mhurhangee/ep-ind-claims huggingface dataset:
A fluid flow control device for controlling flow of coolant in a motor vehicle motor cooling system, the flow control device having first and second coolant inlets (241, 242) and first and second coolant outlets (240B, 240R), an outlet valve means and an inlet valve means, the outlet valve means being provided for selectively directing fluid flowing out of the device and comprising an outlet closure member comprising a first closure portion operable to close the first outlet and a second closure portion operable to close the second outlet, the device being operable to actuate the outlet closure member between first and second positions in dependence on a temperature of fluid flowing through the device, in the first position the outlet closure member being arranged to allow fluid to flow out from the device through the first outlet and not through the second outlet, in the second position the outlet closure member being arranged to allow fluid to flow out from the device through the second outlet and not the first outlet, and the inlet valve means being provided for selectively allowing fluid to flow into the device through the second inlet, the inlet valve means being operable between a closed condition in which fluid is prevented from flowing through the inlet valve means by an inlet closure member and an open condition in which fluid is permitted to flow through the inlet valve means the flow control device being operable to selectively allow or prevent flow of coolant into the device through the second inlet in dependence at least in part on the temperature of the fluid flowing through the device, the fluid flow control device being characterised in that the outlet closure member and the inlet closure member are coaxial with each other, wherein at a position intermediate the first and second positions the outlet closure member of the outlet valve means is arranged to allow flow of fluid out from the device through both the first and second outlets (240B, 240R), and wherein when the temperature of fluid flowing through the device is below a first critical temperature the inlet valve means is in the closed condition and the outlet valve means is in the first position, the device being operable to actuate the inlet valve means to assume the open condition but to maintain the outlet valve means in the first position when a temperature of fluid flowing through the first inlet exceeds the first critical temperature.
Apparatus for receiving a broadcast stream, the apparatus comprising: a receiving module (100,500) configured to receive both key information, and additional information relating to a selected programme through the broadcast stream, the key information identifying one of a plurality of control signals received from a remote controller associated with the apparatus for receiving a broadcast signal, wherein the apparatus is pre-programmed to perform different functions for different types of data, and configured to select one of a plurality of predetermined functions based on the type of data identified by additional information, and perform the selected function in response to the control signal of the remote controller identified by the key information; characterized in that: the additional information includes target device information identifying one or more devices on which the selected function is to be performed, wherein if the target device information identifies the apparatus, the apparatus is configured to perform the selected function, and if the target device information identifies the secondary device, the apparatus is configured to control the secondary device to perform the selected function.
An alkali metal salt of fluorosulfonyl imide represented by the following general formula, wherein a temperature of 210°C or higher at which a mass loss rate becomes 2% when the salt is heated from 25°C at a temperature rise rate of 10°C/minute under an air current: where M a represents Li, and each of R a and R b represents a fluorine atom. a temperature of 210°C or higher at which a mass loss rate becomes 2% when the salt is heated from 25°C at a temperature rise rate of 10°C/minute under an air current: where M a represents Li, and each of R a and R b represents a fluorine atom.
Method for preparing dialkyl dicarbonates by reacting the corresponding alkyl haloformates with at least one alkali metal hydroxide, alkaline earth metal hydroxide and/or carbonate in the presence of at least one water-immiscible organic solvent and in the presence of a catalyst, characterized in that the catalyst used is at least one tertiary amine of the formula NR 1 R 2 R 3 where R 1 = straight-chain or branched C 1 -C 6 -alkyl, R 2 = straight-chain or branched C 16 -C 22 -alkyl and R 3 = -[CH 2 -R 4 -O] n -[CH 2 -R 4]-OH, where n = 0 to 12 and R 4 = -[CH 2 -CH 2]-, -[CH(CH 3)]- or -CH 2 -. R 1 = straight-chain or branched C 1 -C 6 -alkyl, R 2 = straight-chain or branched C 16 -C 22 -alkyl and R 3 = -[CH 2 -R 4 -O] n -[CH 2 -R 4]-OH, where n = 0 to 12 and R 4 = -[CH 2 -CH 2]-, -[CH(CH 3)]- or -CH 2 -.
A method of determining whether the skin of a child is mature or immature in its organization/function, said method comprising the step of: a) taking a skin sample of the said child, wherein said skin sample is a replica of the skin surface of said child; b) assessing the relief of the skin surface, wherein said assessment includes determining the developed surface of said skin sample; and characterized by c) comparing the developed skin surface determined in step b) with the developed skin surface of a sample from a reference subject whose age is known; wherein the degree of maturation of the skin is correlated with the development of the relief of said skin; and wherein three classes of skin maturation are distinguished in relation to the age: - immaturity: 0 to 1 year; - intermediate maturity: ≥ 1 year to 4-5 years; and - maturity: ≥ 4-5 years. a) taking a skin sample of the said child, wherein said skin sample is a replica of the skin surface of said child; b) assessing the relief of the skin surface, wherein said assessment includes determining the developed surface of said skin sample; and characterized by c) comparing the developed skin surface determined in step b) with the developed skin surface of a sample from a reference subject whose age is known; wherein the degree of maturation of the skin is correlated with the development of the relief of said skin; and wherein three classes of skin maturation are distinguished in relation to the age: - immaturity: 0 to 1 year; - intermediate maturity: ≥ 1 year to 4-5 years; and - maturity: ≥ 4-5 years. wherein the degree of maturation of the skin is correlated with the development of the relief of said skin; and wherein three classes of skin maturation are distinguished in relation to the age: - immaturity: 0 to 1 year; - intermediate maturity: ≥ 1 year to 4-5 years; and - maturity: ≥ 4-5 years. - immaturity: 0 to 1 year; - intermediate maturity: ≥ 1 year to 4-5 years; and - maturity: ≥ 4-5 years.
Vehicle which can be driven using motor force and/or pedal force, in particular electric bicycle, comprising - a crank drive with a crank shaft, - an output drive element which is a chain ring which outputs a drive torque for the vehicle, - an electric drive with a reduction gear mechanism, and - a continuously variable planetary gear mechanism, - wherein an output element of the continuously variable planetary gear mechanism transmits the drive torque to the output drive element, characterized in that - an input element of the continuously variable planetary gear mechanism is connected to the crank drive and the electric drive, wherein a pedal drive torque which is applied by a rider and an electric drive torque which is applied by the electric drive are introduced by means of the same input element of the continuously variable planetary gear mechanism, so that the two torques are summed upstream of the continuously variable planetary gear mechanism. - a crank drive with a crank shaft, - an output drive element which is a chain ring which outputs a drive torque for the vehicle, - an electric drive with a reduction gear mechanism, and - a continuously variable planetary gear mechanism, - wherein an output element of the continuously variable planetary gear mechanism transmits the drive torque to the output drive element, - an input element of the continuously variable planetary gear mechanism is connected to the crank drive and the electric drive, wherein a pedal drive torque which is applied by a rider and an electric drive torque which is applied by the electric drive are introduced by means of the same input element of the continuously variable planetary gear mechanism, so that the two torques are summed upstream of the continuously variable planetary gear mechanism.
A composition comprising: a) an organic polymer, and b) a silyl functional compound comprising a N-Si bond, wherein the silyl functional compound comprises one or more compounds of formula a) an organic polymer, and b) a silyl functional compound comprising a N-Si bond,
Method for magnified imaging of a sample, comprising the steps of: - imaging sample sections of a sample section series by means of a first particle-optical apparatus, wherein coordinates of the imaged sample site are captured and stored in such a way that the coordinates of the imaged sample site are assignable to the respective image of this sample site; - selecting a volume of interest, wherein the selected VOI extends over at least two sample sections (203, 204) of the series of sample sections; - transferring the coordinates of the selected VOI to a second particle-optical apparatus; - imaging the selected VOI by means of the second particle-optical apparatus, wherein a plurality of planes of a sample section are imaged in order to obtain a 3D image of the selected VOI. - imaging sample sections of a sample section series by means of a first particle-optical apparatus, wherein coordinates of the imaged sample site are captured and stored in such a way that the coordinates of the imaged sample site are assignable to the respective image of this sample site; - selecting a volume of interest, wherein the selected VOI extends over at least two sample sections (203, 204) of the series of sample sections; - transferring the coordinates of the selected VOI to a second particle-optical apparatus; - imaging the selected VOI by means of the second particle-optical apparatus, wherein a plurality of planes of a sample section are imaged in order to obtain a 3D image of the selected VOI.
A compound represented by formula: wherein R 11 and R 12 each independently represent a halogen atom, a C 1 -C 6 alkyl group, or a C 2 -C 6 alkenyl group; R 13 and R 14 are the same as R 11 and R 12, respectively; n, p, q, and r each independently represent 0 or any integer of 1 to 4; m represents 0 or any integer of 1 to 2; a represents any integer of 1 to 10; R 2 represents a hydrogen atom or a C 1 -C 6 alkyl group; R 3 represents a hydroxy group, an OR 51 group, a NR 52 R 53 group, a SR 54 group, or OM; R 51 represents a C 1 -C 6 alkyl group, a C 2 -C 6 alkenyl group, an optionally substituted phenyl group, or an optionally substituted benzyl group; R 52 to R 54 each represent a hydrogen atom, a C 1 -C 6 alkyl group, a C 2 -C 6 alkenyl group, an optionally substituted phenyl group, or an optionally substituted benzyl group, and R 52 and R 53 together optionally form a saturated or unsaturated C 4 -C 10 ring, which, optionally, further comprises at least one heteroatom selected from S, N, and O; M represents a metal atom; and R 41 and R 42 each represent a hydrogen atom.
Procedure designed for the manufacturing of a pressure measuring cell, said cell having a ceramic meter body and a ceramic measuring membrane, wherein the measuring membrane is joined in a pressure-tight manner to the meter body by means of an active brazing alloy, said procedure comprising: The provision of the meter body, the measuring membrane and the active brazing alloy; The positioning of the active brazing alloy between the meter body and the measuring membrane, The melting of the active brazing alloy by irradiating the active brazing alloy with a laser, wherein the irradiation of the active brazing alloy takes place through the measuring membrane; and The solidification of the active brazing alloy through cooling. The provision of the meter body, the measuring membrane and the active brazing alloy; The positioning of the active brazing alloy between the meter body and the measuring membrane, The melting of the active brazing alloy by irradiating the active brazing alloy with a laser, wherein the irradiation of the active brazing alloy takes place through the measuring membrane; and The solidification of the active brazing alloy through cooling.
A method of making a composition comprising an adenoviral vector comprising the steps of: a. providing an aqueous mixture comprising the adenoviral vector and a cryoprotectant; and b. lyophilizing the aqueous mixture by: i. freezing the aqueous mixture including an annealing step; and ii. drying the frozen aqueous mixture under reduced pressure. a. providing an aqueous mixture comprising the adenoviral vector and a cryoprotectant; and b. lyophilizing the aqueous mixture by: i. freezing the aqueous mixture including an annealing step; and ii. drying the frozen aqueous mixture under reduced pressure. i. freezing the aqueous mixture including an annealing step; and ii. drying the frozen aqueous mixture under reduced pressure.
A cargo aircraft (10") configurable for aerial refueling operations comprising: a fuselage which includes a forward cargo ramp (11") and an aft cargo door (12") oppositely hinged relative to one another at an aft portion of the fuselage so as to be moveable between opened and closed positions to respectively open and close a cargo space (10a") within the fuselage; a tail cone housing; a flying boom mast system having a flying boom mast (13") operably associated with the aft portion of the fuselage and moveable between a stowed and deployed conditions relative to the aft portion of the fuselage, the flying boom mast (13") being received by the tail cone housing when in the stowed position thereof; a fuel supply line (17a") connecting the flying boom mast (13") with an on-board fuel supply (17") of the aircraft (10") so as to allow aerial refueling of a receiver aircraft when the flying boom mast (13") is in the deployed condition thereof; and an actuator assembly positioned at an aft end of the aircraft (10") for reciprocally moving the flying boom mast (13") between retracted and extended positions relative to the tail cone housing, wherein the actuator assembly comprises a tubular receiver for receiving a portion of the flying boom mast when in the retracted position thereof, and a piston member journally connected to a proximal end of the flying boom mast (13") for reciprocally moving the flying boom mast (13") between the retracted and extended positions thereof. a fuselage which includes a forward cargo ramp (11") and an aft cargo door (12") oppositely hinged relative to one another at an aft portion of the fuselage so as to be moveable between opened and closed positions to respectively open and close a cargo space (10a") within the fuselage; a tail cone housing; a flying boom mast system having a flying boom mast (13") operably associated with the aft portion of the fuselage and moveable between a stowed and deployed conditions relative to the aft portion of the fuselage, the flying boom mast (13") being received by the tail cone housing when in the stowed position thereof; a fuel supply line (17a") connecting the flying boom mast (13") with an on-board fuel supply (17") of the aircraft (10") so as to allow aerial refueling of a receiver aircraft when the flying boom mast (13") is in the deployed condition thereof; and an actuator assembly positioned at an aft end of the aircraft (10") for reciprocally moving the flying boom mast (13") between retracted and extended positions relative to the tail cone housing, wherein the actuator assembly comprises a tubular receiver for receiving a portion of the flying boom mast when in the retracted position thereof, and a piston member journally connected to a proximal end of the flying boom mast (13") for reciprocally moving the flying boom mast (13") between the retracted and extended positions thereof.
A control system of an agricultural implement which is to be open-loop and/or closed-loop controlled by way of an ISO data bus comprising a control device and a man-machine interface, wherein the control device exchanges data by way of the ISO data bus on the one hand with the agricultural implement and on the other hand with the man-machine interface, wherein the man-machine interface has an operating terminal and a joystick, wherein functions of the implement can be freely placed by way of the operating terminal by an operator on auxiliary input keys of the operating terminal and/or the joystick to operate those functions by way of the auxiliary input keys, characterised in that the operating terminal and/or a display and input device which can be coupled to the operating terminal or the control device has a voice input device (11, 14) and functions of the implement which can be placed by an operator on the auxiliary input keys of the man-machine interface can be associated by an operator by way of the operating terminal and/or the display and input device with the respective voice input device (11, 14) in order to operate those functions by way of the voice input device (11, 14).
A drug cassette (286, 318, 320, 322, 330) for removable attachment to a drive module (288, 298, 300, 306, 314, 319, 324, 328, 362) to define a medication delivery device (293, 293'', 303, 303', 303′′′), the cassette comprising: a cassette housing (286A, 287, 344, 366, 368) configured to be attached to and detached from the drive module; a container body (248, 334) to hold a medication and defining an outlet; a piston disposed within the container body; a drive ribbon (R, 370) disposed within the cassette housing to advance the piston within the container body, wherein the drive ribbon includes a distal edge section and a proximal edge section, the drive ribbon being incrementally movable between a retracted configuration and an extended configuration about a drive axis, wherein a retracted portion of the drive ribbon in the retracted configuration defines a spiral and an extended portion of the drive ribbon in the extended configuration defines a helix; and a driven member (294, 342, 372) engaged with the drive ribbon, wherein in response to a rotation of the driven member the drive ribbon is axially extended and the piston is advanced within the container body to expel the medication through the outlet. a cassette housing (286A, 287, 344, 366, 368) configured to be attached to and detached from the drive module; a container body (248, 334) to hold a medication and defining an outlet; a piston disposed within the container body; a drive ribbon (R, 370) disposed within the cassette housing to advance the piston within the container body, wherein the drive ribbon includes a distal edge section and a proximal edge section, the drive ribbon being incrementally movable between a retracted configuration and an extended configuration about a drive axis, wherein a retracted portion of the drive ribbon in the retracted configuration defines a spiral and an extended portion of the drive ribbon in the extended configuration defines a helix; and a driven member (294, 342, 372) engaged with the drive ribbon, wherein in response to a rotation of the driven member the drive ribbon is axially extended and the piston is advanced within the container body to expel the medication through the outlet.
A method comprising: receiving a frame from a media access control sublayer; determining a preamble comprising a SIG field comprising a modulation and coding scheme parameter, a bandwidth parameter, a length parameter, a beamforming parameter, a space time block coding parameter, a coding parameter, an aggregation parameter, a short guard interval parameter; generating, by a medium access control sublayer logic, a four-bit cyclic redundancy check sequence for the SIG field, wherein the cyclic redundancy check sequence provides a Hamming distance of two; and encapsulating the frame with the preamble; wherein the beamforming parameter indicates whether transmission of the encapsulated frame is to be beamformed. receiving a frame from a media access control sublayer; determining a preamble comprising a SIG field comprising a modulation and coding scheme parameter, a bandwidth parameter, a length parameter, a beamforming parameter, a space time block coding parameter, a coding parameter, an aggregation parameter, a short guard interval parameter; generating, by a medium access control sublayer logic, a four-bit cyclic redundancy check sequence for the SIG field, wherein the cyclic redundancy check sequence provides a Hamming distance of two; and encapsulating the frame with the preamble; wherein the beamforming parameter indicates whether transmission of the encapsulated frame is to be beamformed.
A cap system for enclosing a metallic fastener assembly extending through a structure of an aircraft, the cap system comprising: a nut member of the metallic fastener assembly, the nut member comprising a first securement mechanism positioned about a periphery of the nut member, wherein the first securement mechanism comprises a plurality of grooves positioned about the periphery of the nut member, wherein the plurality of grooves are spaced apart about the periphery of the nut member, and the nut member further includes a plurality of ridge members which extend in a radial direction away from the nut member and define the plurality of grooves, wherein adjacent ridge members are spaced apart about the nut member; an electrically insulating cap member comprising a sidewall having an inner surface which defines a cavity dimensioned to receive the nut member and defines a second securement mechanism complementary configured to engage the first securement mechanism positioned about the periphery of the nut member, and an end of the sidewall of the cap member defines an opening which provides the nut member to have access into the cavity. a nut member of the metallic fastener assembly, the nut member comprising a first securement mechanism positioned about a periphery of the nut member, wherein the first securement mechanism comprises a plurality of grooves positioned about the periphery of the nut member, wherein the plurality of grooves are spaced apart about the periphery of the nut member, and the nut member further includes a plurality of ridge members which extend in a radial direction away from the nut member and define the plurality of grooves, wherein adjacent ridge members are spaced apart about the nut member; an electrically insulating cap member comprising a sidewall having an inner surface which defines a cavity dimensioned to receive the nut member and defines a second securement mechanism complementary configured to engage the first securement mechanism positioned about the periphery of the nut member, and an end of the sidewall of the cap member defines an opening which provides the nut member to have access into the cavity. a sidewall having an inner surface which defines a cavity dimensioned to receive the nut member and defines a second securement mechanism complementary configured to engage the first securement mechanism positioned about the periphery of the nut member, and an end of the sidewall of the cap member defines an opening which provides the nut member to have access into the cavity.
Method of cleaning industrial plant components to remove contaminants selected from silanes, metal halides, organometallic halides and mixtures thereof wherein said method comprises treating the plant components with a liquid nitrile or with a solution of a nitrile in an aprotic solvent.