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公开(公告)号:US10252709B2
公开(公告)日:2019-04-09
申请号:US15206766
申请日:2016-07-11
IPC分类号: B60W10/06 , B60W40/11 , F01D1/14 , A01G25/16 , A01G25/00 , E02D29/12 , E02D29/14 , E03B7/09 , E03B9/08 , E03B9/10 , E03B11/14 , H02G9/10 , B62K11/02 , B65D25/28 , B65D88/76 , H02G9/02 , H05K5/02
摘要: A motorcycle including a frame to which an internal combustion engine is associated, from which internal combustion engine at least one exhaust pipe of combusted gases departs, the exhaust pipe having an open terminal, the frame mounted on a front wheel and a rear wheel, a control board or unit included, for controlling torque produced by the engine and other parameters such as velocity of the vehicle and spatial position thereof with respect to the road surface. The motorcycle including a system to verify when the front wheel of the motorcycle detaches from the road surface during acceleration. The system includes a choke for partializing the section of the exhaust gases outlet area from the exhaust pipe, during partialization. The partialization obtained as a function of the torque produced by the engine and the position of the front wheel with respect to the road surface.
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公开(公告)号:US20180291741A1
公开(公告)日:2018-10-11
申请号:US16008301
申请日:2018-06-14
申请人: Jeajun Lee , Sanghoon Lee , Sung Keun Oh , Sangmyeong Lee , Juchang Lim
发明人: Jeajun Lee , Sanghoon Lee , Sung Keun Oh , Sangmyeong Lee , Juchang Lim
摘要: Disclosed is a reaction-type steam turbine, including: a housing provided at a first side thereof with a steam inlet tube and at a second side thereof with a steam outlet tube, the housing having a space formed therein; and a turbine shaft provided to pass through the space of the housing, with a plurality of disk blades fitted over the turbine shaft, wherein a guide blade assembly is coupled to the turbine shaft at a position between a duct of the steam inlet tube and the disk blades, the guide blade assembly guiding steam introduced through the steam inlet tube into the space of the housing toward the disk blades.
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公开(公告)号:US09206784B2
公开(公告)日:2015-12-08
申请号:US13505077
申请日:2010-11-02
申请人: Giancarlo Alfonsi
发明人: Giancarlo Alfonsi
CPC分类号: F03B3/08 , F01D1/14 , F03B3/16 , F03B11/02 , F03D3/0427 , F05B2240/13 , F05B2240/217 , Y02E10/223 , Y02E10/226 , Y02E10/74
摘要: A high-performance turbine, particularly with increased specific power, including a rotor and a distribution apparatus which is adapted to convey a fluid stream onto the elements of the rotor for the rotation of the rotor about its own rotation axis, where the rotor includes a plurality of thrust ducts adapted to receive the fluid stream conveyed by the distribution apparatus to generate a rotary thrust on the surrounding walls of the thrust ducts, the turbine further including at least one slot, which is formed on the walls of the thrust ducts and/or of the distribution apparatus and is adapted to connect the fluid stream to the outside environment of the turbine, where at least one of the thrust ducts and the distribution apparatus crossed by the fluid stream includes at least one portion that converges in the direction in which the fluid stream travels, which is defined upstream of the slot in the direction of travel of the fluid stream for the at least local lowering of the pressure inside the thrust ducts and/or the distribution apparatus, which are crossed by the fluid stream, below the value of the pressure of the filling fluid of the outside environment, with consequent suction of the filling fluid into the thrust ducts and/or the distribution apparatus which are crossed by the fluid stream.
摘要翻译: 一种高性能涡轮机,特别是具有增加的比功率,包括转子和分配装置,其适于将流体流输送到转子的元件上,以使转子围绕其自身的旋转轴旋转,其中转子包括 多个推力管道,其适于接收由分配装置输送的流体流,以在推力管道的周围壁上产生旋转推力,涡轮机还包括至少一个狭槽,其形成在推力导管的壁上和/ 或分配装置,并且适于将流体流连接到涡轮机的外部环境,其中推力导管和分配装置中的至少一个与流体流交叉包括至少一个沿其方向会聚的部分, 流体流在流体流的行进方向上限定在槽的上游,用于至少局部地降低加压 e内的推力管道和/或分配装置,其被流体流交叉,低于外部环境的填充流体的压力值,随后将填充流体吸入推力管道和/或 分配装置由流体流交叉。
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公开(公告)号:US2743901A
公开(公告)日:1956-05-01
申请号:US14378350
申请日:1950-02-11
申请人: GARRAWAY GEORGE H
发明人: GARRAWAY GEORGE H
CPC分类号: F01D1/14 , F01D17/145 , F01D17/205 , Y02T50/671 , Y10T137/2943
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公开(公告)号:US2524549A
公开(公告)日:1950-10-03
申请号:US60438345
申请日:1945-07-11
申请人: OSCAR THEIMER
发明人: OSCAR THEIMER
CPC分类号: F01D1/28 , F01D1/14 , F03B1/00 , Y02E10/223
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公开(公告)号:US20180156188A1
公开(公告)日:2018-06-07
申请号:US15730207
申请日:2017-10-11
申请人: Gilbert Ly
发明人: Gilbert Ly
CPC分类号: F03B17/005 , F01D1/06 , F01D1/14 , F03B3/02 , F03B3/106 , F03B3/125 , Y02E10/223
摘要: A power unit including an enclosed housing, a shaft passing through the central section of the enclosed, a motor located outside the housing and mounted to the first end of the shaft, a turbine located inside the housing and mounted into the shaft, the turbine includes a hub, a top end, a bottom end, and blades, sealing fins located at the bottom end of the turbine; and a pump located inside the housing and mounted on the turbine. The pump includes fins that are inserted in grooves located on the hub of the turbine. The fins of the pump are joined to the blades of the turbine creating that the pump, turbine, and shaft move as unitary unit. The fins of the pump maintained by two spaced crowns by insertion form cells that guide a flow of fluid. A space free of fluid with a defined volume occupies the bottom end of the pump. In a non-working position, the space free of fluid has a cylindrical shape. In a working position, because of rotation of the fluid, the space free of fluid has a paraboloid shape. The rotation of the fluid at a minimum angular velocity creates a virtual barrier, and generates a thrust.
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公开(公告)号:US20150159547A1
公开(公告)日:2015-06-11
申请号:US14564700
申请日:2014-12-09
申请人: Pawel Bakula , Andrew Day , James Mawer , James Williams
发明人: Pawel Bakula , Andrew Day , James Mawer , James Williams
IPC分类号: F02B37/22 , F01D17/14 , F02B37/013 , F01D1/14
CPC分类号: F02B37/22 , F01D1/14 , F01D17/141 , F02B37/001 , F02B37/007 , F02B37/24 , F05D2220/40 , Y02T10/144
摘要: A turbocharger (10) with a cross flow turbine (30) where exhaust gas passes through a cross flow turbine wheel (18) on its outer diameter. A cross flow turbine (30) has radial exhaust gas inlet and outlet. Cross flow turbines (30) are suited for variable turbine geometry, including with a single guide vane (44) or multiple guide vanes in the turbine inlet (34) to control variable flow and thus performance of the turbine stage. Cross flow turbines (30) allow reduced size and excellent packaging options, such as a single or dual cross flow turbine wheel (18) between two compressor wheels (12).
摘要翻译: 一种具有横流涡轮机(30)的涡轮增压器(10),其中废气在其外径上通过横流涡轮机叶轮(18)。 横流式涡轮机(30)具有径向排气入口和出口。 横流涡轮机(30)适用于可变涡轮机几何形状,包括在涡轮机入口(34)中具有单个导向叶片(44)或多个导向叶片,以控制涡轮机级的可变流量并由此执行。 横流涡轮机(30)允许减小尺寸和优异的包装选项,例如在两个压缩机叶轮(12)之间的单或双横流涡轮机叶轮(18)。
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公开(公告)号:US4390316A
公开(公告)日:1983-06-28
申请号:US256182
申请日:1981-04-21
申请人: John R. Alison
发明人: John R. Alison
CPC分类号: F01D1/14 , F01D5/141 , Y02T50/673
摘要: A simple, rugged and wide velocity range radial flow turbine wheel, with entry flow radially inward and exhaust flow radially outward, has an efficient integral fluid-dynamic multiple staging system needing no stationary devices for redirecting the fluid. Consequently there are no clearance problems, and it can be used with all fluids, including contaminated ones. The tangentially-entering fluid stream is captured and trapped in an annular passageway between an outer set of circumferentially mounted blades and a carefully coordinated inner set of circumferentially mounted planar surfaces. Energy is extracted from the stream when the flow direction is changed each time the faster-moving fluid is vectored radially inwardly from a blade to an inner surface, then vectored radially outwardly to the next blade, then to the next inner surface, etc. All of the pressure, lift and drag forces contribute to turbine output. Flow of the fluid continues around the annular passageway, which also has integral lateral boundaries, until such time as the relative velocity of the fluid and the rotating blades reaches zero. Then the fluid is exhausted radially outwardly by centrifugal force between the blades, which can no longer maintain their trapping action. Because fluid exhaust can occur anywhere on the periphery except in the entry zone itself, flow conditions in the wheel can adapt to wide ranges of speed and loading. The fluid can experience thousands of degrees of magnitude of angular directional change in a single circumferential passage relative to the moving wheel.
摘要翻译: 一个简单,坚固和宽的速度范围的径向涡轮机叶轮,其入口流径向向内并且排气径向向外流动,具有有效的整体式流体动态多级分级系统,不需要固定装置来重定向流体。 因此,不存在间隙问题,可用于所有流体,包括污染物。 切向进入的流体流被捕获并且被捕获在外部周向安装的叶片组之间的环形通道中以及仔细协调的内部组的周向安装的平面表面之间。 当流动方向改变时,每当快速移动的流体从叶片向内径向向内移动到内表面时,从流中提取能量,然后径向向外定向到下一个叶片,然后到下一个内表面等。所有 的压力,升力和牵引力有助于涡轮机输出。 流体的流动在环形通道周围继续,环形通道也具有积分的横向边界,直到流体和旋转叶片的相对速度达到零的时间为止。 然后通过叶片之间的离心力使流体径向向外排出,这不能维持其捕获作用。 由于流体排放可能发生在外围的任何位置,除了进入区域本身,车轮中的流动条件可适应宽范围的速度和负载。 在相对于移动轮的单个周向通道中,流体可以经历数千度的角度方向变化。
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公开(公告)号:US4231702A
公开(公告)日:1980-11-04
申请号:US069424
申请日:1979-08-24
CPC分类号: F01D1/14 , F04D17/127 , F04D29/286 , Y10S415/913
摘要: A two stage compressor and the like which comprises first and second stage impellers, an inlet to and an outlet from each impeller stage, a crossover passage means from the first outlet to the second inlet located crossing the first inlet, adjustable guide vanes in the first inlet and fixed de-swirl vanes in the first outlet, the inlet to the second stage impeller being located radially inwardly to that of the first stage impeller.
摘要翻译: 包括第一和第二级叶轮的两级压缩机等,每个叶轮级的入口和出口,从第一出口到位于与第一入口相交的第二入口的交叉通道装置,第一 入口和固定的旋流叶片在第一出口处,第二级叶轮的入口径向向内定位到第一级叶轮的入口。
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公开(公告)号:US3833006A
公开(公告)日:1974-09-03
申请号:US31133972
申请日:1972-12-01
申请人: ALLIS CHALMERS
发明人: TEMPLE W
CPC分类号: A01F12/444
摘要: A transverse fan for use in the cleaning and separating mechanism of a combine harvester and wherein such transverse fan is provided with a choke vane mechanism positioned in the air inlet for such fan, and with a damper mechanism positioned in the air outlet of such fan, such mechanisms being adjustable, singularly or in combination to vary the amount of air being delivered by such fan.
摘要翻译: 一种用于联合收割机的清洗和分离机构的横向风扇,其中这种横向风扇设置有位于该风扇的空气入口中的阻风门机构,并且具有定位在该风扇的出风口中的阻尼机构, 这种机构是可调节的,单独的或组合的以改变由这种风扇输送的空气量。
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