mhurhangee/ep-ind-claims huggingface dataset:
A karabiner hook having at least one clip and at least one closure part and at least one insertion opening of the clip, which is closable by the closure part in its closed position, wherein the closure part is mounted on the clip such that it is pivotable between the closed position and a maximally open position by means of a closure-part pivot pin and at least one blocking element is mounted on or in the closure part such that it is pivotable by means of a blocking-element pivot pin, wherein the blocking element, in at least one blocking position, blocks the closure part in its closed position to prevent pivoting of the closure part in the direction towards its maximally open position and, in at least one release position, enables pivoting of the closure part in the direction towards its maximally open position, wherein, for the pivoting out of the blocking position in the direction towards the release position, the blocking element is to be pivoted in the same direction of rotation about the blocking-element pivot pin as the closure part is to be pivoted about the closure-part pivot pin for pivoting the closure part out of the closed position in the direction towards its maximally open position, characterised in that it has at least one common restoring spring for pivoting the closure part back into its closed position and the blocking element back into its blocking position.
A supersonic jet aircraft having at least three turbofan engines (103, 104, 105) and an engine management computer; a first engine of the at least three turbofan engines is configured to be de-activatable during flight to move from an operational state in which it provides thrust to an operational state in which it stops providing thrust; and the other engines (104, 105) of the at least three turbofan engines are configured to provide sufficient thrust to the supersonic jet aircraft when the first engine is de-activated such that the aircraft can perform a supersonic climb operation and/or a supersonic cruise operation; characterised in that the at least three turbofan engines (103, 104, 105) are substantially identical, and the engine management computer is configured to: command thrust from the first engine during a subsonic operation of the supersonic jet aircraft and automatically de-activate the first engine when the subsonic operation is complete.
A rotor blade for a wind turbine, which extends in the longitudinal direction with a profile course from a blade connector to a blade tip, wherein the profile course comprises a profile of a lift coefficient, comprising - a hub portion adjacent to the blade connector and a tip portion adjacent to the blade tip, - a middle portion adjacent to the hub portion and to the tip portion, - wherein the middle portion substantially comprises those profile sections which have a relative profile thickness, which is defined as the ratio of maximum profile thickness to profile depth, of between 20% and 30%, and - wherein the middle portion comprises a local minimum of the course of the lift coefficient, characterized by the rotor blade extending in the longitudinal direction with a course of a thickness setback, wherein the thickness setback of a profile section is defined as the ratio of the distance between the maximum profile thickness and a leading edge of the rotor blade in the direction of the profile chord to the profile depth, wherein the middle portion comprises a local maximum of the thickness setback. - a hub portion adjacent to the blade connector and a tip portion adjacent to the blade tip, - a middle portion adjacent to the hub portion and to the tip portion, - wherein the middle portion substantially comprises those profile sections which have a relative profile thickness, which is defined as the ratio of maximum profile thickness to profile depth, of between 20% and 30%, and - wherein the middle portion comprises a local minimum of the course of the lift coefficient,
A fuel tank inerting system (300, 400, 500) for an aircraft, the system comprising: a ram air duct (312, 412, 512); a fuel tank (306,406,506); a pressurized air source (308, 408, 508); an air separation module ASM (302, 402, 502) arranged between the pressurized air source and the fuel tank, the air separation module configured to generate an inerting gas from pressurized air supplied from the pressurized air source and supply the inerting gas to the fuel tank; an upstream thermal conditioning system (320, 420, 520) arranged upstream of the air separation module, the upstream thermal conditioning system configured to increase a temperature of the pressurized air prior to entry into the air separation module; a downstream thermal conditioning system (332, 432, 532) arranged downstream of the air separation module, the downstream thermal conditioning system configured to decrease a temperature of the inerting gas prior to entry into the fuel tank, characterized in that the downstream thermal conditioning system comprises a product gas cooler (334, 434, 534) located in the ram air duct; and in that the upstream thermal conditioning system comprises an ASM cooling heat exchanger (310, 410, 510) arranged within the ram air duct (312, 412, 512) of the aircraft, wherein the pressurized air passes through the ASM cooling heat exchanger upstream of the air separation module, the upstream thermal conditioning system further comprising a bypass line and a bypass valve, wherein the bypass valve is operable to divert at least a portion of the pressurized air around the ASM cooling heat exchanger (310, 410, 510). a fuel tank (306,406,506); a pressurized air source (308, 408, 508); an air separation module ASM (302, 402, 502) arranged between the pressurized air source and the fuel tank, the air separation module configured to generate an inerting gas from pressurized air supplied from the pressurized air source and supply the inerting gas to the fuel tank; an upstream thermal conditioning system (320, 420, 520) arranged upstream of the air separation module, the upstream thermal conditioning system configured to increase a temperature of the pressurized air prior to entry into the air separation module; a downstream thermal conditioning system (332, 432, 532) arranged downstream of the air separation module, the downstream thermal conditioning system configured to decrease a temperature of the inerting gas prior to entry into the fuel tank, characterized in that the downstream thermal conditioning system comprises a product gas cooler (334, 434, 534) located in the ram air duct; and in that the upstream thermal conditioning system comprises an ASM cooling heat exchanger (310, 410, 510) arranged within the ram air duct (312, 412, 512) of the aircraft, wherein the pressurized air passes through the ASM cooling heat exchanger upstream of the air separation module, the upstream thermal conditioning system further comprising a bypass line and a bypass valve, wherein the bypass valve is operable to divert at least a portion of the pressurized air around the ASM cooling heat exchanger (310, 410, 510).
An image forming apparatus comprising: a detecting unit configured to detect an attack on the apparatus on the basis of a history of logins to the apparatus; a control unit configured to perform a login control process which controls a predetermined process related to a login to the apparatus when an attack is detected; and an auxiliary storage device, characterized in that the detecting unit is configured to detect an attack on the apparatus on the basis of a predetermined condition and the log stored on the auxiliary storage device and to detect the end of the attack on the apparatus on the basis of the log stored on the auxiliary storage device; and the control unit is configured to perform a login control process according to the result of detection of the attack on the apparatus by the detecting unit and to end the login control process according to the result of detection of the end of the attack on the apparatus by the detecting unit. a detecting unit configured to detect an attack on the apparatus on the basis of a history of logins to the apparatus; a control unit configured to perform a login control process which controls a predetermined process related to a login to the apparatus when an attack is detected; and an auxiliary storage device, characterized in that the detecting unit is configured to detect an attack on the apparatus on the basis of a predetermined condition and the log stored on the auxiliary storage device and to detect the end of the attack on the apparatus on the basis of the log stored on the auxiliary storage device; and the control unit is configured to perform a login control process according to the result of detection of the attack on the apparatus by the detecting unit and to end the login control process according to the result of detection of the end of the attack on the apparatus by the detecting unit.
A method for locating a targeted wireless communication device, the method comprising: receiving, at the targeted wireless communication device, a communication data packet having a predetermined format comprising a locating state code associated with one of a plurality of predetermined locating states in which the targeted wireless device is operable, wherein each locating state is stored in a memory on the targeted wireless device and comprises one or more predetermined location routines (22, 24, 26, 27, 28, 30, 31, 32) carried out by the targeted wireless device; and executing at least one of the one or more predetermined location routines (22, 24, 26, 27, 28, 30, 31, 32) on the targeted wireless communication device in response to detecting the locating, state code in the communication data packet, wherein executing further comprises operating the wireless device in a stealth mode that disables output by the wireless device of user-perceptible indicators that would normally be generated during execution of the one or more predetermined location routines (22, 24, 26, 27, 28, 30, 31, 32) in a non-stealth mode. receiving, at the targeted wireless communication device, a communication data packet having a predetermined format comprising a locating state code associated with one of a plurality of predetermined locating states in which the targeted wireless device is operable, wherein each locating state is stored in a memory on the targeted wireless device and comprises one or more predetermined location routines (22, 24, 26, 27, 28, 30, 31, 32) carried out by the targeted wireless device; and executing at least one of the one or more predetermined location routines (22, 24, 26, 27, 28, 30, 31, 32) on the targeted wireless communication device in response to detecting the locating, state code in the communication data packet, wherein executing further comprises operating the wireless device in a stealth mode that disables output by the wireless device of user-perceptible indicators that would normally be generated during execution of the one or more predetermined location routines (22, 24, 26, 27, 28, 30, 31, 32) in a non-stealth mode.
Valve for an aircraft engine fuel circuit, comprising a sleeve in the interior of which is provided a spool, said sleeve comprising two control chambers (231, 232) between which the spool extends, said spool extending along a longitudinal axis and comprising a narrowed intermediate portion extending between two cylindrical end portions (29, 31), a first end portion being separated from the narrowed intermediate portion by a shoulder having a surface arranged perpendicular to the longitudinal axis overall, the narrowed intermediate portion itself including, as an extension of the shoulder, at least one cylindrical section, said sleeve comprising an intermediate chamber provided with a fuel inlet and a fuel outlet in which the first and second end portions (29, 31) and the narrowed intermediate portion of the spool extend, the spool being configured to be displaced relative to the sleeve under the influence of a pressure difference between the two control chambers (231, 232), characterized in that the spool is displaced between a closed position in which the spool blocks the fuel inlet, and an open position in which the spool frees the fuel inlet, and in that the shoulder comprises at least one groove which extends radially from the cylindrical surface of the first end portion, in the direction of the longitudinal axis, until the cylindrical section of the narrowed intermediate portion and which forms a fuel recirculation zone which ensures, when fuel flows along the first end portion in the direction of the narrowed intermediate portion and of the second end portion, that the fuel jet generated arrives on said cylindrical section.
A silicon carbide semiconductor device, comprising: a silicon carbide substrate including a first impurity region having a first conductivity type, a well region being in contact with said first impurity region and having a second conductivity type which is different from said first conductivity type, and a second impurity region being separated from said first impurity region by said well region and having said first conductivity type; a gate insulating film being in contact with said first impurity region and said well region; and a gate electrode being in contact with said gate insulating film and being arranged opposite side to said well region with respect to said gate insulating film, wherein a surface of said well region in contact with said gate insulating film includes a first plane having a plane orientation of, said surface includes said first plane microscopically, and said surface further includes a second plane having a plane orientation of microscopically, and said first plane and said second plane of said surface include a complex plane having a plane orientation of, such that a specific on-resistance at room temperature and at a gate voltage of 9V applied to said gate electrode is smaller than twice said specific on-resistance at room temperature and at a gate voltage of 18V applied to said gate electrode, wherein an impurity concentration of the well region is greater than or equal to 1x10 17 cm -3 and less than or equal to 1x10 18 cm -3. a silicon carbide substrate including a first impurity region having a first conductivity type, a well region being in contact with said first impurity region and having a second conductivity type which is different from said first conductivity type, and a second impurity region being separated from said first impurity region by said well region and having said first conductivity type; a gate insulating film being in contact with said first impurity region and said well region; and a gate electrode being in contact with said gate insulating film and being arranged opposite side to said well region with respect to said gate insulating film, wherein a surface of said well region in contact with said gate insulating film includes a first plane having a plane orientation of, said surface includes said first plane microscopically, and said surface further includes a second plane having a plane orientation of microscopically, and said first plane and said second plane of said surface include a complex plane having a plane orientation of, such that a specific on-resistance at room temperature and at a gate voltage of 9V applied to said gate electrode is smaller than twice said specific on-resistance at room temperature and at a gate voltage of 18V applied to said gate electrode, wherein an impurity concentration of the well region is greater than or equal to 1x10 17 cm -3 and less than or equal to 1x10 18 cm -3.
A shovel comprising: an attachment including a working assembly; a diesel engine provided with a supercharger; an oil hydraulic pump connected to the diesel engine provided with the supercharger; an attachment position retrieval unit configured to retrieve a position of a predetermined part of the attachment based on a detection value of a boom angle sensor and an arm angle sensor; and a controller that executes a preload boost function, wherein the preload boost function is for increasing boost pressure of the supercharger prior to increasing a hydraulic pressure load on the oil hydraulic pump, characterized in that a work range accessible by the position of the predetermined part of the attachment includes a partial work range at which, upon the working assembly being operated, the preload boost function is to be executed and a partial work range at which, upon the working assembly being operated, the preload boost function is not to be executed. an attachment including a working assembly; a diesel engine provided with a supercharger; an oil hydraulic pump connected to the diesel engine provided with the supercharger; an attachment position retrieval unit configured to retrieve a position of a predetermined part of the attachment based on a detection value of a boom angle sensor and an arm angle sensor; and a controller that executes a preload boost function, wherein the preload boost function is for increasing boost pressure of the supercharger prior to increasing a hydraulic pressure load on the oil hydraulic pump, characterized in that a work range accessible by the position of the predetermined part of the attachment includes a partial work range at which, upon the working assembly being operated, the preload boost function is to be executed and a partial work range at which, upon the working assembly being operated, the preload boost function is not to be executed.
Lock (1; 1') comprising a lock case (3; 3') and a lock mechanism (11; 11'), which lock mechanism (11; 11') is arranged inside the lock case (3; 3') and comprises: a bolt (17; 17') so arranged as to adopt a bolting position in which the bolt projects outwards in relation to the lock case (3; 3'), a follower (21; 21') for actuation of the bolt (17; 17'), which follower (21; 21') is rotatably arranged inside the lock case (3; 3'), a driver (23; 23') so arranged as to transfer movement mechanically from the follower (21; 21') to the bolt (17; 17'), which driver (23; 23') is so arranged as to adopt an interlocked position preventing movement of the bolt (17; 17') when the bolt (17; 17') adopts its bolting position, a blocking mechanism (25; 34) for blocking movement of the driver (23; 23'), which blocking mechanism (25; 34) is so arranged as to be capable of being positioned in a blocking position and a non-blocking position, the follower (21; 21') and the blocking mechanism (25; 34) having means (21-3, 25-1; 21'-3, 37-3) for operational interaction whereby the blocking mechanism (25; 34) can be actuated by the follower (21; 21') from the blocking position, the driver (23; 23') having a portion (23-1; 23'-1) in rotating interaction with the follower (21; 21'), which portion (23-1; 23'-1) is arranged concentrically with the follower (21; 21') to permit rotation about the same axis. a bolt (17; 17') so arranged as to adopt a bolting position in which the bolt projects outwards in relation to the lock case (3; 3'), a follower (21; 21') for actuation of the bolt (17; 17'), which follower (21; 21') is rotatably arranged inside the lock case (3; 3'), a driver (23; 23') so arranged as to transfer movement mechanically from the follower (21; 21') to the bolt (17; 17'), which driver (23; 23') is so arranged as to adopt an interlocked position preventing movement of the bolt (17; 17') when the bolt (17; 17') adopts its bolting position, a blocking mechanism (25; 34) for blocking movement of the driver (23; 23'), which blocking mechanism (25; 34) is so arranged as to be capable of being positioned in a blocking position and a non-blocking position, the follower (21; 21') and the blocking mechanism (25; 34) having means (21-3, 25-1; 21'-3, 37-3) for operational interaction whereby the blocking mechanism (25; 34) can be actuated by the follower (21; 21') from the blocking position, the driver (23; 23') having a portion (23-1; 23'-1) in rotating interaction with the follower (21; 21'), which portion (23-1; 23'-1) is arranged concentrically with the follower (21; 21') to permit rotation about the same axis.
An apparatus for generating an output signal having at least two output channels from an input signal having at least one input channel, wherein the apparatus comprises: an ambience extractor being adapted to extract at least one ambient signal with ambient signal portions from the at least one input channel, an ambient modification unit (120; 220; 320; 420) being adapted to modify the at least one ambient signal to obtain at least a first modified ambient signal, and at least two speakers, wherein the apparatus for generating an output signal is adapted to feed the first modified ambient signal into the second speaker, and wherein the apparatus for generating an output signal is adapted to feed the first input channel with direct and ambient signal portions into the first speaker, characterised in a first speaker of the at least two speakers placed at a first height in a listening environment with respect to a listener, and a second speaker of the at least two speakers placed at second height in a listening environment with respect to the listener, the second height being different from the first height. an ambience extractor being adapted to extract at least one ambient signal with ambient signal portions from the at least one input channel, an ambient modification unit (120; 220; 320; 420) being adapted to modify the at least one ambient signal to obtain at least a first modified ambient signal, and at least two speakers, wherein the apparatus for generating an output signal is adapted to feed the first modified ambient signal into the second speaker, and wherein the apparatus for generating an output signal is adapted to feed the first input channel with direct and ambient signal portions into the first speaker, characterised in a first speaker of the at least two speakers placed at a first height in a listening environment with respect to a listener, and a second speaker of the at least two speakers placed at second height in a listening environment with respect to the listener, the second height being different from the first height.