mhurhangee/ep-ind-claims huggingface dataset:
A suture anchor (10; 120; 200) configured for anchoring a suture in bone, comprising: a one-piece blank (12; 122; 202) formed of a sheet material folded to form a body (14; 123; 203) having a proximal end (26; 126), a distal end (28; 128), a floor (30; 130) positioned at the distal end (28; 128), a first sidewall (32; 132; 210) extending from one end of the floor (30; 130) toward the proximal end (26; 126), a second sidewall (34; 134) extending from an opposite end of the floor (30; 130) toward the proximal end (26; 126), a recess (36; 136) defined by the floor (30; 130), the first sidewall (32; 132), and the second sidewall (34; 134), a transverse edge (38; 138; 204) formed on the first sidewall (32; 132; 210), and a crossbar (40; 140) extending inwardly from the second sidewall (34; 134) across the recess (36; 136) such that a free end (42; 142) of the crossbar (40; 140) is disposed distally of the transverse edge (38; 138; 204) of the body (14; 123; 203), wherein the body (14; 123) further has a first bone engaging portion (48; 148) extending outwardly a distance from the first sidewall (32; 132) and a second bone engaging portion (50; 150) extending outwardly a distance from the second sidewall (34; 134), wherein the crossbar (40; 140) is flexible such that when a distally directed force is applied to the crossbar (40; 140), the free end (42; 142) of the crossbar (40; 140) is positionable in the recess (36; 136) and when a proximally directed force is applied to the crossbar (40; 140), the free end (42; 142) of the crossbar is engageable with the transverse edge (38; 138) to limit proximal motion of the crossbar (40; 140). wherein the body (14; 123) further has a first bone engaging portion (48; 148) extending outwardly a distance from the first sidewall (32; 132) and a second bone engaging portion (50; 150) extending outwardly a distance from the second sidewall (34; 134), wherein the crossbar (40; 140) is flexible such that when a distally directed force is applied to the crossbar (40; 140), the free end (42; 142) of the crossbar (40; 140) is positionable in the recess (36; 136) and when a proximally directed force is applied to the crossbar (40; 140), the free end (42; 142) of the crossbar is engageable with the transverse edge (38; 138) to limit proximal motion of the crossbar (40; 140).
Composition comprising: (i) one or more plant oils, (ii) one or more hydrocarbon-based oils other than the plant oils (i), (iii) one or more glycerolated nonionic surfactants, (iv) one or more polysaccharides, (v) one or more C 1 to C 6 monoalcohols and (vi) water; and the sum of the total content of plant oil(s) (i) and of the total content of hydrocarbon-based oil(s) (ii) being greater than or equal to 5% by weight relative to the total weight of the composition. (i) one or more plant oils, (ii) one or more hydrocarbon-based oils other than the plant oils (i), (iii) one or more glycerolated nonionic surfactants, (iv) one or more polysaccharides, (v) one or more C 1 to C 6 monoalcohols and (vi) water; and
A method comprising: initiating, in a blood collection device, a scrub timer having a scrub time period; during the scrub time period, disinfecting tissue of the patient at a proposed needle entry site; and after the scrub time period has elapsed, stopping disinfecting. initiating, in a blood collection device, a scrub timer having a scrub time period; during the scrub time period, disinfecting tissue of the patient at a proposed needle entry site; and after the scrub time period has elapsed, stopping disinfecting.
A medical device or medical implement with high lubricity to flesh or biological fluid and/or inhibited nucleation on its surface, the device or implement comprising: a surface comprising an impregnating liquid, and a plurality of micro-scale solid features spaced sufficiently close to stably contain the impregnating liquid therebetween, wherein said impregnating liquid fills spaces between said solid features, wherein said surface stably contains said impregnating liquid between said solid features, wherein said impregnating liquid is held in place between said plurality of solid features regardless of orientation of said surface, wherein the solid features comprise particles having an average dimension in a range of 1 micron to 50 microns; and optionally wherein the particles are arranged with average spacing of 1 micron to 30 microns between adjacent particles or clusters of particles. a surface comprising an impregnating liquid, and a plurality of micro-scale solid features spaced sufficiently close to stably contain the impregnating liquid therebetween, wherein said impregnating liquid fills spaces between said solid features, wherein said surface stably contains said impregnating liquid between said solid features, wherein said impregnating liquid is held in place between said plurality of solid features regardless of orientation of said surface, wherein the solid features comprise particles having an average dimension in a range of 1 micron to 50 microns; and optionally wherein the particles are arranged with average spacing of 1 micron to 30 microns between adjacent particles or clusters of particles.
A flapper valve assembly for venting pressure in a tank, the flapper valve assembly comprising: a float assembly configured to be disposed within a valve housing, the float assembly having a plurality of vertical supports (23, 23a), including a guide support, that extend from an end portion of the float assembly; and a flapper member movably supported on the float assembly, wherein the flapper member includes a plurality of guide legs and alignment legs that correspond with the vertical supports (23, 23a) of the float assembly to maintain proper alignment of the flapper member relative to the float assembly, wherein the float assembly further includes a guide ring that forms a cage including the vertical supports (23, 23a) of the float assembly to restrict a range of motion of the flapper member, and at least one alignment leg abuts against vertical supports of the float assembly to restrict rotational movement of the flapper member relative to the float assembly, characterized in that a pair of the guide legs of the flapper member define hook portions that extend along opposite sides of at least one guide support of the float assembly. a float assembly configured to be disposed within a valve housing, the float assembly having a plurality of vertical supports (23, 23a), including a guide support, that extend from an end portion of the float assembly; and a flapper member movably supported on the float assembly, wherein the flapper member includes a plurality of guide legs and alignment legs that correspond with the vertical supports (23, 23a) of the float assembly to maintain proper alignment of the flapper member relative to the float assembly, wherein the float assembly further includes a guide ring that forms a cage including the vertical supports (23, 23a) of the float assembly to restrict a range of motion of the flapper member, and at least one alignment leg abuts against vertical supports of the float assembly to restrict rotational movement of the flapper member relative to the float assembly, characterized in that a pair of the guide legs of the flapper member define hook portions that extend along opposite sides of at least one guide support of the float assembly.
A light source device comprising: a first light emitting unit including a light emitting element that emits light having a predetermined wavelength range; a second light emitting unit (5, 23) including a wavelength conversion member (5b, 23a) that receives the light from the light emitting element and emits light having a different wavelength range different than the predetermined wavelength range; an optical unit configured to define a path of the light emitted from the light emitting element and a path of the light emitted from the wavelength conversion member (5b, 23a); an air blowing unit configured to generate a cooling air; and a passage forming member (20a, 20b, 20c) configured to form a passage through which the cooling air flows, the passage being in contact with both of the first light emitting unit and the second light emitting unit (5, 23); wherein the first light emitting unit includes: a light emitting element heat dissipation member disposed inside the passage and to dissipate heat of the light emitting element; characterised in that the passage forming member (20a, 20b, 20c) forms the passage so as to allow the cooling air flow through the passage from the first light emitting unit toward the second light emitting unit (5, 23). a first light emitting unit including a light emitting element that emits light having a predetermined wavelength range; a second light emitting unit (5, 23) including a wavelength conversion member (5b, 23a) that receives the light from the light emitting element and emits light having a different wavelength range different than the predetermined wavelength range; an optical unit configured to define a path of the light emitted from the light emitting element and a path of the light emitted from the wavelength conversion member (5b, 23a); an air blowing unit configured to generate a cooling air; and a passage forming member (20a, 20b, 20c) configured to form a passage through which the cooling air flows, the passage being in contact with both of the first light emitting unit and the second light emitting unit (5, 23); wherein the first light emitting unit includes: a light emitting element heat dissipation member disposed inside the passage and to dissipate heat of the light emitting element; characterised in that the passage forming member (20a, 20b, 20c) forms the passage so as to allow the cooling air flow through the passage from the first light emitting unit toward the second light emitting unit (5, 23). a light emitting element heat dissipation member disposed inside the passage and to dissipate heat of the light emitting element; characterised in that the passage forming member (20a, 20b, 20c) forms the passage so as to allow the cooling air flow through the passage from the first light emitting unit toward the second light emitting unit (5, 23).
Compressor assembly for a compressed-air feed of a compressed-air supply system for operating a pneumatic system, having: - a compressor (100, 101, 102, 103) having at least one con-rod (140, 141, 142), a con-rod bearing, and a cylinder (170, 171), wherein the con-rod has a compressor piston (150, 150A, 150B, 151), - a drive having a drive shaft, a drive housing, wherein the drive shaft is mounted in at least one drive bearing that is disposed within the drive housing, characterized in that - the drive bearing and the con-rod bearing partially or completely overlap one another in the axial direction, or the axial central plane of the drive bearing and the axial central plane of the con-rod bearing lie in one bearing plane, and wherein - a crank disk is fixedly connected to an end portion of the drive shaft, and furthermore the crank disk on a con-rod receptacle portion that is disposed so as to be eccentric to the drive shaft is rotatably connected to the con-rod by way of the con-rod bearing. - a compressor (100, 101, 102, 103) having at least one con-rod (140, 141, 142), a con-rod bearing, and a cylinder (170, 171), wherein the con-rod has a compressor piston (150, 150A, 150B, 151), - a drive having a drive shaft, a drive housing, wherein the drive shaft is mounted in at least one drive bearing that is disposed within the drive housing, - the drive bearing and the con-rod bearing partially or completely overlap one another in the axial direction, or the axial central plane of the drive bearing and the axial central plane of the con-rod bearing lie in one bearing plane, and wherein - a crank disk is fixedly connected to an end portion of the drive shaft, and furthermore the crank disk on a con-rod receptacle portion that is disposed so as to be eccentric to the drive shaft is rotatably connected to the con-rod by way of the con-rod bearing.
Rod belt for rod belt conveyors of agricultural machines with rods arranged transverse to the direction of movement and parallel to one another, wherein the rods have flattened and perforated fastening regions (5.1), with which they rest on tensile elastic belts circulating parallel to one another and are connected to the belts by rivets or similar fastening means, which pass through the fastening region (5.1) and the belts, both ends of which form a joint, characterised in that an auxiliary belt section is arranged in each case laterally adjoining the belts, said auxiliary belt section spans the joint between the belt ends, wherein the belts and the auxiliary belt sections are interlocked with one another by means of the rods.
Method for the manufacture of a welding stud comprising the steps of: - providing a welding part adapted to be welded to a workpiece, the welding part comprising a recess, the welding part being in a first material, wherein the first material is a lightweight material, wherein the recess has a first recess dimension; - providing a shaft extending along a longitudinal axis between a first end portion and a second end portion, wherein the shaft is in a second material, different from the first material, wherein the first end portion has an end portion dimension, - heating the welding part such that the area surrounding the recess is dilated and the first recess dimension is increased or cooling the shaft such that the first end portion is retracted; - fitting the first end portion in the recess; - shrinking the welding part around the first end portion in order to connect the welding part with the shaft. - providing a welding part adapted to be welded to a workpiece, the welding part comprising a recess, the welding part being in a first material, wherein the first material is a lightweight material, wherein the recess has a first recess dimension; - providing a shaft extending along a longitudinal axis between a first end portion and a second end portion, wherein the shaft is in a second material, different from the first material, wherein the first end portion has an end portion dimension, - heating the welding part such that the area surrounding the recess is dilated and the first recess dimension is increased or cooling the shaft such that the first end portion is retracted; - fitting the first end portion in the recess; - shrinking the welding part around the first end portion in order to connect the welding part with the shaft.
A male element for a box-making machine, comprising a central core, being also provided with: - two back plates (2, 2') having through holes (2a, 2a') and arranged on two opposite sides of the central core; - two pressure means (8, 8'; 18, 18'); - a rotating shaft for adjusting the position of the two pressure means (8, 8'; 18, 18') wherein said shaft passes through the through holes of the back plates (2, 2'), said rotating shaft also having two ends (4, 4') threaded in opposite directions; - two sliding parts (6, 6'), each of said sliding parts (6, 6') being joined to one of the threaded ends (4, 4') of the shaft; - two pressure means (8, 8'; 18, 18'), each of said pressure means (8, 8'; 18, 18') being solidly connected to one of the sliding parts (6, 6'), characterized in that - runners (5a, 5b; 5a', 5b') are arranged on both sides of each of the sliding parts (6, 6'); and in that - each of the sliding parts (6, 6') comprises an upper element (6a; 6a') and a lower element (6b, 6b'), the upper elements (6a; 6a') of the sliding parts (6, 6') being guided by longitudinal grooves (5c, 5d) provided in runners (5a, 5b; 5a', 5b'). - two back plates (2, 2') having through holes (2a, 2a') and arranged on two opposite sides of the central core; - two pressure means (8, 8'; 18, 18'); - a rotating shaft for adjusting the position of the two pressure means (8, 8'; 18, 18') wherein said shaft passes through the through holes of the back plates (2, 2'), said rotating shaft also having two ends (4, 4') threaded in opposite directions; - two sliding parts (6, 6'), each of said sliding parts (6, 6') being joined to one of the threaded ends (4, 4') of the shaft; - two pressure means (8, 8'; 18, 18'), each of said pressure means (8, 8'; 18, 18') being solidly connected to one of the sliding parts (6, 6'), characterized in that - runners (5a, 5b; 5a', 5b') are arranged on both sides of each of the sliding parts (6, 6'); and in that - each of the sliding parts (6, 6') comprises an upper element (6a; 6a') and a lower element (6b, 6b'), the upper elements (6a; 6a') of the sliding parts (6, 6') being guided by longitudinal grooves (5c, 5d) provided in runners (5a, 5b; 5a', 5b'). - each of the sliding parts (6, 6') comprises an upper element (6a; 6a') and a lower element (6b, 6b'), the upper elements (6a; 6a') of the sliding parts (6, 6') being guided by longitudinal grooves (5c, 5d) provided in runners (5a, 5b; 5a', 5b').
A revolvable active diffuser for vehicle, comprising a diffuser bracket immovably fixed relative to a vehicle body, an electrical motor fixed on the diffuser bracket and a driving rod driven by the electrical motor to rotate, the diffuser further comprises a diffuser inner plate mounted on the diffuser bracket, a middle part of the diffuser inner plate being connected to the driving rod by means of a connecting rod, wherein under the driving of the electrical motor, the diffuser inner plate performs rotation movement relative to the diffuser bracket, so as to form an airflow channel for air to flow between the diffuser inner plate and the diffuser bracket, wherein the diffuser inner plate comprises a baseplate extending horizontally and a flap extending at an angle to the baseplate, wherein an edge of the diffuser inner plate is fixed to the diffuser bracket by means of a plurality of fixing shafts and bearing blocks, and the diffuser inner plate takes the fixing shafts as its rotation axis, and wherein the bearing blocks are independently formed with the diffuser bracket.
A system for assessing health of an aircraft, comprising: a receiver operable to receive, from an aircraft, a plurality of measurements associated with two or more flight parameters (300x, 300y, 300z, 400x, 400y, P1-P4), the plurality of measurements comprising measurements spanning at least one period of time; a flight spectrum analyzer operable to determine, based on a comparison of the plurality of measurements to a plurality of flight spectrum definitions, each flight spectrum containing zero, one or multiple flight modes, an amount of time the aircraft spent in each flight spectrum of a plurality of flight spectrums (400s-455s) during the at least one period of time; and a health assessment analyzer operable to assess a change in health of the aircraft over the at least one period of time based on the determination of the amount of time the aircraft spent in each flight spectrum and a plurality of spectrum health profiles, each spectrum health profile defining how operating within a corresponding flight spectrum affects the health of the aircraft. a receiver operable to receive, from an aircraft, a plurality of measurements associated with two or more flight parameters (300x, 300y, 300z, 400x, 400y, P1-P4), the plurality of measurements comprising measurements spanning at least one period of time; a flight spectrum analyzer operable to determine, based on a comparison of the plurality of measurements to a plurality of flight spectrum definitions, each flight spectrum containing zero, one or multiple flight modes, an amount of time the aircraft spent in each flight spectrum of a plurality of flight spectrums (400s-455s) during the at least one period of time; and a health assessment analyzer operable to assess a change in health of the aircraft over the at least one period of time based on the determination of the amount of time the aircraft spent in each flight spectrum and a plurality of spectrum health profiles, each spectrum health profile defining how operating within a corresponding flight spectrum affects the health of the aircraft.
Household appliance device, in particular beverage machine device, with an oscillating armature pump (20a; 20b; 20c) comprising a pump chamber, and with at least one flow-through limiter unit (24a; 24b; 24c) which is arranged fluidically at least substantially upstream of the pump chamber, wherein the flow-through limiter unit (24a; 24b; 24c) is configured to achieve, at least in an essential work region, an at least substantially constant output volume flow, characterised in that the oscillating armature pump (20a; 20b; 20c) is designed for a back pressure of at least substantially 4 bar and the flow-through limiter unit (24a; 24b; 24c) has an effective flow-through cross-section of less than 0.95 mm 2, or that the oscillating armature pump (20a; 20b; 20c) is designed for a back pressure of at least substantially 7 bar and the flow-through limiter unit (24a; 24b; 24c) has an effective flow-through cross-section of less than 0.59 mm 2, or that the oscillating armature pump (20a; 20b; 20c) is designed for a back pressure of at least substantially 8 bar and the flow-through limiter unit (24a; 24b; 24c) has an effective flow-through cross-section of less than 0.54 mm 2, or that the oscillating armature pump (20a; 20b; 20c) is designed for a back pressure of at least substantially 12 bar and the flow-through limiter unit (24a; 24b; 24c) has an effective flow-through cross-section of less than 0.40 mm 2. wherein the flow-through limiter unit (24a; 24b; 24c) is configured to achieve, at least in an essential work region, an at least substantially constant output volume flow, characterised in that the oscillating armature pump (20a; 20b; 20c) is designed for a back pressure of at least substantially 4 bar and the flow-through limiter unit (24a; 24b; 24c) has an effective flow-through cross-section of less than 0.95 mm 2, or that the oscillating armature pump (20a; 20b; 20c) is designed for a back pressure of at least substantially 7 bar and the flow-through limiter unit (24a; 24b; 24c) has an effective flow-through cross-section of less than 0.59 mm 2, or that the oscillating armature pump (20a; 20b; 20c) is designed for a back pressure of at least substantially 8 bar and the flow-through limiter unit (24a; 24b; 24c) has an effective flow-through cross-section of less than 0.54 mm 2, or that the oscillating armature pump (20a; 20b; 20c) is designed for a back pressure of at least substantially 12 bar and the flow-through limiter unit (24a; 24b; 24c) has an effective flow-through cross-section of less than 0.40 mm 2.