mhurhangee/ep-ind-claims huggingface dataset:
A solid composition comprising: (a) an aminosilicone polymer, wherein the aminosilicone polymer comprises amino sidechains, and wherein the aminosilicone polymer has a weight average molecular weight of from 10,000 Dalton to 60,000 Dalton; (b) a silicone resin, wherein the silicone resin is a MQ resin; (c) an ether of a water-soluble polyhydric alcohol; (d) one or more pigments or one or more coloured materials; (e) a thickening system comprising: ∘ a deposition enhancer, wherein the deposition enhancer is a hydrophilic and non-ionic polymer, and wherein the deposition enhancer has a weight average molecular weight of from 700,000 Dalton to 3,000,000 Dalton; and ∘ a thickening polymer, wherein the thickening polymer has a weight average molecular weight of at least 10,000 Dalton, and wherein the thickening polymer is a cationic thickening polymer or is a non-ionic thickening polymer. (a) an aminosilicone polymer, wherein the aminosilicone polymer comprises amino sidechains, and wherein the aminosilicone polymer has a weight average molecular weight of from 10,000 Dalton to 60,000 Dalton; (b) a silicone resin, wherein the silicone resin is a MQ resin; (c) an ether of a water-soluble polyhydric alcohol; (d) one or more pigments or one or more coloured materials; (e) a thickening system comprising: ∘ a deposition enhancer, wherein the deposition enhancer is a hydrophilic and non-ionic polymer, and wherein the deposition enhancer has a weight average molecular weight of from 700,000 Dalton to 3,000,000 Dalton; and ∘ a thickening polymer, wherein the thickening polymer has a weight average molecular weight of at least 10,000 Dalton, and wherein the thickening polymer is a cationic thickening polymer or is a non-ionic thickening polymer. ∘ a deposition enhancer, wherein the deposition enhancer is a hydrophilic and non-ionic polymer, and wherein the deposition enhancer has a weight average molecular weight of from 700,000 Dalton to 3,000,000 Dalton; and ∘ a thickening polymer, wherein the thickening polymer has a weight average molecular weight of at least 10,000 Dalton, and wherein the thickening polymer is a cationic thickening polymer or is a non-ionic thickening polymer.
An electronic device for controlling an access ramp to a door of a vehicle, the ramp being able to move from a retracted configuration to a deployed configuration, the electronic device including: - a detection module configured to detect, via at least one sensor, at least one element of interest located in a nearby area near the door, each sensor being able to be linked to the detection module; and - a command module configured to command the passage of the ramp from one of the retracted and deployed configurations to the other as a function of the detection of the at least one element of interest; characterized in that the detection module is configured to assign each element of interest a confidence index as a function of predetermined parameters, the command module being able to command the passage of the ramp from one of the retracted and deployed configurations to the other as a function of the result of the comparison of the confidence index of each element of interest with at least one predetermined threshold value (SB, SH). - a detection module configured to detect, via at least one sensor, at least one element of interest located in a nearby area near the door, each sensor being able to be linked to the detection module; and - a command module configured to command the passage of the ramp from one of the retracted and deployed configurations to the other as a function of the detection of the at least one element of interest;
A cosmetic composition containing: (a) from 3 to 10% by weight of at least one bicarbonate salt, (b) xanthan gum, (c) at least one optionally carboxymethylated glucose homopolymer, and (d) from 40 to 95% by weight of water, the above percentages being expressed relative to the total weight of the composition. (a) from 3 to 10% by weight of at least one bicarbonate salt, (b) xanthan gum, (c) at least one optionally carboxymethylated glucose homopolymer, and (d) from 40 to 95% by weight of water,
A vibration isolation system for a rotary-wing aircraft main rotor system having a mast that is rotatable about an axis of rotation, the vibration isolation system comprising: a first mass attachable to the mast and rotatable relative to the mast coaxially about said axis of rotation, wherein the first mass includes a first weight assembly having a first extension portion extending in a radial direction from the mast towards a distal end of the first weight assembly; and a second mass attachable to the mast and rotatable relative to the mast and the first mass coaxially about said axis of rotation, wherein the second mass includes a second weight assembly having a second extension portion extending in a radial direction from the mast towards a distal end of the second weight assembly; characterized in that: the first weight assembly includes a first armature rotationally attached to the distal end of the first weight assembly, and a spring for urging the positioning of the first weight assembly; the second weight assembly defines a guide slot; and the first armature mechanically links the first extension portion of the first weight assembly to the guide slot of the second weight assembly; and wherein the angular velocity of the first and second masses is operable to reduce in-plane vibration of said main rotor system. a first mass attachable to the mast and rotatable relative to the mast coaxially about said axis of rotation, wherein the first mass includes a first weight assembly having a first extension portion extending in a radial direction from the mast towards a distal end of the first weight assembly; and a second mass attachable to the mast and rotatable relative to the mast and the first mass coaxially about said axis of rotation, wherein the second mass includes a second weight assembly having a second extension portion extending in a radial direction from the mast towards a distal end of the second weight assembly; characterized in that: the first weight assembly includes a first armature rotationally attached to the distal end of the first weight assembly, and a spring for urging the positioning of the first weight assembly; the second weight assembly defines a guide slot; and the first armature mechanically links the first extension portion of the first weight assembly to the guide slot of the second weight assembly; and wherein the angular velocity of the first and second masses is operable to reduce in-plane vibration of said main rotor system. the first weight assembly includes a first armature rotationally attached to the distal end of the first weight assembly, and a spring for urging the positioning of the first weight assembly; the second weight assembly defines a guide slot; and the first armature mechanically links the first extension portion of the first weight assembly to the guide slot of the second weight assembly; and wherein the angular velocity of the first and second masses is operable to reduce in-plane vibration of said main rotor system.
A scintillation element package, comprising: a scintillation element; a scintillation element housing comprising a liner; an outer housing encompassing said scintillation element; and a support mechanism including at least one friction ring, said support mechanism being between said scintillation element and said outer housing, wherein said liner is between said at least one friction ring and said scintillation element, characterized in that said support mechanism further comprises at least one O-ring, and in that said liner is a PEEK liner comprising grooves for accommodating each of said at least one friction ring. a scintillation element; a scintillation element housing comprising a liner; an outer housing encompassing said scintillation element; and a support mechanism including at least one friction ring, said support mechanism being between said scintillation element and said outer housing, wherein said liner is between said at least one friction ring and said scintillation element, characterized in that said support mechanism further comprises at least one O-ring, and in that said liner is a PEEK liner comprising grooves for accommodating each of said at least one friction ring.
A high speed blender comprising a counter-rotating motor, comprising: a stator, comprising an outer winding and an inner winding, wherein a phase sequence of the outer winding is reverse to a phase sequence of the inner winding; an inverter, connected in parallel with the outer winding and the inner winding and configured to supply an excitation current to the outer winding and the inner winding synchronously; an inner rotor, arranged at an inner side of the inner winding and configured to rotate in a first direction by an action of the inner winding; an outer rotor, arranged at an outer side of the outer winding and configured to rotate in a second direction opposite to the first direction by an action of the outer winding. a stator, comprising an outer winding and an inner winding, wherein a phase sequence of the outer winding is reverse to a phase sequence of the inner winding; an inverter, connected in parallel with the outer winding and the inner winding and configured to supply an excitation current to the outer winding and the inner winding synchronously; an inner rotor, arranged at an inner side of the inner winding and configured to rotate in a first direction by an action of the inner winding; an outer rotor, arranged at an outer side of the outer winding and configured to rotate in a second direction opposite to the first direction by an action of the outer winding.
A computer-implemented method for operating an autonomous vehicle, comprising: identifying a driving scenario of an autonomous vehicle for a next movement, wherein the driving scenario is represented by a set of one or more predetermined parameters; and calculating a first next movement of the autonomous vehicle using a physical model corresponding to the driving scenario; characterized in that the method further comprises applying a sideslip predictive model to the set of predetermined parameters to predict a sideslip of the autonomous vehicle given the driving scenario; determining a second next movement of the autonomous vehicle based on the first next movement and the predicted sideslip of the autonomous vehicle, generating planning and control data based on the second next movement; and controlling and driving the autonomous vehicle based on the planning and control data. identifying a driving scenario of an autonomous vehicle for a next movement, wherein the driving scenario is represented by a set of one or more predetermined parameters; and calculating a first next movement of the autonomous vehicle using a physical model corresponding to the driving scenario; characterized in that the method further comprises applying a sideslip predictive model to the set of predetermined parameters to predict a sideslip of the autonomous vehicle given the driving scenario; determining a second next movement of the autonomous vehicle based on the first next movement and the predicted sideslip of the autonomous vehicle, generating planning and control data based on the second next movement; and controlling and driving the autonomous vehicle based on the planning and control data.
A method, comprising: receiving a computerized tomography scan of at least a part of a body of a patient; identifying voxels of the scan that correspond to regions in the body that are traversable by a probe inserted therein; displaying the scan on a screen and marking thereon selected start and termination points for the probe; finding a path from the start point to the termination point comprising a connected set of the identified voxels; using the scan to generate a representation of an external surface of the body and displaying the representation on the screen; and rendering an area of the external surface surrounding the path locally transparent in the displayed representation, so as to make visible on the screen an internal structure of the body in a vicinity of the path. receiving a computerized tomography scan of at least a part of a body of a patient; identifying voxels of the scan that correspond to regions in the body that are traversable by a probe inserted therein; displaying the scan on a screen and marking thereon selected start and termination points for the probe; finding a path from the start point to the termination point comprising a connected set of the identified voxels; using the scan to generate a representation of an external surface of the body and displaying the representation on the screen; and rendering an area of the external surface surrounding the path locally transparent in the displayed representation, so as to make visible on the screen an internal structure of the body in a vicinity of the path.
Mechanism, in particular for a motor vehicle seat, by means of which the displacement of a first fitting part and a second fitting part may be locked and released relative to one another, with a drive means, a detent plate and a detent pawl, the detent pawl being able to be locked relative to the first fitting part by latching thereto, the detent plate being able to be reversibly displaced by means of the drive means, the detent plate locking the displacement of the detent pawl in a detent position, and releasing said displacement in a release position, the drive means comprising a securing segment (7.1) for securing the detent plate against self-opening and comprising a second segment (7.2), characterized in that the securing segment (7.1) comprises a first positive and/or non-positive connecting means (7.11-7.1i) and the second segment (7.2), which is separate therefrom, comprises a second positive and/or non-positive connecting means (7.21-7.2i), and in that the first and the second positive and/or non-positive connecting means (7.11-7.1i, 7.21-7.2i) are at least partially in engagement with a third positive and/or non-positive connecting means (6.1) of the detent plate and the first positive and/or non-positive connecting means (7.11-7.1i) is a securing means which, in the detent position, is in engagement with a front detent tooth of the third positive and/or non-positive connecting means (6.1) of the detent plate such that the detent plate does not inadvertently open.
An aerosol generating device comprising: a liquid source of a liquid aerosol formulation comprising a carrier and insulin; a capilliary flow passage in fluid communication with the liquid source; a heater disposed to heat the liquid aerosol formulation in a heated portion of the capilliary flow passage and operable to heat the liquid aerosol formulation to about 100 °C to 150 °C and to produce a vapor which admixes with air to produce an aerosol; a power supply; and a controller operable to deliver power from the power supply to the heater so as to maintain the heater at a temperature effective to vaporize the liquid aerosol formulation in the capilliary flow passage to produce an aerosol consisting essentially of substantially dry solid particles, wherein the heater is operable. a liquid source of a liquid aerosol formulation comprising a carrier and insulin; a capilliary flow passage in fluid communication with the liquid source; a heater disposed to heat the liquid aerosol formulation in a heated portion of the capilliary flow passage and operable to heat the liquid aerosol formulation to about 100 °C to 150 °C and to produce a vapor which admixes with air to produce an aerosol; a power supply; and a controller operable to deliver power from the power supply to the heater so as to maintain the heater at a temperature effective to vaporize the liquid aerosol formulation in the capilliary flow passage to produce an aerosol consisting essentially of substantially dry solid particles, wherein the heater is operable.
A gas turbine engine comprising: a nacelle defining an interior space; a fan section, a compressor section (15, 16) and a turbine section (23, 25) positioned within said nacelle, an inner cowl surrounding said compressor section (15,16) and said turbine section (23, 25), and said fan section delivering air to said compressor section (15, 16), and bypass air between said cowl and an interior surface of said nacelle; an air inlet for capturing air and communicating the air into the interior space of said nacelle, said interior space defining a plenum, the plenum configured to receive the air leaving said air inlet, flowing through the plenum, and into a passage (103; 105), said passage being configured to communicate the air to a location adjacent an upstream end of said nacelle, wherein the air inlet is a pipe which extends through a wall in the nacelle body, and the outlet of the air inlet pipe then opens into communication with the interior space; and a flow control (115, 200) for selectively blocking or allowing the flow of air through said passage (103; 105) to the location adjacent to the upstream end of said nacelle, and for allowing the flow when it is desirable to create a thicker boundary layer at the upstream end of the nacelle; characterized in that the air inlet pipe extends from an intake end in a bypass air passage, and has an outlet within the interior space. a nacelle defining an interior space; a fan section, a compressor section (15, 16) and a turbine section (23, 25) positioned within said nacelle, an inner cowl surrounding said compressor section (15,16) and said turbine section (23, 25), and said fan section delivering air to said compressor section (15, 16), and bypass air between said cowl and an interior surface of said nacelle; an air inlet for capturing air and communicating the air into the interior space of said nacelle, said interior space defining a plenum, the plenum configured to receive the air leaving said air inlet, flowing through the plenum, and into a passage (103; 105), said passage being configured to communicate the air to a location adjacent an upstream end of said nacelle, wherein the air inlet is a pipe which extends through a wall in the nacelle body, and the outlet of the air inlet pipe then opens into communication with the interior space; and a flow control (115, 200) for selectively blocking or allowing the flow of air through said passage (103; 105) to the location adjacent to the upstream end of said nacelle, and for allowing the flow when it is desirable to create a thicker boundary layer at the upstream end of the nacelle; characterized in that the air inlet pipe extends from an intake end in a bypass air passage, and has an outlet within the interior space.
A high pressure water jet cleaner comprising: - - a casing, - a first pump associated with the casing, which is provided with a suction conduit adapted to be connected to a water network and a delivery conduit, - a dispensing pistol provided with a dispensing nozzle and fluidly connected to the delivery conduit of the first pump, - a second pump associated with the casing, which is provided with a suction conduit in direct fluid communication with a tank, adapted to contain a liquid, and independent from the suction conduit of the first pump, and a delivery conduit independent from the delivery conduit of the first pump, and - a spray pistol provided with a spray nozzle and fluidly connected to the delivery conduit of the second pump, the high pressure water jet cleaner further comprising: - a first electric motor mechanically connected to the first pump for activating it, - a second electric motor (205,210) mechanically connected to the second pump for activating it and - an electric supply device configured to selectively connect to a source of electric energy the first motor or the second motor (205,210). - - a casing, - a first pump associated with the casing, which is provided with a suction conduit adapted to be connected to a water network and a delivery conduit, - a dispensing pistol provided with a dispensing nozzle and fluidly connected to the delivery conduit of the first pump, - a second pump associated with the casing, which is provided with a suction conduit in direct fluid communication with a tank, adapted to contain a liquid, and independent from the suction conduit of the first pump, and a delivery conduit independent from the delivery conduit of the first pump, and - a spray pistol provided with a spray nozzle and fluidly connected to the delivery conduit of the second pump, the high pressure water jet cleaner further comprising: - a first electric motor mechanically connected to the first pump for activating it, - a second electric motor (205,210) mechanically connected to the second pump for activating it and - an electric supply device configured to selectively connect to a source of electric energy the first motor or the second motor (205,210). - a first electric motor mechanically connected to the first pump for activating it, - a second electric motor (205,210) mechanically connected to the second pump for activating it and - an electric supply device configured to selectively connect to a source of electric energy the first motor or the second motor (205,210).
A battery, comprising a housing and a battery cell disposed in the housing; characterized in that: the battery cell comprises electrodes and tabs, and each of the electrodes is integrally connected with a tab, characterized in that each of the electrodes comprises a current collector and an active material layer, and the current collector comprises a coating zone coated with the active material layer and an empty foil zone not coated with the active material layer, and an end of the tab is welded to the empty foil zone by a laser welding process; a surface of the empty foil zone facing away from the tab has a plurality of welding zones which are arranged at intervals, and each of the welding zones comprises at least one line-shaped welding mark; and a surface of the tab facing away from the empty foil zone has no welding mark; wherein a ratio of the height of the line-shaped welding mark to a width of the line-shaped welding mark is less than 1. the battery cell comprises electrodes and tabs, and each of the electrodes is integrally connected with a tab, characterized in that each of the electrodes comprises a current collector and an active material layer, and the current collector comprises a coating zone coated with the active material layer and an empty foil zone not coated with the active material layer, and an end of the tab is welded to the empty foil zone by a laser welding process; a surface of the empty foil zone facing away from the tab has a plurality of welding zones which are arranged at intervals, and each of the welding zones comprises at least one line-shaped welding mark; and a surface of the tab facing away from the empty foil zone has no welding mark; wherein a ratio of the height of the line-shaped welding mark to a width of the line-shaped welding mark is less than 1.