mhurhangee/patent-ind-claim-en huggingface dataset:
Connecting element for fuel injection systems for connecting a fuel injection valve to a fuel-conducting component , wherein a main body is provided in which there is provided a receiving space for a fuel connector of the fuel injection valve , wherein the fuel connector , which is arrangeable at least partially in the receiving space , is supportable at least indirectly on the main body , wherein the fuel connector is supportable elastically on the main body at least in a radial direction , wherein at least one decoupling element is provided which, in the assembled state, is arranged between the fuel connector and the main body , and in that the fuel connector is supportable elastically on the main body at least in the radial direction via the decoupling element , wherein the main body has an inner side , in that the decoupling element has an outer surface , and in that the decoupling element lies areally with its outer surface against a contact surface of the inner side of the main body , characterized in that the decoupling element has an axial extent greater than the radial material thickness of the decoupling element in cross section, such that contact occurs over a large area, wherein the fuel connector has a radial ring and an elastic deformation of the decoupling element in a radial direction is limited by a mechanical abutment of the ring of the fuel connector against the main body , and the ring also serves as an axial abutment for the decoupling element .
Radio frequency apparatus, said apparatus including a first transmission pathway for transmitting one or more radio frequency signals at a first transmit frequency band; a first receive pathway for receiving one or more radio frequency signals at a first receive frequency band; and a transmit/receive pathway for transmitting and receiving one or more radio frequency signals at a second transmit and/or receive frequency band; or a second transmission pathway for transmitting one or more radio frequency signals at a second transmit frequency band; and a second receive pathway for receiving one or more radio frequency signals at a second receive frequency band; said apparatus having a first antenna port connectable directly or indirectly to an antenna in use, said first antenna port connected to the first transmission pathway , the first receive pathway and the transmit/receive pathway and the second transmission pathway and the second receive pathway ; characterised in that : for said first antenna port said apparatus has at least two transceiver device ports associated with the same, the at least two transceiver device ports connectable directly or indirectly to one or more transceiver devices in use; wherein one of the transceiver device ports is connected to the first transmission and receive pathways , and another one of the transceiver device ports is connected to the transmit/receive pathway and/or the second transmission pathway and the second receive pathway ; and wherein amplification means are provided in or associated with at least one of the receive pathways for amplifying the one or more received radio frequency signals received at the first antenna port . for said first antenna port said apparatus has at least two transceiver device ports associated with the same, the at least two transceiver device ports connectable directly or indirectly to one or more transceiver devices in use; wherein one of the transceiver device ports is connected to the first transmission and receive pathways , and another one of the transceiver device ports is connected to the transmit/receive pathway and/or the second transmission pathway and the second receive pathway ; and wherein amplification means are provided in or associated with at least one of the receive pathways for amplifying the one or more received radio frequency signals received at the first antenna port .
Method for producing a stator with a winding with offset air-core coils , comprising: - winding air-core coils with the aid of a winding tool; - arranging the air-core coils in retaining grooves (3; 12; 46) of a production tool in such a way that, for each air-core coil respectively, a first section on one side of the air-core coil is arranged in a retaining groove of a first arrangement of retaining grooves on a first tool part and a second section on an opposite side of the air-core coil is arranged in a retaining groove (12; 46) of a second arrangement of retaining grooves (12; 46) on a second tool part (11; 44); - producing a respective offset for the air-core coils , in that the first tool part and the second tool part are displaced relative to each other; - displacing the air-core coils with offset into the retaining grooves of the first tool part in such a way that, for the air-core coils with the offset , the first and the second sections are respectively arranged in different retaining grooves of the first tool part ; - arranging a stator core with core slots in such a way that the core slots are respectively arranged opposite a retaining groove of the first tool part ; - displacing the air-core coils with offset from the retaining grooves of the first tool part into the respectively assigned core slots ; and - removing the stator core with the air-core coils with offset arranged in the core slots . - winding air-core coils with the aid of a winding tool; - arranging the air-core coils in retaining grooves (3; 12; 46) of a production tool in such a way that, for each air-core coil respectively, a first section on one side of the air-core coil is arranged in a retaining groove of a first arrangement of retaining grooves on a first tool part and a second section on an opposite side of the air-core coil is arranged in a retaining groove (12; 46) of a second arrangement of retaining grooves (12; 46) on a second tool part (11; 44); - producing a respective offset for the air-core coils , in that the first tool part and the second tool part are displaced relative to each other; - displacing the air-core coils with offset into the retaining grooves of the first tool part in such a way that, for the air-core coils with the offset , the first and the second sections are respectively arranged in different retaining grooves of the first tool part ; - arranging a stator core with core slots in such a way that the core slots are respectively arranged opposite a retaining groove of the first tool part ; - displacing the air-core coils with offset from the retaining grooves of the first tool part into the respectively assigned core slots ; and - removing the stator core with the air-core coils with offset arranged in the core slots .
Activity drone comprising: - an aerial vehicle provided with at least one rotor participating in lift and/or propulsion of the said drone , - an activity system comprising: o a structure , o a computer o at least one working camera which is fixed relative to the said aerial vehicle and allows viewing of a working zone, ∘ a distribution device for successively carrying out a plurality of tasks on the said working zone, the said distribution system comprising a plurality of compartments containing at least one object , at least one task being assigned to each compartment , and o a rotary motor allowing rotation of the said distribution device relative to the said aerial vehicle so that the said compartment intended to be used in order to carry out a task lies at a predetermined position of use relative to the said working zone, - a fixing device for fixing the said activity system to the said aerial vehicle , characterised in that the said at least one object contained in a plurality of compartments is a fabric impregnated with at least one component intended to react with a specific gas so as to analyse the air and detect the possible presence of a specific gas. - an aerial vehicle provided with at least one rotor participating in lift and/or propulsion of the said drone , - an activity system comprising: o a structure , o a computer o at least one working camera which is fixed relative to the said aerial vehicle and allows viewing of a working zone, ∘ a distribution device for successively carrying out a plurality of tasks on the said working zone, the said distribution system comprising a plurality of compartments containing at least one object , at least one task being assigned to each compartment , and o a rotary motor allowing rotation of the said distribution device relative to the said aerial vehicle so that the said compartment intended to be used in order to carry out a task lies at a predetermined position of use relative to the said working zone, o a structure , o a computer o at least one working camera which is fixed relative to the said aerial vehicle and allows viewing of a working zone, ∘ a distribution device for successively carrying out a plurality of tasks on the said working zone, the said distribution system comprising a plurality of compartments containing at least one object , at least one task being assigned to each compartment , and o a rotary motor allowing rotation of the said distribution device relative to the said aerial vehicle so that the said compartment intended to be used in order to carry out a task lies at a predetermined position of use relative to the said working zone, - a fixing device for fixing the said activity system to the said aerial vehicle , characterised in that the said at least one object contained in a plurality of compartments is a fabric impregnated with at least one component intended to react with a specific gas so as to analyse the air and detect the possible presence of a specific gas.
A rail system for arranging an X-ray source with respect to an X-ray detector and an object to be imaged, comprising: - a first slide rail adapted to support an X-ray source , - a second slide rail adapted to support an X-ray detector , - a guide rail adapted to guide the first and second slide rails , wherein the first and second slide rails are each adapted to be slidably arranged on the guide rail relative to each other for positioning the X-ray source with respect to the X-ray detector , the first and second slide rails being detachably fixable to the guide rail for fixing a position of the X-ray source with respect to the X-ray detector , and - a carrier adapted to carry the object to be imaged by means of X-rays from the X-ray source , the carrier being further adapted to be slidably arranged on the first slide rail or on the second slide rail for positioning the carrier between the X-ray source and the X-ray detector , wherein the carrier is fixable to the respective slide rail to fix a position of the carrier with respect to the X-ray source and the X-ray detector . - a first slide rail adapted to support an X-ray source , - a second slide rail adapted to support an X-ray detector , - a guide rail adapted to guide the first and second slide rails , wherein the first and second slide rails are each adapted to be slidably arranged on the guide rail relative to each other for positioning the X-ray source with respect to the X-ray detector , the first and second slide rails being detachably fixable to the guide rail for fixing a position of the X-ray source with respect to the X-ray detector , and - a carrier adapted to carry the object to be imaged by means of X-rays from the X-ray source , the carrier being further adapted to be slidably arranged on the first slide rail or on the second slide rail for positioning the carrier between the X-ray source and the X-ray detector , wherein the carrier is fixable to the respective slide rail to fix a position of the carrier with respect to the X-ray source and the X-ray detector .
A turbine airfoil comprising: a suction sidewall and a pressure sidewall , each sidewall extending spanwise from an airfoil base and extending chordwise between a leading edge and a trailing edge ; a tip wall extending chordwise from the leading edge to the trailing edge and joining respective outer spanwise ends of the suction and pressure sidewalls ; and a plurality of tip leakage control channels distributed across at least a chordwise portion of the tip wall between the airfoil leading edge and the airfoil trailing edge , each channel recessed into an outer surface of the tip wall , an inlet of each tip leakage control channel beginning proximate a junction of the airfoil pressure sidewall and the tip wall , an outlet of each tip leakage control channel terminating at a recessed portion of a junction of the tip wall and the suction sidewall , a portion of each tip leakage control channel is curved toward the trailing edge from the inlet to the outlet ; and characterised in that the outer surface includes a tip rib extending chordwise along at least a portion of a pressure side of the tip wall between the airfoil leading edge and airfoil trailing edge ; and in that the channel inlets are aligned with tip rib along a chordwise path at the pressure side of the tip wall between the airfoil leading edge and airfoil trailing edge . a suction sidewall and a pressure sidewall , each sidewall extending spanwise from an airfoil base and extending chordwise between a leading edge and a trailing edge ; a tip wall extending chordwise from the leading edge to the trailing edge and joining respective outer spanwise ends of the suction and pressure sidewalls ; and a plurality of tip leakage control channels distributed across at least a chordwise portion of the tip wall between the airfoil leading edge and the airfoil trailing edge , each channel recessed into an outer surface of the tip wall , an inlet of each tip leakage control channel beginning proximate a junction of the airfoil pressure sidewall and the tip wall , an outlet of each tip leakage control channel terminating at a recessed portion of a junction of the tip wall and the suction sidewall , a portion of each tip leakage control channel is curved toward the trailing edge from the inlet to the outlet ; and characterised in that the outer surface includes a tip rib extending chordwise along at least a portion of a pressure side of the tip wall between the airfoil leading edge and airfoil trailing edge ; and in that the channel inlets are aligned with tip rib along a chordwise path at the pressure side of the tip wall between the airfoil leading edge and airfoil trailing edge .
An indication method, wherein the method comprises: generating (S101) at least two pieces of indication information, wherein each piece of indication information is used to indicate a maximum value of an RI that a network device of at least two network devices associated with the indication information allows a terminal to report, and the at least two network devices associated with the at least two pieces of indication information cooperate to provide a service for the terminal, wherein a sum of maximum values of RIs that the at least two network devices allow the terminal to report is less than or equal to a maximum quantity of transmission layers that is supported by the terminal; and sending (S102) the at least two pieces of indication information; wherein the generating at least two pieces of indication information comprises: setting the maximum value of the RI of each network device based on an uneven distribution rule according to which when a first one of the at least two network devices receives a sounding reference signal at a higher power than a second one of the at least two network devices receives a sounding reference signal, the maximum value of the RI associated with the first one of the at least two network devices is set to be higher than the maximum value of the RI associated with a second one of the at least two network devices. generating (S101) at least two pieces of indication information, wherein each piece of indication information is used to indicate a maximum value of an RI that a network device of at least two network devices associated with the indication information allows a terminal to report, and the at least two network devices associated with the at least two pieces of indication information cooperate to provide a service for the terminal, wherein a sum of maximum values of RIs that the at least two network devices allow the terminal to report is less than or equal to a maximum quantity of transmission layers that is supported by the terminal; and sending (S102) the at least two pieces of indication information; wherein the generating at least two pieces of indication information comprises: setting the maximum value of the RI of each network device based on an uneven distribution rule according to which when a first one of the at least two network devices receives a sounding reference signal at a higher power than a second one of the at least two network devices receives a sounding reference signal, the maximum value of the RI associated with the first one of the at least two network devices is set to be higher than the maximum value of the RI associated with a second one of the at least two network devices.
A packaged structure, comprising: a substrate having a first surface and a second surface opposite to each other, the first surface having at least one strip-shaped groove having two ends extending to edges of the substrate and open to exterior, a depth of the groove being smaller than a thickness of the substrate ; a chip fastened onto the first surface of the substrate in a flipping manner by using solder bumps and electrically connected to the substrate through the solder bumps, at least a portion of the groove located within a projection of the chip on the substrate ; a bottom filling layer filling a gap between the chip and the first surface of the substrate ; and a plastic packaging layer , covering the bottom filling layer and wrapping the chip ; wherein a width of the groove is smaller than a fillable width of the material of the bottom filling layer in a liquid state, and a top of the groove is sealed by the bottom filling layer , and the groove has a continuous gas path formed in the groove . a substrate having a first surface and a second surface opposite to each other, the first surface having at least one strip-shaped groove having two ends extending to edges of the substrate and open to exterior, a depth of the groove being smaller than a thickness of the substrate ; a chip fastened onto the first surface of the substrate in a flipping manner by using solder bumps and electrically connected to the substrate through the solder bumps, at least a portion of the groove located within a projection of the chip on the substrate ; a bottom filling layer filling a gap between the chip and the first surface of the substrate ; and a plastic packaging layer , covering the bottom filling layer and wrapping the chip ;
A local feature descriptor extracting apparatus comprising: a feature point detecting unit configured to detect a plurality of feature points in an image and output feature point information that is information regarding each feature point; a feature point selecting unit configured to select a prescribed number of feature points in an order of importance from the plurality of detected feature points, based on the feature point information; a local region acquiring unit configured to acquire a local region corresponding to each selected feature point; a subregion dividing unit configured to divide each local region into a plurality of subregions; a subregion feature vector generating unit configured to generate a gradient direction histogram of a plurality of dimensions for each subregion in each local region; and a dimension selecting unit configured to select dimensions from the gradient direction histogram for each subregion so that at least one gradient direction differs between adjacent subregions, based on a positional relationship between subregions in each local region and output elements of the selected dimensions as a feature descriptor of the local region. a feature point detecting unit configured to detect a plurality of feature points in an image and output feature point information that is information regarding each feature point; a feature point selecting unit configured to select a prescribed number of feature points in an order of importance from the plurality of detected feature points, based on the feature point information; a local region acquiring unit configured to acquire a local region corresponding to each selected feature point; a subregion dividing unit configured to divide each local region into a plurality of subregions; a subregion feature vector generating unit configured to generate a gradient direction histogram of a plurality of dimensions for each subregion in each local region; and a dimension selecting unit configured to select dimensions from the gradient direction histogram for each subregion so that at least one gradient direction differs between adjacent subregions, based on a positional relationship between subregions in each local region and output elements of the selected dimensions as a feature descriptor of the local region.
A computing environment system for monitoring aircraft engines, said system being connected to a cluster of servers, characterised in that said system includes: - an application interface configured to receive user codes deployed in the cluster of servers for distributed operation on time data of a fleet of aircraft engines and including specifications of input data to be processed in parallel and output data comprising context and health indicators, said user codes specifying calculation of a set of indicators representative of the state of health of an aircraft engine for deployment on a fleet of aircraft engines, - an extraction module configured to extract said indicators by deploying calculations in parallel in the cluster of servers on time flight data from the fleet of aircraft engines and stored in a database distributed on said cluster of servers , - a learning module configured to use said indicators extracted by the extraction module to build in an unsupervised manner from said indicators a monitoring model representative of the indicators by implementing predetermined learning functions, said monitoring model being adapted to identify trends or to classify aircraft engines to determine which are to be maintained as a priority. - an application interface configured to receive user codes deployed in the cluster of servers for distributed operation on time data of a fleet of aircraft engines and including specifications of input data to be processed in parallel and output data comprising context and health indicators, said user codes specifying calculation of a set of indicators representative of the state of health of an aircraft engine for deployment on a fleet of aircraft engines, - an extraction module configured to extract said indicators by deploying calculations in parallel in the cluster of servers on time flight data from the fleet of aircraft engines and stored in a database distributed on said cluster of servers , - a learning module configured to use said indicators extracted by the extraction module to build in an unsupervised manner from said indicators a monitoring model representative of the indicators by implementing predetermined learning functions, said monitoring model being adapted to identify trends or to classify aircraft engines to determine which are to be maintained as a priority.