mhurhangee/patent-ind-claim-en huggingface dataset:
Open end spinning device for an open end spinning machine having a drivable spinning rotor , the rotor cup of which is accommodated in a rotor housing , having a drive for the spinning rotor , which is arranged in a drive housing , and having at least one accommodation for a cover element , which closes the rotor housing during the spinning operation, wherein the open end spinning device has a stop for the cover element for positioning the cover element in the axial direction of the spinning rotor , wherein the stop is of adjustable design, characterized in that the rotor housing has the stop for the cover element .
A composition comprising - water; and - at least one water-soluble polyalkylene glycol of the formula (I) wherein independently of each other - R 1 is -(C 3 H 6 O) x1 -(C 2 H 4 O) y1 -(C 3 H 6 O) z1 -H; - R 2 is -(C 3 H 6 O) x2 -(C 2 H 4 O) y2 -(C 3 H 6 O) z2 -H; and - R 3 is -(C 3 H 6 O) x3 -(C 2 H 4 O) y3 -(C 3 H 6 O) z3 -H; and - x1, x2 and x3 are independently of each other a number of 0 to 6; - y1, y2 and y3 are independently of each other a number of 0 to 40; and - z1, z2 and z3 are independently of each other a number of 0 to 32; and - x1+x2+x3 has an average value of from 1 to 4; - y1+y2+y3 has an average value of from 2 to 30; and - z1+z2+z3 has an average value of from 1 to 25. - water; and - at least one water-soluble polyalkylene glycol of the formula (I) wherein independently of each other - R 1 is -(C 3 H 6 O) x1 -(C 2 H 4 O) y1 -(C 3 H 6 O) z1 -H; - R 2 is -(C 3 H 6 O) x2 -(C 2 H 4 O) y2 -(C 3 H 6 O) z2 -H; and - R 3 is -(C 3 H 6 O) x3 -(C 2 H 4 O) y3 -(C 3 H 6 O) z3 -H; and - x1, x2 and x3 are independently of each other a number of 0 to 6; - y1, y2 and y3 are independently of each other a number of 0 to 40; and - z1, z2 and z3 are independently of each other a number of 0 to 32; and - x1+x2+x3 has an average value of from 1 to 4; - y1+y2+y3 has an average value of from 2 to 30; and - z1+z2+z3 has an average value of from 1 to 25. - R 1 is -(C 3 H 6 O) x1 -(C 2 H 4 O) y1 -(C 3 H 6 O) z1 -H; - R 2 is -(C 3 H 6 O) x2 -(C 2 H 4 O) y2 -(C 3 H 6 O) z2 -H; and - R 3 is -(C 3 H 6 O) x3 -(C 2 H 4 O) y3 -(C 3 H 6 O) z3 -H; and - x1, x2 and x3 are independently of each other a number of 0 to 6; - y1, y2 and y3 are independently of each other a number of 0 to 40; and - z1, z2 and z3 are independently of each other a number of 0 to 32; and - x1+x2+x3 has an average value of from 1 to 4; - y1+y2+y3 has an average value of from 2 to 30; and - z1+z2+z3 has an average value of from 1 to 25.
A column-ceiling node for a reinforced concrete ceiling and two prefabricated concrete columns in storey construction, wherein the upper end of the lower concrete column and/or the lower end of the upper concrete column are arranged adjacent to the reinforced concrete ceiling , the column axes of the concrete columns extending essentially along a common straight line, characterized in that - the cross-section in the region of the upper end of the lower concrete column is larger than a cross-section of the middle half of the longitudinal extension of the lower concrete column ; and that - the-cross section in the region of the lower end of the upper concrete column is larger than a cross-section of the middle half of the longitudinal extension of the upper concrete column . - the cross-section in the region of the upper end of the lower concrete column is larger than a cross-section of the middle half of the longitudinal extension of the lower concrete column ; and that - the-cross section in the region of the lower end of the upper concrete column is larger than a cross-section of the middle half of the longitudinal extension of the upper concrete column .
A spacecraft (200; 300; 400; 500) comprising: a spacecraft main body, including payload equipment disposed on an inner panel surface of at least one radiator panel (211; 311; 411; 511), the at least one radiator panel having an exterior-facing outer panel surface; and at least one electric thruster (223; 323; 423; 523) coupled to an aft facing panel of the spacecraft main body; wherein the at least one electric thruster is thermally coupled with the at least one radiator panel by way of a thermally conductive path that includes one or more heat pipes (230; 330; 430; 530) wherein at least a portion of the one or more heat pipes (230; 330; 430; 530) is disposed on or embedded in the aft facing panel of the spacecraft main body. a spacecraft main body, including payload equipment disposed on an inner panel surface of at least one radiator panel (211; 311; 411; 511), the at least one radiator panel having an exterior-facing outer panel surface; and at least one electric thruster (223; 323; 423; 523) coupled to an aft facing panel of the spacecraft main body; wherein the at least one electric thruster is thermally coupled with the at least one radiator panel by way of a thermally conductive path that includes one or more heat pipes (230; 330; 430; 530) wherein at least a portion of the one or more heat pipes (230; 330; 430; 530) is disposed on or embedded in the aft facing panel of the spacecraft main body.
A drive device for an adjustment installation for adjusting a vehicle part, in particular a power window actuator, having - a carrier element ; - a cable drum ; and - a cable exit housing which is disposable on the carrier element and which mounts the cable drum so as to be rotatable about a rotation axis (D) and which by way of at least one housing portion is attachable to the carrier element ; - a motor unit for electromotively driving the cable drum , and - a drive housing which is disposed on a side of the carrier element that faces away from the cable drum housing and which mounts a drive wheel that in terms of gearing is connected to the motor unit , characterized in that the carrier element has a contact structure having a plurality of elevations and depressions that are successively lined up and are mutually disposed in an alternating manner, the at least one housing portion of the cable exit housing by way of a base portion being attachable to the contact structure , wherein the contact structure extends annularly about the rotation axis (D), and the elevations and depressions are successively lined up in an alternating circumferential manner about the rotation axis (D). - a carrier element ; - a cable drum ; and - a cable exit housing which is disposable on the carrier element and which mounts the cable drum so as to be rotatable about a rotation axis (D) and which by way of at least one housing portion is attachable to the carrier element ; - a motor unit for electromotively driving the cable drum , and - a drive housing which is disposed on a side of the carrier element that faces away from the cable drum housing and which mounts a drive wheel that in terms of gearing is connected to the motor unit ,
A spray gun, comprising: a spray gun main body , having an air intake passage , a first air outlet passage , a second air outlet passage , and a mounting hole defined therein, the mounting hole being in communication with the air intake passage , the first air outlet passage and the second air outlet passage ; and an adjustment valve , mounted to the spray gun main body and located in the mounting hole , the adjustment valve including a first operating member and a second operating member , the first operating member being movable relative to the spray gun main body for adjusting an outflow passing through the air intake passage and the first air outlet passage , the second operating member being movably mounted on the first operating member and corresponding to the second air outlet passage for adjusting an outflow passing through the second air outlet passage wherein the adjustment valve further comprises a valve seat , characterized in that the valve seat has a pivot trough defined therein, the first operating member comprises a cylinder , and the cylinder is pivotally connected to the pivot trough of the valve seat , and in that the valve seat has a first opening and a second opening which are in communication with the pivot trough , the first opening and the second opening are in communication with the air intake passage and the first air outlet passage respectively, the cylinder of the first operating member has at least one perforation , and the perforation is staggered or communicated with the first opening or the second opening by turning the cylinder . a spray gun main body , having an air intake passage , a first air outlet passage , a second air outlet passage , and a mounting hole defined therein, the mounting hole being in communication with the air intake passage , the first air outlet passage and the second air outlet passage ; and an adjustment valve , mounted to the spray gun main body and located in the mounting hole , the adjustment valve including a first operating member and a second operating member , the first operating member being movable relative to the spray gun main body for adjusting an outflow passing through the air intake passage and the first air outlet passage , the second operating member being movably mounted on the first operating member and corresponding to the second air outlet passage for adjusting an outflow passing through the second air outlet passage wherein the adjustment valve further comprises a valve seat , characterized in that the valve seat has a pivot trough defined therein, the first operating member comprises a cylinder , and the cylinder is pivotally connected to the pivot trough of the valve seat , and in that the valve seat has a first opening and a second opening which are in communication with the pivot trough , the first opening and the second opening are in communication with the air intake passage and the first air outlet passage respectively, the cylinder of the first operating member has at least one perforation , and the perforation is staggered or communicated with the first opening or the second opening by turning the cylinder .
A method of wireless communication performed by a user equipment, UE, comprising: receiving activation signaling for a configuration of a semi-persistent transmission procedure; activating the semi-persistent transmission procedure based at least in part on receiving the activation signaling; and deactivating the semi-persistent transmission procedure based at least in part on a deactivation time; detecting further transmission activity during the semi-persistent transmission procedure; and extending the semi-persistent transmission procedure based at least in part on detecting the further transmission activity; and characterised wherein deactivating the semi-persistent transmission procedure comprises deactivating the semi-persistent transmission procedure based at least in part on extending the semi-persistent transmission procedure. receiving activation signaling for a configuration of a semi-persistent transmission procedure; activating the semi-persistent transmission procedure based at least in part on receiving the activation signaling; and deactivating the semi-persistent transmission procedure based at least in part on a deactivation time; detecting further transmission activity during the semi-persistent transmission procedure; and extending the semi-persistent transmission procedure based at least in part on detecting the further transmission activity; and characterised wherein deactivating the semi-persistent transmission procedure comprises deactivating the semi-persistent transmission procedure based at least in part on extending the semi-persistent transmission procedure.
A multi-modulation receiver configured to receive a multicarrier signal comprising data transmitted from multiple transmitters, wherein at least one of the transmitters is an Orthogonal Frequency-Division Multiplexing, OFDM, transmitter; wherein at least one of the transmitters is a transmitter using a modulation scheme other than OFDM, and wherein data transmitted from different transmitters are mapped to different subcarriers in the frequency domain, and wherein, in a first transmission mode, said data are mapped targeting the multi-modulation receiver on a subcarrier signal, using a repetition code matching an OFDM symbol duration of the multi-modulation receiver the multi-modulation receiver comprising: - a radio unit configured to receive the multicarrier signal; - a cyclic prefix unit configured to remove a Cyclic Prefix, CP, from the received multicarrier signal; - a Fast Fourier Transform, FFT, unit configured to separate data received from the individual transmitters into mutually orthogonal subcarriers by transforming the multicarrier signal in the time domain to multiple orthogonal subcarrier signals in the frequency domain; - a demapping unit configured to, for each of the multiple transmitters, demap the corresponding subcarrier signals in accordance with the modulation scheme of the respective transmitter. - a radio unit configured to receive the multicarrier signal; - a cyclic prefix unit configured to remove a Cyclic Prefix, CP, from the received multicarrier signal; - a Fast Fourier Transform, FFT, unit configured to separate data received from the individual transmitters into mutually orthogonal subcarriers by transforming the multicarrier signal in the time domain to multiple orthogonal subcarrier signals in the frequency domain; - a demapping unit configured to, for each of the multiple transmitters, demap the corresponding subcarrier signals in accordance with the modulation scheme of the respective transmitter.
A measurement device, comprising: a mark detection system that has an irradiation system , an objective optical system and a beam receiving system , the irradiation system is configured to irradiate a grating mark (GM) provided at an object that is moved in a first direction, with a measurement beam (L1,L2), while scanning the measurement beam (L1,L2) in the first direction with respect to the grating mark (GM), the objective optical system including an objective optical element capable of facing the object that is moved in the first direction, and the beam receiving system is configured to receive a diffraction beam from the grating mark (GM) of the measurement beam (L1,L2) via the objective optical system ; and a calculation system configured to obtain positional information of the grating mark (GM) on the basis of a detection result of the mark detection system, wherein the objective optical element is configured to deflect or diffract the diffraction beam generated at the grating mark (GM) toward the beam receiving system , and wherein the objective optical element has a first area in which an optical path of the measurement beam (L1,L2) from the irradiation system is provided, and a second area in which an optical component to deflect or diffract the diffraction beam is provided. a mark detection system that has an irradiation system , an objective optical system and a beam receiving system , the irradiation system is configured to irradiate a grating mark (GM) provided at an object that is moved in a first direction, with a measurement beam (L1,L2), while scanning the measurement beam (L1,L2) in the first direction with respect to the grating mark (GM), the objective optical system including an objective optical element capable of facing the object that is moved in the first direction, and the beam receiving system is configured to receive a diffraction beam from the grating mark (GM) of the measurement beam (L1,L2) via the objective optical system ; and a calculation system configured to obtain positional information of the grating mark (GM) on the basis of a detection result of the mark detection system, wherein the objective optical element is configured to deflect or diffract the diffraction beam generated at the grating mark (GM) toward the beam receiving system , and wherein the objective optical element has a first area in which an optical path of the measurement beam (L1,L2) from the irradiation system is provided, and a second area in which an optical component to deflect or diffract the diffraction beam is provided.
Compound of the structure ( I ): where R 1 , R 2 are selected from: -H, - (C 1 -C 12 ) -alkyl, -O-(C 1 -C 12 )-alkyl .
A method for producing an amorphous thin film, the method comprising: forming a multilayered metal layer in which a first metal layer, a second metal layer, and a third metal layer are sequentially provided by sequentially depositing a first metal, a second metal, and a third metal on one surface of a first substrate; positioning one surface of a second substrate so as to face the one surface of the first substrate; and forming an amorphous layer comprising the first metal, the second metal, and the third metal on the one surface of the second substrate by irradiating the first substrate with a laser in a direction from the other surface to the one surface of the first substrate wherein the multilayered metal layer has a thickness of 1.5 μm to 3.0 μm, and wherein a difference between the melting point of the first metal layer and the melting point of the second metal layer is 10°C to 100°C, and a difference between the melting point of the second metal layer and the melting point of the third metal layer is 100°C to 450°C. forming a multilayered metal layer in which a first metal layer, a second metal layer, and a third metal layer are sequentially provided by sequentially depositing a first metal, a second metal, and a third metal on one surface of a first substrate; positioning one surface of a second substrate so as to face the one surface of the first substrate; and forming an amorphous layer comprising the first metal, the second metal, and the third metal on the one surface of the second substrate by irradiating the first substrate with a laser in a direction from the other surface to the one surface of the first substrate wherein the multilayered metal layer has a thickness of 1.5 μm to 3.0 μm, and wherein a difference between the melting point of the first metal layer and the melting point of the second metal layer is 10°C to 100°C, and a difference between the melting point of the second metal layer and the melting point of the third metal layer is 100°C to 450°C.
Method for synthesizing 4-hydroxy-3,5-diiodobenzyl alcohol, characterized in that it comprises the synthesis, in just one step, of 4-hydroxy-3,5-diiodo-benzyl alcohol of formula 1 from 4-hydroxybenzylalcohol, in aqueous solution having an initial pH of at least 7, containing at least 2 equivalents of iodizing agent, in particular iodine or diiodide.
A bicycle simulator comprising: only one front roller that supports a front wheel of a bicycle that is mounted, and rotates together with a rotation of the front wheel ; only one rear roller that supports a rear wheel of the bicycle , and rotates together with a rotation of the rear wheel , a base portion to which both ends of the front roller and both ends of the rear roller are connected; and a frame support portion connected to the base portion and arranged between the front roller and the rear roller and supporting a frame of the bicycle , wherein the front wheel is supported by one point by the front roller and the rear wheel is supported by one point by the rear roller , wherein a first support point at which the front roller supports the front wheel and a second support point at which the rear roller supports the rear wheel are arranged on a same plane, and wherein the front roller , the rear roller , and the frame support portion are movably coupled with respect to the base portion in a length direction and in a thickness direction of the base portion . only one front roller that supports a front wheel of a bicycle that is mounted, and rotates together with a rotation of the front wheel ; only one rear roller that supports a rear wheel of the bicycle , and rotates together with a rotation of the rear wheel , a base portion to which both ends of the front roller and both ends of the rear roller are connected; and a frame support portion connected to the base portion and arranged between the front roller and the rear roller and supporting a frame of the bicycle , wherein the front wheel is supported by one point by the front roller and the rear wheel is supported by one point by the rear roller , wherein a first support point at which the front roller supports the front wheel and a second support point at which the rear roller supports the rear wheel are arranged on a same plane, and wherein the front roller , the rear roller , and the frame support portion are movably coupled with respect to the base portion in a length direction and in a thickness direction of the base portion .
A solid bleaching agent-containing material, comprising: a first layer containing one or more halogen bleaching agents selected from the group consisting of halogenated isocyanuric acids, alkali metal salts of halogenated isocyanuric acids, hydrates of alkali metal salts of halogenated isocyanuric acids, halogenated hydantoins, and mixtures thereof as a solid bleaching agent; and a second layer formed of a coating layer, wherein the coating layer comprises one or more selected from the group consisting of alkali metal salts of aromatic carboxylic acids, alkali metal salts of acyclic dicarboxylic acids, alkali metal salts of acyclic monocarboxylic acids having a carbon number of from 1 to 7, and mixtures thereof.
An inductor core , comprising: a tubular magnetic material body formed of magnetic material, the tubular magnetic material body comprising an inclined portion comprising an inclined surface which constitutes a peripheral surface of a truncated cone having an outer diameter that increases from one end toward the other end of the tubular magnetic material body; a straight trunk portion which is disposed coaxially with the inclined portion and comprises an outer peripheral surface which constitutes a peripheral surface of a cylindrical body which extends from the other end toward the one end of the tubular magnetic material body; characterised by a flange portion which is provided between the inclined portion and the straight trunk portion and connects the inclined portion and the straight trunk portion, an outer peripheral surface of the flange portion having an outer diameter greater than the outer diameter of the inclined portion and an outer diameter of the straight trunk portion . a tubular magnetic material body formed of magnetic material, the tubular magnetic material body comprising an inclined portion comprising an inclined surface which constitutes a peripheral surface of a truncated cone having an outer diameter that increases from one end toward the other end of the tubular magnetic material body; a straight trunk portion which is disposed coaxially with the inclined portion and comprises an outer peripheral surface which constitutes a peripheral surface of a cylindrical body which extends from the other end toward the one end of the tubular magnetic material body; characterised by a flange portion which is provided between the inclined portion and the straight trunk portion and connects the inclined portion and the straight trunk portion, an outer peripheral surface of the flange portion having an outer diameter greater than the outer diameter of the inclined portion and an outer diameter of the straight trunk portion .