mhurhangee/ep-ind-claims huggingface dataset:
A microporous membrane comprising 1.0 wt.% to 20.0 wt.% of a first polyethylene having an Mw in the range of from 1.0 x 10 4 to 4.0 x 10 5 a Tso ≤ 130.0°C, a T 25 ≥ 100.0°C, and T 80 -T 25 ≤ 25.0°C, and a T m in the range of from 120.0°C to 129.0°C, the wt.% being based on the weight of the membrane, the microporous membrane further comprising a second polyethylene having an Mw > 1.0 x 10 6 and/or a third polyethylene having an Mw ≤ 1.0 x 10 6 and a Tso > 132.0°C; and wherein the membrane has a shutdown temperature ≤ 130.5°C, a normalized air permeability ≤ 4.5 x 10 2 seconds/100cm 3 /20μm, and a 105°C heat shrinkage in at least one planar direction in the range of ≤ 10.0%; wherein T m is determined by differential scanning calorimetery in accordance with JIS K7122; T 25 is the temperature at which the area of the lower-temperature region of a differential scanning calorimeter curve obtained in accordance with JIS K7122 reaches 25% of the total area of the curve; Tso is the temperature at which the area of the lower-temperature region of a differential scanning calorimeter curve obtained in accordance with JIS K7122 reaches 80% of the total area of the curve; normalized air permeability is measured according to JIS P8117; shutdown temperature is the temperature at which the air permeability first exceeds 100,000 seconds/100cm 3, and is measured according to the method set out in the description; and heat shrinkage is the shrinkage of the membrane when heated at a temperature of 105°C for 8 hours, and is measured according to the method set out in the description.
A modified polyvinyl alcohol comprising a monomer unit represented by formula, and a structural unit represented by formula: wherein in the formula, R 1 represents a hydrogen atom, or a linear or branched alkyl group having 1 to 8 carbon atoms, and R 2 represents -R 3 -SO 3 - X +, -R 3 -N + (R 4) 3 Cl -, or a hydrogen atom, R 3 representing a linear or branched alkanediyl group having 1 to 10 carbon atoms, X representing a hydrogen atom, a metal atom, or an ammonium group, and R 4 representing a linear or branched alkyl group having 1 to 5 carbon atoms, wherein a plurality of R 4 s are identical or different; and wherein in the formula, R 5 represents a hydrogen atom, or a linear or branched alkyl group having 1 to 8 carbon atoms, wherein: a percentage content of the monomer unit represented by the formula with respect to total monomer units in the modified polyvinyl alcohol is 0.05 mol% or greater and 10 mol% or less; a percentage content of the structural unit represented by the formula with respect to the total monomer units in the modified polyvinyl alcohol is 0.001 mol% or greater and 0.5 mol% or less; a viscosity average degree of polymerization is 300 or greater and 3,000 or less; and a degree of saponification is 82 mol% or greater and 99.5 mol% or less, wherein the percentage content of the monomer unit represented by the formula and the percentage content of the structural unit represented by the formula are values determined by dissolving the modified polyvinyl alcohol in D 2 O and carrying out a measurement by using a 600-MHz 1 H-NMR measurement device at 80 °C, the viscosity average degree of polymerization is a value determined by a method defined in JIS-K6726-1994, and the degree of saponification is a value determined by a method defined in JIS-K6726-1994. R 1 represents a hydrogen atom, or a linear or branched alkyl group having 1 to 8 carbon atoms, and R 2 represents -R 3 -SO 3 - X +, -R 3 -N + (R 4) 3 Cl -, or a hydrogen atom, R 3 representing a linear or branched alkanediyl group having 1 to 10 carbon atoms, X representing a hydrogen atom, a metal atom, or an ammonium group, and R 4 representing a linear or branched alkyl group having 1 to 5 carbon atoms, wherein a plurality of R 4 s are identical or different; and wherein in the formula, R 5 represents a hydrogen atom, or a linear or branched alkyl group having 1 to 8 carbon atoms, a percentage content of the monomer unit represented by the formula with respect to total monomer units in the modified polyvinyl alcohol is 0.05 mol% or greater and 10 mol% or less; a percentage content of the structural unit represented by the formula with respect to the total monomer units in the modified polyvinyl alcohol is 0.001 mol% or greater and 0.5 mol% or less; a viscosity average degree of polymerization is 300 or greater and 3,000 or less; and a degree of saponification is 82 mol% or greater and 99.5 mol% or less, wherein
An image capture system for capturing aerial images of the Earth, the image capture system comprising: an airplane; an image capture device (14; 14a) mounted to the airplane, the image capture device having a sensor for capturing an image; a computer system (20; 20a) configured to execute flight management software monitoring the position of the airplane and outputting signals to the image capture device to cause the image capture device to capture images (104, 106); and a detection computer configured to execute an abnormality detection algorithm for detecting an abnormality in an image immediately after the image is captured, the abnormality detection algorithm configured, when the abnormality is present in the captured image, to cause the detection computer to flag the image as bad and to send a signal to the flight management software executed on the computer system to automatically schedule a re-shoot of the image for a future time. an airplane; an image capture device (14; 14a) mounted to the airplane, the image capture device having a sensor for capturing an image; a computer system (20; 20a) configured to execute flight management software monitoring the position of the airplane and outputting signals to the image capture device to cause the image capture device to capture images (104, 106); and a detection computer configured to execute an abnormality detection algorithm for detecting an abnormality in an image immediately after the image is captured, the abnormality detection algorithm configured, when the abnormality is present in the captured image, to cause the detection computer to flag the image as bad and to send a signal to the flight management software executed on the computer system to automatically schedule a re-shoot of the image for a future time.
A method for diagnosing loss and/or distortion of taste or smell in a subject comprising measuring a level of sonic hedgehog in a biological sample from the subject, wherein the biological sample comprises nasal mucus, saliva, or a combination thereof and diagnosing the subject with loss and/or distortion of taste or smell based on the level of SHH in the biological sample that is lower than a threshold level.
A method to improve security or performance of one or more client computers interacting with a plurality of server computers, comprising a first server computer and a second server computer, the method comprising: generating, at the first server computer, a challenge nonce, wherein the challenge nonce corresponds to a challenge state; generating, at the first server computer, the challenge state based on the challenge nonce, wherein the challenge state comprises a set of instructions which, when executed, generates a corresponding response state; sending, from the first server computer, to a first client computer, the challenge nonce and the challenge state, but not the response state; receiving, at the second server computer, from the first client computer, a test nonce and a test response state, determining, at the second server computer, whether the test response state matches the response state based on the test nonce, wherein determining whether the test response state matches the response state based on the test nonce comprises: generating an expected challenge state based on the test nonce; generating an expected response state based on the expected challenge state, the expected response state being generated by executing the set of instructions comprised in the expected challenge state; and determining whether the test response state matches the response state. generating, at the first server computer, a challenge nonce, wherein the challenge nonce corresponds to a challenge state; generating, at the first server computer, the challenge state based on the challenge nonce, wherein the challenge state comprises a set of instructions which, when executed, generates a corresponding response state; sending, from the first server computer, to a first client computer, the challenge nonce and the challenge state, but not the response state; receiving, at the second server computer, from the first client computer, a test nonce and a test response state, generating an expected challenge state based on the test nonce; generating an expected response state based on the expected challenge state, the expected response state being generated by executing the set of instructions comprised in the expected challenge state; and determining whether the test response state matches the response state.
An annular component (1, 2) of supporting at least one bearing, for a turbine engine, in particular for an aircraft, comprising: - two coaxial annular walls, internal and external respectively, these walls delimiting between them an annular gas flow vein and being connected together by an annular row of arms; - an external annular shell extending around the external annular wall, this shell comprising an internal peripheral edge connected to the external annular wall and an external peripheral edge connected to an annular fixing flange, referred to as "external flange"; - an internal annular shell extending inside the internal annular wall, this shell comprising an external peripheral edge connected to the internal annular wall and an internal peripheral edge comprising an annular fixing flange, referred to as the "internal flange"; the annular component (1, 2) being characterised in that at least one of the shells (40, 50) has its external or internal peripheral edge (41, 51) which is connected to the corresponding annular wall (4, 5) and which has a generally corrugated shape around an axis (X-X) of the annular component (1, 2). - two coaxial annular walls, internal and external respectively, these walls delimiting between them an annular gas flow vein and being connected together by an annular row of arms; - an external annular shell extending around the external annular wall, this shell comprising an internal peripheral edge connected to the external annular wall and an external peripheral edge connected to an annular fixing flange, referred to as "external flange"; - an internal annular shell extending inside the internal annular wall, this shell comprising an external peripheral edge connected to the internal annular wall and an internal peripheral edge comprising an annular fixing flange, referred to as the "internal flange";
A control device for providing a reconfigurable operator interface for a medical apparatus, the control device comprising a control surface, control actuators arranged on the control surface and hardware modules (11, 14, 17, 20, 23, 26, 27, 28, 29, 41, 44, 81, 82, 84) arranged side-by-side, wherein the modules (11, 14, 17, 20, 23, 26, 27, 28, 29, 41, 44, 81, 82, 84) are attached to each-other via their adjacent abutting side surfaces (13, 15, 21, 22, 24, 25, 43, 45), the modules (11, 14, 17, 20, 23, 26, 27, 28, 29, 41, 44, 81, 82, 84) comprising - a first terminal module (11, 41, 81) having a closing end surface (12, 42) and an abutting side surface (13, 43) opposite the closing side surface (12, 42), and - a second terminal module (14, 17, 44, 84) having an abutting side surface (15, 45) facing towards the abutting side surface (13, 43) of the first terminal module (11, 41, 81), and an opposite closing end surface (16, 18, 46), characterized in that - the modules (11, 14, 17, 20, 23, 26, 27,28,29,41,44, 81, 82, 84) are attached to each-other via their adjacent abutting side surfaces (13, 15, 21, 22, 24, 25, 43, 45) in a liquid-tight manner, and - the control device comprises means for enabling an operation of the control device only if all the abutting side surfaces (13, 15, 21, 22, 24, 25, 43, 45) in the control device are in an attached state and are attached in a liquid-tight manner. - a first terminal module (11, 41, 81) having a closing end surface (12, 42) and an abutting side surface (13, 43) opposite the closing side surface (12, 42), and - a second terminal module (14, 17, 44, 84) having an abutting side surface (15, 45) facing towards the abutting side surface (13, 43) of the first terminal module (11, 41, 81), and an opposite closing end surface (16, 18, 46), - the modules (11, 14, 17, 20, 23, 26, 27,28,29,41,44, 81, 82, 84) are attached to each-other via their adjacent abutting side surfaces (13, 15, 21, 22, 24, 25, 43, 45) in a liquid-tight manner, and - the control device comprises means for enabling an operation of the control device only if all the abutting side surfaces (13, 15, 21, 22, 24, 25, 43, 45) in the control device are in an attached state and are attached in a liquid-tight manner.
A constant-velocity drive system (219, 295) for an aircraft rotor (207, 209), the rotor (207, 209) being configured for rotation with a rotor mast, the constant-velocity drive system (219, 295) comprising: a gimbal mechanism (221, 297) having a first gimbal (239, 309) and a second gimbal (241, 311) adapted to be driven in rotation by the rotor mast about a mast axis, the first and second gimbals (239, 309, 241, 311) providing for gimballing relative to the mast about gimbal axes (247, 249, 317, 319) that are generally perpendicular to the mast axis; and a differential torque-combining mechanism (223, 299) connected to the gimbal mechanism (221, 297) and configured to be driven in rotation about the mast axis by the gimbal mechanism (221, 297), the differential torque-combining mechanism (223, 299) being capable of gimballing relative to the mast about the gimbal axes (247, 249, 317, 319) and having an output component adapted to be attached to a yoke of the rotor (207, 209) for driving the yoke in rotation with the differential torque-combining mechanism (223, 299). a gimbal mechanism (221, 297) having a first gimbal (239, 309) and a second gimbal (241, 311) adapted to be driven in rotation by the rotor mast about a mast axis, the first and second gimbals (239, 309, 241, 311) providing for gimballing relative to the mast about gimbal axes (247, 249, 317, 319) that are generally perpendicular to the mast axis; and a differential torque-combining mechanism (223, 299) connected to the gimbal mechanism (221, 297) and configured to be driven in rotation about the mast axis by the gimbal mechanism (221, 297), the differential torque-combining mechanism (223, 299) being capable of gimballing relative to the mast about the gimbal axes (247, 249, 317, 319) and having an output component adapted to be attached to a yoke of the rotor (207, 209) for driving the yoke in rotation with the differential torque-combining mechanism (223, 299).
A detergent composition comprising: (i) from 1 to 60 wt.%, preferably from 2 to 50 wt.%, more preferably from 3 to 45 wt.%, even more preferably from 5 to 40 wt.%, most preferably from 6 to 40 wt.% of a surfactant; and, (ii) from 0.0005 to 5 wt.%, preferably from 0.005 to 2.5 wt.%, more preferably from 0.01 to 1 wt.% of a fatty acid amide hydrolase enzyme; wherein the fatty acid amide hydrolase enzyme has at least 70% sequence identity to SEQ ID NO: 1. (i) from 1 to 60 wt.%, preferably from 2 to 50 wt.%, more preferably from 3 to 45 wt.%, even more preferably from 5 to 40 wt.%, most preferably from 6 to 40 wt.% of a surfactant; and, (ii) from 0.0005 to 5 wt.%, preferably from 0.005 to 2.5 wt.%, more preferably from 0.01 to 1 wt.% of a fatty acid amide hydrolase enzyme;
A method of rendering a user interface of an application operating on a computer system, the method comprising: constructing a first data structure by interfacing with the application, the first data structure having first objects associated with the user interface of the application; constructing a second data structure separate from the first data structure, the second data structure having second objects associated with the first objects of the first data structure; determining implicit animations available for automatically animating properties of the second objects; receiving from the application a change for at least one property of at least one of the first objects from a first state to a second state; changing at least one property of the at least one first object from the first state to the second state; determining one of the implicit animations for animating the change of the at least one property for at least one of the second objects associated with the at least one first object from the first state to the second state, the implicit animation being determined independent of the application and based on what the at least one property is that is subject to the change; and rendering from the second data structure for display with the computer system by implementing the determined animation on the at least one property of the at least one second object. constructing a first data structure by interfacing with the application, the first data structure having first objects associated with the user interface of the application; constructing a second data structure separate from the first data structure, the second data structure having second objects associated with the first objects of the first data structure; determining implicit animations available for automatically animating properties of the second objects; receiving from the application a change for at least one property of at least one of the first objects from a first state to a second state; changing at least one property of the at least one first object from the first state to the second state; determining one of the implicit animations for animating the change of the at least one property for at least one of the second objects associated with the at least one first object from the first state to the second state, the implicit animation being determined independent of the application and based on what the at least one property is that is subject to the change; and rendering from the second data structure for display with the computer system by implementing the determined animation on the at least one property of the at least one second object.
A connector assembly for connecting an antenna element to an antenna transmission line, the connector assembly comprising: - an adaptor comprising: - an antenna element attachment portion, for connection of the antenna element to the adaptor, - a signal attachment portion, for connection of a signal conductor of the transmission line to the adaptor, wherein the antenna element attachment portion is in electrical connection with the signal attachment portion, - a ground attachment portion, for connection of a ground conductor of the transmission line to the adaptor, - an impedance matching part, adapted to match the impedance of the antenna element to the antenna transmission line, the connector assembly further comprising: - a shielding metal cage for shielding radio circuits in three spatial dimensions, wherein the adaptor is physically connected to the metal cage and the metal cage is electrically connected to the ground attachment portion of the adaptor, characterised in that: the adaptor and the metal cage form an integral part with a continuous metallic surface constituting both the metal cage and a surface on the adaptor onto which the antenna element attachment portion, the signal attachment portion and the ground attachment portion are formed, wherein the impedance matching part comprises a slit in a portion of the continuous metallic surface with the signal attachment portion positioned on one side of the slit and the ground attachment portion positioned on another side of the slit. - an adaptor comprising: - an antenna element attachment portion, for connection of the antenna element to the adaptor, - a signal attachment portion, for connection of a signal conductor of the transmission line to the adaptor, wherein the antenna element attachment portion is in electrical connection with the signal attachment portion, - a ground attachment portion, for connection of a ground conductor of the transmission line to the adaptor, - an impedance matching part, adapted to match the impedance of the antenna element to the antenna transmission line, - an antenna element attachment portion, for connection of the antenna element to the adaptor, - a signal attachment portion, for connection of a signal conductor of the transmission line to the adaptor, wherein the antenna element attachment portion is in electrical connection with the signal attachment portion, - a ground attachment portion, for connection of a ground conductor of the transmission line to the adaptor, - an impedance matching part, adapted to match the impedance of the antenna element to the antenna transmission line, - a shielding metal cage for shielding radio circuits in three spatial dimensions,
A camera system on a vehicle, comprising: an electronic control unit; a base sensor (24 B), on a first portion of the vehicle, communicating with the electronic control unit; and a remote sensor (24 R1-R6), on a second portion (14, 16) of the vehicle, communicating with the electronic control unit, the electronic control unit associating the remote sensor (24 R1-R6) with the base sensor (24 B) based on respective signals received from the base sensor (24 B) and the remote sensor (24 R1-R6) representing respective measurements of a horizontal physical quantity by the base sensor (24 B) and the remote sensor (24 R1-R6), characterized in that the base sensor (24 B) is an accelerometer and the remote sensor (24 R1-R6) is an accelerometer, and where the horizontal physical quantity is horizontal acceleration. an electronic control unit; a base sensor (24 B), on a first portion of the vehicle, communicating with the electronic control unit; and a remote sensor (24 R1-R6), on a second portion (14, 16) of the vehicle, communicating with the electronic control unit, the electronic control unit associating the remote sensor (24 R1-R6) with the base sensor (24 B) based on respective signals received from the base sensor (24 B) and the remote sensor (24 R1-R6) representing respective measurements of a horizontal physical quantity by the base sensor (24 B) and the remote sensor (24 R1-R6), characterized in that the base sensor (24 B) is an accelerometer and the remote sensor (24 R1-R6) is an accelerometer, and where the horizontal physical quantity is horizontal acceleration.