mhurhangee/ep-ind-claims huggingface dataset:
An electronics module comprising: a housing comprising: a forced convection chamber including an internal forced convection space; and, a passive chamber including an internal passive space that is separated from the forced convection space of the forced convection chamber; at least one fan (F1, F2) connected to the housing and adapted to induce forced convection airflow in the forced convection space; a heat sink connected to the housing, said heat sink comprising: a heat input portion exposed to the passive space of the passive chamber, wherein said heat input portion comprises a base of said heat sink; and, a heat output portion exposed to the forced convection space of the forced convection chamber; a circuit board assembly located in the passive space, said circuit board assembly comprising at least one electronic component that is thermally engaged with the heat input portion of the heat sink; characterized by a clamping plate secured to the heat sink base, wherein said circuit board assembly is captured between the clamping plate and an outer wall of the heat sink base to secure the circuit board assembly to the heat sink base; and a resilient member located between the clamping plate and the circuit board assembly such that the resilient member applies a clamping force directly to the at least one electronic component of the circuit board assembly. a housing comprising: a forced convection chamber including an internal forced convection space; and, a passive chamber including an internal passive space that is separated from the forced convection space of the forced convection chamber; at least one fan (F1, F2) connected to the housing and adapted to induce forced convection airflow in the forced convection space; a heat sink connected to the housing, said heat sink comprising: a heat input portion exposed to the passive space of the passive chamber, wherein said heat input portion comprises a base of said heat sink; and, a heat output portion exposed to the forced convection space of the forced convection chamber; a circuit board assembly located in the passive space, said circuit board assembly comprising at least one electronic component that is thermally engaged with the heat input portion of the heat sink; characterized by a clamping plate secured to the heat sink base, wherein said circuit board assembly is captured between the clamping plate and an outer wall of the heat sink base to secure the circuit board assembly to the heat sink base; and a resilient member located between the clamping plate and the circuit board assembly such that the resilient member applies a clamping force directly to the at least one electronic component of the circuit board assembly.
A terminal connection device for connecting a terminal portion of a flexible integrated wiring to a connector, comprising: a first member having a mounting portion capable of mounting thereon the terminal portion of the flexible integrated wiring, and an inclined portion formed in a rear end portion located in an extending direction of the flexible integrated wiring whereby the terminal portion is mounted on the mounting portion; and the inclined portion is formed from one side at which the mounting portion is formed towards an other side, a second member having a pressing portion formed so as to press the terminal portion, and a bending portion formed on a rear end portion located in the extending direction of the flexible integrated wiring whereby the terminal portion is mounted on the mounting portion and formed along the inclined portion of the first member, wherein the second member is formed so as to be mountable to the first member in a state where the pressing portion presses the terminal portion and the bending portion bends the flexible integrated wiring along the inclined portion. a first member having a mounting portion capable of mounting thereon the terminal portion of the flexible integrated wiring, and an inclined portion formed in a rear end portion located in an extending direction of the flexible integrated wiring whereby the terminal portion is mounted on the mounting portion; and the inclined portion is formed from one side at which the mounting portion is formed towards an other side, a second member having a pressing portion formed so as to press the terminal portion, and a bending portion formed on a rear end portion located in the extending direction of the flexible integrated wiring whereby the terminal portion is mounted on the mounting portion and formed along the inclined portion of the first member, wherein the second member is formed so as to be mountable to the first member in a state where the pressing portion presses the terminal portion and the bending portion bends the flexible integrated wiring along the inclined portion.
A tunable laser comprising: a substrate comprising a silicon material; a gain medium coupled to the substrate, wherein the gain medium is in a recessed region of the silicon material, and the gain medium includes a compound semiconductor material; a waveguide disposed in the substrate and optically coupled to the gain medium; a first wavelength selective element characterized by a first reflectance spectrum and disposed in the substrate; a second wavelength selective element characterized by a second reflectance spectrum and disposed in the substrate; and an optical coupler disposed in the substrate and joining the waveguide, the first wavelength selective element and the second wavelength selective element; an index matching region filled with index matching material between the gain medium and the waveguide; and an output mirror. a substrate comprising a silicon material; a gain medium coupled to the substrate, wherein the gain medium is in a recessed region of the silicon material, and the gain medium includes a compound semiconductor material; a waveguide disposed in the substrate and optically coupled to the gain medium; a first wavelength selective element characterized by a first reflectance spectrum and disposed in the substrate; a second wavelength selective element characterized by a second reflectance spectrum and disposed in the substrate; and an optical coupler disposed in the substrate and joining the waveguide, the first wavelength selective element and the second wavelength selective element; an index matching region filled with index matching material between the gain medium and the waveguide; and an output mirror.
Aviation radio device having a dynamically reconfigurable circuit element with a given capacity, wherein the aviation radio device has a plurality of functional states each with a plurality of functional blocks (15 - 19, 30 1, 30 2, 31 1, 31 2, 32, 33, 34, 35, 36, 40, 40a), wherein the dynamically reconfigurable circuit element creates at least one functional block (15 - 19, 30 1, 30 2, 31 1, 31 2, 32, 33, 34, 35, 36, 40, 40a), wherein each functional block (15 - 19, 30 1, 30 2, 31 1, 31 2, 32, 33, 34, 35, 36, 40, 40a) created by the dynamically reconfigurable circuit element uses a certain capacity of the dynamically reconfigurable circuit element, wherein the difference between the given capacity of the dynamically reconfigurable circuit element and the maximum required capacity of the functional blocks (15 - 19, 30 1, 30 2, 31 1, 31 2, 32, 33, 34, 35, 36, 40, 40a) of the functional states forms a free capacity, wherein the free capacity provides redundant functional blocks (20 - 23, 30a, 30b, 31a, 31b, 32a, 32b, 33a), wherein the redundant functional blocks (20 - 23, 30a, 30b, 31a, 31b, 32a, 32b, 33a) are dynamically reconfigurable, wherein the functional blocks (15 - 19, 30 1, 30 2, 31 1, 31 2, 32, 33, 34, 35, 36, 40, 40a) of the functional states of the aviation radio device are rated depending on certain applications according to their relevance for system security, wherein the free capacity provides the redundant functional blocks (20 - 23, 30a, 30b, 31a, 31b, 32a, 32b, 33a) with redundancy depending on the relevance for the particular applications.
A method, comprising: determining, by a controller, a first voltage standing wave ratio; selecting, by the controller, a voltage standing wave ratio circle from among a group of voltage standing wave ratio circles based on the first voltage standing wave ratio; identifying, by the controller, a group of sets of tuning settings for variable reactance elements of a matching network, wherein the identifying of the group of sets of tuning settings is based on each set of tuning settings of the group of sets of tuning settings being positioned along a circumference of the voltage standing wave ratio circle; and selecting, by the controller, a set of tuning settings from among the group of sets of tuning settings responsive to a second voltage standing wave ratio, wherein said second voltage standing wave ratio is determined for the set of tuning settings having the lowest voltage standing wave ratio of the sets; and adjusting the variable reactance elements of the matching network based on the selected set of tuning settings. determining, by a controller, a first voltage standing wave ratio; selecting, by the controller, a voltage standing wave ratio circle from among a group of voltage standing wave ratio circles based on the first voltage standing wave ratio; identifying, by the controller, a group of sets of tuning settings for variable reactance elements of a matching network, wherein the identifying of the group of sets of tuning settings is based on each set of tuning settings of the group of sets of tuning settings being positioned along a circumference of the voltage standing wave ratio circle; and selecting, by the controller, a set of tuning settings from among the group of sets of tuning settings responsive to a second voltage standing wave ratio, wherein said second voltage standing wave ratio is determined for the set of tuning settings having the lowest voltage standing wave ratio of the sets; and adjusting the variable reactance elements of the matching network based on the selected set of tuning settings.
A deactivation method in a crosstalk scenario, comprising: switching, by a transceiver on a line, from a data transmission showtime state into a deactivation execution state; switching, by the transceiver, into a silent state or an idle state; characterized by further comprising: during the deactivation execution state, setting, by the transceiver, a downstream signal X d on the line to zero, and transmitting a signal X d ', wherein X d is a signal to be inputted into a crosstalk canceller of the line, and X d ' is an output signal after X d which has been set to zero is inputted into the canceller. switching, by a transceiver on a line, from a data transmission showtime state into a deactivation execution state; switching, by the transceiver, into a silent state or an idle state; characterized by further comprising: during the deactivation execution state, setting, by the transceiver, a downstream signal X d on the line to zero, and transmitting a signal X d ', wherein X d is a signal to be inputted into a crosstalk canceller of the line, and X d ' is an output signal after X d which has been set to zero is inputted into the canceller.
A method comprising: providing one or more scanners in a private network, each scanner including a scan engine and a configuration agent; establishing a first secure tunnel between a configuration manager and a further scanner, and a second secure tunnel between a scan controller and the further scanner, wherein the further scanner is located in a public network and the configuration manager and the scan controller are located in the private network, wherein the further scanner includes a further scan engine and a further configuration agent, wherein the first secure tunnel is distinct from the second secure tunnel; communicating scanner configuration information between the further scanner and the configuration manager over the first secure tunnel; and communicating scan information between the further scanner and the scan controller over the second secure tunnel, including providing, by the scan controller, one or more scan instructions to the further scan engine, wherein the scan controller and the configuration manager communicate with the one or more scanners located in the private network, including providing, by the scan controller, one or more scan instructions to at least one scan engine and providing, by the configuration manager, scanner configuration information to at least one configuration agent over dedicated internal network connections in the private network, wherein each scan engine (16, 32) of the one or more scanners and the further scanner is configured to scan one or more assets (20A-C) according to the scan instructions dictated from the scan controller. providing one or more scanners in a private network, each scanner including a scan engine and a configuration agent; establishing a first secure tunnel between a configuration manager and a further scanner, and a second secure tunnel between a scan controller and the further scanner, wherein the further scanner is located in a public network and the configuration manager and the scan controller are located in the private network, wherein the further scanner includes a further scan engine and a further configuration agent, wherein the first secure tunnel is distinct from the second secure tunnel; communicating scanner configuration information between the further scanner and the configuration manager over the first secure tunnel; and communicating scan information between the further scanner and the scan controller over the second secure tunnel, including providing, by the scan controller, one or more scan instructions to the further scan engine, wherein the scan controller and the configuration manager communicate with the one or more scanners located in the private network, including providing, by the scan controller, one or more scan instructions to at least one scan engine and providing, by the configuration manager, scanner configuration information to at least one configuration agent over dedicated internal network connections in the private network, wherein each scan engine (16, 32) of the one or more scanners and the further scanner is configured to scan one or more assets (20A-C) according to the scan instructions dictated from the scan controller.
An apparatus for the production of a rod component of an aerosol generating article, said apparatus comprising: ∘ a first mover adapted to transport a first sheet along a first direction; ∘ a second mover adapted to transport a second sheet along a second direction; ∘ a third mover adapted to transport a susceptor strip along a third direction, said third mover being adapted to position said susceptor strip between the first and the second sheet during transport; and ∘ a rod forming device being adapted to form a rod from the first and the second sheets (2; 3) and the susceptor strip and having an inlet and an outlet, wherein said first and second sheets (2; 3) and said susceptor strip are introduced in said inlet and said rod is outputted from said outlet. ∘ a first mover adapted to transport a first sheet along a first direction; ∘ a second mover adapted to transport a second sheet along a second direction; ∘ a third mover adapted to transport a susceptor strip along a third direction, said third mover being adapted to position said susceptor strip between the first and the second sheet during transport; and ∘ a rod forming device being adapted to form a rod from the first and the second sheets (2; 3) and the susceptor strip and having an inlet and an outlet, wherein said first and second sheets (2; 3) and said susceptor strip are introduced in said inlet and said rod is outputted from said outlet.
A gas turbine engine article (60, 102) comprising: an article wall (68, 168) defining a cavity (74, 174); and a cooling passage network (76, 176) embedded in the article wall (68, 168) between inner and outer portions (68a, 168a, 68b, 168b) of the article wall (68, 168), the cooling passage network (76, 176) having an inlet orifice through the inner portion (68a 168a) of the article wall (68, 168) to receive cooling air from the cavity (74, 174), a plurality of sub-passages that extend axially from the at least one inlet orifice, at least one outlet orifice through the outer portion (68b, 168b) of the article wall (68, 168), and trip strips (86, 86a, 86b, 186a, 186b) for mixing cooling air in the cooling passage network (76, 176); characterised in that: a first one of the trip strips (86a, 186a) is a partial ring that extends around an interior region greater than 180°, one or more of the trip strips (86b, 186b) are within the interior region, and one of the trip strips (86b, 186b) that is within the interior region is a ring, and at least one of the trip strips (86b, 186b) projects from the outer portion (68b, 168b) of the article wall (68, 168) and is aligned opposite the inlet orifice. an article wall (68, 168) defining a cavity (74, 174); and a cooling passage network (76, 176) embedded in the article wall (68, 168) between inner and outer portions (68a, 168a, 68b, 168b) of the article wall (68, 168), the cooling passage network (76, 176) having an inlet orifice through the inner portion (68a 168a) of the article wall (68, 168) to receive cooling air from the cavity (74, 174), a plurality of sub-passages that extend axially from the at least one inlet orifice, at least one outlet orifice through the outer portion (68b, 168b) of the article wall (68, 168), and trip strips (86, 86a, 86b, 186a, 186b) for mixing cooling air in the cooling passage network (76, 176); characterised in that: a first one of the trip strips (86a, 186a) is a partial ring that extends around an interior region greater than 180°, one or more of the trip strips (86b, 186b) are within the interior region, and one of the trip strips (86b, 186b) that is within the interior region is a ring, and at least one of the trip strips (86b, 186b) projects from the outer portion (68b, 168b) of the article wall (68, 168) and is aligned opposite the inlet orifice.
A computing device for a surgery assisting device (1, 1A) that is configured to hold a surgical instrument on a distal end portion and includes a freely bendable arm portion by including one or a plurality of joint portions (31, 32, 33), characterized in that the computing device comprising: a computing unit that obtains angle information of at least one of the one or the plurality of joint portions (31, 32, 33) in a state where a distal end of the surgical instrument held by the arm portion is positioned at a predetermined position (Pt) and determines a length of the surgical instrument by a geometric computation using the angle information, wherein the geometric computation is based on a trigonometric function or a matrix calculation.
Method for testing a shuttle valve in a pneumatic system, preferably an electronically controllable pneumatic brake system, wherein the shuttle valve has a first shuttle valve connection (2.1), a second shuttle valve connection (2.2) and a third shuttle valve connection (2.3), wherein the higher of the pressures (p1, p2) applied to the first shuttle valve connection (2.1) and second shuttle valve connection (2.2) is controlled at the third shuttle valve connection (2.3), wherein the method comprises the steps of: a) controlling a first pressure at the first shuttle valve connection (2.1); b) determining a value (G1, G1T) indicative of the first pressure at the first shuttle valve connection (2.1); and c) comparing the value (G1, G1T) indicative of the first pressure with a first predetermined comparison value (GV1, GS1) provided for this purpose, and in the case of a deviation which is greater than a first tolerance: determining and/or outputting an error of the shuttle valve, and d) controlling a second pressure at the second shuttle valve connection (2.1); e) determining a value (G2, G2T) indicative of the second pressure at the second shuttle valve connection (2.2); and f) comparing the value (G2, G2T) indicative of the second pressure with a second predetermined comparison value (GV2, GS2) provided for this purpose, and in the case of a deviation which is greater than a second tolerance: determining and/or outputting an error of the shuttle valve. a) controlling a first pressure at the first shuttle valve connection (2.1); b) determining a value (G1, G1T) indicative of the first pressure at the first shuttle valve connection (2.1); and c) comparing the value (G1, G1T) indicative of the first pressure with a first predetermined comparison value (GV1, GS1) provided for this purpose, and in the case of a deviation which is greater than a first tolerance: determining and/or outputting an error of the shuttle valve, and d) controlling a second pressure at the second shuttle valve connection (2.1); e) determining a value (G2, G2T) indicative of the second pressure at the second shuttle valve connection (2.2); and f) comparing the value (G2, G2T) indicative of the second pressure with a second predetermined comparison value (GV2, GS2) provided for this purpose, and in the case of a deviation which is greater than a second tolerance: determining and/or outputting an error of the shuttle valve.