mhurhangee/ep-ind-claims huggingface dataset:
A system for chemical vapor infiltration and densification, the system comprising: a reaction chamber (129,330); a plurality of conduits (163,363) fluidly coupled to an exhaust outlet of the reaction chamber, wherein a first set of conduits of the plurality of conduits define a first flow path (177,377) and a second set of conduits of the plurality of conduits define a second flow path (179,379) wherein the second flow path is fluidly coupled to an inlet of the reaction chamber; a first valve in operable communication with the first set of conduits; a roughing pump downstream of the first valve and configured to drive fluid through the first set of conduits, wherein a portion of effluent gas output from the roughing pump is recirculated into the reaction chamber; a second valve in operable communication with the second set of conduits; a first pump downstream of the second valve and configured to drive fluid through the second set of conduits; and a first hydrogen extraction component in fluid communication with a least one of the first set of conduits or the second set of conduits, wherein the first hydrogen extraction component comprises at least one of a cryogenic-cooler or a pressure swing absorption unit. a reaction chamber (129,330); a plurality of conduits (163,363) fluidly coupled to an exhaust outlet of the reaction chamber, wherein a first set of conduits of the plurality of conduits define a first flow path (177,377) and a second set of conduits of the plurality of conduits define a second flow path (179,379) wherein the second flow path is fluidly coupled to an inlet of the reaction chamber; a first valve in operable communication with the first set of conduits; a roughing pump downstream of the first valve and configured to drive fluid through the first set of conduits, wherein a portion of effluent gas output from the roughing pump is recirculated into the reaction chamber; a second valve in operable communication with the second set of conduits; a first pump downstream of the second valve and configured to drive fluid through the second set of conduits; and a first hydrogen extraction component in fluid communication with a least one of the first set of conduits or the second set of conduits, wherein the first hydrogen extraction component comprises at least one of a cryogenic-cooler or a pressure swing absorption unit.
Process for producing an extruded zeolite-based SCR catalyst, the process comprising: providing individual pulverulent particles of diatomaceous earth having mesoporosity and comprising pores having a pore width of greater than 5 nm; treating the individual pulverulent particles of diatomaceous earth to develop catalytic activity in respect of SCR reactions by: hydrothermal crystallisation at a temperature of 80 to 200°C; autogenous pressurisation over a reaction time of one to ten days to form crystalline material; washing, drying and calcining the crystalline material to form a zeolite, wherein the crystalline material is calcined at a temperature of 400 to 800°C; and ion-exchanging the zeolite with iron or copper to form an ion-exchanged zeolite, extruding a catalyst composition to produce a catalyst body, drying and sintering the catalyst body to produce a catalyst having a composition consisting of 20-50 wt% of the ion-exchanged zeolite as a binder, 50 to 80 wt% of a further catalytically active zeolite and not more than 5 wt% further components, based on the total mass of the catalyst; wherein the further catalytically active zeolite is an aluminosilicate zeolite and/or has an MFI, BEA, CHA, AEI, FAU, AFX or ERI framework, and is ion-exchanged with Cu and/or Fe and/or Ce. providing individual pulverulent particles of diatomaceous earth having mesoporosity and comprising pores having a pore width of greater than 5 nm; treating the individual pulverulent particles of diatomaceous earth to develop catalytic activity in respect of SCR reactions by: hydrothermal crystallisation at a temperature of 80 to 200°C; autogenous pressurisation over a reaction time of one to ten days to form crystalline material; washing, drying and calcining the crystalline material to form a zeolite, wherein the crystalline material is calcined at a temperature of 400 to 800°C; and ion-exchanging the zeolite with iron or copper to form an ion-exchanged zeolite, hydrothermal crystallisation at a temperature of 80 to 200°C; autogenous pressurisation over a reaction time of one to ten days to form crystalline material; washing, drying and calcining the crystalline material to form a zeolite, wherein the crystalline material is calcined at a temperature of 400 to 800°C; and ion-exchanging the zeolite with iron or copper to form an ion-exchanged zeolite, extruding a catalyst composition to produce a catalyst body, drying and sintering the catalyst body to produce a catalyst having a composition consisting of 20-50 wt% of the ion-exchanged zeolite as a binder, 50 to 80 wt% of a further catalytically active zeolite and not more than 5 wt% further components, based on the total mass of the catalyst; wherein the further catalytically active zeolite is an aluminosilicate zeolite and/or has an MFI, BEA, CHA, AEI, FAU, AFX or ERI framework, and is ion-exchanged with Cu and/or Fe and/or Ce.
Deodorization apparatus, to eliminate, reduce or correct the odour of incoherent plastic material, said apparatus comprising: - at least one container with at least one material inlet for introducing incoherent plastic material, at least one material outlet for extracting the incoherent plastic material, at least one gas inlet for introducing a process gas, at least one gas outlet for extracting the process gas; - actuator means for generating a process gas flow which enters said gas inlet and exits from said gas outlet; - outlet olfactory sensor means arranged to detect odorous emissions in the process gas exiting from said container; characterized by comprising: - control means configured to control said apparatus on the basis of signals provided by said outlet olfactory sensor means. - at least one container with at least one material inlet for introducing incoherent plastic material, at least one material outlet for extracting the incoherent plastic material, at least one gas inlet for introducing a process gas, at least one gas outlet for extracting the process gas; - actuator means for generating a process gas flow which enters said gas inlet and exits from said gas outlet; - outlet olfactory sensor means arranged to detect odorous emissions in the process gas exiting from said container; - control means configured to control said apparatus on the basis of signals provided by said outlet olfactory sensor means.
An airfoil for a turbine engine comprising an airfoil having pressure and suction sides (72, 74) extending in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip, wherein the airfoil has a curve corresponding to a relationship between a trailing edge sweep angle and a span position, the trailing edge sweep angle is in a range of 10° to 20° in a range of 40-70% span position, the trailing edge sweep angle is positive from 0% span to at least 95% span, the airfoil has a relationship between a leading edge dihedral and a span position, the leading edge dihedral negative from the 0% span position to the 100% span position, a positive dihedral corresponds to suction side-leaning, and a negative dihedral corresponds to pressure side-leaning.
An inverter comprising - a housing, containing a first housing module, a second housing module, which is connected detachably to the first housing module, and a cooling air channel, which opens out into the surrounding environment of the inverter, and - power electronics component parts in the first housing module and the second housing module, wherein the cooling air channel is delimited in a circumferential direction partially by the first housing module and partially by the second housing module, wherein the first housing module is designed for mounting to an external structure, and the second housing module is designed for an exclusive mounting to the first housing module, wherein the cooling air channel extends with a spacing from a mounting plane of the inverter, which mounting plane is defined by the first housing module with respect to the external structure, characterized in that the power electronics component parts are arranged behind walls of the first housing module and the second housing module, which walls delimit the cooling air channel such that the power electronics component parts are protectively arranged in the housing modules (2, 3). - a housing, containing a first housing module, a second housing module, which is connected detachably to the first housing module, and a cooling air channel, which opens out into the surrounding environment of the inverter, and a first housing module, a second housing module, which is connected detachably to the first housing module, and a cooling air channel, which opens out into the surrounding environment of the inverter, and - power electronics component parts in the first housing module and the second housing module,
A configurable electrical architecture for an eVTOL aircraft having a takeoff and landing power mode and a cruise power mode, the configurable electrical architecture comprising: a power-optimized power source including a high-power battery array; a plurality of energy-optimized power sources (106a-c) selected from a plurality of interchangeable energy-optimized power sources; a distribution system electrically coupled to the power-optimized power source and the plurality of energy-optimized power sources (106a-c); and at least one electric motor (26a-f) electrically coupled to the distribution system; wherein, in the takeoff and landing power mode, both the power-optimized power source and the plurality of energy-optimized power sources (106a-c) provide electrical power to the at least one electric motor (26a-f); and wherein, in the cruise power mode, the plurality of energy-optimized power sources (106a-c) provides electrical power to the at least one electric motor (26a-f) and to the power-optimized power source to recharge the high-power battery array; wherein the plurality of energy-optimized power sources (106a-c) comprises at least two of a high-energy battery array, a hydrogen fuel cell system and a turbo-generator system. a power-optimized power source including a high-power battery array; a plurality of energy-optimized power sources (106a-c) selected from a plurality of interchangeable energy-optimized power sources; a distribution system electrically coupled to the power-optimized power source and the plurality of energy-optimized power sources (106a-c); and at least one electric motor (26a-f) electrically coupled to the distribution system; wherein, in the takeoff and landing power mode, both the power-optimized power source and the plurality of energy-optimized power sources (106a-c) provide electrical power to the at least one electric motor (26a-f); and wherein, in the cruise power mode, the plurality of energy-optimized power sources (106a-c) provides electrical power to the at least one electric motor (26a-f) and to the power-optimized power source to recharge the high-power battery array; wherein the plurality of energy-optimized power sources (106a-c) comprises at least two of a high-energy battery array, a hydrogen fuel cell system and a turbo-generator system.
A heating or cooling body, in particular multi-row flat radiator or heating wall in vertical or horizontal arrangement, consisting of at least two heating panels (11, 12) with embossed upper and lower horizontal collection channels (11.1, 12.1) and vertical heating channels (11.2, 12.2) and a flow and return connector for connection to the pipework of a heating system which supplies a heating or cooling medium to the heating or cooling body, wherein connection fittings are arranged between the heating panels on each upper lateral end portion and/or on each lower lateral end portion, and a fan assembly, which has at least one fan (14.1) and which is mountable by means of holding elements between two of the heating panels (11, 12) of the heating or cooling body, characterised in that the holding elements comprise a connection plate (15.1) which is insertable between the two heating panels (11, 12), wherein the connection plate (15.1), at the ends of the connection plate (15.1) directed towards the two heating panels (11, 12) of the heating or cooling body, has upwardly and downwardly pointing holding webs (15.2, 15.3), which operatively interact with the opposite two heating panels (11, 12), and, in addition, means for fixing at least one fan of the fan assembly are provided in the connection plate (15.1).
A method of receiving secure communications at a first secure communications terminal (104, 104-1, 104-2) having a processor and a memory operably connected to the processor, the method comprising: maintaining an association with a first client account; receiving, from a second secure communications terminal (104, 104-1, 104-2), a message (MSG, MSG1, MSG2) from a second client account, a first portion of the message (MSG, MSG1, MSG2) being encrypted by a shared symmetric key; extracting a key identifier (SSKID, SSKIDA1, SSKIDA2, SSKIDB1, SSKIDB2) from the message (MSG, MSG1, MSG2); obtaining the shared symmetric key based on the key identifier (SSKID, SSKIDA1, SSKIDA2, SSKIDB1, SSKIDB2) included in the message (MSG, MSG1, MSG2), the shared symmetric key and the key identifier (SSKID, SSKIDA1, SSKIDA2, SSKIDB1, SSKIDB2) having been previously generated by the first client account and included as part of a previous message (MSG, MSG1, MSG2) sent to the second client account; decrypting the first portion of the message (MSG, MSG1, MSG2) using the shared symmetric key to obtain a message key (MK, MK1, MK2); and decrypting a second portion of the message (MSG, MSG1, MSG2) using the message key (MK, MK1, MK2), wherein the decrypting the first portion of the message (MSG, MSG1, MSG2) further comprises: decrypting the first portion of the message (MSG, MSG1, MSG2) using a private key (PrK, PKR1, PKRA1) of the first client account. maintaining an association with a first client account; receiving, from a second secure communications terminal (104, 104-1, 104-2), a message (MSG, MSG1, MSG2) from a second client account, a first portion of the message (MSG, MSG1, MSG2) being encrypted by a shared symmetric key; extracting a key identifier (SSKID, SSKIDA1, SSKIDA2, SSKIDB1, SSKIDB2) from the message (MSG, MSG1, MSG2); obtaining the shared symmetric key based on the key identifier (SSKID, SSKIDA1, SSKIDA2, SSKIDB1, SSKIDB2) included in the message (MSG, MSG1, MSG2), the shared symmetric key and the key identifier (SSKID, SSKIDA1, SSKIDA2, SSKIDB1, SSKIDB2) having been previously generated by the first client account and included as part of a previous message (MSG, MSG1, MSG2) sent to the second client account; decrypting the first portion of the message (MSG, MSG1, MSG2) using the shared symmetric key to obtain a message key (MK, MK1, MK2); and decrypting a second portion of the message (MSG, MSG1, MSG2) using the message key (MK, MK1, MK2), wherein the decrypting the first portion of the message (MSG, MSG1, MSG2) further comprises: decrypting the first portion of the message (MSG, MSG1, MSG2) using a private key (PrK, PKR1, PKRA1) of the first client account.
A computer-implemented method, the method comprising: receiving vibration spectrum data from a plurality of different assets; determining, based on a shape of the vibration spectrum data for each of the plurality of assets, clusters for the plurality of assets, assets being grouped in a same cluster having vibration spectrum data of a similar spectral shape; determining for each of the clusters, based on an application of domain derived pattern recognition rules for the vibration spectrum data, one of a plurality of fault classifications; generating an output including an association of each of the plurality of assets with the fault classification of the cluster in which the particular asset is grouped; and saving a record of the output to a data store; and wherein the plurality of assets are each a wind turbine; and wherein the determining of the clusters for the plurality of assets is accomplished by executing an algorithm formulated to identify vibration spectrum data having a similar spectral shape; and wherein the algorithm is one of a hierarchical clustering algorithm, a k-means algorithm, a nearest neighbor algorithm, and at least one algorithm based on a combination of clustering methods. receiving vibration spectrum data from a plurality of different assets; determining, based on a shape of the vibration spectrum data for each of the plurality of assets, clusters for the plurality of assets, assets being grouped in a same cluster having vibration spectrum data of a similar spectral shape; determining for each of the clusters, based on an application of domain derived pattern recognition rules for the vibration spectrum data, one of a plurality of fault classifications; generating an output including an association of each of the plurality of assets with the fault classification of the cluster in which the particular asset is grouped; and saving a record of the output to a data store; and wherein the plurality of assets are each a wind turbine; and wherein the determining of the clusters for the plurality of assets is accomplished by executing an algorithm formulated to identify vibration spectrum data having a similar spectral shape; and wherein the algorithm is one of a hierarchical clustering algorithm, a k-means algorithm, a nearest neighbor algorithm, and at least one algorithm based on a combination of clustering methods.
A modular cutterbar assembly configured to move in a direction of travel along an underlying surface, comprising: a first module forming a first surface, a second surface, a front edge, and a rear edge; a second module coupled to the first module, the second module forming a first surface, a second surface, a front edge, and a rear edge; a joint defined between first and second module (1104, 1108) and defining a joint plane; a first coupler mount defined through the joint of the first and second modules (1104, 1108) at each respective front edge and defining a first coupler axis; and a second coupler mount defined through the joint of the first and second modules (1104, 1108) at each respective rear edge and defining a second coupler axis; characterized in that the joint plane is angled relative to the direction of travel with the cutterbar axis 204 perpendicular to the direction of travel, wherein the first and second coupler mounts (1110, 1112) each define a head portion, a shoulder portion, and a threaded portion; wherein the threaded portion of a first coupler is defined in the first module and the threaded portion of a second coupler is defined in the second module. a first module forming a first surface, a second surface, a front edge, and a rear edge; a second module coupled to the first module, the second module forming a first surface, a second surface, a front edge, and a rear edge; a joint defined between first and second module (1104, 1108) and defining a joint plane; a first coupler mount defined through the joint of the first and second modules (1104, 1108) at each respective front edge and defining a first coupler axis; and a second coupler mount defined through the joint of the first and second modules (1104, 1108) at each respective rear edge and defining a second coupler axis; characterized in that the joint plane is angled relative to the direction of travel with the cutterbar axis 204 perpendicular to the direction of travel, wherein the first and second coupler mounts (1110, 1112) each define a head portion, a shoulder portion, and a threaded portion; wherein the threaded portion of a first coupler is defined in the first module and the threaded portion of a second coupler is defined in the second module.
A substance for use in a therapeutic method of inducing anesthesia in a subject, the method comprising administering to the subject an effective amount of the substance, wherein the substance is a compound or a mixture of compounds selected from the group consisting of: a) 1-Butanol, 4,4,4-trifluoro-3,3-bis(trifluoromethyl)- (CAS# 14115-49-2); and b) 1-Butanol, 3,4,4,4-tetrafluoro-3-(trifluoromethyl)- (CAS# 90999-87-4); the compound having a vapor pressure of at least 0.1 atmospheres (76 mmHg) at 25°C, thereby inducing anesthesia in the subject. a) 1-Butanol, 4,4,4-trifluoro-3,3-bis(trifluoromethyl)- (CAS# 14115-49-2); and b) 1-Butanol, 3,4,4,4-tetrafluoro-3-(trifluoromethyl)- (CAS# 90999-87-4);
A pharmaceutical composition in a solid tablet unit dosage form wherein said unit dosage form comprises a naloxol-polyethylene glycol conjugate oxalate salt, in which the naloxol-polyethylene glycol conjugate has the formula: wherein the salt is in a substantially pure crystalline form and the crystalline form exhibits Form B X-ray powder diffraction peak d values (Å) comprising 13.2; 7.9; 7.0; 6.6; 6.0; 5.7; 5.2; 5.1; 4.44; 4.39; 3.95; 3.88; 3.63; and 3.43, and an opioid agonist, wherein said naloxol-polyethylene glycol conjugate oxalate salt is present in an amount such that significant inhibition of the central analgesic effect of said opioid agonist does not occur when the composition is administered to a subject.