged to receive light from the light source having undergone total internal reflection within the substrate, which is not scattered by the bacteria and output second data ; and a computer system arranged to gather the first and second data , the computer system comprising a processor, the processor being configured to determine a level of vibration of bacteria within the bacteria binding volume in three-dimensions from the first data and to determine whether the first data received from the first detector is correct based on the second data . a detector arranged to receive scattered light from the bacteria binding volume and output first data ; a second detector , arranged to receive light from the light source having undergone total internal reflection within the substrate, which is not scattered by the bacteria and output second data ; and a computer system arranged to gather the first and second data , the computer system comprising a processor, the processor being configured to determine a level of vibration of bacteria within the bacteria binding volume in three-dimensions from the first data and to determine whether the first data received from the first detector is correct based on the second data .
Tyre comprising: - two beads ; - two sidewalls connected to the beads ; - a crown connected on each side to the radially exterior end of each of the two sidewalls, the crown comprising: ▪ a belt reinforcement of axial width W, ▪ a tread , the tread comprising a plurality of tread pattern blocks , two axially adjacent tread pattern blocks being separated by a groove extending at least partially circumferentially, each groove being delimited radially towards the inside by a groove bottom , ▪ the material of which the tread is made having a dynamic shear modulus G*, at 60°C and under 10 Hz alternating stress loading of 0.7 MPa, of less than 1.25 MPa, characterized in that the crown comprises a stiffening ply made up of filamentary reinforcing elements that are rigid in terms of compression, the said filamentary reinforcing elements forming, with the circumferential direction C, an angle of between 50° and 90°, the said filamentary reinforcing elements being arranged radially on the outside of the belt reinforcement and axially under at least one groove of the tread, and extending axially at least over a width WR representing at minimum 50% of the axial width W of the belt reinforcement. - two beads ; - two sidewalls connected to the beads ; - a crown connected on each side to the radially exterior end of each of the two sidewalls, the crown comprising: ▪ a belt reinforcement of axial width W, ▪ a tread , the tread comprising a plurality of tread pattern blocks , two axially adjacent tread pattern blocks being separated by a groove extending at least partially circumferentially, each groove being delimited radially towards the inside by a groove bottom , ▪ the material of which the tread is made having a dynamic shear modulus G*, at 60°C and under 10 Hz alternating stress loading of 0.7 MPa, of less than 1.25 MPa, characterized in that the crown comprises a stiffening ply made up of filamentary reinforcing elements that are rigid in terms of compression, the said filamentary reinforcing elements forming, with the circumferential direction C, an angle of between 50° and 90°, the said filamentary reinforcing elements being arranged radially on the outside of the belt reinforcement and axially under at least one groove of the tread, and extending axially at least over a width WR representing at minimum 50% of the axial width W of the belt reinforcement. ▪ a belt reinforcement of axial width W, ▪ a tread , the tread comprising a plurality of tread pattern blocks , two axially adjacent tread pattern blocks being separated by a groove extending at least partially circumferentially, each groove being delimited radially towards the inside by a groove bottom , ▪ the material of which the tread is made having a dynamic shear modulus G*, at 60°C and under 10 Hz alternating stress loading of 0.7 MPa, of less than 1.25 MPa,
A pump or compressor for the flow of a fluid, comprising: - a casing , and - a centrifugal impeller configured to be driven in rotation relative to the casing about a main axis defining an axial direction (DA), - a restrictive fluid flow passage formed between the casing and the centrifugal impeller defining an axial balancing system , the casing comprising a first balancing portion and the centrifugal impeller comprising a second balancing portion , the first and second balancing portions defining the inlet of the restrictive flow passage, characterized in that the second balancing portion of the centrifugal impeller is configured to switch from a rest position, in which the outer diameter of the second balancing portion is smaller than the inner diameter of the first balancing portion , to an operating position in which the first and second balancing portions overlap along the axial direction (DA), under the effect of the centrifugal force exerted on the rotating centrifugal impeller . - a casing , and - a centrifugal impeller configured to be driven in rotation relative to the casing about a main axis defining an axial direction (DA), - a restrictive fluid flow passage formed between the casing and the centrifugal impeller defining an axial balancing system ,