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公开(公告)号:US12123422B2
公开(公告)日:2024-10-22
申请号:US17856053
申请日:2022-07-01
申请人: Larry P. Lapointe
发明人: Larry P. Lapointe
摘要: A fan apparatus may include a frame, a fan, and a drive mechanism. The fan may be supported for rotation relative to the frame and may include a fan shaft and a plurality of blades extending outward from the fan shaft. The drive mechanism may include a driven wheel, a drive shaft, a first drive wheel, a second drive wheel, and a torque-transmission loop. The driven wheel may be mounted on the fan shaft. The drive shaft may be supported for rotation relative to the frame. The first drive wheel may be mounted on the drive shaft. The second drive wheel may be mounted on the drive shaft. The torque-transmission loop may be engaged with the driven wheel and a selected one of the first and second drive wheels.
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公开(公告)号:US20240011493A1
公开(公告)日:2024-01-11
申请号:US18253638
申请日:2021-11-24
CPC分类号: F04D17/12 , F04D17/02 , F04D25/16 , F04D29/284 , F04D29/582
摘要: The compressor is used for processing a CO2 flow; a first compressor stage has a first row of blades with a first number of blades and a second compressor stage, downstream the first compressor stage, has a second row of blades with a second number of blades; the number of blades of the first compressor stage is less than the number of blades of the second compressor stage; there is an annular gap between the first row of blades and the second row of blades; the first compression stage (200) is designed so to assure that the CO2 flow is in supercritical condition, preferably close to CO2 critical point, at its outlet, and so that the second compressor stage process CO2 in supercritical condition.
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公开(公告)号:US20230067553A1
公开(公告)日:2023-03-02
申请号:US17864236
申请日:2022-07-13
发明人: Mu-Shu FAN , Chien-Yu CHEN , Ming-Yuan CHIANG
摘要: A liquid cooling head includes an upper casing, an impeller, a bottom casing and a skived fin cooling plate. The upper casing has an inlet and an outlet, the upper casing is fixed on the bottom casing, and the impeller is arranged between the upper casing and the skived fin cooling plate. In addition, the skived fin cooling plate is fixed on the bottom casing, and the impeller sucks the heat-dissipating liquid from the inlet and drives the heat-dissipating liquid passing through the skived fin cooling plate, upwardly passing through the impeller and then discharged from the outlet.
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公开(公告)号:US11448235B2
公开(公告)日:2022-09-20
申请号:US16921499
申请日:2020-07-06
IPC分类号: F04D29/46 , F04D17/02 , F04D29/56 , F01D17/16 , F04D19/02 , F04D29/42 , F02C3/04 , F04D29/40
摘要: An example compressor includes a casing having a main portion and an outer skirt collectively defining an annular plenum, an outlet guide vane coupled to the main portion, an actuator mounted outside the outer skirt, and a linkage coupled to the actuator and the outlet guide vane through the annular plenum.
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公开(公告)号:US11041503B2
公开(公告)日:2021-06-22
申请号:US15759838
申请日:2016-09-14
发明人: Giuseppe Iurisci , Simone Corbo
摘要: A turbomachine impeller is disclosed, which includes: a hub having a rotation axis; a shroud; a plurality of blades between the hub and the shroud; and a plurality of flow vanes, each flow vane being defined between the hub, the shroud and neighboring blades, each flow vane having a flow vane inlet and a flow vane outlet. Each flow vane extends radially inwardly from the flow vane inlet towards a radially innermost flow vane section, and from the radially innermost flow vane section to a flow vane outlet.
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公开(公告)号:US20210062824A1
公开(公告)日:2021-03-04
申请号:US16579011
申请日:2019-09-23
发明人: Michael Nesteroff , Jonathan Acker , Jeffrey Crutchfield , Nate Cooper , Mark Whitlock , Nathan Ottow
摘要: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a high pressure air source, an air piston mounted between an engine casing and the shroud and adapted to receive high pressure air from the high pressure air source, a mounting arm coupling the shroud and air piston, and a slidable coupling adapted to allow axial movement of the shroud and joining the shroud to an axial member.
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公开(公告)号:US20200333028A1
公开(公告)日:2020-10-22
申请号:US16850304
申请日:2020-04-16
申请人: Henry I. Patel , Aviraj H. Patel , Niraj H. Patel
发明人: Henry I. Patel , Aviraj H. Patel , Niraj H. Patel
摘要: A blower apparatus designed for PTAC use includes an impeller configured to be capable of rotating about a central axis; a low voltage DC motor arranged to drive the impeller; a housing configured to accommodate the motor and impeller fixed together; an inlet cover which draws fresh air into the apparatus and an outlet port that discharges the fresh air through an outlet port and at least two directional changes perpendicular to the flow of fresh air through the inlet.
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公开(公告)号:US10605256B2
公开(公告)日:2020-03-31
申请号:US16015718
申请日:2018-06-22
申请人: BorgWarner Inc.
IPC分类号: F04D29/16 , F04D29/32 , F04D25/06 , F04D29/54 , F04D19/00 , F04D17/02 , F04D29/66 , F04D29/52 , F04D25/08
摘要: The invention refers to a fan system (10) comprising a fan shroud (14) and a ring fan (12) having a hub (30), a plurality of fan blades (32), and a ring structure (34). The ring structure (34) has a ring member (46) and a flange member (48), the ring member (46) having a hollow cylindrical shape, the flange member (48) extending radially outwardly from the ring member (46). The fan shroud (14) has an annular shroud flange (54), a shroud body (56) and a plurality of shroud guide vanes (58), the shroud flange (54) extending radially outwardly from the shroud body (56) and being disposed along the rotary axis (A) between the flange member (48) and the shroud body (56), the shroud body (56) being disposed about the ring member (46) and having a first body portion (70), a second body portion (72) and a divergent nozzle (74). A recirculation throttle (88) is formed by the shroud body (56) and the ring member (46) at a location where the first and second body portions (70, 72) of the shroud body (56) intersect one another. The divergent nozzle (74) and a trailing end (50) of the ring member (46) cooperate to form a dynamic sealing feature (90).
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公开(公告)号:US10598181B2
公开(公告)日:2020-03-24
申请号:US15827940
申请日:2017-11-30
申请人: Rayne Sung
发明人: Rayne Sung
摘要: A gas turbine engine, with a conical screw integrated compression system, that utilizes at least one conical screw as an intermediary fluid transport device to facilitate the multi-staging of non-axial compressors, such as centrifugal and diagonal compressors, as well as or alternatively to combine non-axial compressors to axial compressors and to the fan. The conical screw in the compression system applies axial flow translation and funnels, as necessary, the exit flow of the impeller, fan or compressor into the next impeller or compressor.
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公开(公告)号:US20200011343A1
公开(公告)日:2020-01-09
申请号:US16503608
申请日:2019-07-04
发明人: Yanhu LIN , Miao ZHANG , Yong LIN , Baixian XIAO
摘要: A wind wheel including a first air plate, a second air plate, and a plurality of blades disposed between the first air plate and the second air plate. The first air plate includes a central part and an air inlet disposed in the central part; each two adjacent blades form an air duct. The plurality of blades each includes an inlet section next to the air inlet, an intermediate section, and an outlet section. The thickness of the intermediate section is greater than the thickness of the inlet section and the thickness of the outlet section.
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