mhurhangee/patent-ind-claim-en huggingface dataset:
Suture anchor , for anchoring soft tissue to a bone , said suture anchor comprising a first element having along a longitudinal axis (X) a first distal end and a first proximal end opposite each other, said first element having successively, from the first distal end to the first proximal end , a distal insertion section , a central anchoring section and a proximal coupling section , where the central anchoring section has externally and along the longitudinal axis (X) a succession of peripheral anchoring notches , wherein at least one longitudinal groove extends along the longitudinal axis (X) and is arranged through and along the succession of peripheral anchoring notches , and wherein a transverse hole is provided in said longitudinal groove and passes through the central anchoring section to form an eye for the passage of a suture thread (3; 4), and wherein a first longitudinal orifice is provided internally in the proximal coupling section and in the central anchoring section along the longitudinal axis (X), said first longitudinal orifice opening onto the first proximal end and opening onto the transverse hole ; said suture anchor further comprising a second element independent of the first element , said second element having a second proximal end and a second distal end opposite each other, wherein the second element has externally at least one anchoring relief , and wherein a second longitudinal orifice is arranged internally in the second element and opens onto the second proximal end and onto the second distal end , said second longitudinal orifice being shaped to be able to engage the second element on the proximal coupling section of the first element with said proximal coupling section inside said second longitudinal orifice ; said suture anchor being characterized in that a bridge is provided inside the transverse hole to separate two passages offset from each other along the longitudinal axis (X), and in that said first longitudinal orifice opens onto the transverse hole in front of the bridge . said suture anchor further comprising a second element independent of the first element , said second element having a second proximal end and a second distal end opposite each other, wherein the second element has externally at least one anchoring relief , and wherein a second longitudinal orifice is arranged internally in the second element and opens onto the second proximal end and onto the second distal end , said second longitudinal orifice being shaped to be able to engage the second element on the proximal coupling section of the first element with said proximal coupling section inside said second longitudinal orifice ; said suture anchor being characterized in that a bridge is provided inside the transverse hole to separate two passages offset from each other along the longitudinal axis (X), and in that said first longitudinal orifice opens onto the transverse hole in front of the bridge .
A backplate assembly for a door fitting comprising: a first pair of holes , wherein the first pair of holes is formed by a first slot hole and a first screw hole , wherein the first slot hole extends along a longitudinal median plane of the backplate assembly and wherein the first screw hole is located on the longitudinal median plane , a second pair of holes , wherein the second pair of holes is formed by a second screw hole and a third screw hole , wherein the second screw hole and the third screw hole are opposite each other with respect to the longitudinal median plane , a third pair of holes , wherein the third pair of holes is formed by a fourth screw hole and a fifth screw hole , wherein the fourth screw hole and the fifth screw hole are positioned on the longitudinal median plane and between the first screw hole and the first slot hole , a fourth pair of holes , wherein the fourth pair of holes is formed by a sixth screw hole and a seventh screw hole , wherein the sixth screw hole and the seventh screw hole are opposite each other with respect to the longitudinal median plane , and wherein a distance between the sixth screw hole and the seventh screw hole is smaller than a distance between the second screw hole and the third screw hole , a second slot hole , which extends along the longitudinal median plane of the backplate assembly and is located on a side of the first slot hole opposite the first screw hole . a first pair of holes , wherein the first pair of holes is formed by a first slot hole and a first screw hole , wherein the first slot hole extends along a longitudinal median plane of the backplate assembly and wherein the first screw hole is located on the longitudinal median plane , a second pair of holes , wherein the second pair of holes is formed by a second screw hole and a third screw hole , wherein the second screw hole and the third screw hole are opposite each other with respect to the longitudinal median plane , a third pair of holes , wherein the third pair of holes is formed by a fourth screw hole and a fifth screw hole , wherein the fourth screw hole and the fifth screw hole are positioned on the longitudinal median plane and between the first screw hole and the first slot hole , a fourth pair of holes , wherein the fourth pair of holes is formed by a sixth screw hole and a seventh screw hole , wherein the sixth screw hole and the seventh screw hole are opposite each other with respect to the longitudinal median plane , and wherein a distance between the sixth screw hole and the seventh screw hole is smaller than a distance between the second screw hole and the third screw hole , a second slot hole , which extends along the longitudinal median plane of the backplate assembly and is located on a side of the first slot hole opposite the first screw hole .
An electronic musical instrument , comprising: an input unit , which inputs a sound instruction of a plurality of tones; a detection unit , which has a detection surface comprising a position sensor configured to detect detection positions on the detection surface ; a musical sound control unit , which applies a musical sound effect to each of the plurality of tones based on the sound instruction input by the input unit and outputs the tones; a musical sound effect change unit , which changes, for each tone, a degree of the musical sound effect applied to each tone by the musical sound control unit corresponding to the detection positions detected by the detection unit ; and an operator which is arranged near the detection unit and inputs an operation of a performer (H), wherein the musical sound effect change unit changes the degrees of the musical sound effects applied to the plurality of tones output by the musical sound control unit corresponding to an operation amount of the operator and the detection result of the detection unit , characterized in that the operator is arranged along a longitudinal side of the detection unit , and the operation amount of the operator is output by operating to recline the operator toward an opposite side of the detection unit . an input unit , which inputs a sound instruction of a plurality of tones; a detection unit , which has a detection surface comprising a position sensor configured to detect detection positions on the detection surface ; a musical sound control unit , which applies a musical sound effect to each of the plurality of tones based on the sound instruction input by the input unit and outputs the tones; a musical sound effect change unit , which changes, for each tone, a degree of the musical sound effect applied to each tone by the musical sound control unit corresponding to the detection positions detected by the detection unit ; and an operator which is arranged near the detection unit and inputs an operation of a performer (H), wherein the musical sound effect change unit changes the degrees of the musical sound effects applied to the plurality of tones output by the musical sound control unit corresponding to an operation amount of the operator and the detection result of the detection unit , characterized in that the operator is arranged along a longitudinal side of the detection unit , and the operation amount of the operator is output by operating to recline the operator toward an opposite side of the detection unit .
A chassis for a roll container , the chassis comprising: - a first arm , - a second arm , and - a crossmember configured to connect the first arm to the second arm so as to form a chassis , wherein the crossmember is configured to be repeatedly attached to and detached from the first and second arm , characterized in that the crossmember is formed to be less resistant to mechanical strain than the first and second arm - a first arm , - a second arm , and - a crossmember configured to connect the first arm to the second arm so as to form a chassis , wherein the crossmember is configured to be repeatedly attached to and detached from the first and second arm ,
An anti-collision radar for a taxiing aircraft, characterized in that , being able to be attached laterally to the body of an aircraft and to detect obstacles on a collision course with a portion of the aircraft facing said radar , it includes at least one emission antennal channel emitting a wave of the FMCW type and a plurality of reception antennal channels placed in the same plane, the form (FO 0 , FO 1 , FO 2 and FO 3 ) of said wave and the field of angular coverage of said radar depending on the velocity of the aircraft, the processing means of said radar carrying out at least the following steps: - establishing , in the coordinate system of the radar , a first distance/Doppler map allowing echoes to be separated into distance and Doppler resolution cells in said plurality of reception antennal channels; - establishing a second distance/Doppler map smaller than the first map by selecting from the latter a subset of distance and Doppler resolution cells that corresponds to the possible positions of targets liable to collide with said portion of the aircraft, said selection depending on the velocity of the aircraft; - Establishing new distance/Doppler maps by forming beams computationally from the subsets of those distance resolution cells that are retained for each reception antennal channel, so as to separate the beam of angular observation in the plane of the antennal channels into at least two beams in conformity with the principle of lobe sharpening by Doppler filtering in unfocused synthetic antenna processing; - temporally integrating , in each formed beam, a plurality of successive distance/Doppler maps obtained in the preceding step in order to obtain a final distance/Doppler map for each beam, the integration duration depending on the waveform used; these steps being followed by at least one detection step in each of the beams formed on the basis of said final distance/Doppler map . - establishing , in the coordinate system of the radar , a first distance/Doppler map allowing echoes to be separated into distance and Doppler resolution cells in said plurality of reception antennal channels; - establishing a second distance/Doppler map smaller than the first map by selecting from the latter a subset of distance and Doppler resolution cells that corresponds to the possible positions of targets liable to collide with said portion of the aircraft, said selection depending on the velocity of the aircraft; - Establishing new distance/Doppler maps by forming beams computationally from the subsets of those distance resolution cells that are retained for each reception antennal channel, so as to separate the beam of angular observation in the plane of the antennal channels into at least two beams in conformity with the principle of lobe sharpening by Doppler filtering in unfocused synthetic antenna processing; - temporally integrating , in each formed beam, a plurality of successive distance/Doppler maps obtained in the preceding step in order to obtain a final distance/Doppler map for each beam, the integration duration depending on the waveform used;
A rotor blade of a wind energy installation, the rotor blade having a longitudinal extent which extends from a rotor blade root to a rotor blade tip , wherein the rotor blade has a cross-sectional profile which is variable in the longitudinal direction and which has a profile leading edge and a profile trailing edge which are connected to one another via a suction side and a pressure side of the cross-sectional profile , wherein, in a region close to the rotor blade root, the rotor blade has a round or an oval profile which, in the direction towards the rotor blade tip , initially changes, in a transition region , into a blunt aerodynamic cross-sectional profile with a blunt trailing edge and, further in the direction towards the rotor blade tip , subsequently changes into an aerodynamic solid profile , in which the profiles on the suction side and on the pressure side meet at an acute angle at the trailing edge , characterised in that , in at least some portions of the cylindrical or oval region close to the blade root, a stall induction device which extends substantially in the longitudinal direction of the rotor blade is arranged on the pressure side of the rotor blade , which stall induction device is continued, at least in some portions of the transition region , at or in the region of the blunt trailing edge of the pressure side of the blunt aerodynamic cross-sectional profile , wherein the stall induction device is constructed in the shape of an "L"; and wherein, in the transition region , at least one series of vortex generators and / or vortex edges are arranged on the suction side of the rotor blade .
A propeller comprising: a hub ; a first blade group having a plurality of first propeller blades , each of the first propeller blades of the first blade group being substantially identical; a second blade group having a plurality of second propeller blades , each of the second propeller blades of the second blade group being substantially identical; and a third blade group having a plurality of third propeller blades , each of the third propeller blades of the third blade group being substantially identical, the propeller blades of each group being mounted to and equidistantly spaced about the hub , wherein the first propeller blades of the first blade group have at least one geometric characteristic different from the second propeller blades of the second blade group , wherein the geometric characteristic is one of chord and twist, and the propeller blades of each group have a first end mounted to the hub , and extend radially outward from the hub such that a second end of each blade is arranged within a plane (B) orientated perpendicularly to an axis of rotation of the hub ; wherein at least one geometric characteristic of the first propeller blades of the first blade group is different from the third propeller blades of the third blade group ; and characterised in that at least one geometric characteristic of the second propeller blades of the second blade group is different from the third propeller blades of the third blade group . a hub ; a first blade group having a plurality of first propeller blades , each of the first propeller blades of the first blade group being substantially identical; a second blade group having a plurality of second propeller blades , each of the second propeller blades of the second blade group being substantially identical; and a third blade group having a plurality of third propeller blades , each of the third propeller blades of the third blade group being substantially identical, the propeller blades of each group being mounted to and equidistantly spaced about the hub , wherein the first propeller blades of the first blade group have at least one geometric characteristic different from the second propeller blades of the second blade group , wherein the geometric characteristic is one of chord and twist, and the propeller blades of each group have a first end mounted to the hub , and extend radially outward from the hub such that a second end of each blade is arranged within a plane (B) orientated perpendicularly to an axis of rotation of the hub ; wherein at least one geometric characteristic of the first propeller blades of the first blade group is different from the third propeller blades of the third blade group ; and characterised in that at least one geometric characteristic of the second propeller blades of the second blade group is different from the third propeller blades of the third blade group .
A pellicle comprising: a supporting member with a ring-like and planar shape and containing Si, and a pellicle film formed on one principal surface of the supporting member , wherein the pellicle film is composed of a SiC film having a thickness of 10 nanometers or more and 100 nanometers or less, and the SiC film includes a first SiC film formed on the one principal surface of the supporting member and having a first average carbon concentration, and a second SiC film formed on one principal surface of the first SiC film and having a second average carbon concentration different from the first average carbon concentration. a supporting member with a ring-like and planar shape and containing Si, and a pellicle film formed on one principal surface of the supporting member , wherein the pellicle film is composed of a SiC film having a thickness of 10 nanometers or more and 100 nanometers or less, and the SiC film includes a first SiC film formed on the one principal surface of the supporting member and having a first average carbon concentration, and a second SiC film formed on one principal surface of the first SiC film and having a second average carbon concentration different from the first average carbon concentration. a first SiC film formed on the one principal surface of the supporting member and having a first average carbon concentration, and a second SiC film formed on one principal surface of the first SiC film and having a second average carbon concentration different from the first average carbon concentration.
A method for manufacturing a cured photocurable resin composition, characterized by : applying infrared ray irradiation having a wavelength range between 1 and 6 microns to a photocurable resin composition including at least one photo polymerization initiator, from which volatile components have been removed by a heating process in advance, before the application of ultraviolet ray irradiation in order to increase a decomposition efficiency of said at least one photo polymerization initiator; and then applying the ultraviolet ray irradiation to the photocurable resin composition for a predetermined period of time shorter than a predetermined irradiation time which would be necessary for the same photocurable resin composition to reach a predetermined degree of curing by the ultraviolet ray irradiation without applying the infrared ray irradiation, thereby producing a degree of curing equal to or above the predetermined degree of curing. applying infrared ray irradiation having a wavelength range between 1 and 6 microns to a photocurable resin composition including at least one photo polymerization initiator, from which volatile components have been removed by a heating process in advance, before the application of ultraviolet ray irradiation in order to increase a decomposition efficiency of said at least one photo polymerization initiator; and then applying the ultraviolet ray irradiation to the photocurable resin composition for a predetermined period of time shorter than a predetermined irradiation time which would be necessary for the same photocurable resin composition to reach a predetermined degree of curing by the ultraviolet ray irradiation without applying the infrared ray irradiation, thereby producing a degree of curing equal to or above the predetermined degree of curing.
A door for a washing machine , comprising a first component and a second component pressed against each other and non-fixedly engaged with each other, wherein the first component has a first surface , the second component has a second surface , the first surface and the second surface are in contact and constitute a friction pair, characterized in that one of the first surface and the second surface has a lower surface roughness, and the other one has a higher surface roughness, wherein the surface having the higher surface roughness is an etched surface and patterns on the etched surface are uniformly distributed.
An article, comprising: a thin film interference pigment; and a coating including a selectively absorbing nanoparticle on the thin film interference pigment; wherein the selectively absorbing nanoparticle is a nanoparticle chosen from a pigment, a dye, a metallic nanoparticle, a metal oxide, a metal carbide, a metal sulfide, a metal nitride, and combinations thereof. a thin film interference pigment; and a coating including a selectively absorbing nanoparticle on the thin film interference pigment; wherein the selectively absorbing nanoparticle is a nanoparticle chosen from a pigment, a dye, a metallic nanoparticle, a metal oxide, a metal carbide, a metal sulfide, a metal nitride, and combinations thereof.
A semi-solid or solid pharmaceutical composition comprising a basic drug compound, Vitamin E TPGS and a physiologically tolerable water-soluble acid characterized in that the acid:drug compound ratio is at least 1:1 by weight; wherein the basic drug compound is 4-[[4-[[4-(2-cyanoethenyl)-2,6-dimethylphenyl]amino]-2-pyrimidinyl]amino]-benzonitrile, 4-[[2-[(cyanophenyl)amino]-4-pyrimidinyl]amino]-3,5-dimethylbenzonitrile, 4-[[4-[(2,4,6-trimethylphenyl)amino]-2-pyrimidinyl]amino]benzonitrile, 4-[[6-amino-5-bromo-2-[(4-cyanophenyl)amino]-4-pyrimidinyl]oxy]-3,5-dimethylbenzonitrile; a N-oxide, an addition salt, a quaternary amine or a stereochemically isomeric form thereof.