mhurhangee/patent-ind-claim-en huggingface dataset:
System for resetting a chronograph, which is provided with a chronograph counting train , which comprises at least a minute counter having a minute wheel set , and a seconds counter, which comprises a chronograph wheel set , the minute wheel set including a heart-piece , constituting a cam shape, mounted on a central arbor of the minute wheel set and the chronograph wheel set including a heart-piece mounted on a central arbor of the chronograph wheel set, the system comprising a hammer immobilised by an immobilising means and capable of being displaced from an inactive position, where the hammer is immobilised by the immobilising means , and an active position, when the hammer is released, to reset the chronograph in contact with the various heart-pieces of the wheel sets , the system comprising a flexible element connected between a reset control means and the hammer used for resetting the chronograph, the flexible element being configured in such a way as to store energy during a displacement of the control means before the hammer is released by the immobilising means in order to be able, when the hammer is released, to output this stored energy and drive the hammer to reset the chronograph, the flexible element being connected by a first end to the hammer , which is used for resetting the chronograph, characterised in that a second end of the flexible element is fastened to the control means which is mounted on a base, frame or plate of a timepiece, and in that the flexible element has an arcuate shape from a rest position between its first end and its second end , this arcuate shape being oriented towards an external activation member (B) of the control means in such a way as to accumulate energy as a result of the external activation member being pressed and to output the accumulated energy when the hammer is released in order to reset the chronograph. the system comprising a flexible element connected between a reset control means and the hammer used for resetting the chronograph, the flexible element being configured in such a way as to store energy during a displacement of the control means before the hammer is released by the immobilising means in order to be able, when the hammer is released, to output this stored energy and drive the hammer to reset the chronograph, the flexible element being connected by a first end to the hammer , which is used for resetting the chronograph, characterised in that a second end of the flexible element is fastened to the control means which is mounted on a base, frame or plate of a timepiece, and in that the flexible element has an arcuate shape from a rest position between its first end and its second end , this arcuate shape being oriented towards an external activation member (B) of the control means in such a way as to accumulate energy as a result of the external activation member being pressed and to output the accumulated energy when the hammer is released in order to reset the chronograph.
A multi-layered film consisting of at least three layers, comprising an outer layer, a sealing layer, and a hot-melt adhesive layer, between the outer layer and the sealing layer, for bonding the outer layer and the sealing layer, characterized in that the hot-melt adhesive layer comprises a hot-melt adhesive containing a) 10 to 40 wt.% of at least one branched styrene-isoprene-styrene block copolymer having a percentual weight proportion by weight of diblocks to the polymer of less than 30% and having a melt flow index of less than 5 g/10 minutes at 200 °C and a test load of 5 kg; b) 0 to 40 wt.% of at least one styrene polymer or a styrene copolymer; c) 20 to 60 wt.% of at least one tackifying resin; d) 0 to 15 wt.% of at least one plasticizer; e) 0 to 16 wt.% additives and admixtures selected from stabilizers, adhesion promoters, fillers or pigments, waxes and/or other polymers. a) 10 to 40 wt.% of at least one branched styrene-isoprene-styrene block copolymer having a percentual weight proportion by weight of diblocks to the polymer of less than 30% and having a melt flow index of less than 5 g/10 minutes at 200 °C and a test load of 5 kg; b) 0 to 40 wt.% of at least one styrene polymer or a styrene copolymer; c) 20 to 60 wt.% of at least one tackifying resin; d) 0 to 15 wt.% of at least one plasticizer; e) 0 to 16 wt.% additives and admixtures selected from stabilizers, adhesion promoters, fillers or pigments, waxes and/or other polymers.
An apparatus to verify the presence, or the absence, of an abrasive element in a machine for finishing surfaces, said machine comprising: - a support body configured to removably engage said abrasive element , said support body and said abrasive element being, respectively, provided, at respective engagement surfaces with first and second engagement elements configured to move from an engagement configuration to a disengagement configuration, and vice versa; - a displacement device configured to move said support body in the space according to at least 1 degree of freedom; said apparatus comprising: - at least a control station arranged to verify the presence, or the absence, of said abrasive element at said support body ; - a control device arranged in said control station and comprising a control element having a control surface , said displacement device being arranged to bring said support body , or the abrasive element constrained to the same, if present, into contact with said control surface of said control element and to cause a movement of said support body ; - a detection device configured to detect if an engagement between said control element and said support body has taken place, during said movement of said support body by said displacement device ; said apparatus being characterized in that said control surface is provided with third engagement elements configured to engage with said first engagement elements of said support body . - a support body configured to removably engage said abrasive element , said support body and said abrasive element being, respectively, provided, at respective engagement surfaces with first and second engagement elements configured to move from an engagement configuration to a disengagement configuration, and vice versa; - a displacement device configured to move said support body in the space according to at least 1 degree of freedom; - at least a control station arranged to verify the presence, or the absence, of said abrasive element at said support body ; - a control device arranged in said control station and comprising a control element having a control surface , said displacement device being arranged to bring said support body , or the abrasive element constrained to the same, if present, into contact with said control surface of said control element and to cause a movement of said support body ; - a detection device configured to detect if an engagement between said control element and said support body has taken place, during said movement of said support body by said displacement device ;
A precipitation hardenable, cobalt-nickel base superalloy comprising in weight percent: C 0.01 to 0.15 Cr 7.00 to 9.8 Ni 34.00 to 45.00 W 3.00 to 12.00 Ti 0.50 to 2.00 Al 3.00 to 7.00 Nb up to 2.50 Ta up to 6.00 Hf up to 1.50 Zr up to 1.50 B up to 0.20 Mo up to 2.50 Si up to 1.50 the balance being cobalt and usual impurities.
A compound, or a pharmaceutically acceptable salt thereof, wherein said compound is selected from the group consisting of:
An RFID tag for being fastened to a textile , the RFID tag having a transponder unit , which is attached to a bendable carrier material and has an integrated circuit having a conductor structure electrically connected via contact surfaces , characterised in that the carrier material is designed as a conductor structure having a longitudinal slot being a T-shaped slot, wherein the long T-leg extending in the longitudinal direction of the carrier material determines the distance of the antenna dipoles extending in the longitudinal direction of the carrier material , whereas the short T-leg separates the contact surfaces of opposite polarity from each other, the carrier material being strip-shaped and having a length (L)-to-width (W) ratio which is a multiple of ten.
A method of joining two sections of lined pipe , each section of lined pipe comprising a pipe lining and a host pipe , the method comprising providing each section of lined pipe with an insulatory sleeve between the pipe lining and the host pipe , and subsequently welding the ends of the host pipes of the two sections of lined pipe together, wherein the insulatory sleeve is provided in the section of lined pipe by locating the insulatory sleeve in an end of the host pipe , temporarily reducing the diameter of the pipe lining and drawing it through the host pipe and the insulatory sleeve , and allowing the pipe lining to revert to form a tight fit against internal surfaces of the host pipe and insulatory sleeve , and wherein the insulatory sleeve extends to or beyond the end of the pipe lining and not beyond the corresponding end of the host pipe , and does not extend the full length of the section of lined pipe .
A method for producing a dashboard of a motor-vehicle by means of additive manufacturing technology, wherein the following steps are envisaged: - arranging a robotic deposition system for a plurality of materials with fused deposition modeling FDM TM technology, - preparing a construction plane associated with said robotic system , on which to deposit said plurality of materials, in such a way as to produce said dashboard , - operating said robotic system so as to start a step of depositing said plurality of materials to produce a first end of the dashboard , and to continue depositing the materials by creating a succession of different layers, alternating materials with different types of filaments, comprising at least one material with structural characteristics and at least one material with sound-absorbing characteristics , - wherein said succession of different layers is performed proceeding from said first end along a direction substantially corresponding to the longitudinal axis of the dashboard , and - continuing to operate said robotic system so as to produce said dashboard as a single monolithic element made of different materials, comprising a casing incorporating a longitudinal hollow bearing-element defining a central ventilation channel, designed to receive further channeling elements of a conditioning system and to perform a function of structural reinforcement of said dashboard . - arranging a robotic deposition system for a plurality of materials with fused deposition modeling FDM TM technology, - preparing a construction plane associated with said robotic system , on which to deposit said plurality of materials, in such a way as to produce said dashboard , - operating said robotic system so as to start a step of depositing said plurality of materials to produce a first end of the dashboard , and to continue depositing the materials by creating a succession of different layers, alternating materials with different types of filaments, comprising at least one material with structural characteristics and at least one material with sound-absorbing characteristics , - wherein said succession of different layers is performed proceeding from said first end along a direction substantially corresponding to the longitudinal axis of the dashboard , and - continuing to operate said robotic system so as to produce said dashboard as a single monolithic element made of different materials, comprising a casing incorporating a longitudinal hollow bearing-element defining a central ventilation channel, designed to receive further channeling elements of a conditioning system and to perform a function of structural reinforcement of said dashboard .
An additional brake device for a passenger transport device, the additional brake device comprising: a brake disc defining a hole and having an inner circumferential surface ; a wheel disc having a wheel disc body and an extension , the extension being fitted into the hole of the brake disc and having an outer circumferential surface , and a first friction plate being provided between the brake disc and the wheel disc body ; and a pressure holding mechanism which maintains a pressure between the brake disc and the wheel disc ; wherein an intermediate member is provided between the inner circumferential surface of the brake disc and the outer circumferential surface of the extension of the wheel disc ; and the intermediate member is coupled to the inner circumferential surface of the brake disc or the outer circumferential surface of the extension of the wheel disc ; characterized in that : the intermediate member comprises a metal or alloy material. a brake disc defining a hole and having an inner circumferential surface ; a wheel disc having a wheel disc body and an extension , the extension being fitted into the hole of the brake disc and having an outer circumferential surface , and a first friction plate being provided between the brake disc and the wheel disc body ; and a pressure holding mechanism which maintains a pressure between the brake disc and the wheel disc ; wherein an intermediate member is provided between the inner circumferential surface of the brake disc and the outer circumferential surface of the extension of the wheel disc ; and the intermediate member is coupled to the inner circumferential surface of the brake disc or the outer circumferential surface of the extension of the wheel disc ; characterized in that : the intermediate member comprises a metal or alloy material.
A gas turbine engine (10; 110) for an aircraft, comprising: a first spool having a low pressure compressor section disposed forward of an air inlet along a direction of travel (D) of the engine (10; 110) and in fluid communication with the air inlet , and a low pressure turbine section disposed forward of the low pressure compressor section and drivingly engaged thereto; a second spool having a high pressure compressor section disposed forward of the low pressure compressor section and in fluid communication therewith to receive pressurized air therefrom, and a high pressure turbine section disposed forward of the high pressure compressor section and drivingly engaged thereto, the high pressure turbine section disposed aft of the low pressure turbine section and in fluid communication therewith; characterised in that the gas turbine engine further comprises an output drive shaft drivingly engaged to the low pressure turbine section and extending forwardly therefrom, the drive shaft configurable to drivingly engage a rotatable load disposed forward of the low pressure turbine section . a first spool having a low pressure compressor section disposed forward of an air inlet along a direction of travel (D) of the engine (10; 110) and in fluid communication with the air inlet , and a low pressure turbine section disposed forward of the low pressure compressor section and drivingly engaged thereto; a second spool having a high pressure compressor section disposed forward of the low pressure compressor section and in fluid communication therewith to receive pressurized air therefrom, and a high pressure turbine section disposed forward of the high pressure compressor section and drivingly engaged thereto, the high pressure turbine section disposed aft of the low pressure turbine section and in fluid communication therewith; characterised in that the gas turbine engine further comprises an output drive shaft drivingly engaged to the low pressure turbine section and extending forwardly therefrom, the drive shaft configurable to drivingly engage a rotatable load disposed forward of the low pressure turbine section .
A compound of formula (I): or a salt thereof, wherein: R 1 is C 1-12 alkyl, C 2-12 alkenyl, C 2-12 alkynyl, 3-12 membered carbocycle, and 3-12 membered heterocycle, wherein each C 1-12 alkyl, C 2-12 alkenyl, C 2-12 alkynyl, 3-12 membered carbocycle, and 3-12 membered heterocycle of R 1 is optionally substituted with one or more groups R d ; R 2 is -C(O)-N(R e )2, wherein -X-Y is selected from the group consisting of: each R d is independently selected from the group consisting of oxo, halo, cyano, hydroxy, amino, C 1-4 alkyl, C 2-4 alkenyl, C 2-4 alkynyl, a cycloalkyl moiety having up to 6 carbon atoms, (a cycloalkyl moiety having up to 6 carbon atoms)-C 1-4 alkyl, C 1-4 alkoxy, C 1-4 alkoxycarbonyl, C 1- 4 alkanoyl, and C 1-4 alkanoyloxy, wherein each C 1-4 alkyl, C 2-4 alkenyl, C 2-4 alkynyl, cycloalkyl moiety having up to 6 carbon atoms, (cycloalkyl moiety having up to 6 carbon atoms)-C 1-4 alkyl, C 1-4 alkoxy, C 1-4 alkoxycarbonyl, C 1-4 alkanoyl, and C 1-4 alkanoyloxy, is optionally substituted with one or more groups independently selected from oxo, halo, amino, hydroxy, C 1-3 alkoxy, and C 1 -C 3 alkyl that is optionally substituted with one or more groups independently selected from halo, wherein the term alkoxy refers to a linear or branched radical represented by the formula -OR in which R is alkyl, alkenyl, alkynyl or carbocycyl; and each R e is independently selected from hydrogen and C 1-4 alkyl; or a compound selected from the group consisting of: or a salt thereof. R 1 is C 1-12 alkyl, C 2-12 alkenyl, C 2-12 alkynyl, 3-12 membered carbocycle, and 3-12 membered heterocycle, wherein each C 1-12 alkyl, C 2-12 alkenyl, C 2-12 alkynyl, 3-12 membered carbocycle, and 3-12 membered heterocycle of R 1 is optionally substituted with one or more groups R d ; R 2 is -C(O)-N(R e )2, wherein -X-Y is selected from the group consisting of: each R d is independently selected from the group consisting of oxo, halo, cyano, hydroxy, amino, C 1-4 alkyl, C 2-4 alkenyl, C 2-4 alkynyl, a cycloalkyl moiety having up to 6 carbon atoms, (a cycloalkyl moiety having up to 6 carbon atoms)-C 1-4 alkyl, C 1-4 alkoxy, C 1-4 alkoxycarbonyl, C 1- 4 alkanoyl, and C 1-4 alkanoyloxy, wherein each C 1-4 alkyl, C 2-4 alkenyl, C 2-4 alkynyl, cycloalkyl moiety having up to 6 carbon atoms, (cycloalkyl moiety having up to 6 carbon atoms)-C 1-4 alkyl, C 1-4 alkoxy, C 1-4 alkoxycarbonyl, C 1-4 alkanoyl, and C 1-4 alkanoyloxy, is optionally substituted with one or more groups independently selected from oxo, halo, amino, hydroxy, C 1-3 alkoxy, and C 1 -C 3 alkyl that is optionally substituted with one or more groups independently selected from halo, wherein the term alkoxy refers to a linear or branched radical represented by the formula -OR in which R is alkyl, alkenyl, alkynyl or carbocycyl; and each R e is independently selected from hydrogen and C 1-4 alkyl; or a compound selected from the group consisting of:
A sound absorbing material having a ventilation resistance in the range of between 0.4 and 20.000 kPa · s/m comprising a sound absorbing surface material having a ventilation resistance in the range of between 0.100 and 1.000 kPa·s/m and an air-permeable porous material sheet laminated onto said sound absorbing surface material, wherein said sound absorbing surface material comprises a fiber sheet and stretchable paper laminated on one side of the fiber sheet , wherein the stretchable paper has an uneven surface, a unit weight of said stretchable paper is in the range of between 10 and 50 g/m 2 , and a ventilation resistance of said stretchable paper (la, 1b) is higher than at least 0.060 kPa · s/m.
A composition for use in the treatment of a solid tumor in a patient having the solid tumor, the composition comprising Coenzyme Q10, wherein the composition is administered intravenously.
Coated granular substance, wherein the coating comprises a resin comprising the reaction product of a polyol component and an isocyanate component and which was cured by the addition of a catalyst, said catalyst comprising at least one hydroxy group-containing amine compound of the general formula (I): wherein R 1 is a C 1 to C 4 alkyl group; R 2 is a C 1 to C 4 alkyl group; R 3 is a C 1 to C 4 alkyl group, a group -(CH 2 ) q -CH(OH)R 5 or a group -CH 2 -(CH 2 ) r -NR 6 R 7 ; R 4 is a hydrogen atom or a C 1 to C 4 alkyl group; R 5 is a hydrogen atom or a C 1 to C 4 alkyl group; R 6 is a C 1 to C 4 alkyl group; R 7 is a C 1 to C 4 alkyl group; m is an integer of from 0 to 10; n is an integer of from 0 to 10; o is an integer of from 1 to 10; p is an integer of from 0 to 10; q is an integer of from 1 to 10; and r is an integer of from 0 to 10. R 1 is a C 1 to C 4 alkyl group; R 2 is a C 1 to C 4 alkyl group; R 3 is a C 1 to C 4 alkyl group, a group -(CH 2 ) q -CH(OH)R 5 or a group -CH 2 -(CH 2 ) r -NR 6 R 7 ; R 4 is a hydrogen atom or a C 1 to C 4 alkyl group; R 5 is a hydrogen atom or a C 1 to C 4 alkyl group; R 6 is a C 1 to C 4 alkyl group; R 7 is a C 1 to C 4 alkyl group; m is an integer of from 0 to 10; n is an integer of from 0 to 10; o is an integer of from 1 to 10; p is an integer of from 0 to 10; q is an integer of from 1 to 10; and r is an integer of from 0 to 10.
A medical system, comprising: a medical device ; and an external computing component ; wherein the medical device comprises: a probe disposed on a distal end portion of the device and configured to be inserted into a body along a trajectory path; a sensor mounted on a displacement tracker portion of the device and disposed on a proximal end portion of the device, the sensor configured to measure a distance parallel to the probe between the displacement tracker portion and a tissue surface such that a position of the probe is determinable relative to the tissue surface upon advance or retraction of the probe along the trajectory path; and a communications module configured to communicate with the external computing component such that a position of the probe is monitored relative to a medical treatment plan; and wherein the external computing component is configured to provide distance values for translating the probe along the trajectory path in accordance with the treatment plan. a medical device ; and an external computing component ; wherein the medical device comprises: a probe disposed on a distal end portion of the device and configured to be inserted into a body along a trajectory path; a sensor mounted on a displacement tracker portion of the device and disposed on a proximal end portion of the device, the sensor configured to measure a distance parallel to the probe between the displacement tracker portion and a tissue surface such that a position of the probe is determinable relative to the tissue surface upon advance or retraction of the probe along the trajectory path; and a communications module configured to communicate with the external computing component such that a position of the probe is monitored relative to a medical treatment plan; and a probe disposed on a distal end portion of the device and configured to be inserted into a body along a trajectory path; a sensor mounted on a displacement tracker portion of the device and disposed on a proximal end portion of the device, the sensor configured to measure a distance parallel to the probe between the displacement tracker portion and a tissue surface such that a position of the probe is determinable relative to the tissue surface upon advance or retraction of the probe along the trajectory path; and a communications module configured to communicate with the external computing component such that a position of the probe is monitored relative to a medical treatment plan; and wherein the external computing component is configured to provide distance values for translating the probe along the trajectory path in accordance with the treatment plan.