mhurhangee/ep-ind-claims huggingface dataset:
A hair care shampoo composition comprising a compound comprising the following structure: R 1 is selected from H, alkyl, amino alkyl, alkoxy; Q = H 2, O, -OR 1, -N(R 1) 2, -OPO(OR 1) x, -PO(OR 1) x, -P(OR 1) x where x = 1-2; V = NR 1, O, -OPO(OR 1) x, -PO(OR 1) x, -P(OR 1) x where x = 1-2; W = H 2, O; X, Y = independently selected from H, aryl, naphthyl for n=0; X, Y = aliphatic CH 2 or aromatic CH for n ≥ 1 and Z is selected from aliphatic CH 2, aromatic CH, or heteroatom; A = aryl, substituted aryl or fused aryl; and stereochemistry is variable at the positions marked*. R 1 is selected from H, alkyl, amino alkyl, alkoxy; Q = H 2, O, -OR 1, -N(R 1) 2, -OPO(OR 1) x, -PO(OR 1) x, -P(OR 1) x where x = 1-2; V = NR 1, O, -OPO(OR 1) x, -PO(OR 1) x, -P(OR 1) x where x = 1-2; W = H 2, O; X, Y = independently selected from H, aryl, naphthyl for n=0; X, Y = aliphatic CH 2 or aromatic CH for n ≥ 1 and Z is selected from aliphatic CH 2, aromatic CH, or heteroatom; A = aryl, substituted aryl or fused aryl; and
A luminaire mounting and suspension assembly comprising: a mounting unit; a plurality of suspension units, characterized in that each suspension unit comprises: a housing coupled to the mounting unit; and a yoke pivotally coupled to the housing at a pivot point so as to be pivotal about a pivot axis, the yoke comprising a pair of cable grippers, each cable gripper positioned on opposing sides of each pivot point and configured to grip a suspension cable for suspending a luminaire; wherein the pivot axis is perpendicular to axes of the suspension cables; and whereby free rotation of the yoke about the pivot axis evenly balances tension between the suspension cables. a mounting unit; a plurality of suspension units, characterized in that each suspension unit comprises: a housing coupled to the mounting unit; and a yoke pivotally coupled to the housing at a pivot point so as to be pivotal about a pivot axis, the yoke comprising a pair of cable grippers, each cable gripper positioned on opposing sides of each pivot point and configured to grip a suspension cable for suspending a luminaire; a housing coupled to the mounting unit; and a yoke pivotally coupled to the housing at a pivot point so as to be pivotal about a pivot axis, the yoke comprising a pair of cable grippers, each cable gripper positioned on opposing sides of each pivot point and configured to grip a suspension cable for suspending a luminaire; wherein the pivot axis is perpendicular to axes of the suspension cables; and whereby free rotation of the yoke about the pivot axis evenly balances tension between the suspension cables.
A method for controlling a marine vessel having a first steering nozzle, a first reversing bucket and one of a second steering nozzle and a second reversing bucket or a bow thruster, comprising: receiving a first vessel control signal from a first vessel control apparatus, the first vessel control signal corresponding to a movement of the first vessel control apparatus along at least one degree of freedom; and receiving a second vessel control signal corresponding to movement of a second vessel control apparatus along a degree of freedom of said second vessel control apparatus controlling a rotation of the marine vessel, generating at least a first actuator control signal and a second actuator control signal corresponding to the vessel control signals; wherein the first actuator control signal is coupled to and controls one of the first or second steering nozzles (158P,158S), the first or second reversing bucket (152P,152S) and the bow thruster, and the second actuator control signal is coupled to and controls a different one of the first or second steering nozzles, the first or second reversing buckets and the bow thruster, wherein the first and second actuator control signals are applied to at least two respective actuators of the first or second steering nozzle, the first or second reversing bucket and the bow thruster to translate to the port or starboard the vessel primarily in a direction of movement of the first vessel control apparatus along a corresponding x-axis, such that substantially no net rotational force is induced to the marine vessel with the second vessel control apparatus in a neutral position. receiving a first vessel control signal from a first vessel control apparatus, the first vessel control signal corresponding to a movement of the first vessel control apparatus along at least one degree of freedom; and receiving a second vessel control signal corresponding to movement of a second vessel control apparatus along a degree of freedom of said second vessel control apparatus controlling a rotation of the marine vessel, generating at least a first actuator control signal and a second actuator control signal corresponding to the vessel control signals; wherein the first actuator control signal is coupled to and controls one of the first or second steering nozzles (158P,158S), the first or second reversing bucket (152P,152S) and the bow thruster, and the second actuator control signal is coupled to and controls a different one of the first or second steering nozzles, the first or second reversing buckets and the bow thruster, wherein the first and second actuator control signals are applied to at least two respective actuators of the first or second steering nozzle, the first or second reversing bucket and the bow thruster to translate to the port or starboard the vessel primarily in a direction of movement of the first vessel control apparatus along a corresponding x-axis, such that substantially no net rotational force is induced to the marine vessel with the second vessel control apparatus in a neutral position.
A slam-shut safety valve comprising: a valve body; an upper case mounted to the valve body; a diaphragm disposed between the valve body and the upper case, at least part of the diaphragm being displaceable into an interior portion of the valve body and into an interior portion of the upper case, the diaphragm having a first side being exposed to gas system pressure; a spring (30, 32) disposed within the interior of the upper case, the spring (30, 32) exerting a spring force on a second side of the diaphragm opposite the gas system pressure; a plunger connected to the first side of the diaphragm; a release element mounted within the interior of the valve body; a relatch plug operatively connected to a reset rod, the relatch plug cooperating with the release element to move a safety disc between an armed position in which the safety disc is spaced apart from a valve seat and an activated position in which the safety disc cooperates with the valve seat to prevent fluid flow through the valve seat; characterized in that the slam-shut safety valve comprises a relatch sheath, which is seated within a bore in the valve body, the relatch sheath receiving a portion of the relatch plug to guide movement of the relatch plug, wherein the relatch plug slides within the relatch sheath. a valve body; an upper case mounted to the valve body; a diaphragm disposed between the valve body and the upper case, at least part of the diaphragm being displaceable into an interior portion of the valve body and into an interior portion of the upper case, the diaphragm having a first side being exposed to gas system pressure; a spring (30, 32) disposed within the interior of the upper case, the spring (30, 32) exerting a spring force on a second side of the diaphragm opposite the gas system pressure; a plunger connected to the first side of the diaphragm; a release element mounted within the interior of the valve body; a relatch plug operatively connected to a reset rod, the relatch plug cooperating with the release element to move a safety disc between an armed position in which the safety disc is spaced apart from a valve seat and an activated position in which the safety disc cooperates with the valve seat to prevent fluid flow through the valve seat; characterized in that the slam-shut safety valve comprises a relatch sheath, which is seated within a bore in the valve body, the relatch sheath receiving a portion of the relatch plug to guide movement of the relatch plug, wherein the relatch plug slides within the relatch sheath.
An apparatus for reducing temperature-induced errors in a flow rate of a fluid determined from a linear flow rate comprising: a housing forming a containment volume and at least partially in contact with a fluid; a transducer for generating an ultrasonic signal and being operatively connectable with the housing; a buffer configured to propagate the ultrasonic signal therethrough, and being at least partially thermally coupled with at least one of the fluid and the housing; and a processing circuit operatively connected with the transducer and configured to: cause the transducer to generate the ultrasonic signal; detect a received reflected portion of the ultrasonic signal reflected from one or more interfaces of the buffer; measure a time of flight of the reflected portion of the ultrasonic signal; and determine a temperature based at least partially on the time of flight, characterised in that the processing circuit is further configured to determine the flow rate of the fluid in response to at least the linear flow rate and the effect of the determined temperature on the housing. a housing forming a containment volume and at least partially in contact with a fluid; a transducer for generating an ultrasonic signal and being operatively connectable with the housing; a buffer configured to propagate the ultrasonic signal therethrough, and being at least partially thermally coupled with at least one of the fluid and the housing; and a processing circuit operatively connected with the transducer and configured to: cause the transducer to generate the ultrasonic signal; detect a received reflected portion of the ultrasonic signal reflected from one or more interfaces of the buffer; measure a time of flight of the reflected portion of the ultrasonic signal; and determine a temperature based at least partially on the time of flight, characterised in that the processing circuit is further configured to determine the flow rate of the fluid in response to at least the linear flow rate and the effect of the determined temperature on the housing. cause the transducer to generate the ultrasonic signal; detect a received reflected portion of the ultrasonic signal reflected from one or more interfaces of the buffer; measure a time of flight of the reflected portion of the ultrasonic signal; and determine a temperature based at least partially on the time of flight, characterised in that the processing circuit is further configured to determine the flow rate of the fluid in response to at least the linear flow rate and the effect of the determined temperature on the housing.
A support intended to be fixed on a ground for the realization of a protection barrier capable of retaining an object moving relative to said ground, the support comprising: - a mast which includes a foot capable of resting on the ground and a head and which is substantially orthogonal to the ground, when the support is in the mounted position on the ground; - a lower holding element substantially perpendicular to the mast, having an upstream end intended to be fixed to the ground and a downstream extreme portion mounted on the foot of the mast; - first limitation means (17, 31, 33) for limiting the displacement of the foot of the mast downstream relative to the ground, in the mounted position; - a rigid upper holding element disposed obliquely with respect to the mast, having an upstream end intended to be fixed to the ground and a downstream extreme portion mounted on the head of the mast; - second limitation means (25, 26, 32, 24) for limiting the displacement of the head of the mast relative to the ground, downstream and upstream, in the mounted position; characterized in that the first limitation means and the second limitation means respectively comprise a first and a second braking devices (31, 32), the braking devices being designed to prevent the displacement of the mast downstream at rest, and to brake the displacement of the mast downstream under the effect of a load exerted on the mast, in the mounted position, the first and second braking devices (31, 32) being distinct and arranged so that the braked displacement of the mast downstream, in the mounted position and under the effect of a load exerted on the mast, is done substantially according to a translation parallel to the ground, without modifying the inclination of the mast with respect to the ground. - a mast which includes a foot capable of resting on the ground and a head and which is substantially orthogonal to the ground, when the support is in the mounted position on the ground; - a lower holding element substantially perpendicular to the mast, having an upstream end intended to be fixed to the ground and a downstream extreme portion mounted on the foot of the mast; - first limitation means (17, 31, 33) for limiting the displacement of the foot of the mast downstream relative to the ground, in the mounted position; - a rigid upper holding element disposed obliquely with respect to the mast, having an upstream end intended to be fixed to the ground and a downstream extreme portion mounted on the head of the mast; - second limitation means (25, 26, 32, 24) for limiting the displacement of the head of the mast relative to the ground, downstream and upstream, in the mounted position;
A method for temporally advancing the detection and characterisation of analog data for temporally advanced responsive actions to such analog data, comprising: providing analog data detection means, said analog data detection means being interfaced, directly or indirectly, with a negative group delay "NGD" circuit means having a NGD signal output means for producing a temporally advanced indicia of analog data received by said analog data detection means; inputting an analog data signal from a source of analog data to the analog data detection means; and outputting temporally advanced indicia produced by said negative group delay circuit means; wherein the NGD circuit means has a negative group delay over a frequency range and any resonant frequencies of the NGD circuit means are outside the frequency range. providing analog data detection means, said analog data detection means being interfaced, directly or indirectly, with a negative group delay "NGD" circuit means having a NGD signal output means for producing a temporally advanced indicia of analog data received by said analog data detection means; inputting an analog data signal from a source of analog data to the analog data detection means; and outputting temporally advanced indicia produced by said negative group delay circuit means;
A wing tip device for fixing to the outboard end of a wing, the wing defining a wing plane, the wing tip device comprising: an upper wing-like element projecting upwardly with respect to the wing plane and having a trailing edge; and a lower wing-like element fixed with respect to the upper wing-like element and having a root chord and a trailing edge, characterised in that the lower wing-like element root chord intersects with the upper wing-like element, and the lower wing-like element projects downwardly from the intersection; the upper wing-like element is larger than the lower wing-like element and the trailing edge of the lower wing-like element is adjacent the trailing edge of the upper wing-like element at the intersection; an included angle between the upper and lower wing-like elements (304, 307) at the intersection on the outboard side of the wing tip device in the spanwise direction is less than, or equal to, 160 degrees, and the lower wing-like element has an element planform area less than approximately 25% of the upper wing-like element planform area. an upper wing-like element projecting upwardly with respect to the wing plane and having a trailing edge; and a lower wing-like element fixed with respect to the upper wing-like element and having a root chord and a trailing edge, characterised in that the lower wing-like element root chord intersects with the upper wing-like element, and the lower wing-like element projects downwardly from the intersection; the upper wing-like element is larger than the lower wing-like element and the trailing edge of the lower wing-like element is adjacent the trailing edge of the upper wing-like element at the intersection; an included angle between the upper and lower wing-like elements (304, 307) at the intersection on the outboard side of the wing tip device in the spanwise direction is less than, or equal to, 160 degrees, and the lower wing-like element has an element planform area less than approximately 25% of the upper wing-like element planform area.
A capacitive-load driver circuit that is connectable to terminals connected to capacitive loads (CL_M,CL_P) and to an output stage of an amplifier for feeding output voltages to the terminals to drive the capacitive loads, the capacitive-load driver circuit feeding a current during a transition period of the output voltages from one of the terminals transitioning from a high voltage state to a low voltage state to another terminal transitioning from a low voltage state to a high voltage state, the capacitive-load driver circuit comprising: a current-variation detector circuit that detects a variation in a current at the output stage; a charge transfer circuit (SW1, SW2, CS1, CS2) that feeds a predetermined current to one of the terminals to transfer charges from a capacitive load connected to a high voltage terminal to a capacitive load connected to a low voltage terminal and a voltage comparator circuit that determines the magnitude relation of voltages at the terminals; wherein the charge transfer circuit feeds the predetermined current to one of the terminals depending on a result detected at the current-variation detector circuit, and wherein, the charge transfer circuit starts feeding the predetermined current to one of the terminals upon detection of a variation in the current at the output stage by the current-variation detector circuit, and the charge transfer circuit interrupts the current between the terminals upon detection of inversion of the magnitude relation of the voltages at the terminals by the voltage comparator circuit. a current-variation detector circuit that detects a variation in a current at the output stage; a charge transfer circuit (SW1, SW2, CS1, CS2) that feeds a predetermined current to one of the terminals to transfer charges from a capacitive load connected to a high voltage terminal to a capacitive load connected to a low voltage terminal and a voltage comparator circuit that determines the magnitude relation of voltages at the terminals; wherein the charge transfer circuit feeds the predetermined current to one of the terminals depending on a result detected at the current-variation detector circuit, and wherein, the charge transfer circuit starts feeding the predetermined current to one of the terminals upon detection of a variation in the current at the output stage by the current-variation detector circuit, and the charge transfer circuit interrupts the current between the terminals upon detection of inversion of the magnitude relation of the voltages at the terminals by the voltage comparator circuit.
Motor vehicle fan propeller comprising a hub and blades which extend radially towards the exterior from the hub, wherein each blade has a profile with a neutral axis and a span which extends between a leading edge and a trailing edge of said blade, the blade having, on at least part of its length, a profile formed in the shape of a flattened S, such that the neutral axis makes possible a point of contraflexure, and has two opposite concavities, i.e. a positive concavity (C 1) between the leading edge and the point of contraflexure, and a negative concavity (C 2) between the point of contraflexure and the trailing edge, the point of contraflexure being situated at between 20% and 80% of a length of the span, starting from the leading edge, characterized in that the blade has a developing profile which starts from said shaped profile in a region at the level of the hub, and ends in a profile of the aircraft wing type, without a point of contraflexure of the neutral axis, in an end region of the blade.
A method for detecting the presence of bladder cancer in a subject comprising detecting the level of each marker of a set of bladder cancer markers in a urine or bladder washing sample from the subject, wherein the set of bladder cancer markers comprises uroplakin 1B (UPK1B), or androgen receptor, or both UPK1B and AR, and wherein detection of an elevated level of at least one marker selected from UPK1B and AR indicates the presence of bladder cancer in the subject.
A method for modeling light in a predetermined physical space, the method comprising: acquiring at least one first light reading at a first spatial location and at least one second light reading at a second spatial location (302, 304, 306); and building a model of the light distribution in the predetermined physical space based on the at least one first and second light readings, the step of building a model including determining a radiance of at least one third spatial location of the predetermined physical space using a triangulation of the at least one first and second light readings. acquiring at least one first light reading at a first spatial location and at least one second light reading at a second spatial location (302, 304, 306); and building a model of the light distribution in the predetermined physical space based on the at least one first and second light readings, the step of building a model including determining a radiance of at least one third spatial location of the predetermined physical space using a triangulation of the at least one first and second light readings.