mhurhangee/ep-ind-claims huggingface dataset:
Measuring device with a measuring tube suitable for guiding a medium, having at least one sensor unit, wherein the sensor unit is designed for capturing at least one parameter of a medium, wherein the sensor unit is at least partially integrated in the measuring tube wall of the measuring tube, and with at least one control and evaluation unit, characterized in that the sensor unit has at least one deflectable measuring sensor with at least one cavity and at least one stationary base unit, wherein the measuring sensor is connected to the base unit via at least one spring element, wherein the base unit is arranged outside the interior of the measuring tube, wherein at least one side of the measuring sensor is in contact with the medium during operation, and wherein the cavity is arranged on the side of the measuring sensor facing the medium, and wherein the measuring sensor is integrated into the measuring tube wall in such a way that it can be deflected at least in the plane of the measuring tube wall, and that the sensor unit has a means for capturing the deflection of the measuring sensor. having at least one sensor unit, wherein the sensor unit is designed for capturing at least one parameter of a medium, wherein the sensor unit is at least partially integrated in the measuring tube wall of the measuring tube, and with at least one control and evaluation unit, characterized in that the sensor unit has at least one deflectable measuring sensor with at least one cavity and at least one stationary base unit, wherein the measuring sensor is connected to the base unit via at least one spring element, wherein the base unit is arranged outside the interior of the measuring tube, wherein at least one side of the measuring sensor is in contact with the medium during operation, and wherein the cavity is arranged on the side of the measuring sensor facing the medium, and wherein the measuring sensor is integrated into the measuring tube wall in such a way that it can be deflected at least in the plane of the measuring tube wall, and that the sensor unit has a means for capturing the deflection of the measuring sensor.
A battery module, wherein comprising: a battery cell group; and a welding assembly, comprising two first weldment and two second weldment; wherein the two first weldments is located at two ends of the battery cell group, respectively; the two second weldments is located at both sides of the battery cell group, respectively; and the adjacent first weldment and the second weldment are welded and fixed; wherein the second weldment is welded and fixed to the first weldment, and forming a welding seam; at least one side of the welding seam is provided with an exhaust channel; and the exhaust channel is located between the first weldment and the second weldment; wherein the first weldment and/or the second weldment comprises a base layer (14, 24) and a coating layer (16, 26); the coating layer (16, 26) is arranged on a surface of the base layer (14, 24); and a boiling point of the coating layer (16, 26) is lower than a melting point of the base layer (14, 24). a battery cell group; and a welding assembly, comprising two first weldment and two second weldment; wherein the two first weldments is located at two ends of the battery cell group, respectively; the two second weldments is located at both sides of the battery cell group, respectively; and the adjacent first weldment and the second weldment are welded and fixed; wherein the second weldment is welded and fixed to the first weldment, and forming a welding seam; at least one side of the welding seam is provided with an exhaust channel; and the exhaust channel is located between the first weldment and the second weldment; wherein the first weldment and/or the second weldment comprises a base layer (14, 24) and a coating layer (16, 26); the coating layer (16, 26) is arranged on a surface of the base layer (14, 24); and a boiling point of the coating layer (16, 26) is lower than a melting point of the base layer (14, 24).
A turbine comprising: a housing having a volute, an inlet and an outlet; an impeller rotatably coupled to the housing having a shaft defining an axial direction; a first shroud disposed within the housing comprising a plurality of nozzle vanes; and a second shroud disposed within the housing adjacent to the first shroud so that a nozzle area is formed between the first shroud and the second shroud, said nozzle area having a variable width, said second shroud movable relative to the first shroud to vary the width so that fluid flow from the inlet to the outlet is variable, said second shroud comprising a piston and the housing comprises a piston receiving pocket, said piston and said piston receiving pocket defining a control cavity fluidically coupled to a port through the housing; a linear guide moving with the piston in the axial direction, said linear guide comprising a first end coupled to the piston and a second end extending through an opening in said housing; a position sensor coupled to the linear guide generating a position signal corresponding to the variable width; said port is selectively coupled to a high pressure source and a low pressure source to move the piston within the pocket and the linear guide into or out of the housing and thereby move the second shroud relative to the first shroud to change the variable width. a housing having a volute, an inlet and an outlet; an impeller rotatably coupled to the housing having a shaft defining an axial direction; a first shroud disposed within the housing comprising a plurality of nozzle vanes; and a second shroud disposed within the housing adjacent to the first shroud so that a nozzle area is formed between the first shroud and the second shroud, said nozzle area having a variable width, said second shroud movable relative to the first shroud to vary the width so that fluid flow from the inlet to the outlet is variable, said second shroud comprising a piston and the housing comprises a piston receiving pocket, said piston and said piston receiving pocket defining a control cavity fluidically coupled to a port through the housing; a linear guide moving with the piston in the axial direction, said linear guide comprising a first end coupled to the piston and a second end extending through an opening in said housing; a position sensor coupled to the linear guide generating a position signal corresponding to the variable width; said port is selectively coupled to a high pressure source and a low pressure source to move the piston within the pocket and the linear guide into or out of the housing and thereby move the second shroud relative to the first shroud to change the variable width.
An inflatable shoulder harness assembly for an aircraft seat, comprising: a shoulder belt for extending across the torso of a passenger; a retractor for paying in and paying out a portion of the shoulder belt length; an inflatable airbag contained within an airbag cover attached to the shoulder belt near a free end of the shoulder belt; a belt guide slidably receiving the shoulder belt, the inflatable airbag and the airbag cover therein when the shoulder belt is retracted, the belt guide defining an elongate channel configured for facilitating free movement of the airbag cover during shoulder belt fastening and retraction; an exit bezel positioned near an exit of the belt guide for receiving the shoulder belt, inflatable airbag and airbag cover slidably therethrough as the shoulder belt is withdrawn and retracted from the belt guide; characterized in that a stiffening element coextensive with the inflatable airbag and the airbag cover for preventing kinking, twisting and gathering of the outer cover as the outer cover slides through the exit bezel is provided. a shoulder belt for extending across the torso of a passenger; a retractor for paying in and paying out a portion of the shoulder belt length; an inflatable airbag contained within an airbag cover attached to the shoulder belt near a free end of the shoulder belt; a belt guide slidably receiving the shoulder belt, the inflatable airbag and the airbag cover therein when the shoulder belt is retracted, the belt guide defining an elongate channel configured for facilitating free movement of the airbag cover during shoulder belt fastening and retraction; an exit bezel positioned near an exit of the belt guide for receiving the shoulder belt, inflatable airbag and airbag cover slidably therethrough as the shoulder belt is withdrawn and retracted from the belt guide; characterized in that a stiffening element coextensive with the inflatable airbag and the airbag cover for preventing kinking, twisting and gathering of the outer cover as the outer cover slides through the exit bezel is provided.
An ultrasound probe being configured to be able to control a reception aperture, comprising: a plurality of ultrasound transducers configured to transmit ultrasound waves at a predetermined cycle and receive ultrasound echoes from the inside of a subject; a plurality of delay circuits configured to receive reception signals from each of the ultrasound transducers and apply a delay processing to each of the reception signals; and a plurality of adder circuits each configured to add and output the reception signals to which the delay processing is applied for one of a plurality of sub-arrays, respectively; and a gate means configured to be able to switch the connection and disconnection of a signal path for each signal path arranged between one of the plurality of ultrasound transducers and the corresponding adder circuit; characterized in that the gate means is further configured to connect only the signal path from the ultrasound transducer corresponding to an initial reception aperture that is initially set after transmitting the ultrasound waves within a cycle of the ultrasound waves and sequentially connect a corresponding signal path so as to gradually widen the reception aperture in transducer units according to the lapse in time of reception period. a plurality of ultrasound transducers configured to transmit ultrasound waves at a predetermined cycle and receive ultrasound echoes from the inside of a subject; a plurality of delay circuits configured to receive reception signals from each of the ultrasound transducers and apply a delay processing to each of the reception signals; and a plurality of adder circuits each configured to add and output the reception signals to which the delay processing is applied for one of a plurality of sub-arrays, respectively; and a gate means configured to be able to switch the connection and disconnection of a signal path for each signal path arranged between one of the plurality of ultrasound transducers and the corresponding adder circuit; characterized in that the gate means is further configured to connect only the signal path from the ultrasound transducer corresponding to an initial reception aperture that is initially set after transmitting the ultrasound waves within a cycle of the ultrasound waves and sequentially connect a corresponding signal path so as to gradually widen the reception aperture in transducer units according to the lapse in time of reception period.
A composite tank for a reusable launch vehicle, the composite tank comprising: a composite wall, having a first coefficient of thermal expansion, wherein the composite wall comprises: a first end; a second end; a central axis, which passes through the first end and through the second end; and a cylindrical interior surface; and slosh baffles, formed from a material having a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion, wherein: each of the slosh baffles is attached to the cylindrical interior surface of the composite wall, each of the slosh baffles is annular and is separated from the cylindrical interior surface of the composite wall by a radial gap, selected, in part, based on a difference between the first coefficient of thermal expansion and the second coefficient of thermal expansion, and the radial gap is configured to change responsive to changes in temperature of the composite tank. a composite wall, having a first coefficient of thermal expansion, wherein the composite wall comprises: a first end; a second end; a central axis, which passes through the first end and through the second end; and a cylindrical interior surface; and a first end; a second end; a central axis, which passes through the first end and through the second end; and a cylindrical interior surface; and slosh baffles, formed from a material having a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion, wherein: each of the slosh baffles is attached to the cylindrical interior surface of the composite wall, each of the slosh baffles is annular and is separated from the cylindrical interior surface of the composite wall by a radial gap, selected, in part, based on a difference between the first coefficient of thermal expansion and the second coefficient of thermal expansion, and the radial gap is configured to change responsive to changes in temperature of the composite tank. each of the slosh baffles is attached to the cylindrical interior surface of the composite wall, each of the slosh baffles is annular and is separated from the cylindrical interior surface of the composite wall by a radial gap, selected, in part, based on a difference between the first coefficient of thermal expansion and the second coefficient of thermal expansion, and the radial gap is configured to change responsive to changes in temperature of the composite tank.
An apparatus for treating a patient having a disorder related to the passageway of the patient's intestines, the apparatus being characterized by a pump for implantation in the patient, said pump being operable externally on at least one selected portion of the patient's normal intestines, adapted to pump intestinal contents through the passageway of the intestines, and to discharge the intestinal contents through a stoma or through anus of the patient, wherein said pump includes a constriction device adapted to alternately constrict and release the selected portion to reduce the volume of the passageway of the intestines along the selected portion when constricting the selected portion, and to release the selected portion to increase the volume of the passageway of the intestines along the selected portion, such that intestinal contents is displaced through the passageway of the intestines.
A belt mounting system comprising: a main body; a device coupled to the main body; a belt mount (22; 72) configured to be coupled to a belt; and a locking element, wherein the locking element includes a pair of flexible arms, each including a locking tab, wherein when the main body and the belt mount (22; 72) are positioned adjacent one another, the main body and the belt mount (22; 72) cooperate to form a slide track (60; 90) and the locking element is inserted into the slide track (60; 90) to couple the main body and the belt mount (22; 72) to one another; wherein the locking tabs secure the locking element within the slide track (60; 90) when the flexible arms are in an extended position; and wherein the locking element may be inserted into or removed from the slide track (60; 90) when the flexible arms are in a deflected position. a main body; a device coupled to the main body; a belt mount (22; 72) configured to be coupled to a belt; and a locking element, wherein the locking element includes a pair of flexible arms, each including a locking tab,
A flush mounted built-in body for a sanitary fitting, comprising at least: a) at least one valve for a liquid, with a rotatable flow regulator and a threaded shaft, wherein the threaded shaft can be actuated for opening and closing the at least one valve in an axial direction of the at least one valve, b) at least one push button for actuating the threaded shaft of the at least one valve in the axial direction, wherein the at least one push button comprises an intermediate part screwable to the threaded shaft for setting a desired position of the at least one push button in the axial direction and a cover cap that can be connected to the threaded shaft in a rotationally fixed manner for securing the intermediate part in the desired position, and c) at least one rotating knob for adjusting the flow of the liquid, wherein the at least one rotating knob is connected to the flow regulator of the at least one valve in a rotationally fixed manner. a) at least one valve for a liquid, with a rotatable flow regulator and a threaded shaft, wherein the threaded shaft can be actuated for opening and closing the at least one valve in an axial direction of the at least one valve, b) at least one push button for actuating the threaded shaft of the at least one valve in the axial direction, wherein the at least one push button comprises an intermediate part screwable to the threaded shaft for setting a desired position of the at least one push button in the axial direction and a cover cap that can be connected to the threaded shaft in a rotationally fixed manner for securing the intermediate part in the desired position, and c) at least one rotating knob for adjusting the flow of the liquid, wherein the at least one rotating knob is connected to the flow regulator of the at least one valve in a rotationally fixed manner.
Device for testing at least one security element of a security document, wherein the device has at least one reference plane, wherein the reference plane is orientated parallel to a surface of the security document to be tested, wherein the device comprises at least one image acquisition device, wherein the at least one image acquisition device is arranged and/or constructed in such a way that a central optical axis of the image acquisition device intersects the reference plane at a predetermined reference angle, wherein the device comprises a first illumination device, wherein the first illumination device is arranged and/or constructed in such a way that a central illumination axis of the first illumination device intersects the reference plane at a first illumination angle, wherein the device comprises at least one further illumination device, wherein the further illumination device is arranged and/or constructed such that a central illumination axis of the further illumination device intersects the reference plane at a further illumination angle, wherein an amount of an angular difference (α) between the reference angle and the first illumination angle is greater than an amount of an angular difference (β) between the reference angle and the further illumination angle, wherein the amount of the angular difference (α) between the reference angle and the first illumination angle assumes an angular value from a first angular interval, wherein the first angular interval comprises angles from 15° to 50°, wherein the amount of the angular difference (β) between the reference angle and the further illumination angle assumes an angular value from a further angular interval, wherein the further angular interval comprises angles from 5° to 20°, wherein the reference angle is 90°, wherein the device comprises at least one further image acquisition device, wherein the further image acquisition device is arranged and/or constructed such that a central optical axis of the further image acquisition device intersects the reference plane at a predetermined further reference angle, characterised in that the predetermined further reference angle is equal to the first predetermined reference angle.
A vertebral body implant (500, 700, 900, 1002, 1202), comprising: a body (510, 710, 910,1010, 1210) with a first end (512, 712, 912, 1012) and a second end (514, 714, 914, 1014); a first rotating member (530, 730, 930, 1030, 1230) rotatably coupled to the first end (512, 712, 912, 1012), the first end (512, 712, 912, 1012) comprises a plurality of first notches (532, 732) inset into the first rotating member (530, 730, 930); a second rotating member (540, 740, 940, 1040, 1240) rotatably coupled to the second end (514, 714, 914, 1014), the second end (514, 714, 914, 1014) comprises a plurality of second notches (542, 742) inset into the second rotating member (540, 740, 940, 1040); a first extension member (550, 750, 950, 1050) moveably coupled to the first end (512, 712, 912, 1012); and a second extension member (570, 770, 970, 1070) moveably coupled to the second end (514, 714, 914, 1014). a body (510, 710, 910,1010, 1210) with a first end (512, 712, 912, 1012) and a second end (514, 714, 914, 1014); a first rotating member (530, 730, 930, 1030, 1230) rotatably coupled to the first end (512, 712, 912, 1012), the first end (512, 712, 912, 1012) comprises a plurality of first notches (532, 732) inset into the first rotating member (530, 730, 930); a second rotating member (540, 740, 940, 1040, 1240) rotatably coupled to the second end (514, 714, 914, 1014), the second end (514, 714, 914, 1014) comprises a plurality of second notches (542, 742) inset into the second rotating member (540, 740, 940, 1040); a first extension member (550, 750, 950, 1050) moveably coupled to the first end (512, 712, 912, 1012); and a second extension member (570, 770, 970, 1070) moveably coupled to the second end (514, 714, 914, 1014).
A method for managing a number of control surfaces for an aircraft, the method comprising: identifying a current configuration for the number of control surfaces for the aircraft during flight of the aircraft; identifying a selected point in time at which the current configuration for the number of control surfaces is to be changed to a new configuration for the number of control surfaces; and identifying a portion of time relative to the selected point in time during which the current configuration for the number of control surfaces is to be changed to the new configuration based on a difference between a current amount of energy for the aircraft and an expected amount of energy for the aircraft. identifying a current configuration for the number of control surfaces for the aircraft during flight of the aircraft; identifying a selected point in time at which the current configuration for the number of control surfaces is to be changed to a new configuration for the number of control surfaces; and identifying a portion of time relative to the selected point in time during which the current configuration for the number of control surfaces is to be changed to the new configuration based on a difference between a current amount of energy for the aircraft and an expected amount of energy for the aircraft.
A thermally dried or ambient evaporative air dried organic polymer aerogel comprising an organic polymer gel matrix and microstructures dispersed or embedded within the aerogel, which microstructures are structures having a smallest dimension that is larger than 100 nm and having at least one dimension that is no larger than 100 μm, wherein the aerogel has an at least bimodal pore size distribution measured according to ASTM D4404-10 as further specified in the description, wherein the pore size distribution has a first peak between 100 and 500 nm and a second peak between 2 and 8 nm, wherein the aerogel has a thermal conductivity of less than or equal to 40 mW/m·K, as measured at a temperature of 20°C and 13.8 kPa pressure using a heat flow meter, and wherein the microstructures are microparticles having an average size between 0.2 μm and 20 μm or microfibers having an average length between 0.1 mm and 10 mm, preferably 0.1 mm and 2 mm.