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1.发明申请公开(公告)号：US20180142619A1
公开(公告)日：2018-05-24
申请号：US15849640
申请日：2017-12-20
申请人： Li SU
发明人： Li SU
IPC分类号： F02C3/067 , F01D5/02 , F04D19/00 , F04D29/32 , F01D5/18 , F01D5/14 , F04D29/54 , F04D29/056 , F02C7/268 , F02C7/36
CPC分类号： F02C3/067 , F01D1/20 , F01D1/26 , F01D5/02 , F01D5/141 , F01D5/18 , F02C7/268 , F02C7/36 , F04D19/005 , F04D25/024 , F04D29/056 , F04D29/321 , F04D29/325 , F04D29/541 , F05D2260/31 , Y02T50/671
摘要： A multiple axle-sleeve driving bidirectional rotating wheel-shaped fan turbine and a bushing wheel-shaped fan compressor, including: a working component, a driving component, a structural and installed component and a starting component. A wheel-shaped fan of the turbine drives a corresponding wheel-shaped fan of compressor to rotate through a driving axle sleeve. A rotating direction of the wheel-shaped fan of the turbine is opposite to a rotating direction of a wheel-shaped fan adjacent to the wheel-fan and rotating speed of the plurality of wheel-shaped fan is different. Each of the auxiliary wheel-shape fans is respectively bushed on each of the wheel-shaped fans of the compressor. A turbojet assembled with this disclosure has a high functionality, a light weight, a quick heat dissipation, an excellent anti-surging and a low energy consumption.
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2.发明申请公开(公告)号：US20150204205A1
公开(公告)日：2015-07-23
申请号：US14161715
申请日：2014-01-23
摘要： The present invention titled: a coasting-wheel with aeronautic levitation for harmonic electric generation is a device to generate electric energy or power via the principle of electromagnetic induction during the phase of energy-in and during the coasting phase; energy-off. It differs from the conventional electric generators and alternators as such the latter include an element of stator and an element of rotor but in the present invention the armature and magnets undergo rotation. Second, all electric generators operate in non-harmonic mode, i.e., when the input fuel is turned off the electric generator or alternator stops but in the present invention the electricity is generated during the coasting phase. It differs from the well-known apparatus flywheel as such the latter is a storage device and not a device for electric generation. In the present invention the coasting wheel is discharging its rotational kinetic energy into electric energy instantaneously during its spinning phase when the source of energy is turned off as well as it generates electricity during the phase of energy-in.The present invention includes a unique method of rotation induced by thruster engines (converging diverging duct) suited in a rectangular wing for levitation. Normally, the electric generator or alternator operates with a piston engine or turbine.
摘要翻译： 本发明题为：具有用于谐波发电的航空悬浮的惯性轮是在能量入射期间和在滑行阶段期间通过电磁感应原理产生电能或电力的装置; 节能。 它与传统的发电机和交流发电机不同之处在于，后者包括定子的元件和转子的元件，但是在本发明中，电枢和磁体经历旋转。 第二，所有发电机以非谐波模式工作，即当输入燃料关闭时，发电机或交流发电机停机，但是在本发明中，在滑行期间产生电力。 它与众所周知的装置飞轮不同，因此后者是存储装置，而不是用于发电的装置。 在本发明中，当能量源被关闭时，滑行轮在其旋转阶段瞬间将其旋转的动能瞬间释放到电能中，并且在能量阶段期间发电。 本发明包括适用于悬挂在矩形翼中的推进器发动机（会聚发散管）引起的旋转的独特方法。 通常，发电机或交流发电机与活塞发动机或涡轮机一起工作。
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公开(公告)号：US08963359B2
公开(公告)日：2015-02-24
申请号：US13235359
申请日：2011-09-17
申请人： Steven Evans , Steven Evans, II , Frank D. Clark
发明人： Steven Evans , Steven Evans, II , Frank D. Clark
CPC分类号： F01D15/10 , F01D1/20 , F01D13/02 , F01D17/085 , F03D9/11 , F03D9/25 , F05B2220/602 , F05D2220/62 , Y02B10/30 , Y02E10/725
摘要： A co-generation apparatus for the generation of electricity from an external source of forced air is described in which the co-generation apparatus comprises a turbine, a generator, a co-generation control unit, and an adjustable standoff. The turbine is connected to the generator for the production of electricity. The generator interface electrically connects the generator to an electrical system. The co-generation control unit is connected to the turbine and generator interface. The forced air drives the turbine. The turbine can be positioned in a turbine housing that receives the forced air. An adjustable standoff is connected to the turbine. The standoff adjusts the position of the turbine relative to the forced air.
摘要翻译： 描述了用于从外部强制空气源产生电力的联合发电装置，其中共发电装置包括涡轮机，发电机，共发电控制单元和可调节支架。 涡轮机连接到发电机用于生产电力。 发电机接口将发电机电连接到电气系统。 联合发电控制单元连接到涡轮和发电机接口。 强制空气驱动涡轮。 涡轮机可以定位在接收强制空气的涡轮机壳体中。 可调节的支座连接到涡轮机。 间隔调整涡轮机相对于强制空气的位置。
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公开(公告)号：US08850813B2
公开(公告)日：2014-10-07
申请号：US13986381
申请日：2013-04-24
CPC分类号： F01D25/24 , F01D1/04 , F01D1/20 , F01D25/16 , F02C6/12 , F05D2220/40 , F05D2240/10
摘要： A turbocharger including a turbine wheel having a hub-to-tip ratio of no more than 60% and blades with a high turning angle, a turbine housing forming an inwardly spiraling primary-scroll passageway that significantly converges to produce highly accelerated airflow into the turbine at high circumferential angles, and a two-sided parallel compressor. The compressor and turbine each produce substantially no axial force, allowing the use of minimal axial thrust bearings. The bearing housing forms a shroud for the internal side of the compressor wheel.
摘要翻译： 一种涡轮增压器，包括具有不超过60％的毂与尖端比率的涡轮机叶轮和具有高转向角度的叶片;涡轮机壳体，其形成向内螺旋形的初级涡旋通道，其显着收缩以产生高度加速的气流进入涡轮机 在高周向角度和双面平行压缩机。 压缩机和涡轮机各自基本上不产生轴向力，允许使用最小的轴向推力轴承。 轴承座形成用于压缩机叶轮内侧的护罩。
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公开(公告)号：US08801360B2
公开(公告)日：2014-08-12
申请号：US12878850
申请日：2010-09-09
CPC分类号： F01D3/02 , E21B43/128 , F01D1/20 , F01D1/22 , F04D29/2266 , F04D29/445 , F05D2240/40
摘要： A centrifugal pump has alternating impellers and diffusers. One or more vent holes extend through one or more vanes of one or more diffusers. In an upthrust condition, high pressure production fluid from an upper impeller is able to pass through the one or more vent holes, and thereby exert force on the preceding impeller. The force exerted on the preceding impeller offsets the upthrust force acting against the preceding impeller.
摘要翻译： 离心泵具有交替的叶轮和扩散器。 一个或多个通气孔延伸穿过一个或多个扩散器的一个或多个叶片。 在上推状态下，来自上叶轮的高压生产流体能够通过一个或多个通气孔，从而对前一叶轮施加力。 施加在前一个叶轮上的力抵消了作用在前一个叶轮上的上推力。
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公开(公告)号：US20130114776A1
公开(公告)日：2013-05-09
申请号：US13289301
申请日：2011-11-04
CPC分类号： F01D1/14 , F01D1/20 , G21C15/182 , G21C2015/185 , G21D1/02 , G21D3/04 , G21D3/08 , Y02E30/40
摘要： A generator is installed on and provides electrical power from a turbine by converting the turbine's mechanical energy to electricity. The generated electrical power is used to power controls of the turbine so that the turbine can remain in use through its own energy. The turbine can be a safety-related turbine in a nuclear power plant, such that, through the generator, loss of plant power will not result in loss of use of the turbine and safety-related functions powered by the same. Appropriate circuitry and electrical connections condition the generator to work in tandem with any other power sources present, while providing electrical power with properties required to safely power the controls.
摘要翻译： 通过将涡轮机械的能量转换为电力来安装发电机并从涡轮机提供电力。 所产生的电力用于对涡轮机的控制进行动力，使得涡轮机可以通过其自身的能量保持在使用中。 涡轮机可以是核电站中的安全相关涡轮机，使得通过发电机，设备功率的损失不会导致涡轮机的使用丧失以及由其驱动的与安全相关的功能。 适当的电路和电气连接使发电机与任何其他电源同时工作，同时为电力提供安全的控制电源所需的性能。
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公开(公告)号：US20110058928A1
公开(公告)日：2011-03-10
申请号：US12878850
申请日：2010-09-09
CPC分类号： F01D3/02 , E21B43/128 , F01D1/20 , F01D1/22 , F04D29/2266 , F04D29/445 , F05D2240/40
摘要： A centrifugal pump has alternating impellers and diffusers. One or more vent holes extend through one or more vanes of one or more diffusers. In an upthrust condition, high pressure production fluid from an upper impeller is able to pass through the one or more vent holes, and thereby exert force on the preceding impeller. The force exerted on the preceding impeller offsets the upthrust force acting against the preceding impeller.
摘要翻译： 离心泵具有交替的叶轮和扩散器。 一个或多个通气孔延伸穿过一个或多个扩散器的一个或多个叶片。 在上推状态下，来自上叶轮的高压生产流体能够通过一个或多个通气孔，从而对前一叶轮施加力。 施加在前一个叶轮上的力抵消了作用在前一个叶轮上的上推力。
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公开(公告)号：US2931170A
公开(公告)日：1960-04-05
申请号：US59416056
申请日：1956-06-27
申请人： MITTELSTAEDT GEORG S
发明人： MITTELSTAEDT GEORG S
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公开(公告)号：US10082038B2
公开(公告)日：2018-09-25
申请号：US14853033
申请日：2015-09-14
申请人： Techspace Aero S.A.
CPC分类号： F01D11/025 , F01D1/20 , F01D11/22 , F01D25/24 , F04D27/0246 , F04D29/164 , F04D29/526 , F05D2260/407 , Y02T50/672
摘要： The invention relates to an axial turbomachine compressor outer casing. The casing comprises a sealing device collaborating with a row of rotor blades. The casing comprises a wall with an annular groove in which the sealing device is housed. The sealing device comprises a segmented outer shroud and a plurality of piezoelectric actuators moving the shroud radially in the groove so as to open or close the functional clearance. The invention also proposes a method for controlling a sealing device for a turbojet engine, the method comprising a step of measuring the altitude and a step of adjusting a clearance according to the altitude.
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公开(公告)号：US20160195010A1
公开(公告)日：2016-07-07
申请号：US14797264
申请日：2015-07-13
发明人： Gary D. Roberge
CPC分类号： F02C3/04 , F01D1/20 , F01D1/26 , F01D5/142 , F01D9/06 , F01D25/162 , F02C7/06 , F02K3/072 , F05D2220/3213 , F05D2240/12 , F05D2260/40311 , Y02T50/673
摘要： A gas turbine engine includes a compressor section, a combustor, and a turbine section. The turbine section includes a first turbine portion and a second turbine portion, with the first and second turbine portions being counter-rotating turbine portions. A transition duct transitions fluid flow from the first turbine portion to the second turbine portion. The transition duct is a vaneless transition duct.
摘要翻译： 燃气涡轮发动机包括压缩机部分，燃烧器和涡轮部分。 涡轮部分包括第一涡轮机部分和第二涡轮机部分，其中第一和第二涡轮机部分是反向旋转的涡轮机部分。 过渡管道将从第一涡轮机部分流向第二涡轮部分的流体流动。 过渡管道是无叶过渡管道。
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