mhurhangee/patent-ind-claim-en huggingface dataset:
A female housing (3; 103) of an electrical connector apparatus (1; 100), comprising: a set of terminal apertures for receiving therein at least a set of terminals; a bottom slot located underneath the female housing (3; 103); and a first terminal position assurance device (5; 105) (TPA) accommodated within the bottom slot, characterised in that the female housing further comprises: ribs (12, 13, 14, 15, 16, 17, 18; 112, 113, 114, 115, 116, 117, 118) provided on the female housing (3; 103) along a periphery of the TPA (5; 105) to protect the TPA (5; 105) from physical contact, wherein the first TPA (5; 105) includes at each of its widthwise outer sides two rib-shaped engagement members extending therefrom for allowing the first TPA (5; 105) to be at a pre-set position during transport of the female housing (3; 103) and at a final lock position for engaging the set of terminals. a set of terminal apertures for receiving therein at least a set of terminals; a bottom slot located underneath the female housing (3; 103); and a first terminal position assurance device (5; 105) (TPA) accommodated within the bottom slot, characterised in that the female housing further comprises: ribs (12, 13, 14, 15, 16, 17, 18; 112, 113, 114, 115, 116, 117, 118) provided on the female housing (3; 103) along a periphery of the TPA (5; 105) to protect the TPA (5; 105) from physical contact, wherein the first TPA (5; 105) includes at each of its widthwise outer sides two rib-shaped engagement members extending therefrom for allowing the first TPA (5; 105) to be at a pre-set position during transport of the female housing (3; 103) and at a final lock position for engaging the set of terminals. ribs (12, 13, 14, 15, 16, 17, 18; 112, 113, 114, 115, 116, 117, 118) provided on the female housing (3; 103) along a periphery of the TPA (5; 105) to protect the TPA (5; 105) from physical contact, wherein the first TPA (5; 105) includes at each of its widthwise outer sides two rib-shaped engagement members extending therefrom for allowing the first TPA (5; 105) to be at a pre-set position during transport of the female housing (3; 103) and at a final lock position for engaging the set of terminals.
A multicast fast re-route switching method, comprising: receiving a Bit Indexed Explicit Replication Traffic Engineering, BIER-TE packet; when forwarding the multicast Bit Indexed Explicit Replication Traffic Engineering, BIER-TE, packet, detecting (S201), by a forwarding node, whether an abnormality occurs in a forwarding link between the forwarding node and a next node; wherein the BIER-TE packet comprises a BIER-TE header and a BIER header; in response to detecting that an abnormality occurs in the forwarding link between the forwarding node and the next node, determining (S202), by the forwarding node, whether the multicast BIER-TE packet is configured with a multicast fast re-route switching tag; and in response to determining that the multicast BIER-TE packet is configured with the multicast fast re-route switching tag, performing (S203), by the forwarding node, multicast fast re-route switching according to the multicast fast re-route switching tag, the method being characterised by comprising the step of: in response to determining that the multicast BIER-TE packet is configured with the multicast fast re-route switching tag, deleting, by the forwarding node, the BIER-TE header in the multicast BIER-TE packet, and performing, by the forwarding node, the multicast fast re-route switching according to the BIER header of the multicast BIER-TE packet. receiving a Bit Indexed Explicit Replication Traffic Engineering, BIER-TE packet; when forwarding the multicast Bit Indexed Explicit Replication Traffic Engineering, BIER-TE, packet, detecting (S201), by a forwarding node, whether an abnormality occurs in a forwarding link between the forwarding node and a next node; wherein the BIER-TE packet comprises a BIER-TE header and a BIER header; in response to detecting that an abnormality occurs in the forwarding link between the forwarding node and the next node, determining (S202), by the forwarding node, whether the multicast BIER-TE packet is configured with a multicast fast re-route switching tag; and in response to determining that the multicast BIER-TE packet is configured with the multicast fast re-route switching tag, performing (S203), by the forwarding node, multicast fast re-route switching according to the multicast fast re-route switching tag, the method being characterised by comprising the step of: in response to determining that the multicast BIER-TE packet is configured with the multicast fast re-route switching tag, deleting, by the forwarding node, the BIER-TE header in the multicast BIER-TE packet, and performing, by the forwarding node, the multicast fast re-route switching according to the BIER header of the multicast BIER-TE packet.
A recombinant lentiviral vector comprising a coding sequence for an OR protein fused to a coding sequence for a fluorescent protein or a subunit of a fluorescent protein, and a promoter active in human cells operatively linked to the coding sequences.
A mount system for alignment and mounting of an optical device, the mount system comprising: an optical device ; a housing ; and an optical device mount , comprising: a sleeve having a bore defining an inner bonding surface and having an outer portion attached to the optical device ; a stud attached to the housing , the stud at least partially extending through the bore of the sleeve and having an outer bonding surface , whereby a volume of space is defined between the inner bonding surface of the sleeve and the outer bonding surface of the stud, the stud having an opening and a plurality of passageways in fluid communication with the opening and the volume of space, the stud having a housing interface that mates to the housing ; and a curable material deposited via the opening and disposed throughout the passageways and the volume of space. an optical device ; a housing ; and an optical device mount , comprising: a sleeve having a bore defining an inner bonding surface and having an outer portion attached to the optical device ; a stud attached to the housing , the stud at least partially extending through the bore of the sleeve and having an outer bonding surface , whereby a volume of space is defined between the inner bonding surface of the sleeve and the outer bonding surface of the stud, the stud having an opening and a plurality of passageways in fluid communication with the opening and the volume of space, the stud having a housing interface that mates to the housing ; and a curable material deposited via the opening and disposed throughout the passageways and the volume of space. a sleeve having a bore defining an inner bonding surface and having an outer portion attached to the optical device ; a stud attached to the housing , the stud at least partially extending through the bore of the sleeve and having an outer bonding surface , whereby a volume of space is defined between the inner bonding surface of the sleeve and the outer bonding surface of the stud, the stud having an opening and a plurality of passageways in fluid communication with the opening and the volume of space, the stud having a housing interface that mates to the housing ; and a curable material deposited via the opening and disposed throughout the passageways and the volume of space.
Installation for treatment of objects such as vehicle bodies and/or vehicle attachment parts, having a. a plurality of treatment modules , wherein each treatment module has b. a treatment zone , c. a separate conveying system for conveying a workpiece carrier along a path within the treatment module , and, d. for each separate conveying system , a receiving point for receiving of a workpiece carrier and a delivery point for delivery of a workpiece carrier , so that there is no continuous conveying system which could convey a workpiece carrier through all the treatment modules , e. wherein each separate conveying system is designed to receive a workpiece carrier at the receiving point , to convey it into the treatment zone and thus through the treatment module and to convey it to the delivery point , which is separate from the receiving point , f. wherein a delivery point of a first treatment module and a receiving point of a second treatment module are configured in such a way that the delivery point of the first treatment module can interact as intended with the receiving point of the second treatment module in such a way that a workpiece carrier is transferable from the first treatment module to the second treatment module , g. wherein the treatment zone of a treatment module comprises a plurality of treatment units . a. a plurality of treatment modules , wherein each treatment module has b. a treatment zone , c. a separate conveying system for conveying a workpiece carrier along a path within the treatment module , and, d. for each separate conveying system , a receiving point for receiving of a workpiece carrier and a delivery point for delivery of a workpiece carrier , so that there is no continuous conveying system which could convey a workpiece carrier through all the treatment modules , e. wherein each separate conveying system is designed to receive a workpiece carrier at the receiving point , to convey it into the treatment zone and thus through the treatment module and to convey it to the delivery point , which is separate from the receiving point , f. wherein a delivery point of a first treatment module and a receiving point of a second treatment module are configured in such a way that the delivery point of the first treatment module can interact as intended with the receiving point of the second treatment module in such a way that a workpiece carrier is transferable from the first treatment module to the second treatment module , g. wherein the treatment zone of a treatment module comprises a plurality of treatment units .
A multiple phase electric machine , comprising: a power source ; a stator and a rotor coaxial with the stator; wherein the stator includes coils grouped in at least two groups of at least three phases each, each of the at least two groups defining a machine portion ; the interconnection of the at least three phases of each machine portion including first contactors and second contactors and being so configured as to be changeable between three configurations including a star configuration in which the first contactors are in their open position and the second contactors are in their closed position, a delta configuration in which the first contactors are in their closed position and the second contactors are in their open position, and a neutral configuration in which both the first contactors and the second contactors are in their open position; and a drive circuit comprising: at least two inverter power circuits each associated with a respective machine portion ; a controller so connected to the at least two inverter power circuits as to independently control the at least two inverter power circuits and configured to change the configuration of the at least two machine portions one at a time between the star configuration and the delta configuration so that the other of the at least two machine portions develop or develops a compensating torque. a power source ; a stator and a rotor coaxial with the stator; wherein the stator includes coils grouped in at least two groups of at least three phases each, each of the at least two groups defining a machine portion ; the interconnection of the at least three phases of each machine portion including first contactors and second contactors and being so configured as to be changeable between three configurations including a star configuration in which the first contactors are in their open position and the second contactors are in their closed position, a delta configuration in which the first contactors are in their closed position and the second contactors are in their open position, and a neutral configuration in which both the first contactors and the second contactors are in their open position; and a drive circuit comprising: at least two inverter power circuits each associated with a respective machine portion ; a controller so connected to the at least two inverter power circuits as to independently control the at least two inverter power circuits and configured to change the configuration of the at least two machine portions one at a time between the star configuration and the delta configuration so that the other of the at least two machine portions develop or develops a compensating torque. at least two inverter power circuits each associated with a respective machine portion ; a controller so connected to the at least two inverter power circuits as to independently control the at least two inverter power circuits and configured to change the configuration of the at least two machine portions one at a time between the star configuration and the delta configuration so that the other of the at least two machine portions develop or develops a compensating torque.
A heat exchanger , comprising: a plurality of flat tubes that are stacked in a direction perpendicular to a refrigerant flow direction; and a plurality of fins that have a first flat tube insertion portion into which a first flat tube among the plurality of flat tubes is inserted, and a second flat tube insertion portion into which a second flat tube adjacent to the first flat tube is inserted, wherein a first fin among the plurality of fins comprises: an inner periphery of the first flat tube insertion portion where the first flat tube comes into contact with the first fin ; and comprises a cut and raised piece for spacing a fin pitch (P) between the first fin and an adjacent second fin , the cut and raised piece being formed on a first inner periphery located at either side in a thickness direction of the first flat tube in the inner periphery of the first flat tube insertion portion ; the heat exchanger being characterized by a cutout portion (C2) obtained by cutting out a second inner periphery in the thickness direction, the cutout portion (C2) being formed on the second inner periphery opposing the first inner periphery of the first flat tube insertion portion , wherein the cut and raised piece is formed to have a length extending from the first inner periphery to the cutout portion (C2), and is formed to extend from the first inner periphery to the second fin , thereby having a raised portion of the same length as the fin pitch (P), and a folded portion that is folded back at the tip of the raised portion and that is in contact with the second fin . a plurality of flat tubes that are stacked in a direction perpendicular to a refrigerant flow direction; and a plurality of fins that have a first flat tube insertion portion into which a first flat tube among the plurality of flat tubes is inserted, and a second flat tube insertion portion into which a second flat tube adjacent to the first flat tube is inserted, wherein a first fin among the plurality of fins comprises: an inner periphery of the first flat tube insertion portion where the first flat tube comes into contact with the first fin ; and comprises a cut and raised piece for spacing a fin pitch (P) between the first fin and an adjacent second fin , the cut and raised piece being formed on a first inner periphery located at either side in a thickness direction of the first flat tube in the inner periphery of the first flat tube insertion portion ; the heat exchanger being characterized by a cutout portion (C2) obtained by cutting out a second inner periphery in the thickness direction, the cutout portion (C2) being formed on the second inner periphery opposing the first inner periphery of the first flat tube insertion portion , wherein the cut and raised piece is formed to have a length extending from the first inner periphery to the cutout portion (C2), and is formed to extend from the first inner periphery to the second fin , thereby having a raised portion of the same length as the fin pitch (P), and a folded portion that is folded back at the tip of the raised portion and that is in contact with the second fin .
Method of thermal treatment of air-dispersible raw material (4, 4', 4"), wherein the raw material is introduced into a riser tube (2, 2', 2") through which hot gases (1, 1', 1") flow and is subjected to thermal treatment by the hot gases therein, and wherein the riser tube is supplied with at least one fuel (11, 11', 11"), wherein the fuel at first dwells within a fuel conditioning region (5, 5', 5") on at least one application surface, wherein the fuel (11, 11', 11") in the fuel conditioning region comes into contact with a portion of the hot gas (1a, 1'a, 1" a) mixed with the raw material and hence is dried and/or at least partly degassed and/or at least partly converted and then goes into the riser tube, and characterized in that the fuel (11, 11', 11") in the fuel conditioning region comes into contact with hot gases that are formed to an extent of at least 50% by a portion of the hot gas (1a, 1'a, 1" a) mixed with the raw material, wherein the at least one application surface (7, 7', 7") of the fuel conditioning region is disposed in a conditioning chamber (6, 6', 6") that opens into the riser tube (2, 2', 2"), wherein a portion of the hot gases (1, 1', 1") mixed with the raw material is deflected into the conditioning chamber and comes into contact with the fuel.
A medical delivery device comprising: a barrel having an inner surface; and a stopper positioned within the barrel, the stopper contacting at least a portion of the inner surface of the barrel; the stopper having a compressibility of greater than 7.9% measured against the barrel, the stopper comprising two or more ribs where each rib having a compressibility of greater than 7.9% provides a contact width (w) with the inner surface of the barrel in a compressed state, the contact width (w) of at least one of said ribs is less than 1.0 mm and the sum of the contact widths of said ribs is less than 2.0 mm; and a plunger rod or actuation mechanism to displace the stopper; wherein the inner surface of the barrel has a water contact angle between 1° and 58°, wherein the stopper comprises an elastomeric body and the stopper is at least partially covered with one or more fluoropolymer layers, and wherein the compressibility (C) is defined by the following formula: C ⁢ % = v − y / v × 100 where v is the maximum outer diameter of the rib(s) in a non-compressed state, and y is the inner diameter of the inner surface of the barrel. a barrel having an inner surface; and a stopper positioned within the barrel, the stopper contacting at least a portion of the inner surface of the barrel; the stopper having a compressibility of greater than 7.9% measured against the barrel, the stopper comprising two or more ribs where each rib having a compressibility of greater than 7.9% provides a contact width (w) with the inner surface of the barrel in a compressed state, the contact width (w) of at least one of said ribs is less than 1.0 mm and the sum of the contact widths of said ribs is less than 2.0 mm; and a plunger rod or actuation mechanism to displace the stopper; wherein the inner surface of the barrel has a water contact angle between 1° and 58°, wherein the stopper comprises an elastomeric body and the stopper is at least partially covered with one or more fluoropolymer layers, and wherein the compressibility (C) is defined by the following formula: C ⁢ % = v − y / v × 100 where v is the maximum outer diameter of the rib(s) in a non-compressed state, and y is the inner diameter of the inner surface of the barrel. v is the maximum outer diameter of the rib(s) in a non-compressed state, and y is the inner diameter of the inner surface of the barrel.
An aircraft control structure for an aircraft , wherein the aircraft control structure is a spoiler having: a side wall ; a first outer surface coupled to the side wall ; a second outer surface coupled to the side wall and opposite the first outer surface ; wherein, in use, the first and second outer surface correspond to upper and lower aerodynamic surfaces of the spoiler and are directly exposed to ambient air during flight of the aircraft; a first stiffening web extending between the first outer surface and the second outer surface , the first stiffening web extending at least partially around a first aperture formed in the first outer surface to define a first stiffening recess ; a second stiffening web extending between the first outer surface and the second outer surface , the second stiffening web extending at least partially around a second aperture formed in the first outer surface or the second outer surface to define a second stiffening recess ; a first skin plate sized to extend over the first stiffening recess and shaped conformally with the first aperture , wherein the first skin plate is joined to the first stiffening web at a first friction stir welded seam ; and a second skin plate sized to extend over the second stiffening recess and shaped conformally with the second aperture , wherein the second skin plate is joined to the second stiffening web at a second friction stir welded seam . a side wall ; a first outer surface coupled to the side wall ; a second outer surface coupled to the side wall and opposite the first outer surface ; wherein, in use, the first and second outer surface correspond to upper and lower aerodynamic surfaces of the spoiler and are directly exposed to ambient air during flight of the aircraft; a first stiffening web extending between the first outer surface and the second outer surface , the first stiffening web extending at least partially around a first aperture formed in the first outer surface to define a first stiffening recess ; a second stiffening web extending between the first outer surface and the second outer surface , the second stiffening web extending at least partially around a second aperture formed in the first outer surface or the second outer surface to define a second stiffening recess ; a first skin plate sized to extend over the first stiffening recess and shaped conformally with the first aperture , wherein the first skin plate is joined to the first stiffening web at a first friction stir welded seam ; and a second skin plate sized to extend over the second stiffening recess and shaped conformally with the second aperture , wherein the second skin plate is joined to the second stiffening web at a second friction stir welded seam .