mhurhangee/patent-ind-claim-en huggingface dataset:
Method for assembling conductive pins in a transfer device, each conductive pin being formed of at least one conductive segment and being intended to be electrically connected to at least one other conductive pin in order to form an electrical winding of a wound part of a rotary electric machine , the transfer device comprising a spindle body having an axis (Z) and a plurality of guide strips radially extending from the body, lateral spaces intended to house at least one conductive segment being defined between two adjacent guide strips, the conductive pins are split into a first set of pins and a second set of pins, the first set of pins being divided into a first sub-set of pins and a second sub-set of pins, the method being characterized in that it comprises, in a first part (A), at least one supply step comprising arranging the pins of the first set of pins in lateral spaces of the transfer device ; and, in a second part (B): - a lifting step , in which the pins of the first sub-set are moved so as to create an insertion space between said first sub-set and the second sub-set of pins; - an insertion step , in which the pins of the second set are inserted into the insertion space so that the conductive pins of the second set are circumferentially aligned with the conductive pins of the second sub-set ; - a lowering step , in which the pins of the first sub-set are moved so that said conductive pins of said first sub-set are circumferentially aligned with the conductive pins of the second set . - a lifting step , in which the pins of the first sub-set are moved so as to create an insertion space between said first sub-set and the second sub-set of pins; - an insertion step , in which the pins of the second set are inserted into the insertion space so that the conductive pins of the second set are circumferentially aligned with the conductive pins of the second sub-set ; - a lowering step , in which the pins of the first sub-set are moved so that said conductive pins of said first sub-set are circumferentially aligned with the conductive pins of the second set .
A resin composition comprising 30 to 120 parts by mass of a white pigment, wherein the average particle size of the white pigment is 0.1 to 0.5 μm, and 0.5 to 30 parts by mass of a flame retarder, wherein the flame retarder comprises an organic halogen compound and the organic halogen compound is an organic bromine compound per 100 parts by mass of a liquid crystal polyester. 30 to 120 parts by mass of a white pigment, wherein the average particle size of the white pigment is 0.1 to 0.5 μm, and 0.5 to 30 parts by mass of a flame retarder, wherein the flame retarder comprises an organic halogen compound and the organic halogen compound is an organic bromine compound per 100 parts by mass of a liquid crystal polyester.
A tool body including a damping apparatus for damping vibrations in a machining tool having besides the tool body a member with at least one cutting edge to be secured to the tool body, wherein the damping apparatus is arranged in an internal room of the tool body and comprises • a damper mass body ) with an axial through bore , and • a central tube extending through said bore and which is rigidly secured to the damper mass body inside the through bore , wherein the central tube is at both ends thereof rigidly connected to a tool body fixed part and the central tube is made of a material with a spring property allowing the damper mass body to oscillate in the internal room perpendicularly to the longitudinal extension of the central tube , characterised in that the internal room contains a damping fluid, such as oil, in an annular cavity separating the damper mass body radially from internal walls defining the internal room . • a damper mass body ) with an axial through bore , and • a central tube extending through said bore and which is rigidly secured to the damper mass body inside the through bore ,
Folding wing for a missile guidance system , comprising: a first wing part having a wing leading edge and a first folding joint edge that lies opposite the wing leading edge ; a second wing part having a wing trailing edge and a second folding joint edge that lies opposite the wing trailing edge ; and a folding hinge that connects the first wing part and the second wing part in a pivotably-jointed manner, said folding hinge comprising a folding axis (K) that is perpendicular with respect to the wing surface of the folding wing , characterised in that the folding hinge is arranged on a wing root of the first and second wing parts (1; 2). a first wing part having a wing leading edge and a first folding joint edge that lies opposite the wing leading edge ; a second wing part having a wing trailing edge and a second folding joint edge that lies opposite the wing trailing edge ; and a folding hinge that connects the first wing part and the second wing part in a pivotably-jointed manner, said folding hinge comprising a folding axis (K) that is perpendicular with respect to the wing surface of the folding wing , characterised in that the folding hinge is arranged on a wing root of the first and second wing parts (1; 2).
Low temperature indicator mixture for indicating/monitoring a temperature transition within a temperature range from -20°C to -160°C, in particular -25°C to -160°C or -50°C to -150°C, which comprises: at least one dye; and at least one alcohol, selected from the group which comprises octan-1-ol, nonan-1-ol, propane-1,2-diol, propane-1,3-diol, butane-1,2-diol, butane-1,3-diol, butan-2-ol, pentane-1,5-diol, pentan-1-ol, cyclopentanol, benzyl alcohol; and wherein the melting temperature of the mixture lies within a temperature range from -20°C to -160°C, in particular -25°C to -160°C or -50°C to -150°C. at least one dye; and at least one alcohol, selected from the group which comprises octan-1-ol, nonan-1-ol, propane-1,2-diol, propane-1,3-diol, butane-1,2-diol, butane-1,3-diol, butan-2-ol, pentane-1,5-diol, pentan-1-ol, cyclopentanol, benzyl alcohol; and wherein the melting temperature of the mixture lies within a temperature range from -20°C to -160°C, in particular -25°C to -160°C or -50°C to -150°C.
An attachment for a vehicle wheel for allowing a driving operation with limited tire function, including a base body having a tread surface for contacting a road surface (F) and at least one bracing means which is configured to engage with a hook portion behind a portion of a rim of the vehicle wheel , wherein the attachment comprises a bracing mechanism having a contact portion which is configured to actuate the bracing means and to bring the hook portion into engagement behind the portion of the rim , when the contact portion is actuated, characterized in that the bracing mechanism is configured to contact the road surface (F) with the contact portion when the attachment is attached to the vehicle wheel and the vehicle wheel is rotating, and thereby to actuate the contact portion , or to contact the rim with the contact portion when the attachment is attached to the vehicle wheel and thereby to actuate the contact portion .
Weight machine, comprising the following features: an inner supporting structure and a housing , which consists of or comprises at least two housing halves (20.1) forming a housing frame and which are divided along a separation plane that extends perpendicularly through a shaft , wherein the housing halves are each mounted on the inner supporting structure so as to be pivoted away from one another about a pivot axis from a closed position into an open position; a rotatable flywheel mass mounted in the housing , on the housing frame or on the inner supporting structure , which changes its direction of rotation during operation, the flywheel mass is fitted on a shaft or is seated on a shaft , a flexible belt-like or strap-like tension element , the flexible tension element is fastened on the shaft or a coil , which is mounted on a freewheel bearing , which is pretensioned in the rolling-up direction of the tension element by means of a spring arrangement . an inner supporting structure and a housing , which consists of or comprises at least two housing halves (20.1) forming a housing frame and which are divided along a separation plane that extends perpendicularly through a shaft , wherein the housing halves are each mounted on the inner supporting structure so as to be pivoted away from one another about a pivot axis from a closed position into an open position; a rotatable flywheel mass mounted in the housing , on the housing frame or on the inner supporting structure , which changes its direction of rotation during operation, the flywheel mass is fitted on a shaft or is seated on a shaft , a flexible belt-like or strap-like tension element , the flexible tension element is fastened on the shaft or a coil , which is mounted on a freewheel bearing , which is pretensioned in the rolling-up direction of the tension element by means of a spring arrangement .
An organic compound having the following structure of Chemical Formula 1: wherein R 1 is a C 6 -C 30 aryl amino group or a C 3 -C 30 hetero-aryl amino group, wherein each of an aromatic ring and a heteroaromatic ring in the C 6 -C 30 aryl amino group and/or the C 3 -C 30 hetero-aryl amino group is unsubstituted or substituted with at least one group selected from cyano, C 1 -C 10 alkyl, C 1 -C 10 alkoxy, C 6 -C 30 aryl and C 3 -C 30 hetero aryl ; R 2 is hydrogen, an unsubstituted or substituted C 1 -C 20 alkyl group, an unsubstituted or substituted C 1 -C 20 alkoxy group, an unsubstituted or substituted aromatic group or an unsubstituted or substituted heteroaromatic group; each of R 3 and R 4 is independently an unsubstituted or substituted aromatic group or an unsubstituted or substituted heteroaromatic group; and each of R 5 and R 6 is independently hydrogen, an unsubstituted or substituted C 1 -C 10 alkyl group, an unsubstituted or substituted C 1 -C 10 alkoxy group, an unsubstituted or substituted aromatic group or an unsubstituted or substituted heteroaromatic group, wherein the aromatic group is a group which has one or more C 6 -C 30 aryl groups, wherein the heteroaromatic group is a group which has one or more C 3 -C 30 heteroaryl groups. wherein R 1 is a C 6 -C 30 aryl amino group or a C 3 -C 30 hetero-aryl amino group, wherein each of an aromatic ring and a heteroaromatic ring in the C 6 -C 30 aryl amino group and/or the C 3 -C 30 hetero-aryl amino group is unsubstituted or substituted with at least one group selected from cyano, C 1 -C 10 alkyl, C 1 -C 10 alkoxy, C 6 -C 30 aryl and C 3 -C 30 hetero aryl ; R 2 is hydrogen, an unsubstituted or substituted C 1 -C 20 alkyl group, an unsubstituted or substituted C 1 -C 20 alkoxy group, an unsubstituted or substituted aromatic group or an unsubstituted or substituted heteroaromatic group; each of R 3 and R 4 is independently an unsubstituted or substituted aromatic group or an unsubstituted or substituted heteroaromatic group; and each of R 5 and R 6 is independently hydrogen, an unsubstituted or substituted C 1 -C 10 alkyl group, an unsubstituted or substituted C 1 -C 10 alkoxy group, an unsubstituted or substituted aromatic group or an unsubstituted or substituted heteroaromatic group, wherein the aromatic group is a group which has one or more C 6 -C 30 aryl groups, wherein the heteroaromatic group is a group which has one or more C 3 -C 30 heteroaryl groups.
Generator comprising a rotor and a stator, - whereby the generator is an radial flux electrical machine, - whereby an outer part of the generator is the stator or the rotor, - whereby the outer part of the generator comprises a support structure, - whereby the support structure is modular and the modules are arranged in rows , - whereby the modules are arranged in a staggered manner, so that a module in a first row of modules is connected to two modules of a second row abutting on the first row , characterized in that the modules comprise holes , so that two modules are connected by bolts, - whereby first holes of the module are arranged close to the upper end of the module, where the module is abutting on the modules of a first neighboring row, and second holes of the module are arranged close to the lower end of the module, where the module is abutting on the modules of a second neighboring row. - whereby the generator is an radial flux electrical machine, - whereby an outer part of the generator is the stator or the rotor, - whereby the outer part of the generator comprises a support structure, - whereby the support structure is modular and the modules are arranged in rows , - whereby the modules are arranged in a staggered manner, so that a module in a first row of modules is connected to two modules of a second row abutting on the first row , characterized in that the modules comprise holes , so that two modules are connected by bolts, - whereby first holes of the module are arranged close to the upper end of the module, where the module is abutting on the modules of a first neighboring row, and second holes of the module are arranged close to the lower end of the module, where the module is abutting on the modules of a second neighboring row.
Process for lightening keratin fibres, in particular human keratin fibres such as the hair, which consists in i) placing the keratin fibres in contact with a substrate comprising on its surface one or more solid chemical oxidizing agents, the said solid chemical oxidizing agent(s) being deposited onto the surface of the said substrate by printing, and then ii) in applying to the fibres an aqueous composition comprising one or more chemical oxidizing agents and one or more alkaline agents.
Retroreflective prism sheeting , comprising a plurality of discrete clusters of cube corners formed from a transparent material that are separated from one another on all sides by surface , each cube corner having a base edge not collinear or parallel with the base edges of cube corners on either side of it, wherein the cube corners in each cluster are defined by a set of straight vee grooves, each groove having substantially a same direction throughout its length, wherein the cube corners have different orientations such that the retroreflectivity of the sheeting is substantially rotationally insensitive, and wherein the cube corners are separated by non-retroreflective prisms within each discrete cluster of cube corners, and wherein each of the cube corners and non-retroreflective prisms have a common vertex . Z
A pneumatic tire for a vehicle, comprising a tread, side walls, and beads; wherein a plurality of tread blocks and grooves are formed in the tread, and kerfs are formed in the tread blocks ; wherein each kerf face of each of the kerfs comprises: a flange portion formed in an outermost portion of the tread that is in contact with a ground; and a plurality of concave kerf portions and convex kerf portions connected to the flange portion and alternately formed in depthwise and lengthwise directions of the kerf ; and wherein concave kerf portions of one kerf face of the kerf are configured to be matched with opposite convex kerf portions of an opposite kerf face of the kerf , convex kerf portions of the one kerf face are configured to be matched with opposite concave kerf portions of the opposite kerf face , and the concave and convex kerf portions (42, 42', 42", 43, 43', 43", 44, 45) that alternate in the lengthwise direction and depthwise direction are configured such that protrusion directions of the concave and convex kerf portions (42, 42', 42", 43, 43', 43", 44, 45) are opposite to each other, characterized in that each of the concave and convex kerf portions (42, 42', 42", 43, 43', 43", 44, 45) comprises: a center portion (42-1, 43-1) disposed on a center part of the concave or convex kerf portion (42, 42', 42", 43, 43', 43", 44, 45), and configured to form a curved tapered surface whose lengthwise width is gradually decreased from the top of one row of concave kerf portions and convex kerf portions toward the bottom of one row of concave kerf portions and convex kerf portions; side portions (42-2, 43-2) disposed in contact with both sides of the center portion (42-1, 43-1), and configured to form a tapered surface inclined to the center portion.
A suture lock for holding a tensioning suture in tension, comprising: a housing having first and second through holes extending between a distal surface and a proximal surface, the first and second through holes being laterally separated, the housing having a side hole through a side surface and adjacent the proximal surface, the side hole communicating with the first through hole; a snare within the first through hole and adapted to move longitudinally through the first through hole, the snare having an opening; an anchor wire passing through a proximal portion of the first through hole and through the side hole; wherein the suture lock has an open configuration in which the opening of the snare is at least partially out of the first through hole and the tensioning suture passes through the opening of the suture and the second through hole of the housing and can be freely translated with respect to the snare and the second through hole of the housing, and a locked configuration in which the opening of the snare is within the first through hole and the tensioning suture is held against translation by the snare in a tortuous configuration. a housing having first and second through holes extending between a distal surface and a proximal surface, the first and second through holes being laterally separated, the housing having a side hole through a side surface and adjacent the proximal surface, the side hole communicating with the first through hole; a snare within the first through hole and adapted to move longitudinally through the first through hole, the snare having an opening; an anchor wire passing through a proximal portion of the first through hole and through the side hole; wherein the suture lock has an open configuration in which the opening of the snare is at least partially out of the first through hole and the tensioning suture passes through the opening of the suture and the second through hole of the housing and can be freely translated with respect to the snare and the second through hole of the housing, and a locked configuration in which the opening of the snare is within the first through hole and the tensioning suture is held against translation by the snare in a tortuous configuration.
Aircraft passenger seat comprising a structural component on which a table top of the aircraft passenger seat is held via a joint arrangement, wherein the table top is pivotable about a pivot axis of the joint arrangement, wherein the aircraft passenger seat has a basic structure, wherein the basic structure is a mechanically supporting structure, wherein the basic structure has the structural component , wherein the basic structure has two respectively elongate, plate-like, upright structural components which are present on both sides in the region of the extent of a backrest of the aircraft passenger seat, wherein the structural components have a sandwich structure in order to obtain high mechanical stability at a low weight, wherein a connecting arrangement for releasably attaching the table top to the structural component is provided, wherein the connecting arrangement comprises adjustment means for adjusting a mounting position of the table top relative to the structural component , wherein the adjustment means are designed in such a manner that the mounting position can be selected from a plurality of different mounting positions of the table top relative to the structural component , wherein the table top of the aircraft passenger seat is attached releasably to a first of the two structural components by a connecting arrangement and releasably to a second of the two structural components by a further connecting arrangement .
A gas turbine engine article (60; 102) comprising: an article wall (68; 168) defining a cavity ; and a cooling passage network embedded in the article wall (68; 168) between inner and outer portions (68a,68b;168a,168b) of the article wall (68;168), the cooling passage network having an inlet orifice through the inner portion (68a; 168a) of the article wall (68;168) to receive cooling air from the cavity (74;174), a sub-passage region including a plurality of sub-passages , at least one outlet orifice through the outer portion (68b;168b) of the article wall (68;168) that is connected to the sub-passage region , and a manifold region having a plenum upstream of the sub-passage region , the outer portion (68b;168b) of the article wall (68;168) having a sloped impingement surface located opposite the inlet orifice in the cooling passage network , the sloped impingement surface being angled to divert flow of cooling air from the inlet orifice toward the plenum , wherein the inlet orifice defines a central axis (A1), and there is an angle in the cooling passage network that opens toward the plenum that is subtended by the central axis (A1) and the sloped impingement surface , characterised in that the angle is from 100° to 160°. an article wall (68; 168) defining a cavity ; and a cooling passage network embedded in the article wall (68; 168) between inner and outer portions (68a,68b;168a,168b) of the article wall (68;168), the cooling passage network having an inlet orifice through the inner portion (68a; 168a) of the article wall (68;168) to receive cooling air from the cavity (74;174), a sub-passage region including a plurality of sub-passages , at least one outlet orifice through the outer portion (68b;168b) of the article wall (68;168) that is connected to the sub-passage region , and a manifold region having a plenum upstream of the sub-passage region , the outer portion (68b;168b) of the article wall (68;168) having a sloped impingement surface located opposite the inlet orifice in the cooling passage network , the sloped impingement surface being angled to divert flow of cooling air from the inlet orifice toward the plenum , wherein the inlet orifice defines a central axis (A1), and there is an angle in the cooling passage network that opens toward the plenum that is subtended by the central axis (A1) and the sloped impingement surface , characterised in that the angle is from 100° to 160°.