mhurhangee/patent-ind-claim-en huggingface dataset:
An isolating decoupler comprising: a hub for connection to a driving shaft; a pulley journalled to the hub , the pulley having a belt engaging surface; a spring engaged between the hub and a spring carrier , the spring being radially expandable when torque is applied to the hub ; a one-way clutch spring disposed radially inward of the spring engaged with the spring carrier and frictionally engagable with the pulley , wherein one-way clutch spring tends to decrease in radial diameter when torque is applied to the spring carrier ; the one-way clutch spring being engagable with the hub whereby the frictional engagement of the one-way clutch spring with the pulley can be progressively released as the one-way clutch spring unwinds; and an inertial member engaged with the hub through a damping member . a hub for connection to a driving shaft; a pulley journalled to the hub , the pulley having a belt engaging surface; a spring engaged between the hub and a spring carrier , the spring being radially expandable when torque is applied to the hub ; a one-way clutch spring disposed radially inward of the spring engaged with the spring carrier and frictionally engagable with the pulley , wherein one-way clutch spring tends to decrease in radial diameter when torque is applied to the spring carrier ; the one-way clutch spring being engagable with the hub whereby the frictional engagement of the one-way clutch spring with the pulley can be progressively released as the one-way clutch spring unwinds; and an inertial member engaged with the hub through a damping member .
A system configured to produce air for a cabin of an aircraft , the system comprising: an air conditioning pack including: a heat exchanger including: a first inlet fluidly coupled to a first outlet via a first flow path , the first inlet configured to receive cabin supply air from a high pressure air source ; and a second inlet fluidly coupled to a second outlet via a second flow path , the second flow path isolated from the first flow path , the second inlet configured to receive cabin exhaust air from the cabin of the aircraft , and the cabin exhaust air configured to reduce a temperature of the cabin supply air via the heat exchanger ; a turbine having a turbine inlet and a turbine outlet , the turbine inlet fluidly coupled to the first outlet of the heat exchanger , the turbine configured to reduce a temperature and pressure of the cabin supply air between the turbine inlet and the turbine outlet , and the turbine outlet fluidly coupled to the cabin to provide the cabin supply air to the cabin , wherein the turbine is not mechanically coupled to or driving a compressor ; and a fan configured to direct the cabin exhaust air from the heat exchanger to atmosphere. a heat exchanger including: a first inlet fluidly coupled to a first outlet via a first flow path , the first inlet configured to receive cabin supply air from a high pressure air source ; and a second inlet fluidly coupled to a second outlet via a second flow path , the second flow path isolated from the first flow path , the second inlet configured to receive cabin exhaust air from the cabin of the aircraft , and the cabin exhaust air configured to reduce a a first inlet fluidly coupled to a first outlet via a first flow path , the first inlet configured to receive cabin supply air from a high pressure air source ; and a second inlet fluidly coupled to a second outlet via a second flow path , the second flow path isolated from the first flow path , the second inlet configured to receive cabin exhaust air from the cabin of the aircraft , and the cabin exhaust air configured to reduce a temperature of the cabin supply air via the heat exchanger ; a turbine having a turbine inlet and a turbine outlet , the turbine inlet fluidly coupled to the first outlet of the heat exchanger , the turbine configured to reduce a temperature and pressure of the cabin supply air between the turbine inlet and the turbine outlet , and the turbine outlet fluidly coupled to the cabin to provide the cabin supply air to the cabin , wherein the turbine is not mechanically coupled to or driving a compressor ; and a fan configured to direct the cabin exhaust air from the heat exchanger to atmosphere.
Coupling part with integrated aerosol generator for use in a breathing circuit, comprising: a housing enclosing a cavity (V), having a first opening at a first end prepared for direct or indirect connection to a ventilator , a second opening at a second end which is suitable for direct or indirect connection to a patient line or an endotracheal tube , and characterised in that an aerosol generator is integrated in one side of the housing and is suitable for delivering an aerosolised liquid, the first end and the second end form an angle between 90° and 120°, the aerosol generator is positioned approximately diametrically opposite the second opening in the second end , and in that an additional volume (V'), construction-conditioned by addition of the aerosol generator, is less than or equal to about 1/10 of the total volume of the cavity (V). a housing enclosing a cavity (V), having a first opening at a first end prepared for direct or indirect connection to a ventilator , a second opening at a second end which is suitable for direct or indirect connection to a patient line or an endotracheal tube , and characterised in that an aerosol generator is integrated in one side of the housing and is suitable for delivering an aerosolised liquid, the first end and the second end form an angle between 90° and 120°, the aerosol generator is positioned approximately diametrically opposite the second opening in the second end , and in that an additional volume (V'), construction-conditioned by addition of the aerosol generator, is less than or equal to about 1/10 of the total volume of the cavity (V).
A delivery system for use with a prosthetic heart valve having a stent frame to which a valve structure is attached, the system comprising: a shaft assembly including a distal end, an intermediate portion, and a first coupling structure disposed near the distal end and configured to be coupled to a distal end of the prosthetic heart valve via a first tether ; a sheath assembly defining a lumen sized to slidably receive the shaft assembly ; and wherein the delivery system is configured to transition from a loaded state in which the sheath assembly encompasses the prosthetic heart valve to a deployed state in which the sheath assembly is withdrawn from the prosthetic heart valve , and wherein the first coupling structure is configured to be manipulated in a first direction to provide a controlled expansion or contraction of the distal end of the prosthetic heart valve ; characterised in that the first tether is configured to be released from the first coupling structure by rotation of the first coupling structure and/or wherein a second tether is configured to be released from a second coupling structure (117; 304) of the shaft assembly by rotation of the second coupling structure (117; 304). a shaft assembly including a distal end, an intermediate portion, and a first coupling structure disposed near the distal end and configured to be coupled to a distal end of the prosthetic heart valve via a first tether ; a sheath assembly defining a lumen sized to slidably receive the shaft assembly ; and wherein the delivery system is configured to transition from a loaded state in which the sheath assembly encompasses the prosthetic heart valve to a deployed state in which the sheath assembly is withdrawn from the prosthetic heart valve , and wherein the first coupling structure is configured to be manipulated in a first direction to provide a controlled expansion or contraction of the distal end of the prosthetic heart valve ; the first tether is configured to be released from the first coupling structure by rotation of the first coupling structure and/or wherein a second tether is configured to be released from a second coupling structure (117; 304) of the shaft assembly by rotation of the second coupling structure (117; 304).
Rear spoiler for a vehicle , in particular a motor vehicle, which rear spoiler is rigidly connected to a vehicle body or a tailgate or rear door of the vehicle , the rear spoiler having a spoiler base body to which two or more spoiler lips are assigned or assignable which respectively form a wind separating edge and from which a selection can be made or which can be exchanged for one another, characterized in that the spoiler base body is formed by two shell elements , which are rigidly connected both to one another and to the vehicle body or to the tailgate or rear door of the vehicle and form a closed hollow profile.
A method performed by a second multi-link device, MLD, in a wireless local area network, WLAN, system, the method comprising: receiving a multi-link, ML, element from a first MLD through a first link (S3010); and decoding the ML element (S3020), wherein the first MLD includes a first access point (AP) operating on the first link and a second AP operating on a second link, wherein the ML element includes common information and link information, wherein the common information includes an MLD Beacon Interval Present subfield, and wherein a beacon interval of the second AP is included in the link information based on the MLD Beacon Interval Present subfield. receiving a multi-link, ML, element from a first MLD through a first link (S3010); and decoding the ML element (S3020), wherein the first MLD includes a first access point (AP) operating on the first link and a second AP operating on a second link, wherein the ML element includes common information and link information, wherein the common information includes an MLD Beacon Interval Present subfield, and wherein a beacon interval of the second AP is included in the link information based on the MLD Beacon Interval Present subfield.
System for the transport and storage of drugs in predetermined temperature ranges provided with - at least one container with an interior space in a lower part surrounded by walls and with a lid , the structure of the walls of the lower part and of the lid in each case resulting in at least one hollow body filled with at least one material or fluid with a high heat storage capacity, and the walls result in a trough-shaped lower part , and the walls result in the trough-shaped lower part with respectively greater length and width facing an open side with cover than on a closed bottom facing away from the cover , characterized in that the thicknesses of the walls vary between 5 to 30 mm and the greater lengths and widths facing the open top side with the cover than on the closed bottom on the side facing away from the cover result in conicities between 8° and 16°, said conicity being conditioned by the respective thicknesses of the walls , to provide for nesting abilities of the piled container . - at least one container with an interior space in a lower part surrounded by walls and with a lid , the structure of the walls of the lower part and of the lid in each case resulting in at least one hollow body filled with at least one material or fluid with a high heat storage capacity, and the walls result in a trough-shaped lower part , and the walls result in the trough-shaped lower part with respectively greater length and width facing an open side with cover than on a closed bottom facing away from the cover ,
A method for intra-prediction or inter-prediction processing of a video frame, comprising the steps of: obtaining at least 4 reference samples; obtaining a value of a subpixel offset; and filtering, using a subpixel 4-tap interpolation filter, the at least 4 reference samples to obtain at least one predicted sample values, characterized in that wherein filter coefficients of the subpixel 4-tap interpolation filter satisfy the following equations: c 0 = 16 − p 2 c 1 = 16 + 16 − p 2 c 2 = 16 + p 2 c 3 = p 2 wherein p is a 1/32 fractional sample position of the value of the subpixel offset, p having a range from 0 to 31, and c 0 , c 1 , c 2 , and c 3 are the filter coefficients of the subpixel 4-tap interpolation filter. obtaining at least 4 reference samples; obtaining a value of a subpixel offset; and filtering, using a subpixel 4-tap interpolation filter, the at least 4 reference samples to obtain at least one predicted sample values, characterized in that wherein filter coefficients of the subpixel 4-tap interpolation filter satisfy the following equations: c 0 = 16 − p 2 c 1 = 16 + 16 − p 2 c 2 = 16 + p 2 c 3 = p 2 wherein p is a 1/32 fractional sample position of the value of the subpixel offset, p having a range from 0 to 31, and c 0 , c 1 , c 2 , and c 3 are the filter coefficients of the subpixel 4-tap interpolation filter.
A water-in-oil emulsion cosmetic comprising the following (A) to (D): (A) 1 to 5 mass % of hydrogenated polyisobutene with respect to the total amount of the cosmetic, (B) an oil containing (b1) a volatile oil of low compatibility with (A), wherein said volatile oil of low compatibility with (A) is selected from the group consisting of decamethylcyclopentasiloxane, decamethyltetrasiloxane, hexamethylcyclotrisiloxane, octamethylcyclotetrasiloxane, decamethylcyclopentasiloxane, dodecamethylcyclohexasiloxane, hexamethyldisiloxane, octamethyltrisiloxane, dodecamethylpentasiloxane, tetradecamethylhexasiloxane, hexadecamethylheptasiloxane, methyltris (trimethylsiloxy) silane, tetrakis (trimethylsiloxy) silane, perfluoromethyl cyclopentane, perfluorodimethyl cyclohexane, methylperfluoro butyl ether, methylperfluoro isobutyl ether, ethylperfluoro butyl ether and ethylperfluoro isobutyl ether, and (b2) an oil with a viscosity less than 1000 mPa•s at a temperature of 25°C, as determined using a viscometer, (C) an emulsifying agent, and (D) 60 to 90 mass % of an aqueous component with respect to the total amount of the cosmetic, wherein the percentage of component (b1) is 45 to 85% with respect to component (A) and component (B), the blending quantity of component (b1) is 12 to 20 mass % with respect to the total amount of the cosmetic, and the blending quantity of component (b2) is two times or less of the blending quantity of component (A). (A) 1 to 5 mass % of hydrogenated polyisobutene with respect to the total amount of the cosmetic, (B) an oil containing (b1) a volatile oil of low compatibility with (A), wherein said volatile oil of low compatibility with (A) is selected from the group consisting of decamethylcyclopentasiloxane, decamethyltetrasiloxane, hexamethylcyclotrisiloxane, octamethylcyclotetrasiloxane, decamethylcyclopentasiloxane, dodecamethylcyclohexasiloxane, hexamethyldisiloxane, octamethyltrisiloxane, dodecamethylpentasiloxane, tetradecamethylhexasiloxane, hexadecamethylheptasiloxane, methyltris (trimethylsiloxy) silane, tetrakis (trimethylsiloxy) silane, perfluoromethyl cyclopentane, perfluorodimethyl cyclohexane, methylperfluoro butyl ether, methylperfluoro isobutyl ether, ethylperfluoro butyl ether and ethylperfluoro isobutyl ether, and (b2) an oil with a viscosity less than 1000 mPa•s at a temperature of 25°C, as determined using a viscometer, (C) an emulsifying agent, and (D) 60 to 90 mass % of an aqueous component with respect to the total amount of the cosmetic,
An oral composition comprising the following ingredients (A), (B), (C), and (D): (A) 0.001 mass% or more and 0.3 mass% or less of myristoyl glutamic acid or a salt thereof; (B) 0.001 mass% or more and 0.3 mass% or less of lauroyl glutamic acid or a salt thereof; (C) an alkylsulfate; and (D) water wherein a mass ratio of the content of ingredient (A) to the content of ingredient (B), ((A)/(B)), is 0.25 or more and 4 or less; and the content of a polyphosphoric acid or a salt thereof is 0.01 mass% or less. (A) 0.001 mass% or more and 0.3 mass% or less of myristoyl glutamic acid or a salt thereof; (B) 0.001 mass% or more and 0.3 mass% or less of lauroyl glutamic acid or a salt thereof; (C) an alkylsulfate; and (D) water
A biopsy device comprising: (a) a body; (b) a needle extending distally from the body; (c) a cutter longitudinally translatable relative to the needle, wherein the cutter defines a cutter lumen; and (d) a tissue sample holder including, (i) a rotatable member, wherein at least a portion of the rotatable member defines an inner chamber divided by a plurality of tray walls extending radially inwardly from an outer wall of the rotatable member, (ii) an individual sample tray including a single sample chamber, wherein the single sample chamber is configured to receive only a single tissue sample, and (iii) one or more bulk sample trays, wherein the bulk sample tray is configured to receive a plurality of tissue samples, characterized in that each bulk sample tray includes a distal end wall having a single sample opening for receiving tissue samples therethrough. (a) a body; (b) a needle extending distally from the body; (c) a cutter longitudinally translatable relative to the needle, wherein the cutter defines a cutter lumen; and (d) a tissue sample holder including, (i) a rotatable member, wherein at least a portion of the rotatable member defines an inner chamber divided by a plurality of tray walls extending radially inwardly from an outer wall of the rotatable member, (ii) an individual sample tray including a single sample chamber, wherein the single sample chamber is configured to receive only a single tissue sample, and (iii) one or more bulk sample trays, wherein the bulk sample tray is configured to receive a plurality of tissue samples, (i) a rotatable member, wherein at least a portion of the rotatable member defines an inner chamber divided by a plurality of tray walls extending radially inwardly from an outer wall of the rotatable member, (ii) an individual sample tray including a single sample chamber, wherein the single sample chamber is configured to receive only a single tissue sample, and (iii) one or more bulk sample trays, wherein the bulk sample tray is configured to receive a plurality of tissue samples,
An image processing device, comprising: circuitry configured to: receive an encoded stream in which motion vector (MV) range limit information is encoded, the MV range limit information including a flag indicating whether an inter-view MV corresponding to a current block for referring to a view different from a view of the current block has a range limit in a vertical direction; and decode the received encoded stream based on the flag included in the MV range limit information. receive an encoded stream in which motion vector (MV) range limit information is encoded, the MV range limit information including a flag indicating whether an inter-view MV corresponding to a current block for referring to a view different from a view of the current block has a range limit in a vertical direction; and decode the received encoded stream based on the flag included in the MV range limit information.
A method of generating a digital signature of a message m in a public key encryption scheme, said method comprising, at a smart card computing for said signature: a first component r = x mod q, with q being a preselected publicly known divisor of an order e of an elliptic curve, P being a starting point on the elliptic curve, k being a secret session key, kP being a point on the elliptic curve, x being a digital data string representing the x-coordinate of the point kP; a second component s' = c (h(m) + a r) mod q, with c being an integer, h(m) being a hash over the message m, and a being a private key of a signatory; and a third component u = c k; and wherein the first, second and third components are forwarded to a terminal ; and wherein the method comprises, at a recipient device, receiving the message m, the first component r, the second component s' and the third component u; obtaining a signature component s by computing s'u -1 ; and using the first component r and the signature component s to verify the origin of the message m.. a first component r = x mod q, with q being a preselected publicly known divisor of an order e of an elliptic curve, P being a starting point on the elliptic curve, k being a secret session key, kP being a point on the elliptic curve, x being a digital data string representing the x-coordinate of the point kP; a second component s' = c (h(m) + a r) mod q, with c being an integer, h(m) being a hash over the message m, and a being a private key of a signatory; and a third component u = c k; and wherein the first, second and third components are forwarded to a terminal ; and wherein the method comprises, at a recipient device, receiving the message m, the first component r, the second component s' and the third component u; obtaining a signature component s by computing s'u -1 ; and using the first component r and the signature component s to verify the origin of the message m..
A method of cryo-curing a plant, comprising the steps of: a. freezing the plant for a period of at least about 1 hour at a temperature of less than about -10° F. (-23 °C); and b. curing the frozen plant for a period of at least about 8 hours at a temperature below 70° F. (21 °C) under vacuum to obtain the plant having a desired moisture content of about 5% to about 20% by weight; wherein curing is performed in about 36 hours or less; and wherein the plant is cannabis, hops or berries. a. freezing the plant for a period of at least about 1 hour at a temperature of less than about -10° F. (-23 °C); and b. curing the frozen plant for a period of at least about 8 hours at a temperature below 70° F. (21 °C) under vacuum to obtain the plant having a desired moisture content of about 5% to about 20% by weight; wherein curing is performed in about 36 hours or less; and wherein the plant is cannabis, hops or berries.
A method , comprising: measuring a first rotational speed, i.e. the speed of an inner raceway of a sprag clutch of a rotorcraft ; measuring a second rotational speed, i.e. the speed of an outer raceway of the sprag clutch : determining if the sprag clutch is in an overrunning condition, wherein the determining is based on the first rotational speed and the second rotational speed; generating an estimation of an instantaneous wear rate of the sprag clutch , wherein the estimation of the instantaneous wear rate is generated based on the overrunning condition, the first rotational speed and the second rotational speed; and displaying an indication of the estimation of the instantaneous wear rate of the sprag clutch . measuring a first rotational speed, i.e. the speed of an inner raceway of a sprag clutch of a rotorcraft ; measuring a second rotational speed, i.e. the speed of an outer raceway of the sprag clutch : determining if the sprag clutch is in an overrunning condition, wherein the determining is based on the first rotational speed and the second rotational speed; generating an estimation of an instantaneous wear rate of the sprag clutch , wherein the estimation of the instantaneous wear rate is generated based on the overrunning condition, the first rotational speed and the second rotational speed; and displaying an indication of the estimation of the instantaneous wear rate of the sprag clutch . determining if the sprag clutch is in an overrunning condition, wherein the determining is based on the first rotational speed and the second rotational speed; generating an estimation of an instantaneous wear rate of the sprag clutch , wherein the estimation of the instantaneous wear rate is generated based on the overrunning condition, the first rotational speed and the second rotational speed; and displaying an indication of the estimation of the instantaneous wear rate of the sprag clutch .
A fountain pen nib characterised in that it consists of a polished natural or a polished synthetic gem which is one of corundum, topaz, emerald, and garnet, wherein the nib has no slit or breather hole, wherein a linear groove is formed longitudinally in a center of an inner side of the nib , and wherein at least the linear groove and surrounding thereof have been subjected to a surface-roughening treatment.