mhurhangee/ep-ind-claims huggingface dataset:
A heat-resistant composite sheet which is a glass fiber fabric impregnated with a fluorine-containing resin, wherein, with the glass fiber fabric as a center, the composite sheet has two opposite surfaces (11, 12) in a thickness direction, at least one of which has a surface roughness, as measured in accordance with the JIS-B0601-1994 test method, of Rz ≤ 21 μm and Ra ≤ 7.5 μm, wherein the glass fiber fabric is treated with a silicon-containing agent represented by a general formula YSiX 3, wherein Y represents a non-hydrolyzable group, including an alkenyl group, and a hydrocarbon group having a functional group selected from Cl, NH 2, -SH, an epoxy group, N 3, a (meth)acryloyloxy group and an isocyanate group at the end; X represents a hydrolyzable group, including Cl, OCH 3, OCH 2 CH 3, OC 2 H 4 OCH 3, and OSi(CH 3) 3, and wherein the amount of the silicon-containing agent is 0.05 to 0.2% by weight based on the total weight of the glass fiber fabric. wherein the glass fiber fabric is treated with a silicon-containing agent represented by a general formula YSiX 3, wherein Y represents a non-hydrolyzable group, including an alkenyl group, and a hydrocarbon group having a functional group selected from Cl, NH 2, -SH, an epoxy group, N 3, a (meth)acryloyloxy group and an isocyanate group at the end; X represents a hydrolyzable group, including Cl, OCH 3, OCH 2 CH 3, OC 2 H 4 OCH 3, and OSi(CH 3) 3, and wherein the amount of the silicon-containing agent is 0.05 to 0.2% by weight based on the total weight of the glass fiber fabric.
An aircraft interior structure, comprising: a social area section including a countertop surface about which passengers may congregate and socialize, the social area section being accessible from a floor area of an aircraft cabin; a passenger seating section proximate to an aircraft seat, the passenger seating section including a footwell; and a partition separating the passenger seating section and a first portion of the social area section, the footwell of the passenger seating section being positioned underneath at least one of the partition or the surface of the social area section in a second portion of the social area section; characterized in that the countertop surface including at least one accessible exterior edge proximate to the floor area, the exterior edge being accessible from the floor area, the countertop surface including at least one accessible interior edge proximate to a bounded space of the floor area, the interior edge being accessible from the bounded space, the countertop surface being surrounded at least in part with standing room in the aircraft cabin, the standing room being configured to not inhibit passage through the floor area of the aircraft cabin. a social area section including a countertop surface about which passengers may congregate and socialize, the social area section being accessible from a floor area of an aircraft cabin; a passenger seating section proximate to an aircraft seat, the passenger seating section including a footwell; and a partition separating the passenger seating section and a first portion of the social area section, the footwell of the passenger seating section being positioned underneath at least one of the partition or the surface of the social area section in a second portion of the social area section; characterized in that the countertop surface including at least one accessible exterior edge proximate to the floor area, the exterior edge being accessible from the floor area, the countertop surface including at least one accessible interior edge proximate to a bounded space of the floor area, the interior edge being accessible from the bounded space, the countertop surface being surrounded at least in part with standing room in the aircraft cabin, the standing room being configured to not inhibit passage through the floor area of the aircraft cabin.
A method for manufacturing a bladed Gas Turbine Engine rotor, the method comprising: arranging bladed pieces in a ring formation such that shank-to-shank junctions are formed between circumferentially-adjacent bladed pieces, characterized in that the method further comprises the following steps: depositing a first alloy along the shank-to-shank junctions utilizing a localized fusion deposition process to produce a plurality of alloy-filled joints bonding the bladed pieces in a bonded blade ring having a central opening; inserting a hub disk into the central opening of the bonded blade ring; and bonding the bonded blade ring to the hub disk; further, during the step of depositing, a local heat input is applied to the first alloy to form each alloy-filled joint in a single pass or to gradually build-up each of the alloy-filled joints along the shank-to-shank junctions. arranging bladed pieces in a ring formation such that shank-to-shank junctions are formed between circumferentially-adjacent bladed pieces, characterized in that the method further comprises the following steps: depositing a first alloy along the shank-to-shank junctions utilizing a localized fusion deposition process to produce a plurality of alloy-filled joints bonding the bladed pieces in a bonded blade ring having a central opening; inserting a hub disk into the central opening of the bonded blade ring; and bonding the bonded blade ring to the hub disk; further, during the step of depositing, a local heat input is applied to the first alloy to form each alloy-filled joint in a single pass or to gradually build-up each of the alloy-filled joints along the shank-to-shank junctions. depositing a first alloy along the shank-to-shank junctions utilizing a localized fusion deposition process to produce a plurality of alloy-filled joints bonding the bladed pieces in a bonded blade ring having a central opening; inserting a hub disk into the central opening of the bonded blade ring; and bonding the bonded blade ring to the hub disk; further, during the step of depositing, a local heat input is applied to the first alloy to form each alloy-filled joint in a single pass or to gradually build-up each of the alloy-filled joints along the shank-to-shank junctions.
A rotary-wing aerodyne, the said aerodyne comprising: - a motor; - a structure supporting at least one passenger seat; - a rotor arranged above the said structure and linked to the motor by a hollow transmission shaft, the transmission shaft being movable in rotation in relation to the structure; - a hollow mast attached to the structure and extending through the transmission shaft; and - a parachute arranged above the rotor, the parachute being attached to the mast and linked to the structure by means of a suspension element passing through the mast; characterised in that the said suspension element is produced from a multi-strand steel cable with a tensile strength of greater than 150 daN/mm 2 in order that the cable resist to the shearing efforts during the dislocation of the transmission shaft. - a motor; - a structure supporting at least one passenger seat; - a rotor arranged above the said structure and linked to the motor by a hollow transmission shaft, the transmission shaft being movable in rotation in relation to the structure; - a hollow mast attached to the structure and extending through the transmission shaft; and - a parachute arranged above the rotor, the parachute being attached to the mast and linked to the structure by means of a suspension element passing through the mast;
A razor cartridge comprising: a housing having a top, front and back areas, a bottom, and a plurality of plastic posts (26a, 26b, 26c) each having an end portion (42a, 42b, 42c) extending towards the housing bottom; and at least one blade (22a, 22b, 22c), each said at least one blade being a bent blade or blade support assembly, and comprising a cutting edge (22a', 22b', 22c') and a bottom portion (22a", 22b", 22c") having front (23a,23b, 23c) and back sides(24a, 24b, 24c), wherein each blade optionally comprises a blade carrier, said bottom portion of said at least one blade disposed adjacent at least of one of said plurality of posts; wherein each of said end portions of said plurality of plastic posts are crushed from said housing bottom providing contact and support to the front and/or back side of said bottom portion of at least one of the blades or of one of the blades comprising said blade carriers in said housing. a housing having a top, front and back areas, a bottom, and a plurality of plastic posts (26a, 26b, 26c) each having an end portion (42a, 42b, 42c) extending towards the housing bottom; and at least one blade (22a, 22b, 22c), each said at least one blade being a bent blade or blade support assembly, and comprising a cutting edge (22a', 22b', 22c') and a bottom portion (22a", 22b", 22c") having front (23a,23b, 23c) and back sides(24a, 24b, 24c), wherein each blade optionally comprises a blade carrier, said bottom portion of said at least one blade disposed adjacent at least of one of said plurality of posts; wherein each of said end portions of said plurality of plastic posts are crushed from said housing bottom providing contact and support to the front and/or back side of said bottom portion of at least one of the blades or of one of the blades comprising said blade carriers in said housing.
An adhesive composition comprising: a) an isocyanate functional polyether based prepolymer having a z molecular weight average (Mz) of 10,000 to 80,000 g/mole; (b) a carbon black having an average oil absorption number of at least 80 to at most 400 cubic centimeters of dibutyl phthalate per 100 grams of the carbon black; (c) reactive silicon in an amount from 0.001% to 10% by weight of the adhesive composition; and (d) one or more catalysts for the reaction of isocyanate with hydroxyl groups.
Process for preparing isophoronediamine, characterized in that A) isophoronenitrile is subjected directly in one stage to aminating hydrogenation to give isophoronediamine in the presence of ammonia, hydrogen, a hydrogenation catalyst and possibly further additions, and in the presence or absence of organic solvents; or B) isophoronenitrile is first converted fully or partly in at least two or more than two stages to isophoronenitrile imine, and this isophoronenitrile imine is subjected to aminating hydrogenation to give isophoronediamine as a pure substance or in a mixture with other components and/or isophoronenitrile, in the presence of at least ammonia, hydrogen and a catalyst, wherein the catalyst has the following properties: I. The catalyst has, after the activation, in its entirety, the following composition in per cent by weight (% by weight), where the proportions add up to 100% by weight, based on the metals present: Cobalt: 55% to 85% by weight Aluminium: 5% to 43.5% by weight Chromium: 0.5% to 3% by weight Nickel: 1% to 7% by weight and II. The catalyst is in the form of irregular particles as a granular material and after activation has particle sizes of 1 to 8 millimetres (mm) measured by screening. A) isophoronenitrile is subjected directly in one stage to aminating hydrogenation to give isophoronediamine in the presence of ammonia, hydrogen, a hydrogenation catalyst and possibly further additions, and in the presence or absence of organic solvents; or B) isophoronenitrile is first converted fully or partly in at least two or more than two stages to isophoronenitrile imine, and this isophoronenitrile imine is subjected to aminating hydrogenation to give isophoronediamine as a pure substance or in a mixture with other components and/or isophoronenitrile, in the presence of at least ammonia, hydrogen and a catalyst, wherein the catalyst has the following properties: I. The catalyst has, after the activation, in its entirety, the following composition in per cent by weight (% by weight), where the proportions add up to 100% by weight, based on the metals present: Cobalt: 55% to 85% by weight Aluminium: 5% to 43.5% by weight Chromium: 0.5% to 3% by weight Nickel: 1% to 7% by weight and II. The catalyst is in the form of irregular particles as a granular material and after activation has particle sizes of 1 to 8 millimetres (mm) measured by screening. I. The catalyst has, after the activation, in its entirety, the following composition in per cent by weight (% by weight), where the proportions add up to 100% by weight, based on the metals present: Cobalt: 55% to 85% by weight Aluminium: 5% to 43.5% by weight Chromium: 0.5% to 3% by weight Nickel: 1% to 7% by weight and Cobalt: 55% to 85% by weight Aluminium: 5% to 43.5% by weight Chromium: 0.5% to 3% by weight Nickel: 1% to 7% by weight II. The catalyst is in the form of irregular particles as a granular material and after activation has particle sizes of 1 to 8 millimetres (mm) measured by screening.
A method in a user node for reducing signalling load in a multimedia broadcast multicast services, MBMS, network, the method comprising: receiving from a network node a broadcasted system information block with information about at least one MBMS service supported by a current frequency for said service; initiating a connection establishment procedure, the connection establishment procedure including one or more connection establishment messages sent between the user node and the network node to set up a connection; and during the connection establishment procedure, transmitting an information to the network node in one of the one or more connection establishment messages (502; 504; 510) indicating that the current frequency is a frequency of interest for the user node. receiving from a network node a broadcasted system information block with information about at least one MBMS service supported by a current frequency for said service; initiating a connection establishment procedure, the connection establishment procedure including one or more connection establishment messages sent between the user node and the network node to set up a connection; and during the connection establishment procedure, transmitting an information to the network node in one of the one or more connection establishment messages (502; 504; 510) indicating that the current frequency is a frequency of interest for the user node.
A melt pressure regulating mechanism for an injection molding apparatus having a melt holder for pressurizing molten plastic prior to injection into a mold, the molten plastic having a melt pressure, and an injection element for advancing the molten plastic from the melt holder into the mold, the melt pressure regulating mechanism comprising: a pressure regulating device disposed between the melt holder and the mold, the pressure regulating device maintaining a substantially constant melt pressure within a mold cavity, the pressure regulating device comprising a fluid pressure regulating valve; characterized in that there is provided a pressure relief valve oriented in series with the fluid pressure regulating valve, the pressure regulating valve being upstream of the pressure relief valve. a pressure regulating device disposed between the melt holder and the mold, the pressure regulating device maintaining a substantially constant melt pressure within a mold cavity, the pressure regulating device comprising a fluid pressure regulating valve; characterized in that there is provided a pressure relief valve oriented in series with the fluid pressure regulating valve, the pressure regulating valve being upstream of the pressure relief valve.
A surgical instrument, comprising: an end effector; a drive member movable to effectuate a motion in said end effector; a motor operable to move said drive member to effectuate said motion in said end effector; and a bailout assembly operable to perform a mechanical bailout of said surgical instrument in response to a bailout error, said bailout error defining the occurrence of one or more intervening events during the normal operation of the surgical instrument, and said bailout assembly comprising: a bailout handle, said bailout handle operable to move said drive member to effectuate a bailout motion in said end effector; characterised in that the bailout assembly further comprises a controller, wherein the controller comprises: a memory; and a processor coupled to said memory, said processor configured to detect said bailout error when one or more bailout errors signals are received by the processor, wherein said processor is programed to stop said motor in response to said detection of said bailout error. an end effector; a drive member movable to effectuate a motion in said end effector; a motor operable to move said drive member to effectuate said motion in said end effector; and a bailout assembly operable to perform a mechanical bailout of said surgical instrument in response to a bailout error, said bailout error defining the occurrence of one or more intervening events during the normal operation of the surgical instrument, and said bailout assembly comprising: a bailout handle, said bailout handle operable to move said drive member to effectuate a bailout motion in said end effector; characterised in that the bailout assembly further comprises a controller, wherein the controller comprises: a memory; and a processor coupled to said memory, said processor configured to detect said bailout error when one or more bailout errors signals are received by the processor, wherein said processor is programed to stop said motor in response to said detection of said bailout error. a memory; and a processor coupled to said memory, said processor configured to detect said bailout error when one or more bailout errors signals are received by the processor, wherein said processor is programed to stop said motor in response to said detection of said bailout error.
A flame retardant resin composition comprising: a polycarbonate resin; a silicon impact modifier; and a flame retardant, wherein the silicon impact modifier is particles having a core-shell structure and comprising 60 wt% or more of a siloxane polymer, and the flame retardant comprises a mixture of magnesium carbonate represented by Formula 1 and magnesium calcium carbonate represented by Formula 2. [Formula 1] Mg a (CO 3) b 2a-2b ·cH 2 O, wherein a is 1 to 6, b is 0 to 5, and c is 0 to 6; [Formula 2] Mg x Ca y (CO 3) x+y ·mH 2 O, wherein x and y are each independently 1 to 5, and m is 0 to 5.
A sweetener composition comprising a sensory modifying amount of one or more of compounds SG201, SG203, or SG204 according to the following structures: Compound SG201 Compound SG203 or Compound SG204 and an amount of one or more of Reb M, Reb D, Reb B or Reb A, wherein one or more of compounds SG201, SG203, or SG204 is present in the composition in an amount in the range of 0.05 % to 10 % (wt) of a total amount of steviol glycosides in the composition, wherein said amount of each of the SG201, SG203 and SG204, individually or in combination, modifies at least one sensory characteristic relative to the composition with only one or more of Reb M, Reb D, Reb B or Reb A.
A pneumatic cleaning gun comprising the following: - a gun housing comprising a gun body and a liquid nozzle, the liquid nozzle being connected to the gun body; - a nozzle jacket comprising a mounting sleeve and a jacket sleeve, the mounting sleeve being mounted on the gun body of the gun housing and the jacket sleeve being rotatably mounted on the mounting sleeve and surrounding the jacketed flow channel, the liquid nozzle being present in the interior of the jacketed flow channel of the jacket sleeve; and - an air intake tube rigidly connected to the jacket sleeve, the air intake tube having an air intake opening and the air intake opening leading into the jacketed flow channel, characterized in that the mounting sleeve has a plurality of first positioning constructs; wherein the jacket sleeve has at least one second positioning construct, wherein the jacket sleeve is rotatable relative to the mounting sleeve; wherein each second positioning construct can selectably be engaged in one of the first positioning constructs, so that the air intake tube has a plurality of usage settings. - a gun housing comprising a gun body and a liquid nozzle, the liquid nozzle being connected to the gun body; - a nozzle jacket comprising a mounting sleeve and a jacket sleeve, the mounting sleeve being mounted on the gun body of the gun housing and the jacket sleeve being rotatably mounted on the mounting sleeve and surrounding the jacketed flow channel, the liquid nozzle being present in the interior of the jacketed flow channel of the jacket sleeve; and - an air intake tube rigidly connected to the jacket sleeve, the air intake tube having an air intake opening and the air intake opening leading into the jacketed flow channel,
Food preparation household electrical appliance comprising a base supporting a bowl closed by a removable lid, an arm attached to the base supporting a working tool dipping into the bowl, a motor connected to means (5, 5A) for driving the working tool and a safety device preventing the motor from operating when the lid is not present on the bowl, characterised in that said motor is also connected to a driver (7, 8) adapted to be coupled to a working accessory, such as a mixing receptacle, and in that the appliance comprises a cover attached underneath the arm covering said means (5, 5A) for driving the working tool, said cover comprising actuation means cooperating with the safety device to allow the motor to operate when the cover is present on the arm.
A method of identifying a fault on a digital subscriber line in a telecommunications network, comprising: measuring a signal to noise ratio related parameter associated with the digital subscriber line; identifying variations in the signal to noise ratio related parameter; comparing the signal to noise ratio related parameter with one or more predetermined conditions, wherein the predetermined conditions are based on signal to noise ratio related parameter characteristics associated with a population of lines operating normally; characterised in that the method further comprises measuring a plurality of weather parameters associated with the digital subscriber line, wherein each weather parameter is obtained from a corresponding sensor having an associated location; and if one or more of the predetermined conditions are not met in the comparing step, then determining the degree of correlation between the variations in the signal to noise ratio related parameter with each of the plurality of weather parameters; and identifying a location of a fault on the digital subscriber line as the location associated with the weather sensor that corresponds to the greatest determined degree of correlation. measuring a signal to noise ratio related parameter associated with the digital subscriber line; identifying variations in the signal to noise ratio related parameter; comparing the signal to noise ratio related parameter with one or more predetermined conditions, wherein the predetermined conditions are based on signal to noise ratio related parameter characteristics associated with a population of lines operating normally; characterised in that the method further comprises measuring a plurality of weather parameters associated with the digital subscriber line, wherein each weather parameter is obtained from a corresponding sensor having an associated location; and if one or more of the predetermined conditions are not met in the comparing step, then determining the degree of correlation between the variations in the signal to noise ratio related parameter with each of the plurality of weather parameters; and identifying a location of a fault on the digital subscriber line as the location associated with the weather sensor that corresponds to the greatest determined degree of correlation.