mhurhangee/ep-ind-claims huggingface dataset:
An intermediate casing of a bypass flow turbojet comprising, at least one annular separator for separating a gas flow into two concentric annular flows (P, S), primary and secondary, respectively, and between an inner hub and an outer cylindrical shroud, a plurality of radial arms, at least one of which is hollow and comprises a first portion passing through the main flow and a second portion passing through the bypass flow, a radial transmission shaft for driving the auxiliary machines being mounted rotatably in said radial arm, a first end of the transmission shaft passing through the inner hub and the second end passing through the outer cylindrical shroud, a casing wherein the inner volume of the radial arm consists of a single compartment housing the transmission shaft and forming a passageway for a lubrication fluid.
A power tool comprising: a housing; a motor disposed in the housing; a tool holder driven by the motor; a control circuit for controlling the motor; a rotary input rotatable by the user, the rotary input being one of the group consisting of a trigger assembly which comprises a trigger disposed within the housing, the trigger being linearly movable relative to the housing for selecting the rotational speed of the motor, and a handle; and a rotational sensor for sensing the rotational position of the rotary input relative to the housing; wherein the control circuit receives input from the rotational sensor; characterized in that: the trigger of the trigger assembly is also rotatable relative to the housing about a first axis for selecting the rotational direction of the motor; and the handle is rotatably attached to the housing. a housing; a motor disposed in the housing; a tool holder driven by the motor; a control circuit for controlling the motor; a rotary input rotatable by the user, the rotary input being one of the group consisting of a trigger assembly which comprises a trigger disposed within the housing, the trigger being linearly movable relative to the housing for selecting the rotational speed of the motor, and a handle; and a rotational sensor for sensing the rotational position of the rotary input relative to the housing; wherein the control circuit receives input from the rotational sensor; the trigger of the trigger assembly is also rotatable relative to the housing about a first axis for selecting the rotational direction of the motor; and the handle is rotatably attached to the housing.
A carrying strap arranged to allow an individual to carry an object on his or her back, comprising a shaping reinforcement (18; 50; 60) comprising an upper reinforcement portion (19; 51; 61) having a curved shape and arranged such that the carrying strap extends over a shoulder of the individual, and a front reinforcement portion (20; 52; 62) arranged such that the carrying strap extends downwards against a front face of the individual's chest, the front reinforcement portion comprising a bearing portion arranged such that the carrying strap comes to bear on a bearing surface of the individual situated on a front face or on a side face of the individual's chest or abdomen, so as to apply at least part of the load of the object against the bearing surface of the individual, characterised in that the bearing portion has a cross-section (23; 26; 27) different from a segment (25; 53) of the front reinforcement portion extending between the bearing portion and the upper reinforcement portion, a shape of a cross-section of the front reinforcement portion varying according to a length of the front reinforcement portion.
Laser for nonlinear microscopy comprising - a source configured to emit a burst of ultrashort pump pulses comprising a first, a second and subsequent pump pulses of a first wavelength λ 1, - an optical resonator formed by at least two mirrors, - a solid-state nonlinear Raman medium placed inside said optical resonator, wherein - the burst of ultrashort pump pulses is arranged to enter the optical resonator with the Raman medium placed on a path of a laser beam and generates a burst of ultrashort pulses of a second wavelength λ 2, - a length of the optical resonator is chosen so that the second and subsequent pump pulses at least partially overlap in time with a pulse of the second wavelength λ 2 circulating inside the resonator when it propagates through the Raman medium, - duration of the pump pulses is from 30fs to 1ps, characterized in that - the first pump pulse from the burst of pump pulses has a higher energy than other pump pulses from the burst; - in the Raman medium, said first pump pulse generates a supercontinuum broadband radiation with a bandwidth overlapping the second wavelength λ 2; - the burst of ultrashort pump pulses consists of three to several tens of pulses. - a source configured to emit a burst of ultrashort pump pulses comprising a first, a second and subsequent pump pulses of a first wavelength λ 1, - an optical resonator formed by at least two mirrors, - a solid-state nonlinear Raman medium placed inside said optical resonator, wherein - the burst of ultrashort pump pulses is arranged to enter the optical resonator with the Raman medium placed on a path of a laser beam and generates a burst of ultrashort pulses of a second wavelength λ 2, - a length of the optical resonator is chosen so that the second and subsequent pump pulses at least partially overlap in time with a pulse of the second wavelength λ 2 circulating inside the resonator when it propagates through the Raman medium, - duration of the pump pulses is from 30fs to 1ps, - the first pump pulse from the burst of pump pulses has a higher energy than other pump pulses from the burst; - in the Raman medium, said first pump pulse generates a supercontinuum broadband radiation with a bandwidth overlapping the second wavelength λ 2; - the burst of ultrashort pump pulses consists of three to several tens of pulses.
A seating structure comprising: a backrest member (84; 160) having a front body-facing surface; an auxiliary support member moveably coupled to said backrest member (84; 160), said auxiliary support member vertically moveable in front of said front body-facing surface of said backrest member (84; 160) between first and second vertical positions, wherein said auxiliary support member is moved forwardly relative to said backrest member (84; 160) from a first position to a second position as said auxiliary support member is moved from said first vertical position to said second vertical position; and a body supporting substrate disposed along said front body-facing surface of said backrest member (84; 160) and covering said auxiliary support member; characterized in that said backrest member (84; 160) has a cutout formed in a lower region thereof and defining a pad portion coupled to opposite side portions with a pair of connectors laterally spaced on opposite sides of said pad portion, wherein said pad portion is pivotable about said pair of connectors relative to said opposite side portions. a backrest member (84; 160) having a front body-facing surface; an auxiliary support member moveably coupled to said backrest member (84; 160), said auxiliary support member vertically moveable in front of said front body-facing surface of said backrest member (84; 160) between first and second vertical positions, wherein said auxiliary support member is moved forwardly relative to said backrest member (84; 160) from a first position to a second position as said auxiliary support member is moved from said first vertical position to said second vertical position; and a body supporting substrate disposed along said front body-facing surface of said backrest member (84; 160) and covering said auxiliary support member; characterized in that said backrest member (84; 160) has a cutout formed in a lower region thereof and defining a pad portion coupled to opposite side portions with a pair of connectors laterally spaced on opposite sides of said pad portion, wherein said pad portion is pivotable about said pair of connectors relative to said opposite side portions.
A surgical hub for controlling a display, the surgical hub comprising: a processor, the processor being configured to: determine a user (31850, 31850), a medical instrument, and a location (31700, 31720) within an operating room; determine contextual data associated with the medical instrument based on the user, the medical instrument, and the location within the operating room by: determining that the medical instrument is at the location; determining that the user is beyond a threshold distance away from the location; determining that the location indicates that the medical instrument is to be powered off; and setting a display instruction to indicate that the medical instrument should be powered off; and send the display instruction to the display that instructs the display to be configured in accordance with the contextual data associated with the medical instrument. determine a user (31850, 31850), a medical instrument, and a location (31700, 31720) within an operating room; determine contextual data associated with the medical instrument based on the user, the medical instrument, and the location within the operating room by: determining that the medical instrument is at the location; determining that the user is beyond a threshold distance away from the location; determining that the location indicates that the medical instrument is to be powered off; and setting a display instruction to indicate that the medical instrument should be powered off; and determining that the medical instrument is at the location; determining that the user is beyond a threshold distance away from the location; determining that the location indicates that the medical instrument is to be powered off; and setting a display instruction to indicate that the medical instrument should be powered off; and send the display instruction to the display that instructs the display to be configured in accordance with the contextual data associated with the medical instrument.
Isolated peptide derived from the human cyclin B1 sequence of SEQ ID NO. 1 and which comprises at least one human cyclin B1 CD4 + T epitope which is immunodominant in vitro, said peptide being selected from the group consisting of: a) the sequences of up to 30 consecutive amino acids of the human cyclin B1 sequence of SEQ ID NO. 1 comprising one of the sequences of SEQ ID NO: 10, 57, 58, 61, 76, 77, 83, 84, 87, 88 and 91, and b) the sequences of 15 to 25 amino acids having at least 85 % identity with a sequence in a), with the exclusion of the sequence of 15 amino acids consisting of residues 279 to 293 of said sequence SEQ ID NO. 1, and said peptide in a) and b) being capable of stimulating a specific human CD4 + T lymphocyte response wherein the average strength of the in vitro response of human CD4 + T lymphocytes specific for said peptide is at least 2.8% in a group of human individuals expressing varied HLA II molecules including at least the HLA-DR1, HLA-DR3, HLA-DR4, HLA-DR7, HLA-DR11, HLA-DR13 and HLA-DR15 molecules, and the frequency of responders in vitro to said peptide is at least 65% in said group of human individuals. a) the sequences of up to 30 consecutive amino acids of the human cyclin B1 sequence of SEQ ID NO. 1 comprising one of the sequences of SEQ ID NO: 10, 57, 58, 61, 76, 77, 83, 84, 87, 88 and 91, and b) the sequences of 15 to 25 amino acids having at least 85 % identity with a sequence in a), with the exclusion of the sequence of 15 amino acids consisting of residues 279 to 293 of said sequence SEQ ID NO. 1, and said peptide in a) and b) being capable of stimulating a specific human CD4 + T lymphocyte response wherein the average strength of the in vitro response of human CD4 + T lymphocytes specific for said peptide is at least 2.8% in a group of human individuals expressing varied HLA II molecules including at least the HLA-DR1, HLA-DR3, HLA-DR4, HLA-DR7, HLA-DR11, HLA-DR13 and HLA-DR15 molecules, and the frequency of responders in vitro to said peptide is at least 65% in said group of human individuals.
Aircraft provided with a rotary wing and three turboshaft engines (11, 12, 13) to set said rotary wing in motion, - said three turboshaft engines include two identical main turboshaft engines (11, 12), each main turboshaft engine being able to operate at at least one specific engine speed associated with a main power (PMD, PIU) that can be developed, characterised in that: - said three turboshaft engines including a secondary turboshaft engine, which develops a power that is equal to no more than half the power developed by each main turboshaft engine, said secondary turboshaft engine being able to operate at said at least one specific engine speed by supplying secondary power (PMD', PIU') proportional to the corresponding main power (PMD, PIU) according to a proportionality coefficient ( k) less than or equal to 0.5, said secondary power therefore being to the main power developed by a main turboshaft engine multiplied by said proportionality coefficient, - said aircraft has a control system to drive the rotary wing by causing each main turboshaft engine (11, 12) to operate constantly during a flight, and in addition the secondary turboshaft engine during at least one predetermined specific phase. - said three turboshaft engines include two identical main turboshaft engines (11, 12), each main turboshaft engine being able to operate at at least one specific engine speed associated with a main power (PMD, PIU) that can be developed, - said three turboshaft engines including a secondary turboshaft engine, which develops a power that is equal to no more than half the power developed by each main turboshaft engine, said secondary turboshaft engine being able to operate at said at least one specific engine speed by supplying secondary power (PMD', PIU') proportional to the corresponding main power (PMD, PIU) according to a proportionality coefficient ( k) less than or equal to 0.5, said secondary power therefore being to the main power developed by a main turboshaft engine multiplied by said proportionality coefficient, - said aircraft has a control system to drive the rotary wing by causing each main turboshaft engine (11, 12) to operate constantly during a flight, and in addition the secondary turboshaft engine during at least one predetermined specific phase.
A release device (100, 100a) for releasing a medical self-expanding implant from an insertion device, in which the self-expanding implant can be released by way of a relative movement between an inner shaft and an outer shaft and the subsequent retraction of the insertion device, the relative movement between the inner shaft and the outer shaft comprising a movement of the outer shaft in the direction of the proximal end of the insertion device, the release device comprising a clamping unit (10, 10a) for clamping the self-expanding implant in the insertion device, having a proximal end, which is distant from a distal end of the insertion device in the state of use, and having a distal end, which faces the distal end of the insertion device in the state of use, the clamping unit (10, 10a) comprising a first component (16, 16a) and at least one second component (18, 18a), the first component (16, 16a) being arranged at the proximal end of the clamping unit (10, 10a) and the second component (18, 18a) being arranged at the distal end of the clamping unit (10, 10a), the first component (16, 16a) and the second component (18, 18a) being arranged on the inner shaft in an axially fixed manner, the self-expanding implant being clamped between the outer shaft and the second component (18, 18a) in the clamped state, the first component (16, 16a) having a sleeve region, the sleeve region in the clamped state surrounding a proximal end of the self-expanding implant in a circumferential direction and thus being able to produce a form-fit connection between the first component (16, 16a) and the self-expanding implant, which holds the self-expanding implant in position, characterised in that the first component (16, 16a) comprises a material that is harder than the material of the at least second component (18, 18a), whereby the first component (16, 16a) can withstand radial forces of the second component and/or the implant.
A therapeutic peptide consisting of a construct and at least two or more arms, the construct having a central framework and each arm consisting of a sequence linked to the central framework via a linker sequence, wherein each sequence is the same or different and is selected from the group consisting of: WNSTL (SEQ ID NO:1), NQHTPR (SEQ ID NO:2), WNSTY (SEQ ID NO:5), YNSTL (SEQ ID NO:6), YQPSL (SEQ ID NO:7), and VQATQS (SEQ ID NO:8)
An ultrasonic sensor array comprising: a plurality of ultrasonic transducers, each transducer including a piezoelectric member, characterized in that: each of the transducers includes an electret member; each of the transducers includes a receive, Rx, layer (303; 503; 603) configured to exhibit a first d33 resonating mode coefficient and a transmit, Tx, layer (301; 501; 601) configured to exhibit a second d33 resonating mode coefficient, the first d33 resonating mode coefficient being different from the second d33 resonating mode coefficient; and the transducers are disposed on a flexible substrate; wherein the first d33 resonating mode coefficient is of opposite sign with respect to the second d33 resonating mode coefficient. each of the transducers includes an electret member; each of the transducers includes a receive, Rx, layer (303; 503; 603) configured to exhibit a first d33 resonating mode coefficient and a transmit, Tx, layer (301; 501; 601) configured to exhibit a second d33 resonating mode coefficient, the first d33 resonating mode coefficient being different from the second d33 resonating mode coefficient; and the transducers are disposed on a flexible substrate; wherein the first d33 resonating mode coefficient is of opposite sign with respect to the second d33 resonating mode coefficient.
A doctor blade (100, 200), In particular for doctoring off printing ink from a surface of a printing form and/or for use as a paper doctor knife, comprising a flat and elongated main body (111, 211) having a working edge region (113, 213) formed in a longitudinal direction, wherein at least the working edge region (113, 213) is covered with a first coating (120, 220) on the basis of a nickel-phosphorus alloy, and monocrystalline and/or polycrystalline diamond particles (120.1, 220.1) are dispersed in the first coating (120, 220), wherein the particle size of the diamond particles (120.1, 220.1) measures at least 5 nm and less than 50 nm, and wherein a second coating on the basis of a further nickel-phosphorus alloy is arranged on the first coating (120, 220), characterized in that a phosphorus content of the further nickel-phosphorus coating of the second coating is less than a phosphorus content of the nickel-phosphorus coating of the first coating,
An accessory (300; 400; 500) for use with a hair dryer, comprising: a housing (302; 402; 502) having a first end with an air inlet (302a; 402a; 502a) and a second end with an air outlet (302b; 402b; 502b); and a collar assembly arranged at the first end and selectively matable with a hair dryer, the collar assembly including an outer collar (304; 404; 504); the outer collar (304; 404; 504) is configured to cause an attachment assembly on a hair dryer to move to a first unique structural configuration that corresponds to a first operational setting of the hair dryer when the accessory (300; 400; 500) is attached to the hair dryer, and characterized in that the collar assembly further includes an inner collar (306; 406; 506) configured to align the accessory (300; 400; 500) in at least one predetermined rotational orientation relative to a hair dryer when the accessory (300; 400; 500) is attached to the hair dryer. a housing (302; 402; 502) having a first end with an air inlet (302a; 402a; 502a) and a second end with an air outlet (302b; 402b; 502b); and a collar assembly arranged at the first end and selectively matable with a hair dryer, the collar assembly including an outer collar (304; 404; 504); the outer collar (304; 404; 504) is configured to cause an attachment assembly on a hair dryer to move to a first unique structural configuration that corresponds to a first operational setting of the hair dryer when the accessory (300; 400; 500) is attached to the hair dryer, and characterized in that the collar assembly further includes an inner collar (306; 406; 506) configured to align the accessory (300; 400; 500) in at least one predetermined rotational orientation relative to a hair dryer when the accessory (300; 400; 500) is attached to the hair dryer.
An article of footwear having an upper and a sole structure secured to the upper, the upper incorporating a knitted component, the knitted component comprising: a first course extending from a first area of the knitted component to a second area of the knitted component along a first knitting direction, the first course including a first loop and a second loop, the first loop and the second loop being separated by a plurality of loops, and a second course extending from the first area to the second area, the second course including a first tuck stitch and a second tuck stitch, the first tuck stitch interacting with the first loop, the second tuck stitch interacting with the second loop, the second course including a floated portion extending from the first tuck stitch to the second tuck stitch, the floated portion extending over the plurality of loops of the first course; wherein the second course is configured to resist stretch in at least a first portion of the upper, the second course further including a third tuck stitch, the third tuck stitch interacting with one of the plurality of loops, the article of footwear being characterized in that the second course includes a plurality of loops between the second tuck stitch and the third tuck stitch, the plurality of loops of the second course interacting with the plurality of loops of the first course. a first course extending from a first area of the knitted component to a second area of the knitted component along a first knitting direction, the first course including a first loop and a second loop, the first loop and the second loop being separated by a plurality of loops, and a second course extending from the first area to the second area, the second course including a first tuck stitch and a second tuck stitch, the first tuck stitch interacting with the first loop, the second tuck stitch interacting with the second loop, the second course including a floated portion extending from the first tuck stitch to the second tuck stitch, the floated portion extending over the plurality of loops of the first course; wherein the second course is configured to resist stretch in at least a first portion of the upper, the second course further including a third tuck stitch, the third tuck stitch interacting with one of the plurality of loops, the article of footwear being characterized in that the second course includes a plurality of loops between the second tuck stitch and the third tuck stitch, the plurality of loops of the second course interacting with the plurality of loops of the first course.