mhurhangee/patent-ind-claim-en huggingface dataset:
A method at an electronic device, the method comprising: receiving a software update notification, wherein the software update notification indicates a security requirement; determining , based on the security requirement, that a network connection is secure for receiving a software update; and downloading the software update using the network connection. receiving a software update notification, wherein the software update notification indicates a security requirement; determining , based on the security requirement, that a network connection is secure for receiving a software update; and downloading the software update using the network connection.
Use of a bacterial biofilm, or of at least one hydrophobicity-conveying component of a bacterial biofilm for the preparation of a hydrophobic cement-based material composition.
A catalytic reactor for chemical reactions, comprising a reactor shell and a reactor support ring or support structure fixed to the inner side of the reactor shell and further comprising a load distributor assembly with load transfer means to transfer a load from the load distributor assembly to the reactor support ring or support structure, wherein said load distributor assembly is adapted to support said load transfer means on the upper side of the reactor support ring or support structure and adjacent to the inner side of the reactor shell, and wherein the load distributor assembly comprises circumference adjusting means which enables the outer circumference of the load distributor assembly to fit the inner side of the reactor shell, the load transfer means comprises a plurality of individually adjustably distribution members, adapted to be adjusted to fit the upper side of the reactor support ring or support structure, the load transfer means comprises a plurality of individually adjustable distribution members, adapted to be adjusted to fit the inner side of the reactor shell, and the position of the load transfer means relative to the load distributor assembly is adapted to be adjusted by load transfer adjusting means.
A method of forming a joint between a coaxial cable and a coaxial connector, comprising the steps of: preparing a cable having an inner conductor , a dielectric layer surrounding the inner conductor , a corrugated outer conductor surrounding the dielectric layer , and a jacket surrounding the outer conductor such that an end of the inner conductor is exposed, an end of the outer conductor is exposed and is flattened to form a ring devoid of corrugations, and a portion of the end of the dielectric layer is cored out to form a solder chamber between the inner conductor and the ring of the outer conductor ; preparing an assembly comprising a coaxial connector and a solder preform , the coaxial connector comprising an inner contact , a dielectric spacer , and an outer conductor body having a tail , the solder preform encircling the tail ; inserting the tail and solder preform into the solder chamber ; and melting the solder preform to create a joint between the ring of the outer conductor and the tail of the outer conductor body . preparing a cable having an inner conductor , a dielectric layer surrounding the inner conductor , a corrugated outer conductor surrounding the dielectric layer , and a jacket surrounding the outer conductor such that an end of the inner conductor is exposed, an end of the outer conductor is exposed and is flattened to form a ring devoid of corrugations, and a portion of the end of the dielectric layer is cored out to form a solder chamber between the inner conductor and the ring of the outer conductor ; preparing an assembly comprising a coaxial connector and a solder preform , the coaxial connector comprising an inner contact , a dielectric spacer , and an outer conductor body having a tail , the solder preform encircling the tail ; inserting the tail and solder preform into the solder chamber ; and melting the solder preform to create a joint between the ring of the outer conductor and the tail of the outer conductor body .
A heat exchanger including multiple hollow fiber membranes that each have a hollow portion through which a heat medium (H) can pass, and exhibiting a shape of a cylinder body as a whole shape in which the multiple hollow fiber membranes are integrated, wherein each of the hollow fiber membranes is tilted with respect to a central axis (O) of the cylinder body and is wound around the central axis (O) of the cylinder body , wherein a tilt angle θ with respect to the central axis (O) of the cylinder body of each of the hollow fiber membranes ranges from 22° to smaller than 67°, and wherein a constituent material of each of the hollow fiber membranes has a Young's modulus E of 2.6 GPa or smaller. wherein each of the hollow fiber membranes is tilted with respect to a central axis (O) of the cylinder body and is wound around the central axis (O) of the cylinder body , wherein a tilt angle θ with respect to the central axis (O) of the cylinder body of each of the hollow fiber membranes ranges from 22° to smaller than 67°, and wherein a constituent material of each of the hollow fiber membranes has a Young's modulus E of 2.6 GPa or smaller.
A method for moving a first and a second drivetrain component in a nacelle of a horizontal axis wind turbine, the nacelle comprising a nacelle structure , the components being connected, in operation of the wind turbine, to a rotor of the wind turbine, the method comprising - connecting a first drive unit between a first location, fixed to the nacelle structure, and the first component or a first vehicle connected to the first component, - moving the first component in relation to the nacelle structure by means of the first drive unit in a direction parallel to the rotational axis of the rotor, wherein said first drive unit is a linear actuator, - connecting a second drive unit between a second location, which is different to the first location and fixed to the nacelle structure, and the second component or a second vehicle connected to the second component, and - moving the second component in relation to the nacelle structure by means of the second drive unit in a direction parallel to the rotational axis of the rotor. - connecting a first drive unit between a first location, fixed to the nacelle structure, and the first component or a first vehicle connected to the first component, - moving the first component in relation to the nacelle structure by means of the first drive unit in a direction parallel to the rotational axis of the rotor, wherein said first drive unit is a linear actuator, - connecting a second drive unit between a second location, which is different to the first location and fixed to the nacelle structure, and the second component or a second vehicle connected to the second component, and - moving the second component in relation to the nacelle structure by means of the second drive unit in a direction parallel to the rotational axis of the rotor.
Method for controlling an aircraft of a specific type, especially a multirotor VTOL aircraft having preferably electrically driven rotors , wherein a) prior to a flight, a finite number of nominal trajectories (NT) for the aircraft and a finite number of contingency trajectories (CT) arranged around the nominal trajectories (NT) are calculated and stored in a database available on board the aircraft ; b) prior to a flight, a finite number of type-specific, permissible flight manoeuvres of the aircraft are pre-planned and stored in the database as a manoeuvre library ; c) optionally, prior to a flight, a number of discrete flight levels at different altitudes are defined and stored in the database ; d) during a flight, the database is accessed by means of a computer-aided transition planning algorithm within a real-time algorithm in order, in dependence upon a state of the aircraft detected by sensors , to change between the nominal trajectories (NT) and the contingency trajectories (CT) and optionally between the defined flight levels using the pre-planned flight manoeuvres and to actuate a path-tracking controller and/or a flight controller of the aircraft accordingly; characterised in that prior to the flight, transition intervals and entry and exit intervals (TI, EN, EX) are defined at least for each nominal trajectory (NT); and a change between nominal trajectories and optionally between flight levels is permissible only within those transition intervals and entry and exit intervals (TI, EN, EX). a) prior to a flight, a finite number of nominal trajectories (NT) for the aircraft and a finite number of contingency trajectories (CT) arranged around the nominal trajectories (NT) are calculated and stored in a database available on board the aircraft ; b) prior to a flight, a finite number of type-specific, permissible flight manoeuvres of the aircraft are pre-planned and stored in the database as a manoeuvre library ; c) optionally, prior to a flight, a number of discrete flight levels at different altitudes are defined and stored in the database ; d) during a flight, the database is accessed by means of a computer-aided transition planning algorithm within a real-time algorithm in order, in dependence upon a state of the aircraft detected by sensors , to change between the nominal trajectories (NT) and the contingency trajectories (CT) and optionally between the defined flight levels using the pre-planned flight manoeuvres and to actuate a path-tracking controller and/or a flight controller of the aircraft accordingly;
Flow conditioner comprising a perforated plate with a central hole and four or more circular paths (2-5) arranged in a radial manner in relation to the central hole, said paths being arranged concentrically in relation to one another, wherein holes (8-11) are arranged on these concentric circular paths (2-5), wherein the majority of the holes of a central circular path have a larger hole diameter in relation to the majority of the holes of the innermost circular path and the majority of the holes of the outermost circular path , and that, starting from the central hole , the innermost circular path is arranged with multiple holes , wherein the ratio r 8 /Di, i.e. the ratio of the radius of a hole of this innermost circular path to Di, the total diameter of the perforated plate , is 2-10% greater than the ratio r 1 /Di, i.e. the ratio of the radius of the central hole to Di, the total diameter of the perforated plate .
A railway braking system including a body delimiting a service brake pressure chamber and/or a parking brake pressure chamber , a parking brake movable relative to said body, a part for unlocking said parking brake connected to said parking brake pressure chamber and accessible from outside said body, and a parking brake indicator device , characterised in that said indicator device is configured to receive a first piece of information representative of a position of said unlocking part , via a state line configured to be connected to said unlocking part , and at least one second piece of information representative of the supply and/or emptying of said service brake pressure chamber and/or of said parking brake pressure chamber , via at least one other state line configured to be connected to a service brake and/or parking brake line, said first piece of information being processed in combination with said at least one second piece of information so as to detect and indicate an engaged state or a released state of said parking brake .
A compound represented by formula (I) or a pharmaceutically acceptable salt thereof, wherein, n is selected from 0, 1, 2 and 3; R 1 is selected from H, halogen, OH, NH 2 , CN, C 3-6 cycloalkyl, C 1-6 alkyl, and C 1-6 alkoxy and the NH 2 , C 3-6 cycloalkyl, C 1-6 alkyl and C 1-6 alkoxy are optionally substituted with 1, 2 or 3 R a ; ring A is selected from 5- to 6-membered heteroaryl, phenyl, C 4-6 cycloalkyl, and 4- to 7-membered heterocycloalkyl; R a is independently selected from F, Cl, Br, I, OH, NH 2 , C 1-10 alkylamino, C 1-10 alkoxy, -C(=O)O-C 1-10 alkyl, 4- to 10-membered heterocycloalkyl, 4- to 10-membered heterocycloalkylamino, C 4-7 cycloalkylamino, C 4-7 cycloalkylmethylamino, wherein the NH 2 , C 1-10 alkylamino, C 1-10 alkoxy, -C(=O)O-C 1-10 alkyl, 4- to 10-membered heterocycloalkyl, 4-to 10-membered heterocycloalkylamino, C 4-7 cycloalkylamino and C 4-7 cycloalkylmethylamino are optionally substituted with 1, 2 or 3 R; R is independently selected from F, Cl, Br, I, OH, NH 2 , Me, and the 5- to 6-membered heteroaryl, 4- to 7-membered heterocycloalkyl, 4- to 10-membered heterocycloalkyl and 4- to 10-membered heterocycloalkylamino comprise 1, 2, 3 or 4 heteroatoms or heteroatom groups independently selected from -NH-, -O-, -S-, and N, respectively. n is selected from 0, 1, 2 and 3; R 1 is selected from H, halogen, OH, NH 2 , CN, C 3-6 cycloalkyl, C 1-6 alkyl, and C 1-6 alkoxy and the NH 2 , C 3-6 cycloalkyl, C 1-6 alkyl and C 1-6 alkoxy are optionally substituted with 1, 2 or 3 R a ; ring A is selected from 5- to 6-membered heteroaryl, phenyl, C 4-6 cycloalkyl, and 4- to 7-membered heterocycloalkyl; R a is independently selected from F, Cl, Br, I, OH, NH 2 , C 1-10 alkylamino, C 1-10 alkoxy, -C(=O)O-C 1-10 alkyl, 4- to 10-membered heterocycloalkyl, 4- to 10-membered heterocycloalkylamino, C 4-7 cycloalkylamino, C 4-7 cycloalkylmethylamino, wherein the NH 2 , C 1-10 alkylamino, C 1-10 alkoxy, -C(=O)O-C 1-10 alkyl, 4- to 10-membered heterocycloalkyl, 4-to 10-membered heterocycloalkylamino, C 4-7 cycloalkylamino and C 4-7 cycloalkylmethylamino are optionally substituted with 1, 2 or 3 R; R is independently selected from F, Cl, Br, I, OH, NH 2 , Me, and the 5- to 6-membered heteroaryl, 4- to 7-membered heterocycloalkyl, 4- to 10-membered heterocycloalkyl and 4- to 10-membered heterocycloalkylamino comprise 1, 2, 3 or 4 heteroatoms or heteroatom groups independently selected from -NH-, -O-, -S-, and N, respectively.
A veneer panel , comprising: a non-flame retardant-treated face veneer ; a two-ply panel bonded to the face veneer, the two-ply panel comprising a first inner layer bonded to the face veneer and a second inner layer bonded to the first inner layer , wherein the first inner layer and the second inner layer are treated with a flame retardant; a thermally conductive backing layer bonded to the two-ply panel , the thermally conductive backing layer disposed opposite the two-ply panel from the face veneer ; and a first adhesive material disposed between the face veneer and the two-ply panel, wherein the first adhesive material bonds the two-ply panel to a back surface of the face veneer; a second adhesive material disposed between the thermally conductive backing layer and the two-ply panel, wherein the second adhesive material bonds the two-ply panel to the thermally conductive backing layer; and a third adhesive material between the first inner layer and the second inner layer ; wherein the first adhesive material comprises a phenolic adhesive and the second adhesive material comprises an acrylic adhesive, and wherein the two-ply panel comprises wood. a non-flame retardant-treated face veneer ; a two-ply panel bonded to the face veneer, the two-ply panel comprising a first inner layer bonded to the face veneer and a second inner layer bonded to the first inner layer , wherein the first inner layer and the second inner layer are treated with a flame retardant; a thermally conductive backing layer bonded to the two-ply panel , the thermally conductive backing layer disposed opposite the two-ply panel from the face veneer ; and a first adhesive material disposed between the face veneer and the two-ply panel, wherein the first adhesive material bonds the two-ply panel to a back surface of the face veneer; a second adhesive material disposed between the thermally conductive backing layer and the two-ply panel, wherein the second adhesive material bonds the two-ply panel to the thermally conductive backing layer; and a third adhesive material between the first inner layer and the second inner layer ; wherein the first adhesive material comprises a phenolic adhesive and the second adhesive material comprises an acrylic adhesive, and wherein the two-ply panel comprises wood.
A manufacturing method of a turbine rotor blade, in a manufacturing method of a turbine rotor blade using an Ni-based forged alloy, comprising: a softening process (S1) of increasing a γ' phase incoherent with a γ phase that is a matrix phase in the Ni-based forged alloy; a first working process (S21) of forming at least two members constituting a rotor blade by using the Ni-based forged alloy after subjected to the softening process; a second working process (S22) of forming cooling structural parts in the respective members; and a third working process (S23) of joining the members by friction stir welding, wherein the cooling structural parts in the respective members are formed in the second working process such that, after being joined in the third working process, they form together a cooling flow passage in the rotor blade. a softening process (S1) of increasing a γ' phase incoherent with a γ phase that is a matrix phase in the Ni-based forged alloy; a first working process (S21) of forming at least two members constituting a rotor blade by using the Ni-based forged alloy after subjected to the softening process; a second working process (S22) of forming cooling structural parts in the respective members; and a third working process (S23) of joining the members by friction stir welding, wherein the cooling structural parts in the respective members are formed in the second working process such that, after being joined in the third working process, they form together a cooling flow passage in the rotor blade.
A method for detecting a utility meter having been tampered with, the meter comprising a flow measurement portion in which flow of water is measured, the method characterized by : detecting a presence of air in the flow measurement portion ; evaluating a fraud condition, wherein the fraud condition comprises that air is present in the flow measurement portion for a first period of time or more, and that a pressure in the flow measurement portion is below a given pressure; and generating an alert in response to the fraud condition being evaluated as met. detecting a presence of air in the flow measurement portion ; evaluating a fraud condition, wherein the fraud condition comprises that air is present in the flow measurement portion for a first period of time or more, and that a pressure in the flow measurement portion is below a given pressure; and generating an alert in response to the fraud condition being evaluated as met.
A white carbonatable calcium silicate cement composition, comprising: one or more discrete crystalline calcium silicate phases selected from CS (wollastonite or pseudowollastonite), C3S2 (rankinite), C2S (belite, larnite, bredigite), and an amorphous calcium silicate phase, wherein the one or more discrete crystalline calcium silicate phases form about 30% or more by mass of the total phases, and wherein elemental Ca and elemental Si are present in the composition at a molar ratio from about 0.8 to about 1.2; metal oxides of Al, Fe and Mg are present at about 30% or less by mass; the total color-imparting oxides of one or more of metals selected from Fe, Ti, Mn and Cr are present in an amount of less than about 1.5% by mass of the total cement composition; wherein the cement composition is characterized by a reflectance value (L*), as measured from the Hunter L*a*B color scale, of greater than about 85%; and wherein each of the crystalline and amorphous phases is suitable for carbonation with CO 2 . one or more discrete crystalline calcium silicate phases selected from CS (wollastonite or pseudowollastonite), C3S2 (rankinite), C2S (belite, larnite, bredigite), and an amorphous calcium silicate phase, wherein the one or more discrete crystalline calcium silicate phases form about 30% or more by mass of the total phases, and wherein elemental Ca and elemental Si are present in the composition at a molar ratio from about 0.8 to about 1.2; metal oxides of Al, Fe and Mg are present at about 30% or less by mass; the total color-imparting oxides of one or more of metals selected from Fe, Ti, Mn and Cr are present in an amount of less than about 1.5% by mass of the total cement composition; wherein the cement composition is characterized by a reflectance value (L*), as measured from the Hunter L*a*B color scale, of greater than about 85%; and wherein each of the crystalline and amorphous phases is suitable for carbonation with CO 2 .
An atmospheric pressure plasma device comprising: a plasma head ; a gas tube configured to supply a gas to the plasma head ; a flow rate controller configured to control a flow rate of the gas supplied to the gas tube ; a pressure sensor arranged downstream of the flow rate controller and configured to detect a pressure in the gas tube ; a determining section configured to determine a state of the device based on how the pressure in the gas tube deviates from a standard value specified for each flow rate of the supplied gas, wherein the determining section is configured to determine the state of the device as abnormal when the pressure in the gas tube is equal to or lower than the standard value, characterized in that: the determining section is configured to determine a leakage amount of the gas according to a decompression amount of the gas, wherein the extent of gas leakage is determinable by the degree of pressure drop with respect to the standard value specified for each flow rate of the supplied gas. a plasma head ; a gas tube configured to supply a gas to the plasma head ; a flow rate controller configured to control a flow rate of the gas supplied to the gas tube ; a pressure sensor arranged downstream of the flow rate controller and configured to detect a pressure in the gas tube ; a determining section configured to determine a state of the device based on how the pressure in the gas tube deviates from a standard value specified for each flow rate of the supplied gas, wherein the determining section is configured to determine the state of the device as abnormal when the pressure in the gas tube is equal to or lower than the standard value,
A floor construction comprising a floor including a gap and a rigid thermal insulation element , characterized in that the floor is formed by concrete slabs , whereas the gap extends between two neighbouring slabs , in which gap the rigid thermal insulation element is mounted, wherein the insulation element comprises an upper side and an opposite lower side , wherein the insulation element is provided with at least one groove extending from the lower side toward the upper side and ending at a groove bottom so as to form tongues at both sides of the groove , which are mutually pivotable about a pivoting axis extending between the groove bottom and the upper side , wherein the upper side of the insulation element extends below an upper surface of the concrete slabs adjacent to the gap and the remaining space between the slabs and above the insulation element is filled with concrete.
Semiconductor component comprising a MESA-shaped bipolar semiconductor chip , wherein a first metallization layer is arranged on a first main surface of the semiconductor chip and a second metallization layer is arranged on a second main surface of the semiconductor chip , said second main surface being arranged opposite the first main surface of the semiconductor chip , characterized in that an aluminium oxide layer is arranged on an edge surface of the semiconductor chip that extends circumferentially around the semiconductor chip and connects the first and second main surfaces , wherein the aluminium oxide layer is arranged on the entire edge surface of the semiconductor chip , wherein a layer consisting of a crosslinked organic material is arranged on the surface of the aluminium oxide layer .