mhurhangee/patent-ind-claim-en huggingface dataset:
A combination of a cylindrical dust cover , having an opening formed at the lower end thereof, and of a buffer member formed of a combination of peaks and troughs and having a through hole , through which a cylinder (C) rod (L) of a shock absorber is intended to pass, the buffer member and the dust cover being connected by means of a connection member so that the buffer member and the dust cover are integrated with each other, wherein a plurality of linear reinforcement protrusions are provided on the connection member so as to extend radially, a plurality of ring-shaped connection protrusions are formed so as to connect the linear reinforcement protrusions , and exhaust grooves are formed so as to be recessed upwards, the combination of dust cover and buffer member being characterized in that : the buffer member is outside the dust cover , the connection member being an annular connection plate and the buffer member extending from the inner edge of the connection plate while the dust cover extends from the outer edge of the connection plate , the plurality of linear reinforcement protrusions are formed on the upper surface of the connection plate and extend from a first boundary point (S1) with respect to the buffer member , located at the inner edge of the connection plate , to a second boundary point (S2) with respect to the dust cover , located at the outer edge of the connection plate , the ring-shaped connection protrusions are formed in the center on the upper surface of the connection plate , the exhaust grooves are each formed on the inside of a respective linear reinforcement protrusion , and connection grooves are each formed on the inside of a respective ring-shaped connection protrusion so as to be depressed upwards, so that the respective exhaust grooves communicate with each other by the connection grooves . the buffer member is outside the dust cover , the connection member being an annular connection plate and the buffer member extending from the inner edge of the connection plate while the dust cover extends from the outer edge of the connection plate , the plurality of linear reinforcement protrusions are formed on the upper surface of the connection plate and extend from a first boundary point (S1) with respect to the buffer member , located at the inner edge of the connection plate , to a second boundary point (S2) with respect to the dust cover , located at the outer edge of the connection plate , the ring-shaped connection protrusions are formed in the center on the upper surface of the connection plate , the exhaust grooves are each formed on the inside of a respective linear reinforcement protrusion , and connection grooves are each formed on the inside of a respective ring-shaped connection protrusion so as to be depressed upwards, so that the respective exhaust grooves communicate with each other by the connection grooves .
A fluid-filter monitor apparatus for operating at a fluid-maintenance site, the fluid-filter monitor apparatus comprising: a fluid filter, a sensor configured and arranged to provide parameters that characterize fluid flowing through the fluid filter, and a wireless interface circuit ; the wireless interface circuit configured and arranged to operate in a set-up mode by communicating authentication data with a mobile data-processing device while the mobile data-processing device is proximate to the fluid-maintenance site, the authentication data being defined by an authentication protocol and including connection-authorization information for connecting to a local WiFi network for transmitting the parameters to a remotely-situated server ; and operate in a normal-operation mode by sending the parameters wirelessly, according to the authentication protocol, to the remotely-situated server via a wireless communication medium and a broadband connection. a fluid filter, a sensor configured and arranged to provide parameters that characterize fluid flowing through the fluid filter, and a wireless interface circuit ; the wireless interface circuit configured and arranged to operate in a set-up mode by communicating authentication data with a mobile data-processing device while the mobile data-processing device is proximate to the fluid-maintenance site, the authentication data being defined by an authentication protocol and including connection-authorization information for connecting to a local WiFi network for transmitting the parameters to a remotely-situated server ; and operate in a normal-operation mode by sending the parameters wirelessly, according to the authentication protocol, to the remotely-situated server via a wireless communication medium and a broadband connection. operate in a set-up mode by communicating authentication data with a mobile data-processing device while the mobile data-processing device is proximate to the fluid-maintenance site, the authentication data being defined by an authentication protocol and including connection-authorization information for connecting to a local WiFi network for transmitting the parameters to a remotely-situated server ; and operate in a normal-operation mode by sending the parameters wirelessly, according to the authentication protocol, to the remotely-situated server via a wireless communication medium and a broadband connection.
A gelatin-based enteric capsule, comprising an alkali-treated gelatin and a carrageenan as an enteric property imparting agent in a capsule coating side or in a coated side coated with a capsule coating, but comprising no gelatin other than the alkali-treated gelatin, and no counter ion to be bound to the carrageenan.
Seal bellows composed of a rubber-elastic material, comprising a first end side and a second end side and also a shell with a central axis , wherein the shell is arranged between the end sides in an axial direction and comprises at least one torsion-compensating element for the substantially torsional stress-free absorption of torsional movements introduced into the seal bellows and wherein the first end side is configured as a first static seal and the second end side is configured as a second static seal , wherein the seal bellows is composed of a TPE material, wherein the torsion-compensating element comprises an origami structure , with folding elements which are connected to one another by kinks so as to be able to move relative to one another, wherein, in the case of torsional movements introduced into the seal bellows, the folding elements can be moved relative to one another in a circumferential direction of the shell in a substantially stress-free manner, wherein the origami structure comprises three-dimensional basic forms with the folding elements , characterized in that each of the basic forms is configured as a concave hexagonal pyramid whose apex is arranged in the direction of the central axis of the seal bellows, wherein the basic forms are arranged in an imaginary first radial plane of the shell and adjacent to one another in the circumferential direction and wherein an imaginary second radial plane of the shell is arranged axially adjacently with respect to the imaginary first radial plane of the shell , further three-dimensional basic forms being arranged adjacent to one another in the circumferential direction in said second radial plane , and wherein the basic forms in the first imaginary radial plane and the second imaginary radial plane , as viewed in the circumferential direction , are arranged so as to be offset relative to one another in each case by half a basic form .
Lap welding method comprising superposing a plurality of steel sheets, wherein at least one steel sheet among said plurality of steel sheets is a steel sheet having a tensile strength of 1180 MPa or more, and firing a laser to form a substantially circular laser weld and a heat affected zone (HAZ) softened part, characterized by firing the laser in a straight line through an outer edge of said substantially circular laser weld up to the outside of the HAZ softened part so as to form a hardened part at the steel sheets, wherein the hardened part comprises a reheated and hardened HAZ softened part formed by the substantially circular laser weld
A structure for protecting a substrate, the structure comprising an inner tie coat layer which can bond to the substrate, a geopolymer foam layer, and an outer protective layer; the geopolymer foam layer being the reaction product of a mixture comprising an aluminosilicate source, an alkali activator, reinforcing fibres, a plurality of microparticles, and water, characterised in that the mixture comprises 20 to 50 weight % of the plurality of microparticles.
An encoder comprising: a synthesizer configured to generate a synthesized high band audio signal based on a high band audio signal ; gain shape circuitry configured to: determine a number of sub-frames of multiple sub-frames that are saturated, wherein determining that a particular sub-frame of the multiple subframes is saturated comprises determining that a number of bits needed to represent an energy value associated with the particular sub-frame exceeds a fixed-point width associated with the encoder, the multiple sub-frames included in a frame of the high band audio signal; apply a first scaling factor to scale the high band audio signal if the particular sub-frame is saturated to generate a first scaled high band audio signal; determine a gain shape parameter of the particular sub-frame based on a first ratio associated with the first scaled high band audio signal and the synthesized high band audio signal ; a gain shape compensator configured to generate a compensated synthesized high band audio signal based on the synthesized high band audio signal and based on the gain shape parameter; gain frame circuitry configured to: apply a second scaling factor to scale the high band audio signal to generate a second scaled high band audio signal based on the number of sub-frames that are saturated; determine a gain frame parameter corresponding to the frame based on the number of sub-frames that are saturated and based on a second ratio associated with the second scaled high band audio signal and the compensated synthesized high band audio signal . determine a number of sub-frames of multiple sub-frames that are saturated, wherein determining that a particular sub-frame of the multiple subframes is saturated comprises determining that a number of bits needed to represent an energy value associated with the particular sub-frame exceeds a fixed-point width associated with the encoder, the multiple sub-frames included in a frame of the high band audio signal; apply a first scaling factor to scale the high band audio signal if the particular sub-frame is saturated to generate a first scaled high band audio signal; determine a gain shape parameter of the particular sub-frame based on a first ratio associated with the first scaled high band audio signal and the synthesized high band audio signal ; apply a second scaling factor to scale the high band audio signal to generate a second scaled high band audio signal based on the number of sub-frames that are saturated; determine a gain frame parameter corresponding to the frame based on the number of sub-frames that are saturated and based on a second ratio associated with the second scaled high band audio signal and the compensated synthesized high band audio signal .
Suspension device for a turbomachine comprising: - a body intended to be attached to a fixed part of an aircraft, extending along a longitudinal axis (A) intended to be parallel to a driving shaft axis (X) of the turbomachine once the suspension device is connected to the turbomachine, - a first connecting rod and a second connecting rod located in the same transverse plane (P) perpendicular to the longitudinal axis (A) of the body, each comprising a first end articulated with respect to the body , and a second end intended to be articulated on a first part of the turbomachine , - a third connecting rod articulated on the body between the first ends of the first and second connecting rods and intended to be articulated on the first part of the turbomachine , between the second ends of the first and second connecting rods , - a rudder hinged to the body , - a fourth connecting rod and a fifth connecting rod , each extending along an axis of extension (L1, L2) and each comprising a first end articulated on the rudder and a second end intended to be articulated on a second part of the turbomachine , - the points of intersection (P1, P2) between the extension axes (L1, L2) of the fourth and fifth connecting rods and the transverse plane (P) being located between the first connecting rod and the second connecting rod and on either side of the third connecting rod in a transverse direction. - a body intended to be attached to a fixed part of an aircraft, extending along a longitudinal axis (A) intended to be parallel to a driving shaft axis (X) of the turbomachine once the suspension device is connected to the turbomachine, - a first connecting rod and a second connecting rod located in the same transverse plane (P) perpendicular to the longitudinal axis (A) of the body, each comprising a first end articulated with respect to the body , and a second end intended to be articulated on a first part of the turbomachine , - a third connecting rod articulated on the body between the first ends of the first and second connecting rods and intended to be articulated on the first part of the turbomachine , between the second ends of the first and second connecting rods , - a rudder hinged to the body , - a fourth connecting rod and a fifth connecting rod , each extending along an axis of extension (L1, L2) and each comprising a first end articulated on the rudder and a second end intended to be articulated on a second part of the turbomachine , - the points of intersection (P1, P2) between the extension axes (L1, L2) of the fourth and fifth connecting rods and the transverse plane (P) being located between the first connecting rod and the second connecting rod and on either side of the third connecting rod in a transverse direction.
A surgical instrument , comprising: a handle portion ; first and second jaw members operably coupled to the handle portion and movable relative to one another in response to an actuation of the handle portion; a first sensor associated with one of the first or second jaw members and configured to measure local perfusion in tissue grasped between the first and second jaw members; a second sensor associated with one of the first or second jaw members and configured to measure a pressure applied to the tissue by the first and second jaw members, and a display disposed on the handle portion and in communication with the first and second sensors, wherein the display is configured to display the measured local perfusion and the measured pressure applied to the tissue by the first and second jaw members, characterised in that : the surgical instrument is pre-programmed to clamp tissue at a predetermined clamping pressure predicted to cease perfusion through the tissue, to reduce the clamping pressure at a predetermined rate, and send sensed pressure to the display at the moment when perfusion through the tissue restarts. a handle portion ; first and second jaw members operably coupled to the handle portion and movable relative to one another in response to an actuation of the handle portion; a first sensor associated with one of the first or second jaw members and configured to measure local perfusion in tissue grasped between the first and second jaw members; a second sensor associated with one of the first or second jaw members and configured to measure a pressure applied to the tissue by the first and second jaw members, and a display disposed on the handle portion and in communication with the first and second sensors, wherein the display is configured to display the measured local perfusion and the measured pressure applied to the tissue by the first and second jaw members, characterised in that : the surgical instrument is pre-programmed to clamp tissue at a predetermined clamping pressure predicted to cease perfusion through the tissue, to reduce the clamping pressure at a predetermined rate, and send sensed pressure to the display at the moment when perfusion through the tissue restarts.
An interface structure for an electronic component comprising; a main portion made of electrically insulating material, the main portion including a first main surface, a second main surface opposite to the first main surface, and a plurality of through holes passing from the first main surface to the second main surface, an inner wall of each through hole applied with a conductive plating ; and a plurality of coil springs made of electrically conductive material, each coil spring being received in the corresponding through hole of the main portion; wherein each coil spring includes a connection portion for connecting a terminal of the electronic component inserted from the through hole at the side of the first main surface, a movable contact portion for contacting with a conductive region at the side of the second main surface, and an elastic portion connected between the connection portion and the movable contact portion , characterized in that the movable contact portion includes an end portion having a respective axial direction that is inclined at an angle θ relative to the axial direction (C) of the coil spring when the coil spring is in an uncompressed state, and wherein the movable contact portion protrudes from the second main surface of the main portion .
A method for simultaneous verification of adapter connection and permeability of endoscope channels in an endoscope preparation machine, wherein this verification is carried out using gas and the gas is conducted via a directional control valve into individual or multiple flow areas, wherein n endoscope channels are connected to a first flow area A and m endoscope channels are connected to a second flow area B, wherein a first endoscope channel connected to the flow area A is connected to an endoscope channel connected to the flow area B, wherein i. the compressed air is conducted completely into the first flow area, which is connected to n endoscope channels of the first flow area, wherein the channel pressure is not measured for the first endoscope channel and the channel pressure is measured for each of the n-1 endoscope channels of the first flow area and m endoscope channels of the second flow area by means of a pressure sensor and transmitted to a control unit, ii. the compressed air is conducted completely into a second flow area, which is connected to m endoscope channels of the second flow area, wherein for all n-1 endoscope channels of the first flow area and m endoscope channels of the second flow area, the channel pressure is measured in each case by means of a pressure sensor and transmitted to a control unit, iii. optionally the compressed air is conducted into the first and the second flow area, and for the n-1 endoscope channels of the first flow area and the m endoscope channels of the second flow area, the channel pressure is measured in each case by means of a pressure sensor and transmitted to the control unit, and iv. in the control unit, the measured channel pressures are compared to reference pressures and evaluated. i. the compressed air is conducted completely into the first flow area, which is connected to n endoscope channels of the first flow area, wherein the channel pressure is not measured for the first endoscope channel and the channel pressure is measured for each of the n-1 endoscope channels of the first flow area and m endoscope channels of the second flow area by means of a pressure sensor and transmitted to a control unit, ii. the compressed air is conducted completely into a second flow area, which is connected to m endoscope channels of the second flow area, wherein for all n-1 endoscope channels of the first flow area and m endoscope channels of the second flow area, the channel pressure is measured in each case by means of a pressure sensor and transmitted to a control unit, iii. optionally the compressed air is conducted into the first and the second flow area, and for the n-1 endoscope channels of the first flow area and the m endoscope channels of the second flow area, the channel pressure is measured in each case by means of a pressure sensor and transmitted to the control unit, and iv. in the control unit, the measured channel pressures are compared to reference pressures and evaluated.
A method for replacing an exhaust aftertreatment component of an exhaust aftertreatment system of a vehicle or vessel, the exhaust aftertreatment system being delimited by an outer casing , the exhaust aftertreatment system comprising a first sleeve containing a first exhaust aftertreatment component mounted directly in the first sleeve , the first sleeve extending in an axial direction, the first exhaust aftertreatment component being a catalyst substrate or a Diesel Particulate Filter substrate, the method comprising the steps of: S1: removing the first exhaust aftertreatment component from the first sleeve , the first sleeve thereby remaining intact in its existing position within the outer casing , S2: providing a second exhaust aftertreatment component being mounted in a second sleeve , the second sleeve being configured to fit within the first sleeve , and S3: mounting the second sleeve with the second exhaust aftertreatment component in the first sleeve by inserting the second sleeve into the first sleeve in the axial direction thereof. the exhaust aftertreatment system comprising a first sleeve containing a first exhaust aftertreatment component mounted directly in the first sleeve , the first sleeve extending in an axial direction, the first exhaust aftertreatment component being a catalyst substrate or a Diesel Particulate Filter substrate, the method comprising the steps of: S1: removing the first exhaust aftertreatment component from the first sleeve , the first sleeve thereby remaining intact in its existing position within the outer casing , S2: providing a second exhaust aftertreatment component being mounted in a second sleeve , the second sleeve being configured to fit within the first sleeve , and S3: mounting the second sleeve with the second exhaust aftertreatment component in the first sleeve by inserting the second sleeve into the first sleeve in the axial direction thereof. S1: removing the first exhaust aftertreatment component from the first sleeve , the first sleeve thereby remaining intact in its existing position within the outer casing , S2: providing a second exhaust aftertreatment component being mounted in a second sleeve , the second sleeve being configured to fit within the first sleeve , and S3: mounting the second sleeve with the second exhaust aftertreatment component in the first sleeve by inserting the second sleeve into the first sleeve in the axial direction thereof.