mhurhangee/patent-ind-claim-en huggingface dataset:
A method for time setting a sympathetic watch by a sympathetic clock , with which said watch forms a sympathetic assembly including a connection mechanism including at least two distinct transmission lines between said clock and said watch when said watch is deposited in a receptacle included in said clock , in a transfer position, said watch including at least one resonator , and a display gear train and a finishing gear train, and, either a stop mechanism arranged to stop the operation of said resonator , or a coupling mechanism allowing to separate the display from the finishing gear train, or else both such a stop mechanism and such a coupling mechanism, and said watch including at least one hour display and one minute display , a reference position of which will be defined, the method being such that the time-setting is carried out, or at request by action of a user on a control means included in said clock or said watch , or periodically automatically controlled by said clock , and being characterized in that to perform said relative time setting, said clock drives said displays (4; 5), of the watch backwards, in the counter-clockwise direction, with a stroke long enough to guarantee the passage of said displays (4; 5), by said reference position.
A method for degrading or converting a cellulosic material, comprising: treating the cellulosic material with an enzyme composition comprising a cellulase in the presence of a GH61 polypeptide having cellulolytic enhancing activity and a liquor arising from treatment of a lignocellulose material, a hemicellulose material, a lignacious material, monosaccharides of the lignocellulose material, monosaccharides of the hemicellulose material, or a combination thereof, wherein the liquor is present in an amount that minimizes inhibition of a cellulase composition of 1 to 20% (v/v), wherein the combination of the GH61 polypeptide having cellulolytic enhancing activity and the liquor enhances hydrolysis of the cellulosic material by the enzyme composition, wherein the enhanced hydrolysis is assessed according to Equation 3: GH 61 effect = % conversion + GH 61 + liquor % conversion no GH 61 + liquor and the equation ratio is greater than 1, wherein the GH61 polypeptide having cellulolytic enhancing activity comprises the following motifs: [ILMV]-P-X -G-X-Y-[ILMV]-X-R-X-[EQ]-X -[HNQ] (SEQ ID NO: 127 or SEQ ID NO: 128) and [FW]-[TF]-K-[AIV], wherein X is any amino acid, X is any amino acid at 4 or 5 contiguous positions, and X is any amino acid at 4 contiguous positions.
A three-dimensional printed object comprising: a first lattice structure comprising a first matrix , the first matrix having a first length , a first width , and a first height ; and a second lattice structure comprising a second matrix , the second matrix having a second length , a second width , and a second height , wherein the second length times two is a factor of the first length, the second width times two is a factor of the first width, and the second height times two is a factor of the first height. a first lattice structure comprising a first matrix , the first matrix having a first length , a first width , and a first height ; and a second lattice structure comprising a second matrix , the second matrix having a second length , a second width , and a second height , wherein the second length times two is a factor of the first length, the second width times two is a factor of the first width, and the second height times two is a factor of the first height.
Turbine nozzle for a turbine engine comprising at least one vane and a foot which has a platform , the platform comprising on one hand a radially external surface from which each vane extends and intended to be partially delimit a gas jet from the turbine engine, and on the other a radially internal surface intended to partially delimit a gas blow-by cavity radially under the platform , the nozzle is equipped with a passive system for reintroducing blow-by gas into the jet, the system comprising gas extraction orifices located on the foot , as well as gas reinjection orifices located on the radially external surface of the platform and/or on an upper surface of said at least one vane , said gas reinjection orifices being configured to redirect the gas flow from the gas blow-by cavity along a reinjection direction comprising a circumferential orientation , and in that said reinjection direction has a radial orientation such that, viewed along an axial cross-section through any one of the gas reinjection orifices , this reinjection direction is parallel or substantially parallel locally with the radially external surface of the platform, characterised in that said gas reinjection orifices open onto a downstream part of the radially external surface of the platform, and/or onto a radially internal part of the upper surface of said at least one vane , and in that the foot includes an axial tab extending downstream, the gas extraction orifices being arranged between the radially internal surface of the platform, and said axial tab , said axial tab extending axially so as to have an axial overlap zone with an upstream spoiler of a mobile wheel arranged downstream from the nozzle. the nozzle is equipped with a passive system for reintroducing blow-by gas into the jet, the system comprising gas extraction orifices located on the foot , as well as gas reinjection orifices located on the radially external surface of the platform and/or on an upper surface of said at least one vane , said gas reinjection orifices being configured to redirect the gas flow from the gas blow-by cavity along a reinjection direction comprising a circumferential orientation , and in that said reinjection direction has a radial orientation such that, viewed along an axial cross-section through any one of the gas reinjection orifices , this reinjection direction is parallel or substantially parallel locally with the radially external surface of the platform, characterised in that said gas reinjection orifices open onto a downstream part of the radially external surface of the platform, and/or onto a radially internal part of the upper surface of said at least one vane , and in that the foot includes an axial tab extending downstream, the gas extraction orifices being arranged between the radially internal surface of the platform, and said axial tab , said axial tab extending axially so as to have an axial overlap zone with an upstream spoiler of a mobile wheel arranged downstream from the nozzle.
Method of production of a multilayer including a non-woven fibrous first layer , a second layer and a core layer of cementitious material including cement and cellulose fibers between the first layer and the second layer , the method comprising i) spreading cementitious material on the second layer , ii) placing the first layer on the cementitious material, iii) needle bonding the first layer and the second layer with elongated elements that drive a plurality of fibers of the first layer through the core layer to attach the said plurality of fibers to the second layer and iv) obtaining of the multilayer that is flexible, it is configured to be curved in two directions and it becomes rigid upon absorbing water.
A wing structure for a supersonic aircraft comprising: two laterally extending wings , a pair of supersonic wave-tripping channels formed on each of the two laterally extending wings of the supersonic aircraft, wherein each of the pair of supersonic wave-tripping channels extend in a span-wise direction of the wings respectively, wherein an upper supersonic wave-tripping channel of the pair of supersonic wave-tripping channels is disposed on an upper surface of each of the wings and a lower supersonic wave-tripping channel of the pair of supersonic wave-tripping channels is disposed on a lower surface of each of the wings, wherein the upper supersonic wave-tripping channel and the lower supersonic wave-tripping channel are set back from a leading edge of the wings respectively. two laterally extending wings , a pair of supersonic wave-tripping channels formed on each of the two laterally extending wings of the supersonic aircraft, wherein each of the pair of supersonic wave-tripping channels extend in a span-wise direction of the wings respectively, wherein an upper supersonic wave-tripping channel of the pair of supersonic wave-tripping channels is disposed on an upper surface of each of the wings and a lower supersonic wave-tripping channel of the pair of supersonic wave-tripping channels is disposed on a lower surface of each of the wings, wherein the upper supersonic wave-tripping channel and the lower supersonic wave-tripping channel are set back from a leading edge of the wings respectively.
Assembly of modular electrical units intended to be mounted on a mounting rail comprising, for at least one of the units, a locking device, said device comprising at least one catch comprising a mobile part able to slide with respect to the casing of the unit, said part comprising a first end portion able to collaborate with one, referred to as the first, of the longitudinal edges of the rail and a second end portion, referred to as the manipulation end portion, able to be manipulated by a user so as to move said catch between a first position in which said catch fixes the unit to the rail in collaboration with a fixed end stop belonging to the casing collaborating with the opposite longitudinal edge to the previous one, and a second position in which said first end portion of the catch no longer collaborates with the edge of the rail so as to allow the unit to be extracted from said rail, this locking device comprising an extension device (P) extending the manipulation portion of said at least one catch , said extension device (P) comprising a first end portion able to be fixed to the manipulation portion of said at least one catch, and a second end portion comprising manipulation means able to be actuated by the user so as to operate the catch or catches, characterized in that the unit is a three-pole electrical protection unit (D) comprising three switching modules or a four-pole electrical protection unit comprising four switching modules (22 to 25), said modules being contiguous via their lateral faces and forming a single-piece assembly, and in that the locking device comprises two catches associated respectively with the two switching modules situated at the end of said assembly in the case of the three-pole unit or associated respectively with two of the switching modules which are separated by a switching module that does not have a catch in the case of the four-pole unit, said extension device comprising two branches , referred to as first fixing branches, comprising catching means for catching respectively on the two manipulation portions of the aforementioned two catches and a branch, referred to as second branch , situated between the two first branches and comprising guide means able to collaborate in sliding with the casing of the module situated between the aforementioned two modules associated with a catch, said so-called first and second branches forming portions of the one same part of the extension device (P).
A fixation system configured for attaching a navigation array to a bony structure for use in a robotic-assisted surgery, comprising: - a fixation device , comprising: - a trocar ; - a cortical pin configured to be inserted into the trocar ; - a dowel configured to be attached to the cortical pin , wherein the dowel is configured to prevent rotation of the cortical pin in the bony structure; and - a navigation array configured to be removably attached to the cortical pin , characterized in that - the dowel is a spring device having a torsion-spring structure configured to be deployed at a tip of the cortical pin . - a fixation device , comprising: - a trocar ; - a cortical pin configured to be inserted into the trocar ; - a dowel configured to be attached to the cortical pin , wherein the dowel is configured to prevent rotation of the cortical pin in the bony structure; and - a navigation array configured to be removably attached to the cortical pin , characterized in that - the dowel is a spring device having a torsion-spring structure - a trocar ; - a cortical pin configured to be inserted into the trocar ; - a dowel configured to be attached to the cortical pin , wherein the dowel is configured to prevent rotation of the cortical pin in the bony structure; and - a navigation array configured to be removably attached to the cortical pin , characterized in that - the dowel is a spring device having a torsion-spring structure
An optical imaging system having a single focus, comprising a negative first lens group , an aperture stop (S), and a positive second lens group arranged in order from an object side, the negative first lens group comprising a positive first front lens group including a positive single lens (L1) and a negative first rear lens group including a negative meniscus lens (L2) and at least one positive lens (L3), arranged in order from the object side, and the positive second lens group comprising a positive second front lens group including a cemented lens of a negative lens and a positive lens (L4, L5) and a positive second rear lens group including at least one positive lens (L6), arranged in order from the object side, wherein: all of the lenses of the optical imaging system are spherical glass lenses; the first lens group includes a positive lens having a convex surface on the object side (L1), a negative meniscus lens having a convex surface on the object side (L2), and a positive lens (L3); and the first lens group is configured to satisfy the following conditions: 2.5 < f 1 ⁢ F / f < 7.1 − 3.7 < f 1 ⁢ R / f < − 0.8 where f is a focal length of the entire optical imaging system relative to a d-line, f1F is a focal length of the first front lens group , and f1R is a focal length of the first rear lens group , and characterized in that : the positive lens (L3) has a convex surface on the object side arranged in order from the object side; and in that the second rear lens group includes a positive meniscus lens (L6) having a convex surface on the image side and a positive lens (L7) having a convex surface on the object side. all of the lenses of the optical imaging system are spherical glass lenses; the first lens group includes a positive lens having a convex surface on the object side (L1), a negative meniscus lens having a convex surface on the object side (L2), and a positive lens (L3); and the first lens group is configured to satisfy the following conditions: 2.5 < f 1 ⁢ F / f < 7.1 − 3.7 < f 1 ⁢ R / f < − 0.8 where f is a focal length of the entire optical imaging system relative to a d-line, f1F is a focal length of the first front lens group , and f1R is a focal length of the first rear lens group , and characterized in that : the positive lens (L3) has a convex surface on the object side arranged in order from the object side; and in that the second rear lens group includes a positive meniscus lens (L6) having a convex surface on the image side and a positive lens (L7) having a convex surface on the object side. the positive lens (L3) has a convex surface on the object side arranged in order from the object side; and in that the second rear lens group includes a positive meniscus lens (L6) having a convex surface on the image side and a positive lens (L7) having a convex surface on the object side.
A fuel injector for a gas turbine engine comprising: a fuel nozzle configured to issue a spray of fuel from a fuel outlet in a downstream direction along an injection axis, the fuel nozzle including a nozzle body that defines a main flow passage therethrough; an injection fuel line in fluid communication with the fuel nozzle to supply fuel to the fuel nozzle; and a torch ignitor with a flame outlet opening into the main flow passage of the fuel nozzle for issuing flame into the main flow passage, wherein the flame outlet meets the main flow passage at a position that is downstream of the fuel outlet with respect to the downstream direction along the injection axis; characterized in that the injection fuel line and torch ignitor define a feed arm that extends perpendicular relative to the injection axis of the fuel nozzle . a fuel nozzle configured to issue a spray of fuel from a fuel outlet in a downstream direction along an injection axis, the fuel nozzle including a nozzle body that defines a main flow passage therethrough; an injection fuel line in fluid communication with the fuel nozzle to supply fuel to the fuel nozzle; and a torch ignitor with a flame outlet opening into the main flow passage of the fuel nozzle for issuing flame into the main flow passage, wherein the flame outlet meets the main flow passage at a position that is downstream of the fuel outlet with respect to the downstream direction along the injection axis; characterized in that the injection fuel line and torch ignitor define a feed arm that extends perpendicular relative to the injection axis of the fuel nozzle .
A pressure sensor , comprising: a sensor housing having a diaphragm , wherein the diaphragm has an anisotropic shape having a short side and a long side, wherein a short-side direction is an X axis direction of the diaphragm and a long-side direction is an Y axis direction of the diaphragm ; and a sensor chip including four strain gauges (7a - 7d), the four strain gauges (7a - 7d) are provided on the sensor chip so as to be positioned in a central portion of the diaphragm ; wherein two strain gauges of the four strain gauges are provided on the sensor chip in the short-side direction of the diaphragm , the other two strain gauges are provided on the sensor chip in the long-side direction of the diaphragm , characterized in that the minimum thickness of the diaphragm in a cross-section in the long-side direction, the cross-section being across the center of the diaphragm , is thinner than the minimum thickness of the diaphragm in a cross-section in the short-side direction, the cross-section being across the center of the diaphragm and wherein the diaphragm has, in the long-side direction, a thin portion whose thickness is thinner than a thickness of a region in which the sensor chip is mounted. a sensor housing having a diaphragm , wherein the diaphragm has an anisotropic shape having a short side and a long side, wherein a short-side direction is an X axis direction of the diaphragm and a long-side direction is an Y axis direction of the diaphragm ; and a sensor chip including four strain gauges (7a - 7d), the four strain gauges (7a - 7d) are provided on the sensor chip so as to be positioned in a central portion of the diaphragm ; wherein two strain gauges of the four strain gauges are provided on the sensor chip in the short-side direction of the diaphragm , the other two strain gauges are provided on the sensor chip in the long-side direction of the diaphragm , characterized in that the minimum thickness of the diaphragm in a cross-section in the long-side direction, the cross-section being across the center of the diaphragm , is thinner than the minimum thickness of the diaphragm in a cross-section in the short-side direction, the cross-section being across the center of the diaphragm and wherein the diaphragm has, in the long-side direction, a thin portion whose thickness is thinner than a thickness of a region in which the sensor chip is mounted.
A drum for a carding machine , comprising a cylindrical drum shell (M) that has a wall thickness (a, d1, d2) and is connected in the interior space (IR) to at least two spokes (S1, S2, S3, S4) that run in a radial direction and are arranged at a distance (b) from one another, as seen in the axial direction of the drum , in which the wall thickness of the drum shell (M) is of a greater dimension (d1) in the area of the connection (V1, V2) from the respective spoke (S3, S4) than the wall thickness outside of this connecting area (V1, V2), in that the wall thickness (d1) of the drum shell - as seen in the axial direction of the drum - decreases to a minimum wall thickness (d2) - at least in the area between the spokes (S3, S4) - starting from the connecting area of the respective spoke, characterized in that the reduction in wall thickness of the drum shell (M) is continuous or in the form of a curve.
Axial ball joint for a length-adjustable two-point link , the axial ball joint having a housing and a ball pin with a joint ball rotatably and pivotably mounted in the housing ), which, in the non-deflected state, extends out of the housing in an axial direction , wherein the ball pin is, inter alia, rotatably mounted in the housing and can be attached in a length-adjustable manner via a threaded connection to a connection component, wherein the ball pin has on its outer circumference a driver geometry , and wherein the housing has a connection pin connected in one piece to the latter, which extends at least substantially at right angles to the axial direction , characterized in that the housing is closed at one axial end by an axial support , which is formed as a rotary part or as a rotationally symmetrical extruded part with a thickness varying in the axial direction .
A communication device for communicating data over a low power wide area, LPWA, communication network , wherein the communication device comprises: a processor configured to process data; a memory configured to store data; a radio configured to transmit and receive data over the LPWA communication network ; and a security system configured to operate one or more logically separated sets of security domains (111 a-c, 113a-c, 115a-c), including a first set of security domains , on the processor and the memory , wherein each set of security domains comprises a processor security domain (111a-c) and a memory security domain (113a-c, 115a-c), wherein the processor security domain of the first set of security domains is configured to implement a monitoring and control function and wherein the processor security domain of the first set of security domains is configured to monitor and control the operation of the communication device on the basis of the monitoring and control function, wherein the processor is configured to implement a real-time execution environment based on a real-time operating system and wherein the security system is configured to operate the respective processor security domains (111a-c) of the one or more sets of security domains (111a-c, 113a-c, 115a-c) in parallel to the real-time execution environment . a processor configured to process data; a memory configured to store data; a radio configured to transmit and receive data over the LPWA communication network ; and a security system configured to operate one or more logically separated sets of security domains (111 a-c, 113a-c, 115a-c), including a first set of security domains , on the processor and the memory , wherein each set of security domains comprises a processor security domain (111a-c) and a memory security domain (113a-c, 115a-c), wherein the processor security domain of the first set of security domains is configured to implement a monitoring and control function and wherein the processor security domain of the first set of security domains is configured to monitor and control the operation of the communication device on the basis of the monitoring and control function, wherein the processor is configured to implement a real-time execution environment based on a real-time operating system and wherein the security system is configured to operate the respective processor security domains (111a-c) of the one or more sets of security domains (111a-c, 113a-c, 115a-c) in parallel to the real-time execution environment .