mhurhangee/patent-ind-claim-en huggingface dataset:
A combination of a covering device of an axle box , an axle box and an axle, the covering device thereof being adapted and configured to be coupled to the axle box so as to define an inner compartment between the axle box and the covering device, wherein the covering device comprises an electric generator housed in the inner compartment and adapted to produce electric power by converting part of the rotational kinetic energy of the axle , wherein: - the electric generator comprises a stator having a stator winding wound on a metal sheet and wherein the covering device comprises a case and the stator is attached to the case ; - the electric generator comprises a rotor attached to an end portion of the axle adapted to rotate integrally with the axle along the rotation axis of the axle ; characterized in that : - the rotor comprises a first portion and a second portion between which the stator is axially interposed; - the case comprises a first portion and a second portion axially overlapping each other and coupled to each other, and wherein the first portion of the case is interposed between the axle box and the second portion of the case and wherein the stator is attached to the first portion of the case . - the electric generator comprises a stator having a stator winding wound on a metal sheet and wherein the covering device comprises a case and the stator is attached to the case ; - the electric generator comprises a rotor attached to an end portion of the axle adapted to rotate integrally with the axle along the rotation axis of the axle ; - the rotor comprises a first portion and a second portion between which the stator is axially interposed; - the case comprises a first portion and a second portion axially overlapping each other and coupled to each other, and wherein the first portion of the case is interposed between the axle box and the second portion of the case and wherein the stator is attached to the first portion of the case .
A locking arrangement for axial locking of a bucket to a rotor disk of a turbine, comprising: a depressed portion disposed on a surface formed by a combination of an end portion of a male dovetail extending from the bucket and an outer side of a seating groove of a female dovetail extending from an outer circumferential surface of the rotor disk ; and a locking member configured to be placed between the male dovetail and the seating groove of the female dovetail and to engage the depressed portion to prevent the bucket mounted on the rotor disk from being separated in the axial direction, wherein the locking member includes: a center beam configured to be placed between the end portion of the male dovetail and the seating groove of the female dovetail in the axial direction of the rotor disk ; and a locking plate disposed on an end of the center beam to be positioned in the depressed portion , wherein the locking plate is positioned in the depressed portion when the center beam is positioned in the seating groove ; and wherein a portion of the locking plate is flat such that the flat portion is disposable towards a radially outward direction of the rotor disk before the male dovetail is inserted into the female dovetail such that the male dovetail is insertable into the female dovetail in the axial direction, and is rotatable within the depression portion to be disposed towards a radially inward direction of the rotor disk after the male dovetail is inserted into the female dovetail . a depressed portion disposed on a surface formed by a combination of an end portion of a male dovetail extending from the bucket and an outer side of a seating groove of a female dovetail extending from an outer circumferential surface of the rotor disk ; and a locking member configured to be placed between the male dovetail and the seating groove of the female dovetail and to engage the depressed portion to prevent the bucket mounted on the rotor disk from being separated in the axial direction, a center beam configured to be placed between the end portion of the male dovetail and the seating groove of the female dovetail in the axial direction of the rotor disk ; and a locking plate disposed on an end of the center beam to be positioned in the depressed portion , wherein the locking plate is positioned in the depressed portion when the center beam is positioned in the seating groove ; and wherein a portion of the locking plate is flat such that the flat portion is disposable towards a radially outward direction of the rotor disk before the male dovetail is inserted into the female dovetail such that the male dovetail is insertable into the female dovetail in the axial direction, and is rotatable within the depression portion to be disposed towards a radially inward direction of the rotor disk after the male dovetail is inserted into the female dovetail .
An industrial transmitter assembly comprising: an industrial transmitter including electronics contained in a housing ; and a transmitter mount configured to attach the housing to a structure , the transmitter mount comprising: a stem member having a first end connected to the housing , and a second end including one of a flange oriented substantially perpendicularly to a longitudinal axis of the stem member and a first twist-lock connector ; an adaptor configured for attachment to the structure and comprising a base member including respectively either a slot configured to receive the flange , or a second twist-lock connector configured to attach to the first twist-lock connector ; and a locking member configured to secure the second end of the stem member to the base member . an industrial transmitter including electronics contained in a housing ; and a transmitter mount configured to attach the housing to a structure , the transmitter mount comprising: a stem member having a first end connected to the housing , and a second end including one of a flange oriented substantially perpendicularly to a longitudinal axis of the stem member and a first twist-lock connector ; an adaptor configured for attachment to the structure and comprising a base member including respectively either a slot configured to receive the flange , or a second twist-lock connector configured to attach to the first twist-lock connector ; and a locking member configured to secure the second end of the stem member to the base member . a stem member having a first end connected to the housing , and a second end including one of a flange oriented substantially perpendicularly to a longitudinal axis of the stem member and a first twist-lock connector ; an adaptor configured for attachment to the structure and comprising a base member including respectively either a slot configured to receive the flange , or a second twist-lock connector configured to attach to the first twist-lock connector ; and a locking member configured to secure the second end of the stem member to the base member .
Method for joining edges and/or surfaces of a profile in a profiling installation for longitudinally forming a virtually endless material strip or profile or a plate into an at least partially closed profile shape, wherein the material strip or profile or the plate is formed in the profiling installation by means of a plurality of roll forming tools into a profile which is closed per se or is partially closed, and said profile is secured in a joining zone of the profiling installation by a joining method, such as, in particular, welding, brazing, adhesive bonding or folding, during a longitudinal pass of the profile , with a longitudinally running joining seam being formed, characterized in that the profile passes in the joining zone through a planar joining arrangement in order to feed the profile in a controlled manner to a joining point and to stabilize said profile in particular at and/or downstream of the joining point , and/or to ensure that the profile is dimensionally stable during and after joining, wherein forces or magnitudes of force components which act on the profile from at least one subsection of the planar joining arrangement are detected in the joining zone , and wherein the planar joining arrangement consists of a number of joining rollers , around which a flexible belt, a link belt, a link chain or a chain-like structure is looped, in particular as in the case of a conveyor belt, in order to make contact with the profile by way of a planar contact region which moves together with the profile and distributes the holding pressure in as planar a manner as possible to the profile . wherein the material strip or profile or the plate is formed in the profiling installation by means of a plurality of roll forming tools into a profile which is closed per se or is partially closed, and said profile is secured in a joining zone of the profiling installation by a joining method, such as, in particular, welding, brazing, adhesive bonding or folding, during a longitudinal pass of the profile , with a longitudinally running joining seam being formed, characterized in that the profile passes in the joining zone through a planar joining arrangement in order to feed the profile in a controlled manner to a joining point and to stabilize said profile in particular at and/or downstream of the joining point , and/or to ensure that the profile is dimensionally stable during and after joining, wherein forces or magnitudes of force components which act on the profile from at least one subsection of the planar joining arrangement are detected in the joining zone , and wherein the planar joining arrangement consists of a number of joining rollers , around which a flexible belt, a link belt, a link chain or a chain-like structure is looped, in particular as in the case of a conveyor belt, in order to make contact with the profile by way of a planar contact region which moves together with the profile and distributes the holding pressure in as planar a manner as possible to the profile .
A method of brake actuator operation sensor error compensation comprising: polling , by an aircraft electro-mechanical brake actuator controller, a plurality of inputs comprising at least one of: a plurality of load cell forces; a plurality of current sensor currents; and a plurality of position sensor positions; performing , by the controller, a conformance test in response to the polling; rejecting , by the controller, non-conforming inputs in response to the conformance test; and outputting , by the controller, a compensation signal to a command force controller ; wherein the command force controller comprises the aircraft electro-mechanical brake actuator controller; and wherein the conformance test comprises: performing a least squares fit of the plurality of inputs whereby non-conforming inputs are identified for rejection. a plurality of load cell forces; a plurality of current sensor currents; and a plurality of position sensor positions; performing , by the controller, a conformance test in response to the polling; rejecting , by the controller, non-conforming inputs in response to the conformance test; and outputting , by the controller, a compensation signal to a command force controller ; wherein the command force controller comprises the aircraft electro-mechanical brake actuator controller; and wherein the conformance test comprises: performing a least squares fit of the plurality of inputs whereby non-conforming inputs are identified for rejection.
A method of bringing a first member including a first substrate and a first projection projecting from the first substrate into contact with a second member including a second substrate and a second projection projecting from the second substrate to be joined to each other, wherein the first member and the second member each have a thickness that varies depending on parts at a joint position (J), and the method being characterized by : a groove formation step of removing part of the first projection opposed to the second projection and part of the second projection opposed to the first projection to form a groove region (R g ) between the first projection and the second projection , wherein a first substrate end surface and a second substrate end surface are brought into contact with each other after the execution of the groove formation step; a first welding step of joining the first member and the second member to each other by butt welding after the groove formation step; and a second welding step of filling the groove region (R g ) by buildup welding after the first welding step, wherein the groove formation step forms a first inclined surface in the first projection facing the groove region (R g ) to be gradually distant from the joint position (J) joined with the second projection as the first inclined surface is closer to an outer surface of the first projection , and forms a second inclined surface in the second projection facing the groove region (R g ) to be gradually distant from the joint position (J) joined with the first projection as the second inclined surface is closer to an outer surface of the second projection . a groove formation step of removing part of the first projection opposed to the second projection and part of the second projection opposed to the first projection to form a groove region (R g ) between the first projection and the second projection , wherein a first substrate end surface and a second substrate end surface are brought into contact with each other after the execution of the groove formation step; a first welding step of joining the first member and the second member to each other by butt welding after the groove formation step; and a second welding step of filling the groove region (R g ) by buildup welding after the first welding step, wherein the groove formation step forms a first inclined surface in the first projection facing the groove region (R g ) to be gradually distant from the joint position (J) joined with the second projection as the first inclined surface is closer to an outer surface of the first projection , and forms a second inclined surface in the second projection facing the groove region (R g ) to be gradually distant from the joint position (J) joined with the first projection as the second inclined surface is closer to an outer surface of the second projection .
Method for manufacturing a part made of composite material comprising a reinforcement made up of fibres impregnated with a resin matrix, the method comprising the following successive steps: - flat laying and covering dry fibres on a planar surface of a laying tool ; - infusing flat dry fibres with the resin; - forming the dry fibres infused with the resin on a counter-mould; - first polymerization at a first polymerization temperature (T1), the first polymerization being configured to obtain 20% to 30% hardening of the resin in order to obtain an intermediate reinforcement, the first polymerization being subsequent to the step of infusing and of forming ; - demoulding and machining the intermediate reinforcement; - second polymerization of the machined intermediate reinforcement at a second polymerization temperature (T2), the value of the second temperature (T2) being greater than the value of the first temperature (T1). - flat laying and covering dry fibres on a planar surface of a laying tool ; - infusing flat dry fibres with the resin; - forming the dry fibres infused with the resin on a counter-mould; - first polymerization at a first polymerization temperature (T1), the first polymerization being configured to obtain 20% to 30% hardening of the resin in order to obtain an intermediate reinforcement, the first polymerization being subsequent to the step of infusing and of forming ; - demoulding and machining the intermediate reinforcement; - second polymerization of the machined intermediate reinforcement at a second polymerization temperature (T2), the value of the second temperature (T2) being greater than the value of the first temperature (T1).
A chimeric protein which comprises a multi-spanning transmembrane protein fused to a FAS endodomain, wherein the multi-spanning transmembrane protein binds an extracellular ligand, leading to activation of the FAS endodomain and wherein the multi-spanning transmembrane protein comprises CD20 or a truncated version thereof lacking an amino-terminal endodomain or a carboxy-terminal endodomain.
A motor home with a wet room , including a toilet , arranged in the vehicle interior, and a closable access arranged in the transverse direction of the vehicle, which comprises a closing device , such as a door and/or a stretchable tarpaulin and/or a sliding door and can be brought into two closed positions, wherein in both closed positions the wet room is of a different size, characterised in that the motor home can be made into an configuration having an enlarged living area comprising at least four seats and a table , wherein the table can be brought into a position in which it can be optimally reached from all four seats and wherein the wet room is not accessible when the table is in this position.
A reciprocating compressor comprising: a shell having an inner space ; at least one stator disposed in the inner space of the shell , and provided with a stator core having at least one air gap , and a coil fixed to the stator core and generating magnetic energy in response to power applied; a mover provided with a magnet and reciprocating with respect to the stator ; a piston mechanically connected with the mover , and reciprocating by the magnetic energy generated in the stator and interaction with the magnet ; a cylinder having the piston inserted therein and forming a compression space ; a suction valve opening and closing a suction side of the compression space; a discharge valve opening and closing a discharge side of the compression space; and an electromagnetic resonance spring formed between the stator core and the magnet by a restoring force generated by the magnetic energy, characterized in that an electromagnetic center of the magnet is located more eccentric toward the compression space than an electromagnetic center of the stator. a shell having an inner space ; at least one stator disposed in the inner space of the shell , and provided with a stator core having at least one air gap , and a coil fixed to the stator core and generating magnetic energy in response to power applied; a mover provided with a magnet and reciprocating with respect to the stator ; a piston mechanically connected with the mover , and reciprocating by the magnetic energy generated in the stator and interaction with the magnet ; a cylinder having the piston inserted therein and forming a compression space ; a suction valve opening and closing a suction side of the compression space; a discharge valve opening and closing a discharge side of the compression space; and an electromagnetic resonance spring formed between the stator core and the magnet by a restoring force generated by the magnetic energy, characterized in that an electromagnetic center of the magnet is located more eccentric toward the compression space than an electromagnetic center of the stator.
A method for displaying information of a battery pack based on a mobile terminal, the battery pack being used to supply electric energy to an electric tool, wherein the method comprises: establishing (S10) wireless communication with the battery pack; determining by the battery pack that a distance from the mobile terminal according to a received wireless signal strength or a time of flight is less than or equal to a first threshold; acquiring (S20) status information of the battery pack; and displaying (S30) the status information on the mobile terminal according to the acquired status information. establishing (S10) wireless communication with the battery pack; determining by the battery pack that a distance from the mobile terminal according to a received wireless signal strength or a time of flight is less than or equal to a first threshold; acquiring (S20) status information of the battery pack; and displaying (S30) the status information on the mobile terminal according to the acquired status information.
A method for wireless communication, the method comprising: determining , at a first wireless communication device , that low-latency data more delay intolerant than data of an on-going data session is available; transmitting , from the first wireless communication device, the low-latency data during a first symbol period of a first transmission time interval, TTI, instead of at least one of a pilot symbol or a control symbol that is scheduled to be transmitted during the first symbol period; transmitting , from the first wireless communication device, the at least one pilot symbol or control symbol during a second symbol period of the first TTI instead of a data symbol of the on-going data session that is scheduled to be transmitted during the second symbol period, wherein the second symbol is transmitted after the first symbol; and transmitting a first subset of one or more code blocks of the data symbol during the second symbol period of the first TTI. determining , at a first wireless communication device , that low-latency data more delay intolerant than data of an on-going data session is available; transmitting , from the first wireless communication device, the low-latency data during a first symbol period of a first transmission time interval, TTI, instead of at least one of a pilot symbol or a control symbol that is scheduled to be transmitted during the first symbol period; transmitting , from the first wireless communication device, the at least one pilot symbol or control symbol during a second symbol period of the first TTI instead of a data symbol of the on-going data session that is scheduled to be transmitted during the second symbol period, wherein the second symbol is transmitted after the first symbol; and transmitting a first subset of one or more code blocks of the data symbol during the second symbol period of the first TTI.
A vacuum pump, in particular a turbomolecular pump, comprising a housing; and a rotor which is rotatably supported in the housing and which can be driven to make a rotation which brings about a conveying of a process gas from an inlet to an outlet of the vacuum pump, wherein the rotor is rotatably supported in the housing at least at one side by a rolling element bearing , and wherein an actuator is provided by means of which a stiffness and/or a damping effect of the rolling element bearing can be varied, characterized in that the actuator comprises an electroactive and/or magnetoactive polymer; and in that the actuator has a length of at least 1 mm in an actuation direction. a housing; and a rotor which is rotatably supported in the housing and which can be driven to make a rotation which brings about a conveying of a process gas from an inlet to an outlet of the vacuum pump, wherein the rotor is rotatably supported in the housing at least at one side by a rolling element bearing , and wherein an actuator is provided by means of which a stiffness and/or a damping effect of the rolling element bearing can be varied, characterized in that the actuator comprises an electroactive and/or magnetoactive polymer; and in that the actuator has a length of at least 1 mm in an actuation direction.