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公开(公告)号:US12129865B2
公开(公告)日:2024-10-29
申请号:US17900185
申请日:2022-08-31
申请人: BorgWarner Inc.
发明人: Markus Eisenbarth , Martin Schön
CPC分类号: F04D29/284 , F04D17/10 , F04D29/30 , F05D2220/40 , F05D2240/20
摘要: A compressor wheel for a compressor of a turbocharger has a hub (16) and a multiplicity of blades (12) on the hub (16). In intermediate spaces of the multiplicity of blades (12), a channel is in each case formed between a suction side (24) and a pressure side (26). The channel guides fluid that flows in axially in relation to a rotation axis (22) radially or radially-axially outward. The hub (16) in relation to the rotation axis (22) in at least one channel is contoured with a rotationally symmetrical portion (18′) and a non-rotationally symmetrical portion (18). The non-rotationally symmetrical portion (18) is formed by radii that are variable in the flow direction, and a transition region (28) between the hub (16) and the blade (12) adjoins the non-rotationally symmetrical portion (18).
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公开(公告)号:US12129856B2
公开(公告)日:2024-10-29
申请号:US17715916
申请日:2022-04-07
申请人: Yuriy Radzikh
发明人: Yuriy Radzikh
CPC分类号: F04D1/12 , F04D29/2255 , F04D29/288
摘要: A rotor having spiral pathways to enable liquid or gas to flow from a center to an exterior thereof. The spiral pathways increases power generated (input force) as liquid/gas travels therethrough. The spiral pathway rotor includes an inner disk and an outer disk. Inner disk includes a central opening for receiving the liquid/gas and is connected to a plurality of pathways that extend toward an outer edge in a spiral manner. Nozzles may be utilized to expel the liquid/gas. Outer disk includes an open interior having a plurality of teeth formed on an interior surface. The teeth are configured to receive the liquid/gas expelled from inner disk which causes the rotor to rotate and thus increases the input force thereof. The input force is amplified to an output force on a shaft connected thereto.
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公开(公告)号:US20240352941A1
公开(公告)日:2024-10-24
申请号:US18634974
申请日:2024-04-14
发明人: Fujin FENG , Xuesong LIU , Tao SHU , Yunjian SONG
CPC分类号: F04D29/286 , F04D17/12 , F04D29/624
摘要: The present invention discloses an air-floating centrifugal compressor, including a motor, an impeller, an air inlet, an outlet port, and a connection pipe. The motor includes a housing and a rotor, a first chamber and a second chamber are arranged at two ends inside the housing, and an air-floating radial bearing is arranged on the rotor. The impeller is fixed to the end of the rotor and is located in the first chamber and/or the second chamber. The air inlet of the first chamber is connected to the air inlet, and the air outlet is connected to one end of the connecting pipe, the air outlet of the second chamber is connected to the outlet port, and the air inlet is connected to the other end of the connecting pipe.
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公开(公告)号:US20240342412A1
公开(公告)日:2024-10-17
申请号:US18751603
申请日:2024-06-24
申请人: ResMed Pty Ltd
IPC分类号: A61M16/00 , A61M16/06 , A61M16/08 , F04D17/12 , F04D17/16 , F04D25/06 , F04D27/00 , F04D29/28 , F04D29/42 , F04D29/66
CPC分类号: A61M16/0066 , A61M16/0057 , A61M16/021 , A61M16/06 , A61M16/0666 , A61M16/0683 , A61M16/0694 , A61M16/0816 , A61M16/0875 , F04D17/12 , F04D17/164 , F04D25/0673 , F04D27/004 , F04D29/281 , F04D29/4206 , F04D29/664 , A61M2205/42 , A61M2205/8206 , A61M2205/8237 , A61M2209/086 , A61M2209/088
摘要: A head-mountable flow generator is configured to deliver a flow of breathable gas at a continuously positive pressure with respect to ambient air pressure to a patient interface in communication with an entrance to a patient's airways including at least an entrance of the patient's nares, while the patient is sleeping, to ameliorate sleep disordered breathing. The flow generator includes a motor, an impeller assembly and housing that encases the motor and the impeller assembly. The housing is configured to be mounted on the patient's head and comprises an inlet to receive the flow of breathable gas and a pair of opposing outlets to deliver the flow of breathable gas. In addition, the impeller assembly is configured to pressurize the flow of breathable gas received from the inlet, and the housing is configured to convey the pressurized flow of breathable gas through both outlets.
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公开(公告)号:US12115293B2
公开(公告)日:2024-10-15
申请号:US18483134
申请日:2023-10-09
发明人: Xuefeng Chen , Bang Yu Wang , Qing Hao Wang , De Bin Cao
CPC分类号: A61L9/205 , F04D29/281 , F04D29/4226 , F04D29/701 , F24F1/0022 , A61L2209/12 , A61L2209/16 , F24F8/22
摘要: A centrifugal fan for a heating, ventilation, air conditioning, and refrigeration (HVACR) system is disclosed. The centrifugal fan includes a volute housing having an inner surface and a curved inlet shroud. The volute housing defines an air outlet. The curved inlet shroud defines an air inlet. The air inlet has an inlet airflow cross-sectional area that lies substantially perpendicular to an outlet airflow cross-sectional area of the air outlet. The centrifugal fan also includes an impeller mounted for rotation about a rotational axis within the volute housing. The impeller has a plurality of fan blades. The plurality of fan blades has an outer surface. The centrifugal fan further includes a light source. The inner surface of the volute housing and the outer surface of the plurality of fan blades includes a photocatalyst layer. The light source is configured to emit light on the photocatalyst layer.
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公开(公告)号:US20240310062A1
公开(公告)日:2024-09-19
申请号:US18276384
申请日:2021-11-18
CPC分类号: F24F7/025 , F04D17/16 , F04D29/283
摘要: A rotary roof vent consisting of a base, an impeller, an axle holding/supporting a rotating rim with blades and a cover. The impeller is solid and formed as a rim with stiffeners, and the blades are located at the outside edges of the rim. A hollow sleeve is positioned at the central part for receiving an axle. The blades are formed having a convex shape. A protrusion positioned at an acute angle disposed at the end of each blade. Another protrusion is disposed at obtuse angle to the blade and is positioned closer to the center. The blades are inserted into the impeller by 20% in relation to the base diameter. The impeller stiffeners having arch shaped configuration are adapted to follow a contour of the blades.
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公开(公告)号:US12078186B2
公开(公告)日:2024-09-03
申请号:US18153685
申请日:2023-01-12
申请人: Carrier Corporation
发明人: Huiliang Zhang , Kai Deng
CPC分类号: F04D29/266 , F04D29/284
摘要: A locking structure of a compressor impeller, which includes: a rotary shaft; a lock nut arranged on an end of the rotary shaft by means of a threaded connection and provided with waist-shaped holes extending along a circumferential direction thereof; an impeller sleeved on the end of the rotary shaft and located on an inner side of the lock nut, the impeller is provided with threaded holes in communication with the waist-shaped holes of the lock nut; a nose piece located on an outer side of the lock nut and provided with through holes in communication with the waist-shaped holes of the lock nut; and bolts passing through the through holes and the waist-shaped holes in turn into the threaded holes, thereby fixing the nose piece, the lock nut and the impeller together.
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公开(公告)号:US12078184B2
公开(公告)日:2024-09-03
申请号:US18200763
申请日:2023-05-23
发明人: Kengo Shimojo , Kentaro Suzuki , Hidetaka Okui
CPC分类号: F04D27/002 , F04D27/0246 , F04D29/284 , F04D29/287 , F04D19/02 , F04D29/563 , F05D2250/51 , F05D2270/303
摘要: A compressor control device includes: an inlet guide vane disposed in an inlet section of a compressor; a variable stationary blade disposed downstream of the inlet guide vane; a rotor blade disposed between the inlet guide vane and the variable stationary blade; a first actuator for adjusting a first opening degree of the inlet guide vane; a second actuator for adjusting a second opening degree of the variable stationary blade; a compressor inlet temperature detection part for detecting a compressor inlet temperature in the inlet section; and a control part for controlling the first actuator and the second actuator. The control part controls the first actuator and the second actuator such that an opening degree ratio of the first opening degree to the second opening degree increases as the compressor inlet temperature decreases, if the compressor inlet temperature is less than a threshold.
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公开(公告)号:US12066027B2
公开(公告)日:2024-08-20
申请号:US18447852
申请日:2023-08-10
发明人: Shawn P. Lawlor
IPC分类号: F04D17/12 , F04D21/00 , F04D27/00 , F04D29/056 , F04D29/28
CPC分类号: F04D17/127 , F04D21/00 , F04D27/004 , F04D29/056 , F04D29/286
摘要: A counter-rotating supersonic compressor. A first subsonic rotor includes a plurality of unshrouded impulse rotor blades operating at sub-sonic conditions. A second, supersonic rotor includes a fixed second rotor portion and an adjustable second rotor portion. The fixed second rotor portion includes a plurality of supersonic passageways having converging-diverging sidewalls, and internal boundary layer bleed passageways. The adjustable second rotor portion includes a plurality of centerbodies which are disposed in the supersonic passageways. Helical movement (circumferential and axial) movement of the adjustable second rotor portion with respect to the fixed second rotor portion enables upstream and downstream movement of the centerbodies in the supersonic passageways. This movement facilitates ease of supersonic startup, and automatic adjustment for changes in operation conditions, such as pressure, temperature, or mass flow rate of a working fluid such as carbon dioxide.
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公开(公告)号:US20240255001A1
公开(公告)日:2024-08-01
申请号:US18257775
申请日:2021-11-25
发明人: Igor Makarenko , Stefan Reuter , Bernhard Lehmayr
CPC分类号: F04D29/284 , F04D25/024 , F04D29/30 , F05D2220/40 , F05D2240/301 , F05D2240/303
摘要: A compressor wheel is provided for an exhaust-gas turbocharger of an internal combustion engine. The compressor wheel has a hub, which extends around a central axis of the compressor wheel, and compressor wheel blades, which are connected to the hub and the blade leading edges of which extend in a radial direction and have a hub-side end region and an end region that is radially remote from the hub. The blade leading edges are blunt in their end region that is radially remote from the hub.
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