mhurhangee/ep-ind-claims huggingface dataset:
Air spring comprising at least the following components, specifically an air spring bellows which is composed of an elastomeric material, an air spring cover, an air spring piston and a sleeve-like outer guide which encloses the air spring bellows in a tangential manner, wherein the air spring bellows, by way of its first end, is fastened in an air-tight manner to the air spring cover and, by way of its second end, is fastened in an air-tight manner to the air spring piston and forms an elastic-volume hollow chamber together with the air spring cover and the air spring piston, wherein the air spring has an integrated and releasable transport securing means (18, 19, 20) which fixes the air spring cover against the air spring piston, characterized in that the transport securing means (18, 19, 20) is designed as a releasable, latching clip connection.
Controller, in particular for a motor vehicle, having: - a printed circuit board; - a high-impedance circuit section which is arranged on the printed circuit board and which has an impedance of 1 kΩ or higher with respect to an earth of the controller; and - at least one protection element (110, 210) which is electrically conductively connected to the earth, which has a press-in pin that is held in an opening in the printed circuit board, wherein the press-in pin fixes the printed circuit board in the controller, which is arranged next to the high-impedance circuit section on the printed circuit board and which, within a protection distance (d) from the high-impedance circuit section, has a height (h) which is at least equal to the protection distance (d). - a printed circuit board; - a high-impedance circuit section which is arranged on the printed circuit board and which has an impedance of 1 kΩ or higher with respect to an earth of the controller; and - at least one protection element (110, 210) which is electrically conductively connected to the earth, which has a press-in pin that is held in an opening in the printed circuit board, wherein the press-in pin fixes the printed circuit board in the controller, which is arranged next to the high-impedance circuit section on the printed circuit board and which, within a protection distance (d) from the high-impedance circuit section, has a height (h) which is at least equal to the protection distance (d).
A laundry washing machine comprising: - a laundry treating chamber; - at least one detergent storing compartment for storing a detergent; - an outlet through which the detergent is delivered from said detergent storing compartment to said laundry treating chamber; - a partitioning device for at least partially preventing passage of detergent through a bottom portion of said detergent storing compartment towards said outlet, said partitioning device comprising: - a pivotable partition element arranged in said detergent compartment and pivotable about a horizontal axis such that it can displaced between a first, lowered, position, in which passage of detergent through said bottom portion is at least partially prevented, and a second, lifted, position in which passage through said bottom portion of detergent is allowed; - an operative element extending in a direction opposite to said pivotable partition element with respect to said horizontal axis, characterized in that said operative element is formed by a rotary knob, radially extending from a shaft (22, 25) of said partitioning device rotatable about said horizontal axis and to which said partition element is connected and in that said operative element comprises a grip portion positioned above an horizontal plane (α) comprising said horizontal axis both in said first and said second position, such that said grip portion can be reached by the hand of a user when said partition element is both in said first and said second position and rotated in order to displace said pivotable partition element between said first and second positions. - a laundry treating chamber; - at least one detergent storing compartment for storing a detergent; - an outlet through which the detergent is delivered from said detergent storing compartment to said laundry treating chamber; - a partitioning device for at least partially preventing passage of detergent through a bottom portion of said detergent storing compartment towards said outlet, - a pivotable partition element arranged in said detergent compartment and pivotable about a horizontal axis such that it can displaced between a first, lowered, position, in which passage of detergent through said bottom portion is at least partially prevented, and a second, lifted, position in which passage through said bottom portion of detergent is allowed; - an operative element extending in a direction opposite to said pivotable partition element with respect to said horizontal axis,
A system for determining altitude of an aircraft during flight, the system comprising: a vortex-shedding projection configured to extend from an exterior surface of the aircraft so as to project into and cause vortex-shedding turbulence of the airstream adjacent to the exterior surface of the aircraft; one or more sound-pressure detectors (16A - 16G) configured to be attached to the exterior surface of the aircraft downstream from the vortex-shedding projection, each of the one or more sound-pressure detectors configured to detect sound pressure indicative of the vortex-shedding turbulence caused by the vortex-shedding projection; and a processor configured to determine a vortex-shedding frequency f of the vortex-shedding turbulence as indicated by the sound pressure detected by the one or more sound-pressure detectors, the processor further configured to determine the altitude of the aircraft based, at least in part, on the vortex-shedding frequency f determined. a vortex-shedding projection configured to extend from an exterior surface of the aircraft so as to project into and cause vortex-shedding turbulence of the airstream adjacent to the exterior surface of the aircraft; one or more sound-pressure detectors (16A - 16G) configured to be attached to the exterior surface of the aircraft downstream from the vortex-shedding projection, each of the one or more sound-pressure detectors configured to detect sound pressure indicative of the vortex-shedding turbulence caused by the vortex-shedding projection; and a processor configured to determine a vortex-shedding frequency f of the vortex-shedding turbulence as indicated by the sound pressure detected by the one or more sound-pressure detectors, the processor further configured to determine the altitude of the aircraft based, at least in part, on the vortex-shedding frequency f determined.
A surface treated article having a recoatable surface treatment that does not change the appearance of the treated surface comprising: a painted or coated article or elastomer film surface treated with a surface treatment of one or more dispersion or emulsion of an aqueous acrylic or vinyl polymer that is the polymerization product of, based on the total weight of polymerized monomers, (i) an ethylenically unsaturated (poly)carboxylic acid monomer in the amount of from 0.1 to 47 wt.%, and (ii) the remainder of one or more non-ionic acrylic and/or vinyl comonomer having a solubility in water of less than 5g/100g of water at 25°C, the polymer having a glass transition temperature (Tg) of -10°C or higher, and a number average molecular weight (Mn) of from 1,000 to 100,000, wherein said surface treatment is substantially fluorine and silicone free. a painted or coated article or elastomer film surface treated with a surface treatment of one or more dispersion or emulsion of an aqueous acrylic or vinyl polymer that is the polymerization product of, based on the total weight of polymerized monomers, (i) an ethylenically unsaturated (poly)carboxylic acid monomer in the amount of from 0.1 to 47 wt.%, and (ii) the remainder of one or more non-ionic acrylic and/or vinyl comonomer having a solubility in water of less than 5g/100g of water at 25°C, the polymer having a glass transition temperature (Tg) of -10°C or higher, and a number average molecular weight (Mn) of from 1,000 to 100,000, wherein said surface treatment is substantially fluorine and silicone free.
A method of determining the condition of a component for exhaust emission control by period diagnostic check, said diagnostic check indicating behaviour corresponding to 'normal' and 'fault' by reference to one or more pre-determined values, the method comprising: providing a numerical scale of possible values for each of one or more variable parameters of the component, said values have progressively increasing quality from one end of said scale to the other end; defining in each said scale a plurality of successive thresholds, and providing for each threshold a virtual data bin; continually measuring said one or more variable parameters at a pre-determined time interval to obtain successive values of said parameters; for each successive value, placing the value in every corresponding data bin having a threshold on the lower quality side of said value; continually summing the values in respective data bins; defining for every data bin a trigger limit corresponding to a maximum sum of values; upon reaching the trigger limit in any bin, calculating the average value in said bin; using said average value in said diagnostic check by reference to said pre-determined value, and clearing the bin in which the trigger limit was reached for re-accumulation of successive values. providing a numerical scale of possible values for each of one or more variable parameters of the component, said values have progressively increasing quality from one end of said scale to the other end; defining in each said scale a plurality of successive thresholds, and providing for each threshold a virtual data bin; continually measuring said one or more variable parameters at a pre-determined time interval to obtain successive values of said parameters; for each successive value, placing the value in every corresponding data bin having a threshold on the lower quality side of said value; continually summing the values in respective data bins; defining for every data bin a trigger limit corresponding to a maximum sum of values; upon reaching the trigger limit in any bin, calculating the average value in said bin; using said average value in said diagnostic check by reference to said pre-determined value, and clearing the bin in which the trigger limit was reached for re-accumulation of successive values.
An aqueous oral care composition comprising: a cationic steroidal compound of Formula: wherein R 1 is selected from -OH and NH-R 2, wherein R 2 is C 2 -C 14 alkyl, C 2 -C 14 alkenyl or C 2 -C 14 akynyl, and n is 3 or 4; and a quaternary ammonium compound selected from the group consisting of benzalkonium chloride, benzethonium chloride, methylbenzethonium chloride, cetalkonium chloride, cetylpyridinium chloride, cetrimonium, cetrimide, dofanium chloride, didecyldimethylammonium chloride and domiphen bromide. a cationic steroidal compound of Formula: wherein R 1 is selected from -OH and NH-R 2, wherein R 2 is C 2 -C 14 alkyl, C 2 -C 14 alkenyl or C 2 -C 14 akynyl, and n is 3 or 4; and a quaternary ammonium compound selected from the group consisting of benzalkonium chloride, benzethonium chloride, methylbenzethonium chloride, cetalkonium chloride, cetylpyridinium chloride, cetrimonium, cetrimide, dofanium chloride, didecyldimethylammonium chloride and domiphen bromide.
An aircraft comprising: a fuselage; a wing extending from each lateral side of the fuselage, wherein the wings are configured to rotate relative to the fuselage to transition the aircraft from an airplane mode to a hover mode; a rotor secured to each wing, the rotor having a rotor tip path plane defined by rotation of the rotor about a rotor axis of rotation; a flight control system configured to apply a cyclic pitch change to each of the rotors based on pilot input; wherein, when the rotor tip path plane is changed relative to the rotor axis of rotation, the wing is configured to twist to reduce an angle of attack of the wing relative to a rotor wake of the rotor; wherein the wing is configured to twist in a same direction as the rotor tip path plane change; and wherein the reduced angle of attack of the wing reduces a magnitude of a yaw or roll opposing force (36,44); characterized in that an amount of wing twist is communicated to the flight control system; and the flight control system adjusts the rotor tip path plane change based on the amount of wing twist. a fuselage; a wing extending from each lateral side of the fuselage, wherein the wings are configured to rotate relative to the fuselage to transition the aircraft from an airplane mode to a hover mode; a rotor secured to each wing, the rotor having a rotor tip path plane defined by rotation of the rotor about a rotor axis of rotation; a flight control system configured to apply a cyclic pitch change to each of the rotors based on pilot input; wherein, when the rotor tip path plane is changed relative to the rotor axis of rotation, the wing is configured to twist to reduce an angle of attack of the wing relative to a rotor wake of the rotor; wherein the wing is configured to twist in a same direction as the rotor tip path plane change; and wherein the reduced angle of attack of the wing reduces a magnitude of a yaw or roll opposing force (36,44); characterized in that an amount of wing twist is communicated to the flight control system; and the flight control system adjusts the rotor tip path plane change based on the amount of wing twist.
Seal for an angled connector, the seal having a planar plate-shaped configuration and the seal having a rim wall that encloses a central opening, wherein at least one sealing passage extends from outside the seal through the rim wall into the central opening, characterized in that the seal is penetrated by the central opening in an axial direction, allowing a wire, to be inserted into the central opening via the sealing passage, to be accessible from either side in said axial direction.
A neutron porosity measurement device (300, 400), comprising: a neutron source configured to emit neutrons having a first energy; a segmented semiconductor detector (330, 200) comprising a plurality of semiconductor neutron detection cells (210, 410, 100) configured to detect neutrons having a second energy smaller than the first energy, the cells being arranged in a plurality of coplanar subsets (R1-R8), each subset comprising a plurality of cells arranged at a same level about an axis between a first distance and a second distance from the neutron source, the coplanar subsets (R1-R8) being grouped into at least two different groupings, whereby multiple porosity estimates may be extracted using the different groupings based on a single measurement using the neutron detection cells, wherein one or more of the neutron detection cells (210, 410, 100) are configured to acquire data related to detected neutrons independently from one or more other of the neutron detection cells. a neutron source configured to emit neutrons having a first energy; a segmented semiconductor detector (330, 200) comprising a plurality of semiconductor neutron detection cells (210, 410, 100) configured to detect neutrons having a second energy smaller than the first energy, the cells being arranged in a plurality of coplanar subsets (R1-R8), each subset comprising a plurality of cells arranged at a same level about an axis between a first distance and a second distance from the neutron source, the coplanar subsets (R1-R8) being grouped into at least two different groupings, whereby multiple porosity estimates may be extracted using the different groupings based on a single measurement using the neutron detection cells, wherein one or more of the neutron detection cells (210, 410, 100) are configured to acquire data related to detected neutrons independently from one or more other of the neutron detection cells.
Surgical apparatus, having a needle containing a first tissue anchor deployable out from the needle after piercing a first tissue fold, the needle also containing a second tissue anchor connected to the first tissue anchor to form a tissue anchor pair having a tissue anchor pair loop; and a tether loop attached on a tether; characterized by: a gastrointestinal implant attached to the tether; and a clasp having a movable arm, the clasp attached to the tether loop on the gastrointestinal implant, the tissue anchor pair loop engageable with the clasp by moving the tissue anchor pair loop onto the clasp to attach the gastrointestinal implant to the tissue anchor pair. a gastrointestinal implant attached to the tether; and a clasp having a movable arm, the clasp attached to the tether loop on the gastrointestinal implant, the tissue anchor pair loop engageable with the clasp by moving the tissue anchor pair loop onto the clasp to attach the gastrointestinal implant to the tissue anchor pair.
Device for performing thermal compensation of a weapon barrel of a gun having at least one weapon barrel which is mounted in a barrel cradle, and in a barrel support as a prolongation of the barrel cradle, wherein a plurality of temperature sensors (p1-p16) are integrated into the barrel cradle and the barrel support and are connected via data lines to a data box, and the data box is connected to a data processing device, wherein the data processing device calculates a barrel inclination by means of temperature differences, and in order to perform thermal compensation the data processing device can act on actuators in order to change the orientation of the weapon barrel.
A composite for heat storage comprising a thermochemical material encapsulated in a water vapour permeable polymeric material, wherein the polymeric material is ethylcellulose.
A internal combustion engine comprising at least one cylinder (120, 130) provided with corresponding pistons (140, 150, 160, 170) arranged to reciprocate along the longitudinal axis of each cylinder (120, 130), and at least first and second power cams (300, 400) mutually opposed and connected to respective first and second rotary shafts (500, 600), whereby reciprocation of the pistons (140, 150, 160, 170) results in that pistons (140, 150, 160, 170) act on the first and second power cams (300, 400) thereby imparting a rotating motion to the first and second rotary shafts (500, 600) to drive the engine, wherein it further comprises an attachment device for connecting the first and second rotary shafts (500, 600) to each other so that they can be rotated together, the attachment device comprising shifting means for changing the relative angular position of the first and second rotary shafts (500, 600), wherein the engine comprises counter cams (305, 405) associated with each power cam (300, 400) for preventing pistons (140, 150, 160, 170) from losing contact with the power cams (300, 400), wherein the pistons (140, 150, 160, 170) comprise at least one counter follower wheel adapted to roll onto a counter cam (305, 405) and the cylinders (120, 130) have an indentation (125, 135) formed in opposite ends thereof for allowing the counter cam follower wheel and its shaft do not collide with the cylinders (120, 130).
Method of manufacturing a bicycle component having at least one component body, formed at least partially of at least one fibrous composite material in at least one shaping mold, wherein at least one shaping area of the shaping mold, which serves to shape at least one outer section of the component body, is provided with at least one intended surface roughness, and wherein the surface roughness of the shaping area also serves to provide an intentional surface roughness for the outer section during the generation of the outer section, characterized in that the shaping area is roughened to an average roughness of at least 1 micrometer and maximally 4 micrometers, in particular to inhibit surface imperfections of the shaped outer section.
Device for breaking a glass pane at a breaking station, comprising at least one first breaking body that is displaceable along the front side of the glass pane and at least one second breaking body that is displaceable along the back side of the glass pane, characterized by a flexible support that is arranged between the two breaking bodies (71, 72) and is displaceable for transporting the glass pane from a cutting station to the breaking station.
A linear movable rotary union comprising: a driving shaft comprising a plurality of fluid supply path (112,113,114,115); a hollow middle housing surrounding an outside of the driving shaft and comprising a plurality of first through holes (254,256,258,260) in a sidewall; a plurality of first sealing members provided between the middle housing and the driving shaft to prevent leakage of a fluid; a hollow outer housing surrounding an outside of the middle housing and comprising a plurality of second through holes (304,306,308,310) in a sidewall; and a plurality of second sealing members provided between the middle housing and the outer housing to prevent leakage of the fluid, and wherein the driving shaft is provided to be capable of rotational motion in the middle housing, and the middle housing is provided to be capable of reciprocating motion in an axial direction in the outer housing, characterized in that the linear movable rotary union further comprises: a driving unit connected to one end portion of the driving shaft to allow the driving shaft to perform rotational motion with respect to the middle housing and connected to one end portion of the middle housing to allow the middle housing to perform reciprocating motion in the axial direction with respect to the outer housing, and wherein the driving unit comprises a linear guide connected to the middle housing. a driving shaft comprising a plurality of fluid supply path (112,113,114,115); a hollow middle housing surrounding an outside of the driving shaft and comprising a plurality of first through holes (254,256,258,260) in a sidewall; a plurality of first sealing members provided between the middle housing and the driving shaft to prevent leakage of a fluid; a hollow outer housing surrounding an outside of the middle housing and comprising a plurality of second through holes (304,306,308,310) in a sidewall; and a plurality of second sealing members provided between the middle housing and the outer housing to prevent leakage of the fluid, and wherein the driving shaft is provided to be capable of rotational motion in the middle housing, and the middle housing is provided to be capable of reciprocating motion in an axial direction in the outer housing, characterized in that the linear movable rotary union further comprises: a driving unit connected to one end portion of the driving shaft to allow the driving shaft to perform rotational motion with respect to the middle housing and connected to one end portion of the middle housing to allow the middle housing to perform reciprocating motion in the axial direction with respect to the outer housing, and wherein the driving unit comprises a linear guide connected to the middle housing.
A method performed in a first node of a communication network, said node being connected to a Lawful Interception, LI, system, said method comprising: - receiving from a Radio Access Network, RAN, a LI notification message indicating that service related content, pre-stored or cached in a storage in a wireless User Equipment, UE, or the RAN, has been used by the UE; - processing the LI notification message for identifying the service related content; - sending the identified service related content to the LI system as Content of Communication, CC, together with Intercept Related Information, IRI. - receiving from a Radio Access Network, RAN, a LI notification message indicating that service related content, pre-stored or cached in a storage in a wireless User Equipment, UE, or the RAN, has been used by the UE; - processing the LI notification message for identifying the service related content; - sending the identified service related content to the LI system as Content of Communication, CC, together with Intercept Related Information, IRI.