mhurhangee/ep-ind-claims huggingface dataset:
A nacelle for an aircraft engine, comprising: - a fixed front frame, - a thrust reverser cowl slidably mounted relative to said front frame between a direct jet position and a reverse jet position, - an adaptive nozzle (13, 13a, 13b) disposed in the downstream extension of this thrust reverser cowl, - thrust reverser cylinders, interposed between said front frame and said thrust reverser cowl, - adaptive nozzle cylinders (23, 23a, 23b), interposed between said thrust reverser cowl and said adaptive nozzle (13, 13a, 13b), - drive shafts (35a, 35b), mounted on said front frame, - transmission shafts (27a, 27b) extending along said thrust reverser cowl up to said adaptive nozzle cylinders (23, 23a, 23b), and - means (33a, 33b) for mechanically coupling said transmission shafts (27a, 27b) to said drive shafts (35a, 35b), adapted to ensure the torque transmission from said drive shafts (35a, 35b) to said transmission shafts (27a, 27b) when said cowl is in the direct jet position, and to decouple the transmission shafts (27a, 27b) from the drive shafts (35a, 35b) when the cowl slides towards its reverse jet position, characterized in that the nacelle comprises - means (47, 49) for locking the rotation of said transmission shafts (27a, 27b) before the complete decoupling of these transmission shafts (27a, 27b) from their respective drive shafts (35a, 35b), and when this decoupling is achieved. - a fixed front frame, - a thrust reverser cowl slidably mounted relative to said front frame between a direct jet position and a reverse jet position, - an adaptive nozzle (13, 13a, 13b) disposed in the downstream extension of this thrust reverser cowl, - thrust reverser cylinders, interposed between said front frame and said thrust reverser cowl, - adaptive nozzle cylinders (23, 23a, 23b), interposed between said thrust reverser cowl and said adaptive nozzle (13, 13a, 13b), - drive shafts (35a, 35b), mounted on said front frame, - transmission shafts (27a, 27b) extending along said thrust reverser cowl up to said adaptive nozzle cylinders (23, 23a, 23b), and - means (33a, 33b) for mechanically coupling said transmission shafts (27a, 27b) to said drive shafts (35a, 35b), adapted to ensure the torque transmission from said drive shafts (35a, 35b) to said transmission shafts (27a, 27b) when said cowl is in the direct jet position, and to decouple the transmission shafts (27a, 27b) from the drive shafts (35a, 35b) when the cowl slides towards its reverse jet position, characterized in that the nacelle comprises - means (47, 49) for locking the rotation of said transmission shafts (27a, 27b) before the complete decoupling of these transmission shafts (27a, 27b) from their respective drive shafts (35a, 35b), and when this decoupling is achieved.
A head maintenance device for use in a liquid discharge apparatus having a conveyor to convey a medium in one direction, the head maintenance device comprising: a housing; a wiper in the housing to wipe a nozzle face of a liquid discharge head of the liquid discharge apparatus; and a cap in the housing to cover nozzles arrayed on the nozzle face of the liquid discharge head in the one direction, characterized in that the housing is detachably attachable to the conveyor. a housing; a wiper in the housing to wipe a nozzle face of a liquid discharge head of the liquid discharge apparatus; and a cap in the housing to cover nozzles arrayed on the nozzle face of the liquid discharge head in the one direction, characterized in that the housing is detachably attachable to the conveyor.
A fluid latent heat absorption electric induction heater for raising the temperature of a fluid supplied to a fluid-driven turbine in a turbine-driven electric power generation system, the fluid latent heat absorption electric induction heater comprising: a containment vessel; at least one susceptor disposed within the containment vessel, the at least one susceptor having an interior fluid passage; at least one inductor disposed within the interior fluid passage; an inlet opening (INLET) in the containment vessel for an inlet supply of the fluid in a low temperature liquid state to the interior fluid passage; an outlet opening (OUTLET) in the containment vessel for an outlet supply of the fluid in a high temperature liquid state for fluid change state processing to drive the fluid-driven turbine; characterised by the interior fluid passage forming an at least two-turn serpentine fluid passage within the containment vessel between the inlet opening (INLET) and the outlet opening (OUTLET), the inlet opening disposed in an inlet end of the containment vessel opposite the outlet opening of the containment vessel. a containment vessel; at least one susceptor disposed within the containment vessel, the at least one susceptor having an interior fluid passage; at least one inductor disposed within the interior fluid passage; an inlet opening (INLET) in the containment vessel for an inlet supply of the fluid in a low temperature liquid state to the interior fluid passage; an outlet opening (OUTLET) in the containment vessel for an outlet supply of the fluid in a high temperature liquid state for fluid change state processing to drive the fluid-driven turbine;
A spacer profile for use in a spacer frame of an insulating pane unit for door or window or facade elements, the insulating pane unit comprising panes (51, 52) having an intervening space defined therebetween, the spacer profile comprising a hollow profile body made of a synthetic material comprising a chamber for accommodating hygroscopic material, the hollow profile body - extending in a longitudinal direction, and - comprising an inner wall, which faces the intervening space between the panes (51, 52) of the insulating pane unit in the assembled state of the insulating pane unit and delimits the chamber, an outer wall on the side of the chamber that is opposite to the inner wall in a height direction, which is perpendicular to the longitudinal direction Z, and, laterally in a transverse direction, which is perpendicular to the longitudinal direction and to the height direction, a first side wall and an opposing second side wall, which are connected with the inner wall and the outer wall to form the chamber, a first reinforcement layer made of a first metal material having a first specific heat conductivity (λ 1), the first reinforcement layer extending in one piece on and/or in the first side wall with a constant cross section perpendicular to and in the longitudinal direction, and having a first thickness, a second reinforcement layer made of a second metal material having a second specific heat conductivity (λ 2), the second reinforcement layer extending in one piece on and/or in the second side wall with a constant cross-section perpendicular to and in the longitudinal direction spaced by a first distance from the first reinforcement layer, and having a second thickness, and a diffusion barrier layer made of at least one first layer made of a diffusion-proof synthetic material having a third thickness and a third specific heat conductivity (λ 33), the diffusion barrier layer being formed on the outer wall at least between the first reinforcement layer and the second reinforcement layer and being connected in a diffusion-proof manner with the same to form a diffusion barrier, wherein the product of the third specific heat conductivity (λ 33) and the third thickness is smaller than the product of the first specific heat conductivity (λ 1) and the first thickness and smaller than the product of the second specific heat conductivity (λ 2) and the second thickness, and the diffusion barrier layer is formed in an overlapping manner with the first and the second reinforcement layer (22, 24). - extending in a longitudinal direction, and - comprising an inner wall, which faces the intervening space between the panes (51, 52) of the insulating pane unit in the assembled state of the insulating pane unit and delimits the chamber, an outer wall on the side of the chamber that is opposite to the inner wall in a height direction, which is perpendicular to the longitudinal direction Z, and, laterally in a transverse direction, which is perpendicular to the longitudinal direction and to the height direction, a first side wall and an opposing second side wall, which are connected with the inner wall and the outer wall to form the chamber,
A semen storage container comprising: an outer case with a bottom in a cylindrical shape having an open upper end; an inner case with a bottom, the inner case having an open upper end and being provided on an inner side of the outer case to close an opening portion at the upper end of the outer case; and a removable lid laid over an upper end portion of the outer case to close an opening portion at the upper end of the inner case, the inner case including a semen guide which communicates with the opening portion at the upper end of the inner case and has an inner circumferential surface provided as an inclined surface which spreads upward, characterized in that the inner case further includes a cylindrical semen pool which communicates with an opening portion at a lower end of the semen guide and includes a tapered bottom portion. an outer case with a bottom in a cylindrical shape having an open upper end; an inner case with a bottom, the inner case having an open upper end and being provided on an inner side of the outer case to close an opening portion at the upper end of the outer case; and a removable lid laid over an upper end portion of the outer case to close an opening portion at the upper end of the inner case, the inner case including a semen guide which communicates with the opening portion at the upper end of the inner case and has an inner circumferential surface provided as an inclined surface which spreads upward, characterized in that the inner case further includes a cylindrical semen pool which communicates with an opening portion at a lower end of the semen guide and includes a tapered bottom portion.
An electric power-feeding structure for feeding electric power to a moving body which is driven to be raised or lowered, comprising: an arm having an obverse surface, a reverse surface, opposite sides surfaces, a distal end connected to the moving body movably in a direction perpendicular to a raising or lowering direction of the moving body and a proximal end adapted to be rotatably driven so as to swing, to thereby control the raising or lowering of the moving body, characterized in that an electrical wire is routed alongside one of the side surfaces of the arm, and one end of the electrical wire extending from the distal end of the arm is connected to the moving body to feed electric power to the moving body. an arm having an obverse surface, a reverse surface, opposite sides surfaces, a distal end connected to the moving body movably in a direction perpendicular to a raising or lowering direction of the moving body and a proximal end adapted to be rotatably driven so as to swing, to thereby control the raising or lowering of the moving body, characterized in that an electrical wire is routed alongside one of the side surfaces of the arm, and one end of the electrical wire extending from the distal end of the arm is connected to the moving body to feed electric power to the moving body.
A system for increasing the operational efficiency of an operating gas turbine engine, the operating gas turbine engine having at least two spools, the system comprising: a first electrical machine associated with a first spool of the operating gas turbine engine, wherein the first electrical machine is configured to receive mechanical power from the first spool to thereby generate electrical power; a second electrical machine associated with a second spool of the operating gas turbine engine; and a power controller associated with the second electrical machine, wherein the power controller is configured to selectively change the configuration of the second electrical machine from a generator mode to a motor mode during aircraft operations, wherein in the generator mode of the second electrical machine is configured to receive mechanical power from the second spool to thereby generate electrical power, and wherein in the motor mode the second electrical machine is configured to generate and supply mechanical output power to the second spool, and wherein in the motor mode, at least a part of the electrical power generated by the first electrical machine is transferred to the second electrical machine to generate and supply mechanical output power to the second spool; a DC bus electrically connecting the first and second electrical machines; wherein the power controller is further configured to operate in a starter mode during engine start operations, and wherein in the starter mode, electrical power is supplied to the second electrical machine from the DC bus for starting the gas turbine engine. a first electrical machine associated with a first spool of the operating gas turbine engine, wherein the first electrical machine is configured to receive mechanical power from the first spool to thereby generate electrical power; a second electrical machine associated with a second spool of the operating gas turbine engine; and a power controller associated with the second electrical machine, wherein the power controller is configured to selectively change the configuration of the second electrical machine from a generator mode to a motor mode during aircraft operations, wherein in the generator mode of the second electrical machine is configured to receive mechanical power from the second spool to thereby generate electrical power, and wherein in the motor mode the second electrical machine is configured to generate and supply mechanical output power to the second spool, and wherein in the motor mode, at least a part of the electrical power generated by the first electrical machine is transferred to the second electrical machine to generate and supply mechanical output power to the second spool; a DC bus electrically connecting the first and second electrical machines; wherein the power controller is further configured to operate in a starter mode during engine start operations, and wherein in the starter mode, electrical power is supplied to the second electrical machine from the DC bus for starting the gas turbine engine.
A processing method for preventing a packet attack, comprising: monitoring a network protocol negotiation status of a port of a network device; setting, according to the detected network protocol negotiation status of the port of the network device, a port that succeeds in network protocol negotiation to a trusted port; selecting, according to a first access control list, a protocol packet from packets received by the trusted port, and limiting, according to a first committed access rate, a rate at which the protocol packet is sent to a central processing unit; setting, according to the detected network protocol negotiation status of the port of the network device, a port that fails in network protocol negotiation to an untrusted port; and selecting, according to a second access control list, a protocol packet from packets received by the untrusted port, and limiting, according to a second committed access rate, a rate at which the protocol packet is sent to the central processing unit, wherein a value of the first committed access rate is greater than a value of the second committed access rate. monitoring a network protocol negotiation status of a port of a network device; setting, according to the detected network protocol negotiation status of the port of the network device, a port that succeeds in network protocol negotiation to a trusted port; selecting, according to a first access control list, a protocol packet from packets received by the trusted port, and limiting, according to a first committed access rate, a rate at which the protocol packet is sent to a central processing unit; setting, according to the detected network protocol negotiation status of the port of the network device, a port that fails in network protocol negotiation to an untrusted port; and selecting, according to a second access control list, a protocol packet from packets received by the untrusted port, and limiting, according to a second committed access rate, a rate at which the protocol packet is sent to the central processing unit, wherein a value of the first committed access rate is greater than a value of the second committed access rate.
Cutting section for a drill bit, wherein the cutting section is connectable to a drill shaft section of the drill bit via a releasable connecting device, having: ▪ a first tubular element which is in the form of a first hollow cylinder with a first outer lateral surface, a first inner lateral surface, a first lower end surface and a first upper end surface and which has a first hollow cylinder height (H 1), a first inside diameter (d 1) and a first outside diameter (D 1), ▪ a second closed tubular element which is in the form of a second hollow cylinder with a second outer lateral surface, a second inner lateral surface, a second lower end surface and a second upper end surface and which has a second hollow cylinder height (H 2), a second inside diameter (d 2) and a second outside diameter (D 2), wherein the first outside diameter (D 1) is larger than or equal to the second inside diameter (d 2), and ▪ one or more drill segments, wherein the one or the more drill segments is or are connected to the first tubular element and to the second closed tubular element, wherein the second closed tubular element has at least one slot-shaped recess, wherein the at least one slot-shaped recess comprises a transverse slot and a connecting slot, and the connecting slot connects the transverse slot to the second upper end surface of the second closed tubular element, characterized in that the first tubular element is pushed into the second closed tubular element, and the first tubular element is open. ▪ a first tubular element which is in the form of a first hollow cylinder with a first outer lateral surface, a first inner lateral surface, a first lower end surface and a first upper end surface and which has a first hollow cylinder height (H 1), a first inside diameter (d 1) and a first outside diameter (D 1), ▪ a second closed tubular element which is in the form of a second hollow cylinder with a second outer lateral surface, a second inner lateral surface, a second lower end surface and a second upper end surface and which has a second hollow cylinder height (H 2), a second inside diameter (d 2) and a second outside diameter (D 2), wherein the first outside diameter (D 1) is larger than or equal to the second inside diameter (d 2), and ▪ one or more drill segments, wherein the one or the more drill segments is or are connected to the first tubular element and to the second closed tubular element, wherein the second closed tubular element has at least one slot-shaped recess, wherein the at least one slot-shaped recess comprises a transverse slot and a connecting slot, and the connecting slot connects the transverse slot to the second upper end surface of the second closed tubular element, characterized in that the first tubular element is pushed into the second closed tubular element, and the first tubular element is open.
A method of determining operating modes in a receiver for demodulating a received signal, wherein the receiver comprises one of a RAKE receiver and a chip equalization receiver, the method comprising: • identifying a signal image in the received signal, wherein identifying the signal image comprises generating a power delay profile and detecting a local maxima in the power delay profile; characterized by • determining a first signal quality metric for a single-delay receiver mode in which the identified signal image is processed using a single delay, wherein said single-delay receiver mode comprises placement of a single RAKE finger of the RAKE receiver or a single delay tap of the chip equalization receiver at a delay corresponding to said local maxima; • determining a second signal quality metric for a multi-delay receiver mode in which the identified signal image is processed using multiple delays, wherein said multi-delay receiver mode comprises placement of multiple RAKE fingers of the RAKE receiver or multiple delay taps of the chip equalization receiver at respective delays proximate said local maxima; and • selecting the single-delay receiver mode or the multi-delay receiver mode based on a comparison of said first and second signal quality metrics. • identifying a signal image in the received signal, wherein identifying the signal image comprises generating a power delay profile and detecting a local maxima in the power delay profile; characterized by • determining a first signal quality metric for a single-delay receiver mode in which the identified signal image is processed using a single delay, wherein said single-delay receiver mode comprises placement of a single RAKE finger of the RAKE receiver or a single delay tap of the chip equalization receiver at a delay corresponding to said local maxima; • determining a second signal quality metric for a multi-delay receiver mode in which the identified signal image is processed using multiple delays, wherein said multi-delay receiver mode comprises placement of multiple RAKE fingers of the RAKE receiver or multiple delay taps of the chip equalization receiver at respective delays proximate said local maxima; and • selecting the single-delay receiver mode or the multi-delay receiver mode based on a comparison of said first and second signal quality metrics.