mhurhangee/patent-ind-claim-en huggingface dataset:
A particle filter for removing particulates, carbon monoxide, hydrocarbons and nitrogen oxides from the exhaust gas of internal combustion engines operating with stoichiometric air/fuel mixture, comprising a wall flow filter of length L and two different coatings Y and Z, wherein the wall flow filter comprises channels E and A which extend in parallel between a first and a second end of the wall flow filter and which are separated by porous walls forming surfaces O E and O A , respectively, and wherein the channels E at the second end and the channels A at the first end are closed, characterized in that coating Y is located in the channels E on the surfaces O E and extends from the first end of the wall flow filter over a length of 51 to 90% of the length L and coating Z is located in the porous walls and extends from the second end of the wall flow filter over a length of 60 to 100% of the length L and in that the coatings Y and Z each contain the precious metals palladium and rhodium fixed to one or more carrier materials and contain one or more oxygen storage components.
A threaded fitting , comprising: a first plurality of threads (T) configured to provide a labyrinth type seal minimizing migration of at least hazardous dust or gases; a second plurality of threads (S) configured to provide a labyrinth type seal for attenuating vibration while minimizing migration of at least fluids; and a transition thread (TT) between the first plurality of threads and the second plurality of threads, wherein the first and second plurality of threads are serially-arranged and may be used for either thin or thick-walled enclosures to retard a passage of at least one of gas, fluid, dust or flame, wherein each thread of the first plurality of threads has a root diameter (D1) which tapers from the transition thread to a reference plane zero, and a crest diameter (D3) which forms a straight angle or is parallel to an elongate axis of the thread fitting, wherein the second plurality of threads has a root diameter (D4) which is straight or parallel to the elongate axis of the threaded fitting. a first plurality of threads (T) configured to provide a labyrinth type seal minimizing migration of at least hazardous dust or gases; a second plurality of threads (S) configured to provide a labyrinth type seal for attenuating vibration while minimizing migration of at least fluids; and a transition thread (TT) between the first plurality of threads and the second plurality of threads, wherein the first and second plurality of threads are serially-arranged and may be used for either thin or thick-walled enclosures to retard a passage of at least one of gas, fluid, dust or flame, wherein each thread of the first plurality of threads has a root diameter (D1) which tapers from the transition thread to a reference plane zero, and a crest diameter (D3) which forms a straight angle or is parallel to an elongate axis of the thread fitting, wherein the second plurality of threads has a root diameter (D4) which is straight or parallel to the elongate axis of the threaded fitting.
Analysis method for a sample, wherein the sample is picked up with a sampling instrument and at least one processing step is carried out on the sample on a discoid sample holder , wherein the sampling instrument containing the picked-up sample is inserted into a slot of the sample holder , wherein the sample is detached from the sampling instrument and provided for the at least one processing step, wherein the sample is detached from the sampling instrument by a movement of the sample holder , characterized in that the slot for an insertion of the sampling instrument is oriented in a disk plane predefined by the sample holder or at an angle of less than 45° to said plane.
A method of training a data link including: providing a noise source from which a noise signal is obtained; selectively applying noise from the noise source to a data signal to obtain a first signal having noise added thereto; and supplying the first signal having noise added thereto for processing by a link training operation that is training a data link between a display data source and a display data sink, wherein the noise from the noise source is obtained by one of changing clock distribution methods associated with the data link, removing a first noise filter from cascaded phase-locked loops associated with the data link and increasing a level of a spread spectrum setting associated with the data link. providing a noise source from which a noise signal is obtained; selectively applying noise from the noise source to a data signal to obtain a first signal having noise added thereto; and supplying the first signal having noise added thereto for processing by a link training operation that is training a data link between a display data source and a display data sink, wherein the noise from the noise source is obtained by one of changing clock distribution methods associated with the data link, removing a first noise filter from cascaded phase-locked loops associated with the data link and increasing a level of a spread spectrum setting associated with the data link.
An aircraft comprising: a first wing having a first guide ; a second wing having a second guide , the first and second guides configured to guide the aircraft to be aligned with a second and a third aircraft respectively during flight or hovering of the aircraft; a first lock coupled to the first wing, the first lock configured to secure the first wing to a third wing (1 10b) of the second aircraft when the first wing and the third wing are aligned; and a second lock coupled to the second wing, the second lock configured to secure the second wing to a fourth wing of the third aircraft when the second wing and the fourth wing are aligned, wherein the first and second guides include angled winglets , each winglet comprising a first distal shallow angle portion and a second steep angle portion extending from the first distal shallow angle portion, the first and second angle portions being angled relative to an exterior surface of the wing, wherein the winglets of the first wing face in an opposing direction to the winglets of the second wing. a first wing having a first guide ; a second wing having a second guide , the first and second guides configured to guide the aircraft to be aligned with a second and a third aircraft respectively during flight or hovering of the aircraft; a first lock coupled to the first wing, the first lock configured to secure the first wing to a third wing (1 10b) of the second aircraft when the first wing and the third wing are aligned; and a second lock coupled to the second wing, the second lock configured to secure the second wing to a fourth wing of the third aircraft when the second wing and the fourth wing are aligned, wherein the first and second guides include angled winglets , each winglet comprising a first distal shallow angle portion and a second steep angle portion extending from the first distal shallow angle portion, the first and second angle portions being angled relative to an exterior surface of the wing, wherein the winglets of the first wing face in an opposing direction to the winglets of the second wing.
A switching apparatus comprising first and second current paths, each current path configured to be capable of conducting an electrical current, the first current path including a first switching element connected in parallel with a first diode , the switching apparatus further including a switching controller configured to selectively control the switching of the first switching element , wherein the switching controller is configured to selectively switch the first switching element at a first intra-current path switching speed to commutate the electrical current between the first switching element and the first diode , the switching controller is configured to selectively switch the first switching element at a first inter-current path switching speed to commutate the electrical current between the first and second current paths, and the first intra-current path switching speed is faster or slower than the first inter-current path switching speed.
A system comprising: an initiator ; a target ; and a socket enabling communication of information between the initiator and the target , the socket consisting of: a first channel ; a second channel ; and a third channel , wherein the socket allows communication of information relating to cache-coherency, and wherein the initiator sends command requests through the first channel and receives command responses through the second channel ; and the target sends intervention requests through the second channel and receives intervention responses through the third channel . an initiator ; a target ; and a socket enabling communication of information between the initiator and the target , the socket consisting of: a first channel ; a second channel ; and a third channel , a first channel ; a second channel ; and a third channel , wherein the socket allows communication of information relating to cache-coherency, and wherein the initiator sends command requests through the first channel and receives command responses through the second channel ; and the target sends intervention requests through the second channel and receives intervention responses through the third channel .
A sports device comprising an abutment formed as a rod having a rigid support at its first end and a second end , which second end is formed as a free end and to which second end a person performing a movement can be connected at a body part via a rope by exerting a force on the second end , characterised in that a subregion of the rod has a rod cross-section, which rod cross-section has an element having an element height increasing from the central point of the rod cross-section towards a peripheral zone.
A closure device for a bag comprising: - a first support web carrying a first closure element , the first closure element comprising at least a first profile ; - a second support web carrying a second closure element complementary to the first closure element , the second closure element comprising at least a second profile and a third profile extending substantially in parallel along an axis of extension (X) the closure device being characterised in that the second profile and the third profile are each notched so as to be formed by a series of successive profile sections separated in pairs by notches , the sections of the second profile being offset with respect to the sections of the third profile along the extension axis (X), the closure device being characterised in that the sections of the second profile are longer along the axis of extension (X) than the sections of the third profile and the notches of the second profile are shorter than the notches of the third profile . - a first support web carrying a first closure element , the first closure element comprising at least a first profile ; - a second support web carrying a second closure element complementary to the first closure element , the second closure element comprising at least a second profile and a third profile extending substantially in parallel along an axis of extension (X) the closure device being characterised in that the second profile and the third profile are each notched so as to be formed by a series of successive profile sections separated in pairs by notches , the sections of the second profile being offset with respect to the sections of the third profile along the extension axis (X), the closure device being characterised in that the sections of the second profile are longer along the axis of extension (X) than the sections of the third profile and the notches of the second profile are shorter than the notches of the third profile . the closure device being characterised in that the second profile and the third profile are each notched so as to be formed by a series of successive profile sections separated in pairs by notches , the sections of the second profile being offset with respect to the sections of the third profile along the extension axis (X), the closure device being characterised in that the sections of the second profile are longer along the axis of extension (X) than the sections of the third profile and the notches of the second profile are shorter than the notches of the third profile .
A method of joining two thermoplastic components comprising: producing a first thermoplastic composite component by placing a first amorphous thermoplastic film on a first stack of thermoplastic pre-preg , and co-consolidating the first amorphous thermoplastic film and the first stack of thermoplastic pre-preg to provide a layer of the first amorphous thermoplastic film on the first stack of thermoplastic pre-preg; producing a second thermoplastic composite component by placing a second amorphous thermoplastic film on a second stack of thermoplastic pre-preg , and co-consolidating the second amorphous thermoplastic film and the second stack of thermoplastic pre-preg to provide a layer of the second amorphous thermoplastic film on the second stack of thermoplastic pre-preg; assembling the first and second thermoplastic composite components, including placing the first and second amorphous thermoplastic films against each other; pressing the first and second amorphous thermoplastic films against each other by applying pressure to the first and second thermoplastic composite components; and fusing the first and second amorphous thermoplastic films together at a temperature below approximately 475°F (246°C) ; wherein each of the first and second thermoplastic pre-preg is PEEK and each of the first and second amorphous thermoplastic films is PES. producing a first thermoplastic composite component by placing a first amorphous thermoplastic film on a first stack of thermoplastic pre-preg , and co-consolidating the first amorphous thermoplastic film and the first stack of thermoplastic pre-preg to provide a layer of the first amorphous thermoplastic film on the first stack of thermoplastic pre-preg; producing a second thermoplastic composite component by placing a second amorphous thermoplastic film on a second stack of thermoplastic pre-preg , and co-consolidating the second amorphous thermoplastic film and the second stack of thermoplastic pre-preg to provide a layer of the second amorphous thermoplastic film on the second stack of thermoplastic pre-preg; assembling the first and second thermoplastic composite components, including placing the first and second amorphous thermoplastic films against each other; pressing the first and second amorphous thermoplastic films against each other by applying pressure to the first and second thermoplastic composite components; and fusing the first and second amorphous thermoplastic films together at a temperature below approximately 475°F (246°C) ; wherein each of the first and second thermoplastic pre-preg is PEEK and each of the first and second amorphous thermoplastic films is PES.
Applicator for a cosmetic product comprising: - a core having a longitudinal axis (X) and presenting a first end, called proximal end , and a second free end, called distal end , and - a plurality of protrusions moulded with the core, said protrusions extending from the core and having a base located at the core and a free end, the core comprising at least one bending zone between its distal end and its proximal end, said core having a cross-section whose diameter varies with the longitudinal axis (X), the smallest diameter being at the centre of the bending zone , said applicator being characterized in that said bending zone has a minimum diameter in a portion of the brush located at more than half of the total length (L t ) of the brush, along the longitudinal axis (X), starting from the proximal end , the diameter of the core being higher at the centre of the proximal part than at the centre of the distal part of said core. - a core having a longitudinal axis (X) and presenting a first end, called proximal end , and a second free end, called distal end , and - a plurality of protrusions moulded with the core, said protrusions extending from the core and having a base located at the core and a free end,
A method for preserving erythrocytes comprising the steps of: a. obtaining an erythrocyte concentrate; b. placing said erythrocyte concentrate in a container, wherein at least a portion of said container is permeable to a gas system; c. removing oxygen from the erythrocyte concentrate while said erythrocyte concentrate is in said container, said oxygen being removed from said erythrocyte concentrate and said container by diffusion of said oxygen through said container; d. subjecting said erythrocyte concentrate while in said container to said gas system by causing said gas system to diffuse through said container to said erythrocyte concentrate in said container, said gas system includes xenon at a concentration that is greater than 50% by volume and includes oxygen in a concentration of less than 5% by volume; and, e. maintaining said erythrocyte concentrate that has been subjected to the gas system at a temperature that is above the freezing point of the erythrocyte concentrate and up to a temperature of 30°C. a. obtaining an erythrocyte concentrate; b. placing said erythrocyte concentrate in a container, wherein at least a portion of said container is permeable to a gas system; c. removing oxygen from the erythrocyte concentrate while said erythrocyte concentrate is in said container, said oxygen being removed from said erythrocyte concentrate and said container by diffusion of said oxygen through said container; d. subjecting said erythrocyte concentrate while in said container to said gas system by causing said gas system to diffuse through said container to said erythrocyte concentrate in said container, said gas system includes xenon at a concentration that is greater than 50% by volume and includes oxygen in a concentration of less than 5% by volume; and, e. maintaining said erythrocyte concentrate that has been subjected to the gas system at a temperature that is above the freezing point of the erythrocyte concentrate and up to a temperature of 30°C.
A venting valve for venting a drive assembly of a motor vehicle, in particular of a hybrid module, comprising a first chamber for forming a first flow path along a first flow direction , wherein the first chamber has an arrangement side for mechanically fixing on a housing of the drive assembly and, on the side opposite the arrangement side , has an oblique boundary wall , the plane of which runs at an acute angle with respect to the first flow direction and projects laterally beyond the first chamber so that, when the venting valve is oriented perpendicularly, gas rising through the first chamber can be deflected from the oblique boundary wall and condensate adhering to the oblique boundary wall can run off the oblique boundary wall and can drip down next to the first chamber , wherein a second chamber is arranged next to the first chamber which is closed on one side by the oblique boundary wall and has an opening on the side opposite the oblique boundary wall , the second chamber which at least partially surrounds the opening has a spray protection with which a flow resistance for inflowing liquid is increased or a barrier against spray liquid is formed, characterised in that starting from the edge of the opening of the second chamber , the spray protection extends radially inwards relative to a longitudinal axis of the second chamber , so that the cross-section of the opening of the second chamber is thereby restricted. the second chamber which at least partially surrounds the opening has a spray protection with which a flow resistance for inflowing liquid is increased or a barrier against spray liquid is formed, characterised in that starting from the edge of the opening of the second chamber , the spray protection extends radially inwards relative to a longitudinal axis of the second chamber , so that the cross-section of the opening of the second chamber is thereby restricted.
A peptide represented by the formula (I): wherein P 1 is a hydrogen atom or a methyl group R A10 is Pal or Oda A11 is Aib, Ala or Ser; A12 is Ile or Lys; A15 is Asp or Glu; A18 is Ala or Arg; and A35 is Tyr or Phe(2-F), or a salt thereof. P 1 is a hydrogen atom or a methyl group R A10 is Pal or Oda A11 is Aib, Ala or Ser; A12 is Ile or Lys; A15 is Asp or Glu; A18 is Ala or Arg; and A35 is Tyr or Phe(2-F), or a salt thereof.
An alpha-amylase variant comprising a substitution at a position corresponding to position 188 and at least one further substitution at a position corresponding to position 242 or 279 or 275 of SEQ ID NO: 1, wherein the substitutions are selected from the group consisting of E188P+S242Y, E188P+S242F, E188P+S242H, E188P+S242W, E188P+S242P, E188P+S242I, E188P+S242T, E188P+S242L, E188P+K279W, E188P+K279Y, E188P+K279F, E188P+K279H, E188P+K279I, E188P+K279L, E188P+K279D, E188P+K279M, E188P+K279S, E188P+K279T, E188P+K279N, E188P+K279Q, E188P+K279V, E188P+K279A, E188P+N275F, E188P+N275Y, E188P+N275W, and E188P+N275H, wherein the variant has at least 70%, at least 75%, at least 80%, at least 85%, at least 90%, at least 95%, at least 96%, at least 97%, at least 98%, or at least 99%, but less than 100% sequence identity to a parent alpha amylase selected from the group consisting of: SEQ ID NO: 1, SEQ ID NO: 2, SEQ ID NO: 3, SEQ ID NO: 4, SEQ ID NO: 5, SEQ ID NO: 6, SEQ ID NO: 7, SEQ ID NO: 8, SEQ ID NO: 9, SEQ ID NO: 10, SEQ ID NO: 11, SEQ ID NO: 12, SEQ ID NO: 13, SEQ ID NO: 14, SEQ ID NO: 16, SEQ ID NO: 17, and SEQ ID NO: 27, and wherein the variant has increased thermo-stability at pH 4.5 over the parent alpha-amylase or increased chelator stability in model detergent A over the parent alpha-amylase.
A managed system , comprising: a processor , configured to determine whether at least one type of alarm information of an alarm is changed, wherein the alarm information comprises: a backup status identifier of an object of the alarm, a backup object identifier of the alarm, an identifier of a change trend of the alarm, threshold information of the alarm, change information of a configured object, a monitored attribute of a managed object, a repair suggestion for the alarm, and additional content that is of the alarm and that is used to indicate an attribute of the managed object; and a transmitter , configured to: after the processor determines that at least one type of the alarm information of the alarm is changed, send changed alarm information and an identifier of the alarm to a management system. a processor , configured to determine whether at least one type of alarm information of an alarm is changed, wherein the alarm information comprises: a backup status identifier of an object of the alarm, a backup object identifier of the alarm, an identifier of a change trend of the alarm, threshold information of the alarm, change information of a configured object, a monitored attribute of a managed object, a repair suggestion for the alarm, and additional content that is of the alarm and that is used to indicate an attribute of the managed object; and a transmitter , configured to: after the processor determines that at least one type of the alarm information of the alarm is changed, send changed alarm information and an identifier of the alarm to a management system.