mhurhangee/ep-ind-claims huggingface dataset:
A pneumatic tire comprising: on a tread surface, one or more land portions each of which is sandwiched between a plurality of circumferential main grooves (21, 22) continuously extending in a tire circumferential direction, wherein at least one of the one or more land portions is partitioned into a plurality of blocks (71, 72, 73) by auxiliary grooves including at least an inclined groove extending while being inclined with respect to a tire width direction, and in a developed view of the tread surface, the plurality of blocks (71, 72, 73) include: a first block located on a tire equatorial plane and having a recess that is inclined with respect to the tire width direction; and a second block located to face the recess of the first block, characterised in that, in one block portion and an other block portion of the first block that define the recess of the first block, respective sidewalls (71e, 71f) defining the recess of the first block are chamfered on a tread surface side, and in the developed view of the tread surface, a connecting portion connecting, in the recess of the first block, the respective sidewalls (71e, 71f) of the one block portion and the other block portion defining the recess of the first block has a curved shape. on a tread surface, one or more land portions each of which is sandwiched between a plurality of circumferential main grooves (21, 22) continuously extending in a tire circumferential direction, wherein at least one of the one or more land portions is partitioned into a plurality of blocks (71, 72, 73) by auxiliary grooves including at least an inclined groove extending while being inclined with respect to a tire width direction, and in a developed view of the tread surface, the plurality of blocks (71, 72, 73) include: a first block located on a tire equatorial plane and having a recess that is inclined with respect to the tire width direction; and a second block located to face the recess of the first block, characterised in that, in one block portion and an other block portion of the first block that define the recess of the first block, respective sidewalls (71e, 71f) defining the recess of the first block are chamfered on a tread surface side, and in the developed view of the tread surface, a connecting portion connecting, in the recess of the first block, the respective sidewalls (71e, 71f) of the one block portion and the other block portion defining the recess of the first block has a curved shape. a first block located on a tire equatorial plane and having a recess that is inclined with respect to the tire width direction; and a second block located to face the recess of the first block, characterised in that, in one block portion and an other block portion of the first block that define the recess of the first block, respective sidewalls (71e, 71f) defining the recess of the first block are chamfered on a tread surface side, and in the developed view of the tread surface, a connecting portion connecting, in the recess of the first block, the respective sidewalls (71e, 71f) of the one block portion and the other block portion defining the recess of the first block has a curved shape.
A packaging and dispenser device, comprising: - at least two reservoirs (2, 3), in particular formed by at least two spaces inside a same enclosure, containing two different compositions (P; P') for application to the human body, in particular on the skin or mucous membranes, - a product application surface onto which at least two dispensing orifices (7; 8) emerge, fed by the first and second reservoirs, respectively, the application surface being flocked at least in part, and the device comprising a duct (21; 22; 46; 83; 84) in communication with at least one dispenser orifice and with a corresponding reservoir, formed at least in part by molding with a wall at least partially defining the application surface. - at least two reservoirs (2, 3), in particular formed by at least two spaces inside a same enclosure, containing two different compositions (P; P') for application to the human body, in particular on the skin or mucous membranes, - a product application surface onto which at least two dispensing orifices (7; 8) emerge, fed by the first and second reservoirs, respectively, the application surface being flocked at least in part, and the device comprising a duct (21; 22; 46; 83; 84) in communication with at least one dispenser orifice and with a corresponding reservoir, formed at least in part by molding with a wall at least partially defining the application surface.
A shock-absorbing device (10; 20; 30; 300; 310; 40; 50; 60; 111) comprising a first holding element (11; 31 41; 51;61; 1111) and a plurality of slender metallic structures (12, 12', 12",12 n; 32, 32', 32",32 n, 33; 42, 42', 42", 42 n; 52, 52'; 1112, 1112',1112 n, 1113, 1113',1113 n) having a first end and a second end, said slender metallic structures respectively having a slenderness ratio equal to or higher than 10, wherein the slender metallic structures are respectively fixed at their first ends to said first holding element, wherein the slender metallic structures are fixed at different points of said holding element, characterized in that: - the mutual distance between the slender metallic structures of at least one pair of slender metallic structures (12, 12'; 32, 33; 42, 42'; 52; 52', 62, 62';1112,1113) is equal to or lower than 0.75 times their length L, said distance being measured with respect to their first ends, - at least 90% of the planes perpendicular to adjacent slender structures are mutually parallel or form an angle equal to or lower than 20°, - the slender metallic structures are flat laminar or sheet elements and/or straight filiform or wire elements, and in that the slender metallic structures are arranged so as to absorb energy of impacts acting in a direction perpendicular to planes that are in turn perpendicular to the slender structures. - the mutual distance between the slender metallic structures of at least one pair of slender metallic structures (12, 12'; 32, 33; 42, 42'; 52; 52', 62, 62';1112,1113) is equal to or lower than 0.75 times their length L, said distance being measured with respect to their first ends, - at least 90% of the planes perpendicular to adjacent slender structures are mutually parallel or form an angle equal to or lower than 20°, - the slender metallic structures are flat laminar or sheet elements and/or straight filiform or wire elements,
A computer-implemented method for optimizing a turbine blade based on analysing design data representing the optimization of the turbine blade as a 3D aerodynamic design according to at least one physical criterion indicating a location dependent aerodynamic drag, aerodynamic lift or pressure loss, wherein - the design data representing modifications of the 3D aerodynamic design are provided, wherein the design data are represented by unstructured triangular surface meshes, - a displacement measure representing the local differences between two modifications of the 3D aerodynamic design is calculated based on the unstructured triangular surface meshes representing the design data, - an aerodynamic performance difference of the location dependent aerodynamic drag, aerodynamic lift or pressure loss, expressed by the at least one physical criterion, between the two design modifications is calculated, - a sensitivity information is generated representing the interrelation between the displacement measure and the performance difference, and - the sensitivity information is output indicating a location dependent aerodynamic performance sensitivity to changes in the modifications of the analysed design data, - setting initial design parameters for an initial 3D aerodynamic design depending on the output sensitivity information, - running an optimization algorithm starting from the initial 3D aerodynamic design until a stop criterion has been reached to generate an optimized 3D aerodynamic design, wherein strategy parameters of the optimization algorithm are set based on the output sensitivity information, and - outputting design data representing the optimized 3D aerodynamic design. - the design data representing modifications of the 3D aerodynamic design are provided, wherein the design data are represented by unstructured triangular surface meshes, - a displacement measure representing the local differences between two modifications of the 3D aerodynamic design is calculated based on the unstructured triangular surface meshes representing the design data, - an aerodynamic performance difference of the location dependent aerodynamic drag, aerodynamic lift or pressure loss, expressed by the at least one physical criterion, between the two design modifications is calculated, - a sensitivity information is generated representing the interrelation between the displacement measure and the performance difference, and - the sensitivity information is output indicating a location dependent aerodynamic performance sensitivity to changes in the modifications of the analysed design data, - setting initial design parameters for an initial 3D aerodynamic design depending on the output sensitivity information, - running an optimization algorithm starting from the initial 3D aerodynamic design until a stop criterion has been reached to generate an optimized 3D aerodynamic design, - outputting design data representing the optimized 3D aerodynamic design.
A wind turbine nacelle configured for mounting on a wind turbine tower and for supporting a rotor assembly, - the nacelle comprising at least a first and a second nacelle module (201, 202), - the first nacelle module comprising a first frame structure and a main bearing system for a main shaft of the rotor assembly, and - the second nacelle module comprising a second frame structure and a drive train system for the wind turbine, - wherein, when the nacelle is mounted on the wind turbine tower, the main bearing system is supported by the wind turbine tower, and the drive train system is attached to the main bearing such that the weight of the drive train system is transferred to the main bearing system and thereby to the wind turbine tower, the wind turbine nacelle being characterized by - the first frame structure is configured to support the main bearing system during transportation and prior to mounting of the nacelle, and - the second frame structure is configured to support the drive train system during transportation and prior to mounting of the nacelle, and - the first and second frame structures form a load carrying structure of a first and a second shipping freight container such that the first and second nacelle module (201, 202) can be transported as shipping freight containers. - the nacelle comprising at least a first and a second nacelle module (201, 202), - the first nacelle module comprising a first frame structure and a main bearing system for a main shaft of the rotor assembly, and - the second nacelle module comprising a second frame structure and a drive train system for the wind turbine, - wherein, when the nacelle is mounted on the wind turbine tower, the main bearing system is supported by the wind turbine tower, and the drive train system is attached to the main bearing such that the weight of the drive train system is transferred to the main bearing system and thereby to the wind turbine tower, the wind turbine nacelle being characterized by - the first frame structure is configured to support the main bearing system during transportation and prior to mounting of the nacelle, and - the second frame structure is configured to support the drive train system during transportation and prior to mounting of the nacelle, and - the first and second frame structures form a load carrying structure of a first and a second shipping freight container such that the first and second nacelle module (201, 202) can be transported as shipping freight containers.
A composition comprising a compound with the following formula for use in a method of treating or preventing bacterial infections in a mammal, wherein the method comprises administering the composition parenterally.
Method for filling the cooling system of a polymer electrolyte membrane fuel cell having at least one first bipolar plate with cooling water, the polymer electrolyte membrane fuel cell being used to supply a submarine with energy independently of external air, where the method comprises the following steps: a) connecting a pump, where the method is carried out on board a submarine, wherein the pump is not carried on board, e) evacuating a cooling system of the polymer electrolyte membrane fuel cell to a pressure of less than 500 hPa, d) heating the polymer electrolyte membrane fuel cell to 40°C to 90°C, wherein step d) is carried out before or during step e), f) introducing gaseous water, m) filling the cooling system with cooling liquid. a) connecting a pump, where the method is carried out on board a submarine, wherein the pump is not carried on board, e) evacuating a cooling system of the polymer electrolyte membrane fuel cell to a pressure of less than 500 hPa, d) heating the polymer electrolyte membrane fuel cell to 40°C to 90°C, wherein step d) is carried out before or during step e), f) introducing gaseous water, m) filling the cooling system with cooling liquid. where the method is carried out on board a submarine, wherein the pump is not carried on board, e) evacuating a cooling system of the polymer electrolyte membrane fuel cell to a pressure of less than 500 hPa, d) heating the polymer electrolyte membrane fuel cell to 40°C to 90°C, wherein step d) is carried out before or during step e), f) introducing gaseous water, m) filling the cooling system with cooling liquid.
Closing arrangement for a vessel, specifically a tank container, with a first sealing area surrounding a vessel opening a lid which covers the vessel opening and comprises a second sealing area corresponding to the first sealing area, and a sealing arrangement (29, 30, 31, 32) disposed between the first and second sealing area, wherein the sealing arrangement (29, 30, 31, 32) comprises an outer and inner sealing ring (31, 32) which define a gap in between which comprises a germ barrier (35, 38, 39), characterized in that the germ barrier comprises the sterilising fluid, specifically alcohol.
A co-crystal of CDK inhibitor LEE011 and MEK inhibitor MEK162, wherein the structure of the co-crystal is as shown in formula: x is a number between 0 and 3.
An apparatus (105, 205, 405, 503, 600) comprising: a transceiver that is configured to receive a session initiation protocol, SIP, message from a remote unit, the SIP message comprising a first request to initiate a session for an Internet Protocol Multimedia Subsystem, IMS, Multimedia Telephony Communication Service, MMTEL; and a processor that is configured to: determine that the received SIP message is communicated using transmission control protocol, TCP, as a transport layer protocol; and forward the first request comprised in the received SIP message to a network entity, wherein the first request is forwarded to the network entity using user datagram protocol, UDP, as the transport layer protocol. a transceiver that is configured to receive a session initiation protocol, SIP, message from a remote unit, the SIP message comprising a first request to initiate a session for an Internet Protocol Multimedia Subsystem, IMS, Multimedia Telephony Communication Service, MMTEL; and a processor that is configured to: determine that the received SIP message is communicated using transmission control protocol, TCP, as a transport layer protocol; and forward the first request comprised in the received SIP message to a network entity, wherein the first request is forwarded to the network entity using user datagram protocol, UDP, as the transport layer protocol. determine that the received SIP message is communicated using transmission control protocol, TCP, as a transport layer protocol; and forward the first request comprised in the received SIP message to a network entity, wherein the first request is forwarded to the network entity using user datagram protocol, UDP, as the transport layer protocol.
A device for inserting into an anal canal extending from a rectal neck surrounded by a rectal wall downward to an anal orifice to treat incontinence, said device comprising: an anchoring element connected to a biasing element by a stem portion, wherein said anchoring element is positionable within the rectal neck and said biasing element engages an external surface of the anus and is characterized in that it applies a gentle force through said stem portion that causes stretching and adjustment of the length of the stem portion, wherein the anchoring element does not apply any substantial radial forces to the rectal wall when said anchoring element is biased against said rectal neck and is a cupped or flat disc and has a thickness from 10 microns to 3000 microns and a diameter in the range from 1 cm to 5 cm. an anchoring element connected to a biasing element by a stem portion, wherein said anchoring element is positionable within the rectal neck and said biasing element engages an external surface of the anus and is characterized in that it applies a gentle force through said stem portion that causes stretching and adjustment of the length of the stem portion, wherein the anchoring element does not apply any substantial radial forces to the rectal wall when said anchoring element is biased against said rectal neck and is a cupped or flat disc and has a thickness from 10 microns to 3000 microns and a diameter in the range from 1 cm to 5 cm.
A method of forming a multi-layered tire component, the method comprising the steps of: providing a mechanical system, the system including a plurality of cutting members; and a sheet generator; introducing input material into a sheet generator; forming a sheet of material with the sheet generator; translating a sheet of material along a translation path through the mechanical system; wherein the translation path is a closed-loop path extending from the sheet generator and returning at least a portion of the sheet to the sheet generator for use as input material; cutting one or more strips (41, 41a, 41b, 41c, 41d) from the sheet with one or more of the plurality of cutting members, this step occurring during the step of translating; mechanically applying the one or more strips (41, 41a - 41d) to a building surface on a building drum, this step occurring during the step of translating and after the step of cutting one or more strips has initiated; wherein the step of mechanically applying the one or more strips (41, 41a - 41 d) includes placing each of the strips (41, 41a - 41d) into pressurized contact against the building surface by translating at least one of the building surface and an applicator drum toward the other to force the one or more strips (41, 41a - 41d) against the building surface. providing a mechanical system, the system including a plurality of cutting members; and a sheet generator; introducing input material into a sheet generator; forming a sheet of material with the sheet generator; translating a sheet of material along a translation path through the mechanical system; wherein the translation path is a closed-loop path extending from the sheet generator and returning at least a portion of the sheet to the sheet generator for use as input material; cutting one or more strips (41, 41a, 41b, 41c, 41d) from the sheet with one or more of the plurality of cutting members, this step occurring during the step of translating; mechanically applying the one or more strips (41, 41a - 41d) to a building surface on a building drum, this step occurring during the step of translating and after the step of cutting one or more strips has initiated; wherein the step of mechanically applying the one or more strips (41, 41a - 41 d) includes placing each of the strips (41, 41a - 41d) into pressurized contact against the building surface by translating at least one of the building surface and an applicator drum toward the other to force the one or more strips (41, 41a - 41d) against the building surface.
A press-fit terminal made of a wire material of a predetermined length, the press-fit terminal comprising: a distal section formed at one end of the wire material to be inserted into a substrate; a connecting section formed at the other end of the wire material to be connected to a complementary terminal; and a press-fit section formed at a distal section side of the wire material to be press-fitted into a through-hole formed in the substrate; wherein the press-fit section is formed at the central part thereof with a hole vertically elongated along an axis direction of the wire material; the inner circumferential surface of the hole is formed with an extending section protruding toward the center of the hole along the inner circumferential surface of the hole; characterized in that the extending section is formed at the distal end thereof with an erected section extending into a vertical direction with respect to the axis direction of the wire material, the erected section being formed so as to protrude and encircle the hole with a predetermined height. a distal section formed at one end of the wire material to be inserted into a substrate; a connecting section formed at the other end of the wire material to be connected to a complementary terminal; and a press-fit section formed at a distal section side of the wire material to be press-fitted into a through-hole formed in the substrate; wherein the press-fit section is formed at the central part thereof with a hole vertically elongated along an axis direction of the wire material; the inner circumferential surface of the hole is formed with an extending section protruding toward the center of the hole along the inner circumferential surface of the hole; characterized in that the extending section is formed at the distal end thereof with an erected section extending into a vertical direction with respect to the axis direction of the wire material, the erected section being formed so as to protrude and encircle the hole with a predetermined height.