mhurhangee/patent-ind-claim-en huggingface dataset:
A gas turbine engine (20; 100) comprising: a primary flowpath (C) fluidly connecting a compressor section (24; 110), a combustor section (26; 120), and a turbine section (28; 130); and a heat exchanger disposed in the primary flowpath (C), aft of and downstream of the turbine section (28; 130), the heat exchanger including a first inlet for receiving fluid from the primary flowpath (C) and a first outlet for expelling fluid received at the first inlet, the heat exchanger further including a second inlet fluidly connected to a supercritical CO2 (sCO2) bottoming cycle and a second outlet connected to the sCO2 bottoming cycle , wherein the sCO2 bottoming cycle is an overexpanded, recuperated Brayton cycle , characterised in that the heat exchanger is disposed within an exhaust casing , and wherein the heat exchanger is a plate/fin style heat exchanger disposed on one or more internal surface of the exhaust casing . a primary flowpath (C) fluidly connecting a compressor section (24; 110), a combustor section (26; 120), and a turbine section (28; 130); and a heat exchanger disposed in the primary flowpath (C), aft of and downstream of the turbine section (28; 130), the heat exchanger including a first inlet for receiving fluid from the primary flowpath (C) and a first outlet for expelling fluid received at the first inlet, the heat exchanger further including a second inlet fluidly connected to a supercritical CO2 (sCO2) bottoming cycle and a second outlet connected to the sCO2 bottoming cycle , wherein the sCO2 bottoming cycle is an overexpanded, recuperated Brayton cycle , characterised in that the heat exchanger is disposed within an exhaust casing , and wherein the heat exchanger is a plate/fin style heat exchanger disposed on one or more internal surface of the exhaust casing .
A wind turbine rotor blade imaging arrangement , comprising - a multi-axis gimbal mounted to the exterior of the wind turbine and configured to adjust its orientation in response to one or more received gimbal settings (10_α, 10_β, 10_γ), in particular wherein the gimbal settings comprise any of a pitch angle (10_α), a roll angle (10_β), a yaw angle (10_γ); - a camera mounted on the multi-axis gimbal and arranged to capture images of a rotor blade ; - an image analysis unit configured to analyze the captured images and generating image analysis output (110_out); and characterized by - a camera orientation controller configured to compute updated gimbal settings (10_α, 10_β, 10_γ) on the basis of the image analysis output (110_out). - a multi-axis gimbal mounted to the exterior of the wind turbine and configured to adjust its orientation in response to one or more received gimbal settings (10_α, 10_β, 10_γ), in particular wherein the gimbal settings comprise any of a pitch angle (10_α), a roll angle (10_β), a yaw angle (10_γ); - a camera mounted on the multi-axis gimbal and arranged to capture images of a rotor blade ; - an image analysis unit configured to analyze the captured images and generating image analysis output (110_out); and characterized by - a camera orientation controller configured to compute updated gimbal settings (10_α, 10_β, 10_γ) on the basis of the image analysis output (110_out).
A seat restraint system for use in a vehicle seat, the system comprising a vehicle seat being adjustable in a height direction and in a longitudinal direction, said vehicle seat comprising a seat frame with a slider which slidingly engages a guiding rail which is configured to be fixedly supported by a vehicle body ; and wherein the system further comprises a retraction arrangement configured to extend along a longitudinally extending inner or exterior wall portion of the guiding rail ; and a connector having a free length allowing the vehicle seat to be adjusted between minimum and maximum height positions and/or minimum and maximum longitudinal positions of the vehicle seat , and the connector having a first end connected to a driver of the retraction arrangement , and a second end connected to a reinforcing tube extending in the transverse direction between a respective rear end portion of two opposing longitudinally extending frame members of the seat frame ; and wherein the retraction arrangement is configured to, upon an activation signal, be activated to eliminate any slack of the connector . a vehicle seat being adjustable in a height direction and in a longitudinal direction, said vehicle seat comprising a seat frame with a slider which slidingly engages a guiding rail which is configured to be fixedly supported by a vehicle body ; and wherein the system further comprises a retraction arrangement configured to extend along a longitudinally extending inner or exterior wall portion of the guiding rail ; and a connector having a free length allowing the vehicle seat to be adjusted between minimum and maximum height positions and/or minimum and maximum longitudinal positions of the vehicle seat , and the connector having a first end connected to a driver of the retraction arrangement , and a second end connected to a reinforcing tube extending in the transverse direction between a respective rear end portion of two opposing longitudinally extending frame members of the seat frame ; and wherein the retraction arrangement is configured to, upon an activation signal, be activated to eliminate any slack of the connector .
A method for transmitting, by a user equipment, UE, (12; 900) uplink control information, UCI, in a wireless communication system , wherein the UCI includes a hybrid automatic repeat request, HARQ, acknowledgement, ACK, feedback, the method comprising: splitting (S100) the UCI for a plurality of cells into a physical uplink control channel, PUCCH, and a physical uplink shared channel, PUSCH, wherein splitting the UCI includes: allocating a first portion of a HARQ-ACK feedback included in the UCI to the PUCCH up to a maximum allowed bits first; and allocating a second portion of the HARQ-ACK feedback included in the UCI to the PUSCH, which second portion remains after allocating the first portion of the HARQ-ACK feedback to the PUCCH; and transmitting (S110) the split UCI, wherein the first portion and the second portion of the HARQ-ACK feedback are transmitted via the PUCCH and the PUSCH, respectively, wherein the UCI further includes channel state information, CSI, feedback. splitting (S100) the UCI for a plurality of cells into a physical uplink control channel, PUCCH, and a physical uplink shared channel, PUSCH, wherein splitting the UCI includes: allocating a first portion of a HARQ-ACK feedback included in the UCI to the PUCCH up to a maximum allowed bits first; and allocating a second portion of the HARQ-ACK feedback included in the UCI to the PUSCH, which second portion remains after allocating the first portion of the HARQ-ACK feedback to the PUCCH; and allocating a first portion of a HARQ-ACK feedback included in the UCI to the PUCCH up to a maximum allowed bits first; and allocating a second portion of the HARQ-ACK feedback included in the UCI to the PUSCH, which second portion remains after allocating the first portion of the HARQ-ACK feedback to the PUCCH; and transmitting (S110) the split UCI, wherein the first portion and the second portion of the HARQ-ACK feedback are transmitted via the PUCCH and the PUSCH, respectively, wherein the UCI further includes channel state information, CSI, feedback.
A friction damper, particularly suitable for a bogie suspension system, suitable to be placed in a guide of the bogie suspension system, the friction damper containing a guide cylinder suitable to be mounted between a fifth wheel coupling of the bogie suspension system and the guide of the bogie suspension system, which guide cylinder is closed from one side and has a spring element inside, which guide cylinder comprises a slidable friction element , characterised in that the guide cylinder is closed from one side by a closing cap , in the shape of a horizontal C that includes the outer wall of the guide cylinder when mounted horizontally, with an inner flange on the opposite side, whereas the spring element placed inside the guide cylinder is adjacent to the slidable friction element in the shape of a cylinder fitted with a flange the diameter of which corresponds to the inner diameter of the guide cylinder , whereas the flange is located inside the guide cylinder , while the remaining part of the friction element protrudes outside the guide cylinder ; wherein, when the spring element is most stretched, the flange of the friction element rests on the inner flange of the guide cylinder .
Method for processing plate-shaped workpieces , in particular of wood or wood substitutes, in which the following steps are carried out: a. Providing a large-format plate , in particular of wood or wood substitutes, and supplying (P1) the large-format plate to a singulating station , b. singulating plate-shaped workpieces by dividing up the supplied large-format plate in the singulating station wherein cuts are made in the large-format plate by at least one singulating assembly , c. supplying the thus singulated workpieces to at least one downstream processing station (2, 3; 110, 111, 112) in order to finish off the plate-shaped workpiece , wherein in step b. at least one part of each singulated workpiece receives from the singulating assembly an alignment section for engagement by gripping elements and/or for introducing reference bores, wherein the alignment section is a section which protrudes beyond the subsequently obtained finished format of the separated workpiece, wherein the workpiece provided with the alignment section is, after its singulation, taken over by means of a gripping element , engagement element or grasping element which engages with form-locking engagement on the alignment section , wherein the gripping element, engagement element or grasping element which engages with form-locking engagement on the alignment section of the workpiece runs after the take-over through a circuit , characterised in that the alignment section is removed in or after step c. by a finishing or separating cut. a. Providing a large-format plate , in particular of wood or wood substitutes, and supplying (P1) the large-format plate to a singulating station , b. singulating plate-shaped workpieces by dividing up the supplied large-format plate in the singulating station wherein cuts are made in the large-format plate by at least one singulating assembly , c. supplying the thus singulated workpieces to at least one downstream processing station (2, 3; 110, 111, 112) in order to finish off the plate-shaped workpiece ,
An air turbine starter , comprising: a housing defining an inlet , an outlet , and a flow path extending between the inlet and the outlet for communicating a flow of gas there through; a turbine member journaled within the housing and disposed within the flow path for rotatably extracting mechanical power from the flow of gas; a drive shaft operably coupled with the turbine member and configured to provide a rotational output; the air turbine starter being characterised in that it comprises a foil-air bearing assembly configured to rotatably support the drive shaft at a forward side of the turbine member . a housing defining an inlet , an outlet , and a flow path extending between the inlet and the outlet for communicating a flow of gas there through; a turbine member journaled within the housing and disposed within the flow path for rotatably extracting mechanical power from the flow of gas; a drive shaft operably coupled with the turbine member and configured to provide a rotational output; the air turbine starter being characterised in that it comprises a foil-air bearing assembly configured to rotatably support the drive shaft at a forward side of the turbine member .
A fan for a gas turbine engine , comprising: a rotor disk ; a plurality of airfoils extending radially outwardly from the rotor disk , each airfoil of the plurality of airfoils being circumferentially spaced apart from one another; a plurality of discrete fan platforms being disposed between adjacent ones of the plurality of airfoils , wherein each fan platform comprises a flow path surface extending between a first and a second side , an inner surface extending between the first and second sides , the inner surface radially opposing the flow path surface ; wherein each of: said fan platforms further comprises a body portion extending radially inwardly from the inner surface and attached to the rotor disk ; and characterized by further comprising: a plurality of sheaths , each sheath covering a leading edge of a respective airfoil wherein the sheath is formed from a different material than the airfoil ; and at least a first conductive path for grounding one of the plurality of sheaths , the at least first conductive path (90; 490) traveling from the sheath via the first side and the body portion of one of the plurality of discrete fan platforms to the rotor disk . a rotor disk ; a plurality of airfoils extending radially outwardly from the rotor disk , each airfoil of the plurality of airfoils being circumferentially spaced apart from one another; a plurality of discrete fan platforms being disposed between adjacent ones of the plurality of airfoils , wherein each fan platform comprises a flow path surface extending between a first and a second side , an inner surface extending between the first and second sides , the inner surface radially opposing the flow path surface ; wherein each of: said fan platforms further comprises a body portion extending radially inwardly from the inner surface and attached to the rotor disk ; and characterized by further comprising: a plurality of sheaths , each sheath covering a leading edge of a respective airfoil wherein the sheath is formed from a different material than the airfoil ; and at least a first conductive path for grounding one of the plurality of sheaths , the at least first conductive path (90; 490) traveling from the sheath via the first side and the body portion of one of the plurality of discrete fan platforms to the rotor disk . a plurality of sheaths , each sheath covering a leading edge of a respective airfoil wherein the sheath is formed from a different material than the airfoil ; and at least a first conductive path for grounding one of the plurality of sheaths , the at least first conductive path (90; 490) traveling from the sheath via the first side and the body portion of one of the plurality of discrete fan platforms to the rotor disk .
A sorbent comprising a titanium-glyoxal complex and a porous support material, wherein the porous support material comprises at least one of activated carbon, graphene, graphene oxide, silicon, or porous silicon.
A method for treating pea soluble fractions, comprising: a) a step of preparation of soluble fractions comprising (i) the preparation of a starch milk, by mixing pea flour and water in a kneading machine, (ii) the preparation of a protein-rich product by extraction of the starch and the fibers from said starch milk from step i), (iii) a flocculation operation by thermocoagulation on said protein-rich product from step ii); (iv) a separation operation of the product obtained from step iii) to obtain a floc and a supernatant called soluble fractions, b) a step of microfiltration or centrifugation of said soluble fractions resulting in a microfiltration permeate or a centrifugation supernatant, c) followed by a step of ultrafiltration of the microfiltration permeate or of the centrifugation supernatant, resulting in an ultrafiltration permeate and an ultrafiltration retentate, d) followed by an optional step of reverse osmosis of said ultrafiltration permeate, resulting in a permeate and a retentate from the reverse osmosis. a) a step of preparation of soluble fractions comprising (i) the preparation of a starch milk, by mixing pea flour and water in a kneading machine, (ii) the preparation of a protein-rich product by extraction of the starch and the fibers from said starch milk from step i), (iii) a flocculation operation by thermocoagulation on said protein-rich product from step ii); (iv) a separation operation of the product obtained from step iii) to obtain a floc and a supernatant called soluble fractions, (i) the preparation of a starch milk, by mixing pea flour and water in a kneading machine, (ii) the preparation of a protein-rich product by extraction of the starch and the fibers from said starch milk from step i), (iii) a flocculation operation by thermocoagulation on said protein-rich product from step ii); (iv) a separation operation of the product obtained from step iii) to obtain a floc and a supernatant called soluble fractions, b) a step of microfiltration or centrifugation of said soluble fractions resulting in a microfiltration permeate or a centrifugation supernatant, c) followed by a step of ultrafiltration of the microfiltration permeate or of the centrifugation supernatant, resulting in an ultrafiltration permeate and an ultrafiltration retentate, d) followed by an optional step of reverse osmosis of said ultrafiltration permeate, resulting in a permeate and a retentate from the reverse osmosis.
An air conditioner, comprising: a base , an air duct component provided on the base , wherein the air duct component comprises a bottom case with a water passage ; a water receiving structure provided on the base and comprising: a housing provided with a water catcher and a drainage pipe wherein the drainage pipe is in communication with the water catcher and extends out of the housing ; a connecting passage between the water catcher and the water passage ; a lug , wherein the lug is fixedly mounted on the housing ; and a switch matching structure , the air conditioner characterized in that the switch matching structure is provided on the base , and the lug is configured to match with the switch matching structure to switch a connecting passage between the water catcher and the water passage of the bottom case of the air duct component. a base , an air duct component provided on the base , wherein the air duct component comprises a bottom case with a water passage ; a water receiving structure provided on the base and comprising: a housing provided with a water catcher and a drainage pipe wherein the drainage pipe is in communication with the water catcher and extends out of the housing ; a connecting passage between the water catcher and the water passage ; a lug , wherein the lug is fixedly mounted on the housing ; and a switch matching structure , the air conditioner characterized in that the switch matching structure is provided on the base , and the lug is configured to match with the switch matching structure to switch a connecting passage between the water catcher and the water passage of the bottom case of the air duct component. a housing provided with a water catcher and a drainage pipe wherein the drainage pipe is in communication with the water catcher and extends out of the housing ; a connecting passage between the water catcher and the water passage ; a lug , wherein the lug is fixedly mounted on the housing ; and a switch matching structure , the air conditioner characterized in that the switch matching structure is provided on the base , and the lug is configured to match with the switch matching structure to switch a connecting passage between the water catcher and the water passage of the bottom case of the air duct component.
An aircraft landing gear shock absorber strut including: an outer cylinder defining a bore; a sliding tube slidingly coupled to the outer cylinder to permit the shock absorber strut to extend and compress and having a piston at one end mounted within the bore; one of the outer cylinder and the sliding tube being formed from a titanium part and being arranged to define a bearing counter-face ; and a non-metallic bearing arranged to run against the titanium counter-face, wherein the bearing counter-face is defined by a layer of the titanium part which has received a hardening surface modification distinct from a heat treatment such that the bearing counter-face is relatively hard in comparison to the titanium material behind the counter-face, wherein, the hardening surface modification does not substantially change the dimension of the part after machining, characterised in that the surface modification treatment comprises boriding. an outer cylinder defining a bore; a sliding tube slidingly coupled to the outer cylinder to permit the shock absorber strut to extend and compress and having a piston at one end mounted within the bore; one of the outer cylinder and the sliding tube being formed from a titanium part and being arranged to define a bearing counter-face ; and a non-metallic bearing arranged to run against the titanium counter-face, wherein the bearing counter-face is defined by a layer of the titanium part which has received a hardening surface modification distinct from a heat treatment such that the bearing counter-face is relatively hard in comparison to the titanium material behind the counter-face, wherein, the hardening surface modification does not substantially change the dimension of the part after machining, characterised in that the surface modification treatment comprises boriding.
A system for the identification of micro-organisms, the system comprising: an irradiation unit adapted to sequentially provide coherent electromagnetic radiation of multiple wavelengths along a common optical path; a holder adapted to retain a substrate having a surface adapted for growth of a micro-organism colony; a beamsplitter adapted to direct the coherent electromagnetic radiation from the common optical path towards the retained substrate; an imager arranged opposite the beamsplitter from the retained substrate and adapted to obtain images of backward-scattered light patterns from the micro-organism colony irradiated by the respective wavelengths of the directed coherent electromagnetic radiation; and a controller configured to: operate the imager to obtain a first image and a second image of backward-scattered light patterns from the micro-organism colony, the first image corresponding to a first wavelength and the second image corresponding to a second, different wavelength. an irradiation unit adapted to sequentially provide coherent electromagnetic radiation of multiple wavelengths along a common optical path; a holder adapted to retain a substrate having a surface adapted for growth of a micro-organism colony; a beamsplitter adapted to direct the coherent electromagnetic radiation from the common optical path towards the retained substrate; an imager arranged opposite the beamsplitter from the retained substrate and adapted to obtain images of backward-scattered light patterns from the micro-organism colony irradiated by the respective wavelengths of the directed coherent electromagnetic radiation; and a controller configured to: operate the imager to obtain a first image and a second image of backward-scattered light patterns from the micro-organism colony, the first image corresponding to a first wavelength and the second image corresponding to a second, different wavelength.