mhurhangee/ep-ind-claims huggingface dataset:
A mobile terminal control apparatus comprising: a device control unit that is arranged to detect whether plural mobile terminals are connected or not and that is arranged to hold device information and application information in a connection history; and an application control unit that is arranged to determine an application to be controlled, out of plural applications held on the connected mobile terminals, on the basis of the connection history and an application DB, wherein, if it is determined that plural mobile terminals are connected when connection of a mobile terminal is detected, the application control unit is arranged to acquire a controlled application ID of a controlled application that is under control in an already connected mobile terminal, to acquire a held application ID of a held application that is held on the mobile terminal detected as connected from the connection history, to determine whether a category of the controlled application and a category of the held application match each other or not, and to decide the held application that is determined as different in category from the controlled application as a control target; the connection history being a history of control of the device information and the application information of the connected mobile terminals, and the application DB being a list holding a list of controllable application IDs by each category indicating a type of application. a device control unit that is arranged to detect whether plural mobile terminals are connected or not and that is arranged to hold device information and application information in a connection history; and an application control unit that is arranged to determine an application to be controlled, out of plural applications held on the connected mobile terminals, on the basis of the connection history and an application DB, wherein, if it is determined that plural mobile terminals are connected when connection of a mobile terminal is detected, the application control unit is arranged to acquire a controlled application ID of a controlled application that is under control in an already connected mobile terminal, to acquire a held application ID of a held application that is held on the mobile terminal detected as connected from the connection history, to determine whether a category of the controlled application and a category of the held application match each other or not, and to decide the held application that is determined as different in category from the controlled application as a control target; the connection history being a history of control of the device information and the application information of the connected mobile terminals, and the application DB being a list holding a list of controllable application IDs by each category indicating a type of application.
A system for data processing with management of a cache consistency in a network (14, 16) of processors (μP 1, μP 2,..., μP 16) equipped with cache memories (L2, L1 1, L1 2,..., L1 16), said network (14, 16) having a main memory shared between the processors and comprising a plurality of nodes (N; 16A, 16B, 16C, 16D, 16E, 16F) for access to the main memory interconnected with one another, said system comprising: - a set of directories (18; 18A, 18B, 18C, 18D, 18E, 18F) distributed between the nodes (N; 16A, 16B, 16C, 16D, 16E, 16F) of the network (14, 16), each directory comprising a table of correspondence between cache lines and information fields on said cache lines, - a first sub-network for interconnection of the nodes (N; 16A, 16B, 16C, 16D, 16E, 16F) with one another implementing a first message transmission protocol, this first protocol providing read/write access to the correspondence tables of the directories (18; 18A, 18B, 18C, 18D, 18E, 18F) during any passage, in the corresponding nodes, of a message passing through this first sub-network, and - a second sub-network for interconnection of the nodes (N; 16A, 16B, 16C, 16D, 16E, 16F) with one another, different from the first sub-network, implementing a second message transmission protocol, characterized in that this second protocol excludes any read/write access to the correspondence tables of the directories (18; 18A, 18B, 18C, 18D, 18E, 18F) during any passage, in the corresponding nodes, of a message passing through this second sub-network. - a set of directories (18; 18A, 18B, 18C, 18D, 18E, 18F) distributed between the nodes (N; 16A, 16B, 16C, 16D, 16E, 16F) of the network (14, 16), each directory comprising a table of correspondence between cache lines and information fields on said cache lines, - a first sub-network for interconnection of the nodes (N; 16A, 16B, 16C, 16D, 16E, 16F) with one another implementing a first message transmission protocol, this first protocol providing read/write access to the correspondence tables of the directories (18; 18A, 18B, 18C, 18D, 18E, 18F) during any passage, in the corresponding nodes, of a message passing through this first sub-network, and - a second sub-network for interconnection of the nodes (N; 16A, 16B, 16C, 16D, 16E, 16F) with one another, different from the first sub-network, implementing a second message transmission protocol,
A process for producing at least one of tetrafluoroethylene and hexafluoropropylene, comprising: pyrolyzing a low molecular weight fluorine compound by continuous reaction in a microreactor, wherein the low molecular weight fluorine compound is a perfluoroalkene and the pyrolysis is performed in the temperature range of 620°C to 720°C.
A power steering system for a vehicle having at least one steered axle joining two wheels (8, 8a, 8b), the power steering system comprising a first steering mechanism designed to control the steering of at least one of the wheels, and comprising: - a mechanical transmission of the movement from a steering wheel of the vehicle to at least one of the wheels by means of an upper steering arm, wherein the mechanical movement is transmitted to the second wheel by the means of a lower steering arm and a track rod; - a first actuator controlled by a parameter related to the steering wheel movement and capable of providing a steering assistance effort to at least one of the wheels; - a second steering mechanism designed to control the steering of at least one of the wheels of said same axle, said second steering mechanism including a second actuator capable of providing a steering assistance effort to at least one of the wheels of said axle, the second actuator having: - a housing which is secured to the axle; - a first and a second piston rod (35, 36) able to slide through the housing and extending, on opposite sides, from inside to outside of the housing, with said piston rods being substantially parallel to said axle, and wherein said piston rods form part of the track rod. - a mechanical transmission of the movement from a steering wheel of the vehicle to at least one of the wheels by means of an upper steering arm, wherein the mechanical movement is transmitted to the second wheel by the means of a lower steering arm and a track rod; - a first actuator controlled by a parameter related to the steering wheel movement and capable of providing a steering assistance effort to at least one of the wheels; - a second steering mechanism designed to control the steering of at least one of the wheels of said same axle, said second steering mechanism including a second actuator capable of providing a steering assistance effort to at least one of the wheels of said axle, the second actuator having: - a housing which is secured to the axle; - a first and a second piston rod (35, 36) able to slide through the housing and extending, on opposite sides, from inside to outside of the housing, with said piston rods being substantially parallel to said axle, and wherein said piston rods form part of the track rod.
A preparation method of a super absorbent polymer, comprising the steps of: cross-linking an acrylic acid-based monomer having at least partially neutralized acidic groups in the presence of an internal cross-linking agent to form a hydrogel polymer; drying the hydrogel polymer to form a base resin; and heating the base resin in the presence of a surface cross-linking agent to perform surface modification to the base resin, wherein the internal cross-linking agent contains a compound represented by the following Chemical Formula 1: wherein, in Chemical Formula 1, R1 and R2 are each independently hydrogen or methyl, R3 and R4 are each independently a C1 to C20 alkyl, R5 is a linear or branched C1 to C20 alkylene substituted with a linear or branched C2 to C10 alkenyl, or a linear or branched C2 to C20 alkenylene, and n is an integer of 0 to 10. cross-linking an acrylic acid-based monomer having at least partially neutralized acidic groups in the presence of an internal cross-linking agent to form a hydrogel polymer; drying the hydrogel polymer to form a base resin; and heating the base resin in the presence of a surface cross-linking agent to perform surface modification to the base resin, wherein the internal cross-linking agent contains a compound represented by the following Chemical Formula 1: R1 and R2 are each independently hydrogen or methyl, R3 and R4 are each independently a C1 to C20 alkyl, R5 is a linear or branched C1 to C20 alkylene substituted with a linear or branched C2 to C10 alkenyl, or a linear or branched C2 to C20 alkenylene, and n is an integer of 0 to 10.
A computer-implemented method of controlling an aircraft at high angles of attack, the method comprising: measuring an actual angle of attack (α) for the aircraft; calculating a short term alpha (α1) which is equal to or less than alpha stall; calculating a long term alpha (α2) which is less than the short term alpha (α1) and which is coincident with the ceiling of the aircraft operational envelope or a predetermined angle of attack associated with optimum aerodynamic performance to maximize an aircraft energy state; calculating an activation alpha (α3) which is less than the short term alpha (α1) and is less than, equal to, or greater than the long term alpha (α2); determining if the actual angle of attack (α) is greater than the activation alpha (α3); limiting the actual angle of attack (α) to the short term alpha (α1) if the actual angle of attack (α) is greater than the activation alpha (α3); evaluating if a predetermined criteria has been met; and limiting the actual angle of attack (α) to the long term alpha (α2) if the predetermined criteria have been met. measuring an actual angle of attack (α) for the aircraft; calculating a short term alpha (α1) which is equal to or less than alpha stall; calculating a long term alpha (α2) which is less than the short term alpha (α1) and which is coincident with the ceiling of the aircraft operational envelope or a predetermined angle of attack associated with optimum aerodynamic performance to maximize an aircraft energy state; calculating an activation alpha (α3) which is less than the short term alpha (α1) and is less than, equal to, or greater than the long term alpha (α2); determining if the actual angle of attack (α) is greater than the activation alpha (α3); limiting the actual angle of attack (α) to the short term alpha (α1) if the actual angle of attack (α) is greater than the activation alpha (α3); evaluating if a predetermined criteria has been met; and limiting the actual angle of attack (α) to the long term alpha (α2) if the predetermined criteria have been met.
A glass fiber-reinforced resin molded article, wherein glass fiber included in the glass fiber-reinforced resin molded article comprises a flat cross-sectional shape having a minor axis D1 in a range of 3.0 to 6.4 μm and a major axis D2 in a range of 11.0 to 26.0 μm, a number average fiber length L (μm) of the glass fiber included in the glass fiber-reinforced resin molded article is in a range of 150 to 300 μm, a glass fiber content C (wt%) in the glass fiber-reinforced resin molded article is in a range of 40.0 to 65.0 wt%, and the D1, D2, L, and C satisfy following formula: 260.0 ≤ C 2 × L / D 1 × D 2 2 ≤ 400.0 glass fiber included in the glass fiber-reinforced resin molded article comprises a flat cross-sectional shape having a minor axis D1 in a range of 3.0 to 6.4 μm and a major axis D2 in a range of 11.0 to 26.0 μm, a number average fiber length L (μm) of the glass fiber included in the glass fiber-reinforced resin molded article is in a range of 150 to 300 μm, a glass fiber content C (wt%) in the glass fiber-reinforced resin molded article is in a range of 40.0 to 65.0 wt%, and the D1, D2, L, and C satisfy following formula: 260.0 ≤ C 2 × L / D 1 × D 2 2 ≤ 400.0
Method for producing a roadway structure, comprising the steps (i) applying pellets of an adhesive composition to a non-tacky surface of a substrate comprising a support structure, preferably a concrete structure or asphalt structure, wherein the adhesive composition comprises at least one solid epoxy resin and at least one thermoplastic polymer that is solid at room temperature; and (ii) applying a bitumen-based bearing course, characterized in that the non-tacky surface of the substrate is formed of concrete, asphalt, or a bitumen membrane, wherein the pellets have a diameter in a range from 1 to 3 mm and wherein the amount of pellets applied is in the range from 50 to 300 g/m 2. (i) applying pellets of an adhesive composition to a non-tacky surface of a substrate comprising a support structure, preferably a concrete structure or asphalt structure, wherein the adhesive composition comprises at least one solid epoxy resin and at least one thermoplastic polymer that is solid at room temperature; and (ii) applying a bitumen-based bearing course, characterized in that the non-tacky surface of the substrate is formed of concrete, asphalt, or a bitumen membrane, wherein the pellets have a diameter in a range from 1 to 3 mm and wherein the amount of pellets applied is in the range from 50 to 300 g/m 2.
A method of generating derived cryptographic keys for a reversible symmetric cryptographic algorithm enciphering /deciphering information blocks, implemented within a security microprocessor, wherein derived key K' is generated within the security microprocessor by a key derivation function KDF from a permanent master key K, a variable parameter X on which the derived key will depend and an additional salt parameter S, with K':= KDF(K,X,S), characterized in that the key derivation function KDF is: KDF K X S: = F K X S ⊕ F K, X, ∼ S where: - F(K,X,S) = E K (X ⊕ Y), wherein E K is a cryptographic function, controlled by key K, of said reversible enciphering/deciphering algorithm implemented within the security microprocessor, - the notation U ⊕ V denotes a commutative operation that, when performed on operands U and V, gives a result independent of the order of these operands, and - the notation ∼U denotes an involutive operation that when performed on an operand U gives a result such that ∼(∼U) = U, from the group comprised of: bitwise complement of U; sign change of U; exclusive OR of U with a constant; an involutive bit permutation of U; and a combination of distinct operations chosen among the preceding operations, and in that each calculation of the function KDF(K,X,S) comprises the following steps, performed by the security microprocessor: a) randomly selecting a variable T:= S or T:= ~S; b) calculating K' 1:= F(K,X,T) and K' 2:= F(K,X,∼T); and c) combining K' 1 and K' 2 to produce the derived key K':= K' 1 ⊕ K' 2, so that the value of the produced result is independent of the selection made at step a), whereas the values handled at step b) depend thereon. - F(K,X,S) = E K (X ⊕ Y), wherein E K is a cryptographic function, controlled by key K, of said reversible enciphering/deciphering algorithm implemented within the security microprocessor, - the notation U ⊕ V denotes a commutative operation that, when performed on operands U and V, gives a result independent of the order of these operands, and - the notation ∼U denotes an involutive operation that when performed on an operand U gives a result such that ∼(∼U) = U, from the group comprised of: bitwise complement of U; sign change of U; exclusive OR of U with a constant; an involutive bit permutation of U; and a combination of distinct operations chosen among the preceding operations, a) randomly selecting a variable T:= S or T:= ~S; b) calculating K' 1:= F(K,X,T) and K' 2:= F(K,X,∼T); and c) combining K' 1 and K' 2 to produce the derived key K':= K' 1 ⊕ K' 2, so that the value of the produced result is independent of the selection made at step a), whereas the values handled at step b) depend thereon.
A non-crosslinked natural rubber latex composition for an inflatable stopper comprising a homogeneous mixture of: a) natural rubber latex; b) a surfactant; c) an amine based chemical antiozonant; d) ammonia. a) natural rubber latex; b) a surfactant; c) an amine based chemical antiozonant; d) ammonia.
An object detecting device comprising: a light source; a deflector which deflects light from the light source in a first direction; and an optical detector which includes a plurality of light receiving units and receives light deflected by the deflector and reflected by an object, characterized in that the light source includes a plurality of light emitting units arranged in a second direction which is orthogonal to the first direction, the plurality of light receiving units are arranged in the second direction so as to correspond to the plurality of light emitting units, the plurality of light emitting units includes a plurality of light emitting unit groups each formed of at least two light emitting units which are electrically connected to each other for simultaneously turning on the at least two light emitting units, and the at least two light emitting units correspond to different light receiving units of the plurality of light receiving units. a light source; a deflector which deflects light from the light source in a first direction; and an optical detector which includes a plurality of light receiving units and receives light deflected by the deflector and reflected by an object, characterized in that the light source includes a plurality of light emitting units arranged in a second direction which is orthogonal to the first direction, the plurality of light receiving units are arranged in the second direction so as to correspond to the plurality of light emitting units, the plurality of light emitting units includes a plurality of light emitting unit groups each formed of at least two light emitting units which are electrically connected to each other for simultaneously turning on the at least two light emitting units, and the at least two light emitting units correspond to different light receiving units of the plurality of light receiving units.
A system with - a radiographic device for recording a radiograph on an imaging plate and - a readout device for the imaging plate, wherein the imaging plate comprises a data carrier, wherein the radiographic device and/or the readout device includes a data device (18, 20) with a write/read device for writing imaging parameters related to the radiograph to the data carrier and for reading information stored on the data carrier, wherein the write/read device is configured to transmit the information, which has been read, to the readout device, so that the imaging parameters used for the recording of the radiograph are available to the readout device for a readout of the imaging plate prior to the readout process, and wherein the readout of the imaging plate can be adapted to the imaging parameters. - a radiographic device for recording a radiograph on an imaging plate and - a readout device for the imaging plate, wherein the imaging plate comprises a data carrier, wherein
A drain mast configured to be positioned in an aircraft enclosure comprising an aircraft engine cowling surrounding an aircraft engine, the drain mast being configured to drain fluids from the aircraft enclosure, the drain mast having: a self-supporting tube section configured to be positioned within the aircraft enclosure, the tube section including a plurality of generally aligned fluid passages extending from an upper end to a lower end of the tube section and each fluid passage having a peripheral wall; a substantially aerodynamic fairing configured to extend from the outer surface of the aircraft engine cowling, the fairing including a plurality of fairing fluid passages each of which is connected at one end to a respective fluid passage and at the other end to a respective one of a plurality of fluid outlets located in the fairing, the cross sectional shape of said self-supporting tube section corresponding substantially to the collective width of the plurality of generally aligned fluid passages and their respective peripheral walls so as to minimize said cross sectional shape at a respective position along said tube section, characterized by: each fluid passage having at least a portion of its peripheral wall in common with at least a portion of an adjacent, aligned fluid passage, the upper end of each fluid passage being configured to be in fluid communication with one or more aircraft components a self-supporting tube section configured to be positioned within the aircraft enclosure, the tube section including a plurality of generally aligned fluid passages extending from an upper end to a lower end of the tube section and each fluid passage having a peripheral wall; a substantially aerodynamic fairing configured to extend from the outer surface of the aircraft engine cowling, the fairing including a plurality of fairing fluid passages each of which is connected at one end to a respective fluid passage and at the other end to a respective one of a plurality of fluid outlets located in the fairing, the cross sectional shape of said self-supporting tube section corresponding substantially to the collective width of the plurality of generally aligned fluid passages and their respective peripheral walls so as to minimize said cross sectional shape at a respective position along said tube section, characterized by: each fluid passage having at least a portion of its peripheral wall in common with at least a portion of an adjacent, aligned fluid passage, the upper end of each fluid passage being configured to be in fluid communication with one or more aircraft components
Housing for an electrical appliance comprising - a housing body, which at least partially houses a respective electrical component of the electrical appliance, wherein the housing body has at least one support point for being supported on a respective plate to which the electrical component is connected, - at least one temperature sensor for sensing the temperature of the respective plate, wherein the respective temperature sensor in the housing body is arranged in the region of the respective support point, characterised in that the housing body in each case has a single-pole electrical line to the respective temperature sensor. - a housing body, which at least partially houses a respective electrical component of the electrical appliance, wherein the housing body has at least one support point for being supported on a respective plate to which the electrical component is connected, - at least one temperature sensor for sensing the temperature of the respective plate, wherein the respective temperature sensor in the housing body is arranged in the region of the respective support point,