mhurhangee/ep-ind-claims huggingface dataset:
An aircraft seat pan assembly, comprising: left and right spreaders (26, 28); a seat pan including left and right seat pan members (22, 24) each pivotably attached proximate a forward end to the left and right spreaders (26, 28) and free of attachment at a rearward end to the left and right spreaders (26, 28) such that the left and right seat pan members (22, 24) are configured to pivot to adjust seat pan angle; a first transverse beam interconnecting the left and right spreaders (26, 28); a second transverse beam interconnecting the left and right seat pan members (22, 24); a third transverse beam arranged to travel along guide slots of the left and right spreaders (26, 28); a link interconnecting the second and third transverse beams (32, 40); and a gas spring (46; 56) connected between the first and third transverse beams (30, 40); wherein seat pan recline in response to passenger body weight drives the third transverse beam toward the first transverse beam to compress the gas spring (46; 56), and removal of passenger body weight from the seat pan causes the gas spring (46; 56) to unload to drive the third transverse beam apart from the first transverse beam to assist in returning the seat pan from a reclined position to an upright position. left and right spreaders (26, 28); a seat pan including left and right seat pan members (22, 24) each pivotably attached proximate a forward end to the left and right spreaders (26, 28) and free of attachment at a rearward end to the left and right spreaders (26, 28) such that the left and right seat pan members (22, 24) are configured to pivot to adjust seat pan angle; a first transverse beam interconnecting the left and right spreaders (26, 28); a second transverse beam interconnecting the left and right seat pan members (22, 24); a third transverse beam arranged to travel along guide slots of the left and right spreaders (26, 28); a link interconnecting the second and third transverse beams (32, 40); and a gas spring (46; 56) connected between the first and third transverse beams (30, 40); wherein seat pan recline in response to passenger body weight drives the third transverse beam toward the first transverse beam to compress the gas spring (46; 56), and removal of passenger body weight from the seat pan causes the gas spring (46; 56) to unload to drive the third transverse beam apart from the first transverse beam to assist in returning the seat pan from a reclined position to an upright position.
A method of making a phenylethylamine of formula B: wherein R 2, R 3, R 4, R 5, R 6, R β and R n are hydrogen, and R α is a -CH 3 group; or R 2, R 3, R 4, R 5, R 6 and R β are hydrogen, and R α and R n are -CH 3 groups; said method comprising the reduction of a compound of formula A in a solvent in the absence of acid or base: wherein R 2, R 3, R 4, R 5, R 6, R α, R β and R n are as defined above. R 2, R 3, R 4, R 5, R 6, R β and R n are hydrogen, and R α is a -CH 3 group; or R 2, R 3, R 4, R 5, R 6 and R β are hydrogen, and R α and R n are -CH 3 groups;
A photonics integrated system, the photonics integrated system being configured for cooperating with a radiation source having a bandwidth and for cooperating with a detector, the photonics integrated system comprising - a substrate, - an integrated interferometer integrated in the substrate and being configured for receiving radiation from a radiation source having a bandwidth, and - an integrated spectral filter integrated in the substrate and being configured for receiving radiation from the interferometer, wherein the integrated interferometer has a period (P ii) and the integrated spectral filter has a bandwidth (BW sa) such that the period (P ii) of the integrated interferometer is smaller than the bandwidth (BW sa) of the integrated spectral filter, characterised in that the integrated spectral filter has a periodic transfer characteristic with a period (P sa) and the photonics integrated system has a bandwidth (BW system) determined by the bandwidth of the components of the photonics integrated system, such that the period (P sa) of the periodic transfer characteristic of the integrated spectral filter is larger than the bandwidth (BW system) of the system. - a substrate, - an integrated interferometer integrated in the substrate and being configured for receiving radiation from a radiation source having a bandwidth, and - an integrated spectral filter integrated in the substrate and being configured for receiving radiation from the interferometer,
A bulb-type lighting source that receives electric power supplied via a base, comprising: a bowl-shaped case which accommodates a power supply circuit in an inner space thereof and to which the base is attached; a first heat sink member that closes a mouth of the bowl-shaped case; a mounting substrate that is in surface contact with a front surface of the first heat sink member opposite a rear surface of the first heat sink member that faces the inner space of the bowl-shaped case; a light-emitting unit that is mounted on a front surface of the mounting substrate opposite a rear surface of the mounting substrate which is in surface contact with the first heat sink member and that includes (i) a light-emitting element that emits light upon receiving electric power supplied by the power supply circuit and; a globe that at least covers the light-emitting unit in light emission directions thereof; characterized by a second heat sink member that has a first part in surface contact with a region of the front surface of the mounting substrate where the light-emitting unit is not mounted and that has a second part in surface contact with the first heat sink member, and a wavelength conversion element that converts wavelengths of the light emitted by the light-emitting element. a bowl-shaped case which accommodates a power supply circuit in an inner space thereof and to which the base is attached; a first heat sink member that closes a mouth of the bowl-shaped case; a mounting substrate that is in surface contact with a front surface of the first heat sink member opposite a rear surface of the first heat sink member that faces the inner space of the bowl-shaped case; a light-emitting unit that is mounted on a front surface of the mounting substrate opposite a rear surface of the mounting substrate which is in surface contact with the first heat sink member and that includes (i) a light-emitting element that emits light upon receiving electric power supplied by the power supply circuit and; a globe that at least covers the light-emitting unit in light emission directions thereof; characterized by a second heat sink member that has a first part in surface contact with a region of the front surface of the mounting substrate where the light-emitting unit is not mounted and that has a second part in surface contact with the first heat sink member, and a wavelength conversion element that converts wavelengths of the light emitted by the light-emitting element.
A diffraction grating (100, 103, 150, 160, 190, 200, 210), comprising: a plurality of different diffracting zones (108A-1...108A-n, 108B-1... 108B-n, 148A-1...148B-n, 154A-1, 154A-2, 164A-1, 164A-2, 198-1...198-n, 208-1, 208-2) having a periodically repeating lateral dimension corresponding to a grating period adapted for light diffraction; and a plurality of different liquid crystal layers (116A-1... 116B-n, 144A-1...144B-2, 156A-1...156C-2, 186-1...186-n, 196-1, 196-2) corresponding to the different diffracting zones, wherein the different liquid crystal layers have liquid crystal molecules (112, 212-1L...212-nR) that are aligned differently, such that the different diffracting zones have different optical properties associated with light diffraction, characterized in that the different diffracting zones include at least three diffracting zones each having different liquid crystal layers that are aligned differently or having different duty cycles from each other, and in that each of the different liquid crystal layers (116, 186, 196) includes a first region (116A-1L,..., 116C-nL, 144A-1a... 144B-2g, 156A-1L,...156A-nL) and a second region (116A-1R,..., 116C-nR, 144A-1a...144B-2g, 156A-1R,...156A-nR) that are laterally adjacent to each other, and wherein liquid crystal molecules (112, 212-1L) within the first regions of the different liquid crystal layers have the same alignment. a plurality of different diffracting zones (108A-1...108A-n, 108B-1... 108B-n, 148A-1...148B-n, 154A-1, 154A-2, 164A-1, 164A-2, 198-1...198-n, 208-1, 208-2) having a periodically repeating lateral dimension corresponding to a grating period adapted for light diffraction; and a plurality of different liquid crystal layers (116A-1... 116B-n, 144A-1...144B-2, 156A-1...156C-2, 186-1...186-n, 196-1, 196-2) corresponding to the different diffracting zones, wherein the different liquid crystal layers have liquid crystal molecules (112, 212-1L...212-nR) that are aligned differently, such that the different diffracting zones have different optical properties associated with light diffraction, characterized in that the different diffracting zones include at least three diffracting zones each having different liquid crystal layers that are aligned differently or having different duty cycles from each other, and in that each of the different liquid crystal layers (116, 186, 196) includes a first region (116A-1L,..., 116C-nL, 144A-1a... 144B-2g, 156A-1L,...156A-nL) and a second region (116A-1R,..., 116C-nR, 144A-1a...144B-2g, 156A-1R,...156A-nR) that are laterally adjacent to each other, and wherein liquid crystal molecules (112, 212-1L) within the first regions of the different liquid crystal layers have the same alignment.
A drive gear assembly for rotatably driving a driven gear, said drive gear assembly comprising: a drive shaft extending longitudinally along an axis; a main drive gear operatively coupled to said drive shaft; a scissor gear aligned coaxially with said main drive gear; a scissor spring disposed and operatively coupled between said main drive gear and said scissor gear and biased therebetween wherein said main drive gear and said scissor gear rotate about said axis relative to each other; and an isolation mechanism operatively coupled between said main drive gear and said drive shaft for absorbing impulse loads generated by the driven gear when engaged with said main drive gear, characterized in that said isolation mechanism includes a drive bar fixedly secured to said drive shaft and an isolation spring operatively coupled between said drive bar and said main drive gear to rotatably couple said main drive gear to said drive shaft, wherein said main drive gear includes a base plate having at least one recessed cavity formed therein for receiving at least a portion of said drive bar and wherein said drive bar includes a hub fixedly secured to said drive shaft and at least one arm (58, 60) extending from said hub and received in said recessed cavity in said main drive gear. a drive shaft extending longitudinally along an axis; a main drive gear operatively coupled to said drive shaft; a scissor gear aligned coaxially with said main drive gear; a scissor spring disposed and operatively coupled between said main drive gear and said scissor gear and biased therebetween wherein said main drive gear and said scissor gear rotate about said axis relative to each other; and an isolation mechanism operatively coupled between said main drive gear and said drive shaft for absorbing impulse loads generated by the driven gear when engaged with said main drive gear, characterized in that said isolation mechanism includes a drive bar fixedly secured to said drive shaft and an isolation spring operatively coupled between said drive bar and said main drive gear to rotatably couple said main drive gear to said drive shaft, wherein said main drive gear includes a base plate having at least one recessed cavity formed therein for receiving at least a portion of said drive bar and wherein said drive bar includes a hub fixedly secured to said drive shaft and at least one arm (58, 60) extending from said hub and received in said recessed cavity in said main drive gear.
A grounding clamp mountable, when in use, onto a hot-stick, the grounding clamp having a safety lock-out cooperating with the hot-stick and comprising: a frame and a clamping member defining a capture cavity and an opening, said opening providing access into said cavity for a conductor to be captured in said cavity, said clamping member cooperating with said frame and selectively biasable by a user between an unclamped position wherein said clamping member is retracted to open the cavity and opening and a clamped position wherein the cavity and opening are closed so that the conductor is clamped against said frame by said clamping member when the conductor is positioned in said cavity, characterised by: a lock-out mounted on said frame, said lock-out adapted to lock movement of said clamping member in the absence of the hot-stick so as to prevent movement of said clamping member relative to said frame, and to unlock said clamping member to allow movement of said clamping member relative to said frame when coupled to the hot-stick, whereby, when said frame is mounted on the hot-stick, the clamping member is moveable to clamp a conductor positioned in the cavity. a frame and a clamping member defining a capture cavity and an opening, said opening providing access into said cavity for a conductor to be captured in said cavity, said clamping member cooperating with said frame and selectively biasable by a user between an unclamped position wherein said clamping member is retracted to open the cavity and opening and a clamped position wherein the cavity and opening are closed so that the conductor is clamped against said frame by said clamping member when the conductor is positioned in said cavity, characterised by: a lock-out mounted on said frame, said lock-out adapted to lock movement of said clamping member in the absence of the hot-stick so as to prevent movement of said clamping member relative to said frame, and to unlock said clamping member to allow movement of said clamping member relative to said frame when coupled to the hot-stick, whereby, when said frame is mounted on the hot-stick, the clamping member is moveable to clamp a conductor positioned in the cavity. a lock-out mounted on said frame, said lock-out adapted to lock movement of said clamping member in the absence of the hot-stick so as to prevent movement of said clamping member relative to said frame, and to unlock said clamping member to allow movement of said clamping member relative to said frame when coupled to the hot-stick, whereby, when said frame is mounted on the hot-stick, the clamping member is moveable to clamp a conductor positioned in the cavity.
An ice detection system comprising: a first sensor located on a leading edge of a vertical stabilizer on an aircraft, wherein the first sensor is configured to detect a first type of icing condition for the aircraft; a second sensor located on a first side of the vertical stabilizer, wherein the second sensor is configured to detect a second type of icing condition for the aircraft; and a third sensor located on a second side of the vertical stabilizer, wherein the third sensor is configured to detect the second type of icing condition for the aircraft; wherein a first location of the first sensor on the leading edge is configured to expose the first sensor to first drops of water for the first type of icing condition and wherein a second location of the second sensor on the first side and a third location of the third sensor on the second side are configured to expose the second sensor and the third sensor to second drops of water for the second type of icing condition; and wherein the first location is a first height above a fuselage of the aircraft, the second location is a second height above the fuselage of the aircraft, and the third location is a third height above the fuselage of the aircraft. a first sensor located on a leading edge of a vertical stabilizer on an aircraft, wherein the first sensor is configured to detect a first type of icing condition for the aircraft; a second sensor located on a first side of the vertical stabilizer, wherein the second sensor is configured to detect a second type of icing condition for the aircraft; and a third sensor located on a second side of the vertical stabilizer, wherein the third sensor is configured to detect the second type of icing condition for the aircraft; wherein a first location of the first sensor on the leading edge is configured to expose the first sensor to first drops of water for the first type of icing condition and wherein a second location of the second sensor on the first side and a third location of the third sensor on the second side are configured to expose the second sensor and the third sensor to second drops of water for the second type of icing condition; and wherein the first location is a first height above a fuselage of the aircraft, the second location is a second height above the fuselage of the aircraft, and the third location is a third height above the fuselage of the aircraft.
A method performed by a user equipment "UE" for wireless communication, the method comprising: establishing a signaling radio link with a cellular access node "AN" via a cellular radio access technology "RAT"; transmitting, to the cellular AN via the signaling radio link, a connectivity request comprising a packet data network "PDN" connectivity type set to "Ethernet" for establishing connectivity to a local area network "LAN", wherein the connectivity request further includes at least a first parameter configured to be one of a physical address of the UE, an Ethernet frame type, and at least a first virtual LAN "VLAN" tag; establishing a data radio link "DRL" with the cellular AN based at least in part on an acceptance of the connectivity request by the cellular AN, wherein the acceptance of the connectivity request comprises the UE receiving an accept message that includes at least a second parameter for configuring the connectivity to the LAN, wherein the second parameter is at least the physical address of the UE and one of: the Ethernet frame type and the at least first VLAN tag, and wherein establishing the DRL includes configuring the DRL based on the accept message, and mapping the DRL to the physical address of the UE; and signaling successful completion of connectivity to the LAN for establishing a data flow for exchanging data link layer packets with the LAN via the DRL. establishing a signaling radio link with a cellular access node "AN" via a cellular radio access technology "RAT"; transmitting, to the cellular AN via the signaling radio link, a connectivity request comprising a packet data network "PDN" connectivity type set to "Ethernet" for establishing connectivity to a local area network "LAN", wherein the connectivity request further includes at least a first parameter configured to be one of a physical address of the UE, an Ethernet frame type, and at least a first virtual LAN "VLAN" tag; establishing a data radio link "DRL" with the cellular AN based at least in part on an acceptance of the connectivity request by the cellular AN, wherein the acceptance of the connectivity request comprises the UE receiving an accept message that includes at least a second parameter for configuring the connectivity to the LAN, wherein the second parameter is at least the physical address of the UE and one of: the Ethernet frame type and the at least first VLAN tag, and wherein establishing the DRL includes configuring the DRL based on the accept message, and mapping the DRL to the physical address of the UE; and signaling successful completion of connectivity to the LAN for establishing a data flow for exchanging data link layer packets with the LAN via the DRL.
Pellet press comprising a supporting shaft with a drum rotation axis, the shaft being fixed in a frame at a shaft mounting side and having at a roller supporting side a roller shaft part, a roller being rotatably mounted around a roller axis of the roller shaft part, the roller axis being situated parallel to and at a distance Δ from the drum rotation axis, wherein a drive member is rotatably mounted on the shaft via a first bearing near the shaft mounting side and second bearing near the roller supporting side, the drive member being attached to a perforated annular drum coaxial with the drum rotation axis, for rotating the drum around this axis, an inner drum surface being situated near a roller outer surface, characterised in that a single roller is provided, wherein an outer roller diameter (D r) is larger than a radius (Rd) of an inner drum surface, the first bearing being a radial bearing, the second bearing being an axial-radial bearing that is situated at a larger radial distance B 1 from the drum rotation axis than the radial bearing, each bearing (9,11) comprising a bearing casing (10,13) and a roller member, an axially movable locking bushing being placed around the shaft between the bearing housings (10,13) of the axial and the axial-radial bearings, the bushing engaging both casings (10,13).
Use of a VH4-34 encoded antibody that binds the CDIM epitope, which is the epitope recognized by mAb 216, for the manufacture of a medicament for the treatment of a mammal suffering from a condition characterized by a hyperproliferation of B cells, wherein said VH4-34 antibody binds to the CDIM epitope on the surface of the hyperproliferating B cells, and wherein said VH4-34 antibody is administered in an amount effective to preferentially kill the hyperproliferating B cells relative to normal B cells.
A bed comprising longitudinally spaced apart end supports and a side barrier comprising a lower bar, a middle bar and an upper bar adapted to extend between the end supports, the bars, as installed on the bed, forming a substantially horizontal stack and being movable to different heights, at least two of the bars (15, 16) having the same profiles and at least two of the bars (25, 16) being arranged so that they can vertically overlap each other, characterized in that the upper bar, middle bar and lower bar have the same profiles and in that the lower and upper bars (15, 17) are installed in such a way to be substantially symmetrical with respect to a horizontal plane.
An aqueous alkyl ketene dimer dispersion comprising (a) an alkyl ketene dimer of the formula and/or of the formula in which R 1 and R 2 are identical or different hydrocarbon radicals comprising 10 to 24 carbon atoms; (b) at least one emulsifier having a nitrogen content in the range from 0.05 to 1 % by weight and a Brookfield viscosity (20 °C; spindle 61 or 62; 12 rpm) in the range from about 10 to about 500 mPas in a 10% w/w aqueous solution, the emulsifier being selected from the group consisting of a starch, cellulose, starch derivative or cellulose derivative; (c) a condensation product of phenol sulfonic acid and formaldehyde, naphthalene sulfonic acid and formaldehyde or naphthalene sulfonic acid, phenol, formaldehyde and urea wherein the sulfonic acid groups may optionally be present in protonated or deprotonated or partly in protonated and partly in deprotonated form; wherein the dispersion has a charge density in the range from -5 to -150 μeq/g, wherein the charge density is determined according to the method defined in the description. (a) an alkyl ketene dimer of the formula and/or of the formula in which R 1 and R 2 are identical or different hydrocarbon radicals comprising 10 to 24 carbon atoms; (b) at least one emulsifier having a nitrogen content in the range from 0.05 to 1 % by weight and a Brookfield viscosity (20 °C; spindle 61 or 62; 12 rpm) in the range from about 10 to about 500 mPas in a 10% w/w aqueous solution, the emulsifier being selected from the group consisting of a starch, cellulose, starch derivative or cellulose derivative; (c) a condensation product of phenol sulfonic acid and formaldehyde, naphthalene sulfonic acid and formaldehyde or naphthalene sulfonic acid, phenol, formaldehyde and urea wherein the sulfonic acid groups may optionally be present in protonated or deprotonated or partly in protonated and partly in deprotonated form;