mhurhangee/patent-ind-claim-en huggingface dataset:
Belt for bridle or harness with a first end section forming a first end of the belt (3, 3.1; 4; 17, 17.1), with a second end section (8.1) forming the other end of the belt (3, 3.1; 4; 17, 17.1), and a middle section connecting the two end sections (8, 8.1, 8.2), this middle section being provided by a cushion element (7, 7.1; 18, 18.1) arranged in respect of its effect on the animal's body, wherein the cushion element (7, 7.1; 18, 18.1) comprises a tension-resistant upper layer continuing into the end sections, by means of which the imposition of tensile force is divided over the width of the cushion element (7, 7.1; 18, 18.1), wherein in each case at least one securing means is connected to the end sections (8, 8.1, 8.2) of the upper layer , such as a securing belt (10, 10.1, 10.2, 19, 19.1), for connecting the belt (3, 3.1; 4; 17, 17.1) to another part or to another belt of a bridle or harness , and therefore the securing means are separated from one another, in relation to the securing effect which initiates their tensile strength, by the middle section of the cushion element (7, 7.1; 18, 18.1), and wherein the cushion element (7, 7.1; 18, 18.1) forming the middle section exhibits a greater width than the at least one securing means (10, 10.1, 10.2, 19, 19.1) connected to each end section (8, 8.1, 8.2) of the belt (3, 3.1; 4; 17, 17.1) is formed from the tension-resistant upper layer , an open-pored under layer peripherally connected to it, and an elastic spacing element , located in the pocket formed from the upper layer and the under layer , wherein the cushion element (7, 7.1; 18, 18.1) is provided by the spacing element and the under layer .
A method for a user equipment, UE, operating in a wireless communication system, the method comprising: checking (S1201) whether a value of queuing delay of a packet data convergence protocol service data unit, PDCP SDU, is above a threshold; and generating and transmitting (S1203) a PDCP protocol data unit, PDU, including the PDCP SDU in a data field and a time stamp for the PDCP SDU, when the value of the queuing delay is above the threshold, wherein a value of the time stamp for the PDCP SDU is set to a time when the PDCP SDU is received from the upper layer, wherein the PDCP PDU further includes a data/control, D/C, field, a PDCP sequence number, SN, field, and wherein only the data field in the PDCP PDU is ciphered and not the D/C field, the PDCP SN field and the time stamp. checking (S1201) whether a value of queuing delay of a packet data convergence protocol service data unit, PDCP SDU, is above a threshold; and generating and transmitting (S1203) a PDCP protocol data unit, PDU, including the PDCP SDU in a data field and a time stamp for the PDCP SDU, when the value of the queuing delay is above the threshold, wherein a value of the time stamp for the PDCP SDU is set to a time when the PDCP SDU is received from the upper layer, wherein the PDCP PDU further includes a data/control, D/C, field, a PDCP sequence number, SN, field, and wherein only the data field in the PDCP PDU is ciphered and not the D/C field, the PDCP SN field and the time stamp.
A method for manufacturing a structural composite component , said method comprising the following steps: - stacking, in a first heating mold , a first mat , a spacer and a second mat ; the spacer being positioned between the first and second mats; at least one of the first and second mats including a continuous web of fibers impregnated with a composition including a thermosetting resin ; and - compression and heating of the stack by the first heating mold, the heating being done at a temperature and for a duration allowing polymerization or cross-linking of the thermosetting resin; said method being characterized in that : it includes, before the stacking step in the first heating mold, a step of compressing the spacer in a non-heated second mold , a first inner surface of said non-heating second mold including at least one first raised and/or hollow cavity die , said first inner surface being substantially oriented in a compression direction , so as to configure the spacer according to said cavity die, - a second inner surface of the first heating mold includes at least one second raised and/or hollow cavity die corresponding to the first cavity die of the first inner surface of the non-heating second mold, said second inner surface being substantially oriented in the compression direction, such that, during the step for compression and heating by the first mold, an air gap between the spacer and said second inner surface is substantially constant over said second inner surface. - stacking, in a first heating mold , a first mat , a spacer and a second mat ; the spacer being positioned between the first and second mats; at least one of the first and second mats including a continuous web of fibers impregnated with a composition including a thermosetting resin ; and - compression and heating of the stack by the first heating mold, the heating being done at a temperature and for a duration allowing polymerization or cross-linking of the thermosetting resin; - a second inner surface of the first heating mold includes at least one second raised and/or hollow cavity die corresponding to the first cavity die of the first inner surface of the non-heating second mold, said second inner surface being substantially oriented in the compression direction, such that, during the step for compression and heating by the first mold, an air gap between the spacer and said second inner surface is substantially constant over said second inner surface.
Car body for a railway vehicle, comprising a chassis , side walls and a roof , characterised in that at least two traction mechanisms aligned at right angles to the longitudinal axis of the car body are arranged laterally reversed between specific points of the car body on the interior of the car body in the roof area and reinforce the roof structure so that low-frequency natural oscillations of the car body are largely suppressed.
A joint device with an upper part and a lower part which are mounted on each other so as to be pivotable about a pivot axis , with a hydraulic unit secured on the upper part and the lower part , with a housing in which a cylinder is arranged, in which a working piston connected to a piston rod is mounted displaceably and divides the cylinder into two chambers , wherein the housing and the piston rod are connected to the upper part and the lower part , respectively, characterized in that the working piston is coupled to at least one spring device which transmits tensile forces and compressive forces and which engages on at least one abutment which is arranged inside the cylinder .
Converter for a motor vehicle, comprising a switching unit which is connected to an intermediate circuit of the converter and which can be operated with a predetermined switching frequency, and several filter elements (7-11) connected in the intermediate circuit having respectively one intermediate circuit capacitor , wherein a minimum of the magnitude frequency response of a respective filter element (7-11) lies within another frequency interval, which has a harmonic of the switching frequency as a centre frequency and an interval length corresponding to the switching frequency, than a perspective minimum of the magnitude frequency response of the remaining filter elements (7-11), wherein the intermediate circuit capacitor of a respective filter element (7-11) is realised by a capacitor , wherein at least one or a respective filter element (7-11) has an inductance element connected in series with its intermediate circuit capacitor , characterised in that the inductivity element is formed by a line connection to the intermediate circuit capacitor , the length and/or shape and/or arrangement of which within several planes of a circuit board specifies the inductance of the inductance element , wherein the capacitors of several filter elements (7-11) or of all filter elements (7-11) are identical in construction.
An energy dissipater comprising a plurality of shells , all surfaces of the shells being formed as periodic hyperbolic paraboloidal surfaces forming a continuous solid, thin shell surface-structure that envelopes contiguous tunnels there through, the tunnels being arranged according to a dual-intertwined cubic network pair.
Aerodynamic system for a motor vehicle, which can be arranged close to at least one region of detachment of at least one bodywork element of a vehicle, characterised in that the system comprises at least one vortex generator which generates a vortex by creating a periodic air jet and is supplied by exhaust gases from an outlet of the exhaust line of the vehicle.
A display apparatus comprising a plurality of subpixels (SP1, SP2, SP3) and configured to emit light based on each of the plurality of subpixels, the display apparatus comprising: a substrate ; a driving layer provided on the substrate and comprising a plurality of driving elements which are configured to apply current to the display apparatus; and a light-emitting resonance layer (LR) provided on the driving layer, comprising: a plurality of first electrodes electrically connected to the driving layer; a first semiconductor layer provided on the plurality of first electrodes; an active layer provided on the first semiconductor layer; a second semiconductor layer provided on the active layer; a second electrode provided on the second semiconductor layer; and a reflective layer provided on the second semiconductor layer, wherein light emitted from the active layer resonates between the plurality of first electrodes and the reflective layer, characterized in that the display apparatus further comprises a plurality of color conversion layers , provided on the reflective layer and configured to convert light emitted from the active layer into light having different colors based on each of the plurality of subpixels. a substrate ; a driving layer provided on the substrate and comprising a plurality of driving elements which are configured to apply current to the display apparatus; and a light-emitting resonance layer (LR) provided on the driving layer, comprising: a plurality of first electrodes electrically connected to the driving layer; a first semiconductor layer provided on the plurality of first electrodes; an active layer provided on the first semiconductor layer; a second semiconductor layer provided on the active layer; a second electrode provided on the second semiconductor layer; and a reflective layer provided on the second semiconductor layer, wherein light emitted from the active layer resonates between the plurality of first electrodes and the reflective layer, characterized in that the display apparatus further comprises a plurality of color conversion layers , provided on the reflective layer and configured to convert light emitted from the active layer into light having different colors based on each of the plurality of subpixels. a plurality of first electrodes electrically connected to the driving layer; a first semiconductor layer provided on the plurality of first electrodes; an active layer provided on the first semiconductor layer; a second semiconductor layer provided on the active layer; a second electrode provided on the second semiconductor layer; and a reflective layer provided on the second semiconductor layer, wherein light emitted from the active layer resonates between the plurality of first electrodes and the reflective layer, characterized in that the display apparatus further comprises a plurality of color conversion layers , provided on the reflective layer and configured to convert light emitted from the active layer into light having different colors based on each of the plurality of subpixels.
Method for dynamic control of runway illumination on aircraft, suitable for controlling the illumination of a light equipment comprising a LED matrix and refraction optics during a flight phase, the method comprising the following steps: a) Determination of predefined flight dynamic movement equations for the flight phase b) Obtention of real data from autonomous sensors independent from the aircraft sensors c) Use of extended Kalman Filter and algorithm taking into account the data from the autonomous sensors to obtain the aircraft dynamics data, the aircraft dynamics data comprising the aircraft speed V and at least one of the pitch, roll and yaw, this step comprising the following phases: c1) Predict phase c2) Update phase d) Application of the obtained aircraft dynamics data to light control laws affecting the light equipment. a) Determination of predefined flight dynamic movement equations for the flight phase b) Obtention of real data from autonomous sensors independent from the aircraft sensors c) Use of extended Kalman Filter and algorithm taking into account the data from the autonomous sensors to obtain the aircraft dynamics data, the aircraft dynamics data comprising the aircraft speed V and at least one of the pitch, roll and yaw, this step comprising the following phases: c1) Predict phase c2) Update phase c1) Predict phase c2) Update phase d) Application of the obtained aircraft dynamics data to light control laws affecting the light equipment.
A method for producing a composition containing C 8 F 17 Br, and further containing C 7 F 15 COOH, comprising reacting C 8 F 17 I and a brominating agent to obtain C 8 F 17 Br; and alkali-washing the obtained C 8 F 17 Br to reduce the C 7 F 15 COOH content to ≤ 25 ppb based on the total weight of C 8 F 17 Br, wherein the alkali-washing is repeatedly performed until the alkali layer after alkali-washing has a pH of ≥ 8.
A 3D printer nozzle comprising a heating element, the heating element comprising: at least one sheath comprising a first inner diameter and a first outer diameter, the at least one sheath sized to engage around an outer circumference of the 3D printer nozzle ; at least one wire coil at least partially contacting the first inner diameter of the at least one sheath ; and at least one energy receiver associated with the at least one wire coil , characterized in that , the at least one wire coil comprises a high density winding at a taper portion of the 3D printer nozzle and a lower density winding along a non-taper portion of the 3d printer nozzle . at least one sheath comprising a first inner diameter and a first outer diameter, the at least one sheath sized to engage around an outer circumference of the 3D printer nozzle ; at least one wire coil at least partially contacting the first inner diameter of the at least one sheath ; and at least one energy receiver associated with the at least one wire coil , characterized in that ,
System for distributing semisolid lubricant, comprising a semisolid lubricant tank (S) and a high pressure pumping system that intermittently feeds, during a lubrication cycle, at least one first duct , the at least one first duct feeding a plurality of distributors adapted to sort the semisolid lubricant to a plurality of users (U), wherein is present, fluidly associated with said first duct , a controlled suction/delivery device of a part of the semisolid lubricant conveyed by said first duct, the controlled suction/delivery device being configured to suck a volume of semisolid lubricant from said first duct during a step of inactivity of the pumping system on said first duct , and to introduce the previously suctioned semisolid lubricant in said first duct during a step of activity of the pumping system on said first duct , characterized in that the controlled suction/delivery device comprises a pressure sensor functionally associated with said first duct and configured to control the suction/delivery device in its phases of sucking and of introducing the lubricant in said first duct on the base of the pressure read by the sensor .
A method of providing a detent sensation, said method of providing a detent sensation includes providing a first background force signal, said first background force signal followed with a second below background force drop signal, and said second below background force drop signal followed with a third above background stop force signal to provide a mechanical ball detent mechanism snap sensation at a targeted location
A compressed air braking system (DBA*) of a motor vehicle, which has a compressed air supply unit with a compressor and a plurality of brake circuits connected to the compressed air supply unit via a multiple circuit protection valve , including at least one parking brake circuit with parking brake cylinders (25.1, 25.2), characterized in that the parking brake cylinders (25.1, 25.2) per wheel or per vehicle axle can each be vented via a rapid bleeder valve connected to a connecting line as well as a changeover valve arranged downstream thereof alternately to the ambient atmosphere or to an additional reservoir .
A method of altering a generator output voltage in anticipation of a change with respect to a specific electrical load, the method characterised by comprising: receiving, at a first time T1, by a bus power control unit BPCU , a request to switch on the specific electrical load comprising an inrush current to cause the generator output voltage to exceed a transient voltage limit; transmitting, at a second time T2, by the bus power control unit communication signals indicating that the specific electrical load will be applied within an expected time TX; receiving, at a generator control unit CGU , the communication signals indicating that the specific electrical load will be applied within an expected time TX; altering, by a voltage regulator of the generator control unit , a set point to produce an altered set point in response to the communication signals; implementing, by the voltage regulator, a change of the altered set point; matching the generator output voltage to the altered set point to produce a matched generator output voltage;transmitting, by the bus power control unit in communication with the generator control unit, a command to close a contactor ; and providing the matched generator output voltage to the specific electrical load based on a closing operation of the contactor, the closing operation being in accordance with a delay between receiving the command and an actual closing and mitigating the inrush current. receiving, at a first time T1, by a bus power control unit BPCU , a request to switch on the specific electrical load comprising an inrush current to cause the generator output voltage to exceed a transient voltage limit; transmitting, at a second time T2, by the bus power control unit communication signals indicating that the specific electrical load will be applied within an expected time TX; receiving, at a generator control unit CGU , the communication signals indicating that the specific electrical load will be applied within an expected time TX; altering, by a voltage regulator of the generator control unit , a set point to produce an altered set point in response to the communication signals; implementing, by the voltage regulator, a change of the altered set point; matching the generator output voltage to the altered set point to produce a matched generator output voltage;transmitting, by the bus power control unit in communication with the generator control unit, a command to close a contactor ; and providing the matched generator output voltage to the specific electrical load based on a closing operation of the contactor, the closing operation being in accordance with a delay between receiving the command and an actual closing and mitigating the inrush current.
A device for reproducing display information suitable for integration into a wrist watch comprising a basic watch movement having at least a plate and/or a bridge (3.3), wherein the device consists of a watch module that comprises at least a base plate (1.2) and/or a module bridge (1.3) and that is or is not in direct cooperation with the basic watch movement and allows to implement at least one additional function of the watch, or consists of the basic watch movement , the device comprising at least one opening (1.1, 3.2), in each of which an associated image guide is mounted, the device further comprising for each of these image guides means for fastening the image guide in the associated opening (1.1), such that the image guide allows display information displayed on a representation plane to be reproduced on a display plane, the means for fastening the image guide in the associated opening (1.1) being implemented by fastening clamps and/or fastening sockets , said clamps and/or sockets being mounted on said plate and/or bridge (3.3) of the basic watch movement and/or on said base plate (1.2) and/or module bridge (1.3) of the watch module .
Locking device for a switch cabinet , with a lock door and a secondary door , wherein the secondary door , on a vertical outer edge opposite its hinge side, has a U-profile formed on a door leaf of the secondary door with a receptacle for a lock mechanism of the lock door , which receptacle is offset back relative to the door leaf and which is open towards the door leaf , characterized in that on an outer free profile side of the U-profile which is an outer end face of the secondary door, a swivelling lever of a lock of the secondary door is pivotably mounted about an axis of rotation (x) between an open position and a locking position.
A spacecraft for removing space debris (SD), the spacecraft comprising: a satellite bus ; a shield member foldable on an outer side face of the satellite bus and configured to be disposed facing towards space debris (SD) to reduce a movement speed of the space debris (SD); and a support member configured to support the shield member with respect to the satellite bus , wherein the shield member comprises: a central panel configured to overlap one face of the satellite bus ; a plurality of first panels connected to peripheral sides of the central panel and radially extended; and a plurality of second panels connected between the first panels , wherein the satellite bus is provided in a form of a polygonal column, wherein the first panels correspond in number to side faces of the satellite bus , and are configured to individually overlap an associated side face of the satellite bus , and the second panels overlap the first panels when the shield member is folded, characterized in that the spacecraft comprises a detection member configured to detect the space debris (SD), wherein the detection member is configured to measure the movement speed of the space debris (SD) or a distance between the space debris (SD) and the shield member . a satellite bus ; a shield member foldable on an outer side face of the satellite bus and configured to be disposed facing towards space debris (SD) to reduce a movement speed of the space debris (SD); and a support member configured to support the shield member with respect to the satellite bus , wherein the shield member comprises: a central panel configured to overlap one face of the satellite bus ; a plurality of first panels connected to peripheral sides of the central panel and radially extended; and a plurality of second panels connected between the first panels , wherein the satellite bus is provided in a form of a polygonal column, wherein a central panel configured to overlap one face of the satellite bus ; a plurality of first panels connected to peripheral sides of the central panel and radially extended; and a plurality of second panels connected between the first panels , wherein the satellite bus is provided in a form of a polygonal column, wherein the first panels correspond in number to side faces of the satellite bus , and are configured to individually overlap an associated side face of the satellite bus , and the second panels overlap the first panels when the shield member is folded, characterized in that the spacecraft comprises a detection member configured to detect the space debris (SD), wherein the detection member is configured to measure the movement speed of the space debris (SD) or a distance between the space debris (SD) and the shield member .