mhurhangee/patent-ind-claim-en huggingface dataset:
Method for using a delivery system comprising: transporting a first stream of a carrier gas to a delivery device of the delivery system ; the delivery device containing a liquid precursor compound; the first stream of carrier gas being at a temperature greater than or equal to 20°C; where the liquid precursor compound is in a liquid state in the delivery device ; transporting a second stream of the carrier gas to a point downstream of the delivery device ; wherein a flow direction of the first stream and a flow direction of the second stream are not opposed to each other; and mixing the first stream after emanating from the outlet portion of the delivery device and the second stream in a mixing chamber at a point downstream from the delivery device to form a third stream ; maintaining a dew point of a vapor of the liquid precursor compound in the third stream that is lower than an ambient temperature; analyzing a chemical content of the third stream using a physical chemical sensor , where the physical chemical sensor is disposed downstream of the delivery device providing the physical chemical sensor in communication with a first proportional valve ; and transmitting a signal from the physical-chemical sensor to a first pressure/flow controller , where the first pressure/flow controller is operative to control a flow rate of the carrier gas in the first stream . transporting a first stream of a carrier gas to a delivery device of the delivery system ; the delivery device containing a liquid precursor compound; the first stream of carrier gas being at a temperature greater than or equal to 20°C; where the liquid precursor compound is in a liquid state in the delivery device ; transporting a second stream of the carrier gas to a point downstream of the delivery device ; wherein a flow direction of the first stream and a flow direction of the second stream are not opposed to each other; and mixing the first stream after emanating from the outlet portion of the delivery device and the second stream in a mixing chamber at a point downstream from the delivery device to form a third stream ; maintaining a dew point of a vapor of the liquid precursor compound in the third stream that is lower than an ambient temperature; analyzing a chemical content of the third stream using a physical chemical sensor , where the physical chemical sensor is disposed downstream of the delivery device providing the physical chemical sensor in communication with a first proportional valve ; and transmitting a signal from the physical-chemical sensor to a first pressure/flow controller , where the first pressure/flow controller is operative to control a flow rate of the carrier gas in the first stream .
An apparatus to recover an aircraft , the apparatus comprising: a base ; a mast extending from the base ; a boom extending from the mast at a first end of the boom to a second end of the boom opposite the first end ; a tether line extending between the mast and the base , said tether line being guided by the boom , a portion of the tether line extending between the second end of the boom and the base ; a kite coupled to the tether line via a support line ; and a mount configured to operatively couple the support line to the tether line , the kite being configured to support the tether line as the aircraft contacts the portion of the tether line extending between the second end of the boom and the base for recovery of the aircraft , wherein the mount is configured to move and/or displace along with the tether line during deceleration of the aircraft , thereby causing the kite to move. a base ; a mast extending from the base ; a boom extending from the mast at a first end of the boom to a second end of the boom opposite the first end ; a tether line extending between the mast and the base , said tether line being guided by the boom , a portion of the tether line extending between the second end of the boom and the base ; a kite coupled to the tether line via a support line ; and a mount configured to operatively couple the support line to the tether line , the kite being configured to support the tether line as the aircraft contacts the portion of the tether line extending between the second end of the boom and the base for recovery of the aircraft , wherein the mount is configured to move and/or displace along with the tether line during deceleration of the aircraft , thereby causing the kite to move.
A compound having the formula: or a stereoisomer or salt thereof, wherein R is selected from substituted or unsubstituted C1-C6 alkyl group and substituted or unsubstituted phenyl group; R a , R b , R c , and R d are independently selected from hydrogen, C1-C3 alkyl, C1-C3 haloalkyl, C1-C3 alkoxy, and halo; R C is hydrogen, a counter ion, or a carboxyl protecting group; and R N is hydrogen or an amine protecting group. wherein R is selected from substituted or unsubstituted C1-C6 alkyl group and substituted or unsubstituted phenyl group; R a , R b , R c , and R d are independently selected from hydrogen, C1-C3 alkyl, C1-C3 haloalkyl, C1-C3 alkoxy, and halo; R C is hydrogen, a counter ion, or a carboxyl protecting group; and R N is hydrogen or an amine protecting group.
An aerosol delivery device (100; 200) comprising: a housing (216; 402; 502) defining a refillable reservoir (218; 404; 504) for storing an aerosol precursor composition; a heating element (222; 406; 506) contained within the housing (216; 402; 502) and configured to activate and vaporize components of the aerosol precursor composition in response to a flow of air through at least a portion of the housing (216; 402; 502), the air being combinable with a thereby formed vapor to form an aerosol; and an adapter (410; 510) coupled to the housing (216; 402; 502) and removably, sealably connectable with a container (300; 700; 1100) for refilling the reservoir (218; 404; 504) with aerosol precursor composition, the adapter (410; 510) configured to engage a valve of the container (300; 700; 1100) during refilling of the reservoir (218; 404; 504), the adapter (410; 510) including a body defining separate and distinct filling and airflow ports , the filling port being for transfer of aerosol precursor composition from the container (300; 700; 1100) into the reservoir (218; 404; 504) during engagement of the adapter (410; 510) and valve in which the airflow port is closed by the valve to prevent the aerosol precursor composition from passing through the airflow port , the airflow port being for the flow of air through at least the portion of the housing (216; 402; 502) when the adapter (410; 510) and valve are disengaged, where the airflow port is on the aerosol delivery device (100; 200) and the valve is on the container (300; 700; 1100). a housing (216; 402; 502) defining a refillable reservoir (218; 404; 504) for storing an aerosol precursor composition; a heating element (222; 406; 506) contained within the housing (216; 402; 502) and configured to activate and vaporize components of the aerosol precursor composition in response to a flow of air through at least a portion of the housing (216; 402; 502), the air being combinable with a thereby formed vapor to form an aerosol; and an adapter (410; 510) coupled to the housing (216; 402; 502) and removably, sealably connectable with a container (300; 700; 1100) for refilling the reservoir (218; 404; 504) with aerosol precursor composition, the adapter (410; 510) configured to engage a valve of the container (300; 700; 1100) during refilling of the reservoir (218; 404; 504), the adapter (410; 510) including a body defining separate and distinct filling and airflow ports , the filling port being for transfer of aerosol precursor composition from the container (300; 700; 1100) into the reservoir (218; 404; 504) during engagement of the adapter (410; 510) and valve in which the airflow port is closed by the valve to prevent the aerosol precursor composition from passing through the airflow port , the airflow port being for the flow of air through at least the portion of the housing (216; 402; 502) when the adapter (410; 510) and valve are disengaged, where the airflow port is on the aerosol delivery device (100; 200) and the valve is on the container (300; 700; 1100).
A heating system for an inhaler device for generating an aerosol and/or a vapor (V) from a substance (L) to be heated, the system comprising: a body member ; at least one supply channel for conveying a substance to be heated from a supply reservoir under capillary action or surface tension forces within the at least one supply channel , wherein the at least one supply channel is formed in a periphery of, and/or through, the body member ; characterized in that a heating means is configured to heat the substance (L) as it is conveyed through the at least one supply channel , and in that the heating means comprises at least one first heating element that is provided within the at least one supply channel . a body member ; at least one supply channel for conveying a substance to be heated from a supply reservoir under capillary action or surface tension forces within the at least one supply channel , wherein the at least one supply channel is formed in a periphery of, and/or through, the body member ; characterized in that a heating means is configured to heat the substance (L) as it is conveyed through the at least one supply channel , and in that the heating means comprises at least one first heating element that is provided within the at least one supply channel .
Surface acoustic wave component, consisting at least of a piezoelectric material, interdigital transducers, a non-piezoelectric material and electrical contact-connections, wherein the interdigital transducers are connected to the non-piezoelectric material at least in a force-locking and/or a positively locking manner and they can excite surface waves in the piezoelectric material, and, at least partly in the region of the aperture of the interdigital transducers, by means of the realisation of a spacing between the interdigital transducers and the piezoelectric material, which spacing is delimited minimally by the roughness of the surfaces of the interdigital transducers and of the piezoelectric material and maximally by a spacing of 1,000 nm, is realised, by means of which the interdigital transducers and the piezoelectric material are mechanically decoupled, wherein the spacing is realised by spacers outside the aperture of the interdigital transducers and/or by the removal of sacrificial layers or of one or more other layers in order to produce a free surface on the interdigital transducers or in order to realise a smaller layer thickness between the interdigital transducers and the piezoelectric material.
A system for magnetic density separation of products (la,lb), the system comprising - a magnet configured to amplify a density gradient (D) in a magnetic liquid (L) for separating the products (la,lb) in the magnetic liquid (L) according to their different density (Da, Db); - a plate disposed along a product path (P) where respective products travel through the magnetic liquid (L); and - a driving mechanism for driving the plate , whereby the system is characterized in that the driving mechanism is configured to drive the plate with a reciprocating motion (R) for lowering a static friction of the respective products (lb") coming into contact with the plate , wherein the reciprocating motion (R) is directed along an in plane direction of the plate for displacing a minimum of magnetic liquid (L) while moving. - a magnet configured to amplify a density gradient (D) in a magnetic liquid (L) for separating the products (la,lb) in the magnetic liquid (L) according to their different density (Da, Db); - a plate disposed along a product path (P) where respective products travel through the magnetic liquid (L); and - a driving mechanism for driving the plate , whereby the system is characterized in that the driving mechanism is configured to drive the plate with a reciprocating motion (R) for lowering a static friction of the respective products (lb") coming into contact with the plate , wherein the reciprocating motion (R) is directed along an in plane direction of the plate for displacing a minimum of magnetic liquid (L) while moving.
A system comprising: a magnetic resonance (MR) safe temperature probe comprising a temperature sensor ; a bone anchor fixture configured to maintain a target distance between the MR safe temperature probe and a laser diffusion fiber (LDF) ; a processor to: perform proton resonance frequency shift (PRF) thermometry on magnetic resonance imaging (MRI) data to generate a temperature model indicating calculated temperatures for pixels in a magnetic resonance image; receive measured temperature data from the MR safe temperature probe ; correlate a pixel in the magnetic resonance image with a location of the temperature sensor ; compare a calculated temperature of the pixel from the temperature model with the measured temperature data from the MR safe temperature probe ; and determine when a difference between the calculated temperature and the measured temperature data exceeds a threshold, wherein when the threshold is exceeded, the processor causes an intervening action to occur. a magnetic resonance (MR) safe temperature probe comprising a temperature sensor ; a bone anchor fixture configured to maintain a target distance between the MR safe temperature probe and a laser diffusion fiber (LDF) ; a processor to: perform proton resonance frequency shift (PRF) thermometry on magnetic resonance imaging (MRI) data to generate a temperature model indicating calculated temperatures for pixels in a magnetic resonance image; receive measured temperature data from the MR safe temperature probe ; correlate a pixel in the magnetic resonance image with a location of the temperature sensor ; compare a calculated temperature of the pixel from the temperature model with the measured temperature data from the MR safe temperature probe ; and determine when a difference between the calculated temperature and the measured temperature data exceeds a threshold, wherein when the threshold is exceeded, the processor causes an intervening action to occur. perform proton resonance frequency shift (PRF) thermometry on magnetic resonance imaging (MRI) data to generate a temperature model indicating calculated temperatures for pixels in a magnetic resonance image; receive measured temperature data from the MR safe temperature probe ; correlate a pixel in the magnetic resonance image with a location of the temperature sensor ; compare a calculated temperature of the pixel from the temperature model with the measured temperature data from the MR safe temperature probe ; and determine when a difference between the calculated temperature and the measured temperature data exceeds a threshold, wherein when the threshold is exceeded, the processor causes an intervening action to occur.
A method for producing cellular plastic particles, comprising: providing a plastic material in the form of pre-expanded polyolefin-based plastic material particles, loading the pre-expanded polyolefin-based plastic material particles with a blowing agent under the influence of pressure, and expanding the pre-expanded polyolefin-based plastic material particles loaded with the blowing agent in order to produce cellular polyolefin-based plastic particles, under the influence of temperature, wherein the expanding of the polyolefin-based plastic material particles loaded with the blowing agent is carried out under the influence of temperature by irradiation of the polyolefin-based plastic material particles loaded with the blowing agent infrared radiation, wherein the polyolefin-based plastic material particles loaded with the blowing agent are conveyed on at least one conveyor line along at least one corresponding radiation generating device generating respective infrared radiation. providing a plastic material in the form of pre-expanded polyolefin-based plastic material particles, loading the pre-expanded polyolefin-based plastic material particles with a blowing agent under the influence of pressure, and expanding the pre-expanded polyolefin-based plastic material particles loaded with the blowing agent in order to produce cellular polyolefin-based plastic particles, under the influence of temperature, wherein the expanding of the polyolefin-based plastic material particles loaded with the blowing agent is carried out under the influence of temperature by irradiation of the polyolefin-based plastic material particles loaded with the blowing agent infrared radiation, wherein the polyolefin-based plastic material particles loaded with the blowing agent are conveyed on at least one conveyor line along at least one corresponding radiation generating device generating respective infrared radiation.
A liquid/moisture resistant polymeric film or coating for packaging comprising hemicellulose and at least one component to improve film-formability selected from the group consisting of plasticizers, cellulose and an oligomer or polymer, said polymeric film or coating further comprising at least one additive/reactant increasing the liquid/moisture resistance of the film, wherein the additive/reactant comprises nanoparticulate platelets of a 2:1 layered phyllosilicate in the hemicellulose as a matrix.
A nacelle housing of a nacelle of a wind turbine , comprising: - a ventilation opening of a cooling system of the wind turbine , - a cover closing the ventilation opening , the cover being configured to allow an airflow through the cover and the ventilation opening , and - a service hatch for hoisting a load into or out of the nacelle housing , wherein the service hatch is provided by the ventilation opening and the cover , wherein the cover is configured as a service door of the service hatch that can be opened to allow the hoisting of a load through the ventilation opening into or out of the nacelle housing , characterized in that the service door comprises a grating, a grille or plural openings to allow the airflow through the service door and the ventilation opening when the service door is closed. - a ventilation opening of a cooling system of the wind turbine , - a cover closing the ventilation opening , the cover being configured to allow an airflow through the cover and the ventilation opening , and - a service hatch for hoisting a load into or out of the nacelle housing , wherein the service hatch is provided by the ventilation opening and the cover , wherein the cover is configured as a service door of the service hatch that can be opened to allow the hoisting of a load through the ventilation opening into or out of the nacelle housing , characterized in that the service door comprises a grating, a grille or plural openings to allow the airflow through the service door and the ventilation opening when the service door is closed.
A rotation device for rotating a wind turbine generator configured to be rotated by wind and to convert wind energy into electrical energy, the rotation device comprising: at least one rotary device configured to couple with an outer surface of the wind turbine generator , and a motor device for driving the rotary device such as to thereby rotate the wind turbine generator about a generator rotation axis (GA), wherein the rotation device comprises a support device for holding the rotary device , the support device being configured to elevate and lower the rotary device such that the rotary device couples with the outer surface of the wind turbine generator in an elevated position and such that the rotary device is separated from the outer surface of the wind turbine generator in a lowered position. at least one rotary device configured to couple with an outer surface of the wind turbine generator , and a motor device for driving the rotary device such as to thereby rotate the wind turbine generator about a generator rotation axis (GA), wherein the rotation device comprises a support device for holding the rotary device , the support device being configured to elevate and lower the rotary device such that the rotary device couples with the outer surface of the wind turbine generator in an elevated position and such that the rotary device is separated from the outer surface of the wind turbine generator in a lowered position.
A method for verifying and accepting a patch request from a patch initiator, the method comprising the steps of: receiving, by an agent in a network element, the patch request from the patch initiator; determining, by the agent, with a blockchain network peer, whether the patch request is included in a plurality of patch requests being accepted by the blockchain network peer; determining, by the agent, whether the patch request is next in an order specified by the blockchain network peer, and applying, by the agent, the patch of the patch request to the network element if the patch request is accepted by the blockchain network peer and is next in the order specified by the blockchain network peer. receiving, by an agent in a network element, the patch request from the patch initiator; determining, by the agent, with a blockchain network peer, whether the patch request is included in a plurality of patch requests being accepted by the blockchain network peer; determining, by the agent, whether the patch request is next in an order specified by the blockchain network peer, and applying, by the agent, the patch of the patch request to the network element if the patch request is accepted by the blockchain network peer and is next in the order specified by the blockchain network peer.
Aircraft turbomachine vane comprising an aerodynamic part extending along a span axis (EV) and made of one piece by additive manufacturing, said aerodynamic part comprising a lower surface wall and an upper surface wall comprising respectively an inner lower surface face and an inner upper surface face , these inner lower and upper surface faces facing one another and delimiting jointly an internal fluid passage comprising at least one channel (44; 46) defining a general fluid propagation direction (X1; X2) therein, this channel being traversed by a plurality of flow disruptive elements connecting the lower and upper surface walls each having a first connection point on the inner lower surface face , and a second connection point on the inner upper surface face , characterised in that the flow disruptive elements extend in relation to the general fluid propagation direction (X1; X2) by forming a variable angle from one flow disruptive element to another relative to the general fluid propagation direction, and in that the flow disruptive elements are irregularly spaced from one another such that the first connection points are arranged in a disorganised manner on the inner lower surface face , and/or the second connection points are arranged in a disorganised manner on the inner upper surface face .