公开(公告)号：US11866160B2

公开(公告)日：2024-01-09

申请号：US17982629

申请日：2022-11-08

Applicant: Xiaoyi Zhu

Inventor： Xiaoyi Zhu

IPC: B64C27/16 ,  F01D5/12 ,  F01D1/32 ,  B64C11/16 ,  B64C1/16 ,  F02F3/00 ,  F02B23/04 ,  F02B19/00 ,  B64C11/24 ,  B64C27/473 ,  F01K25/02 ,  F02B39/02 ,  F02C3/107

CPC classification number: B64C27/16 ,  B64C1/16 ,  B64C11/24 ,  B64C27/473 ,  F01D1/32 ,  F01D5/12 ,  F01K25/02 ,  F02B19/00 ,  F02B23/04 ,  F02B39/02 ,  F02C3/107 ,  F02F3/0076

Abstract: The present invention provides a power device generating greater propelling force and finds that traditional power devices do not include all propelling forces based on the fundamental core propelling force source problem. External pressure is guided to the traditional power devices since the inner speed is higher the outer speed, power consumption for overcoming fluid resistance is high, and mutual contradiction results are obtained. The unique difference between the present invention and general common sense lies in opposite fluid pressure directions; inner fluid channels and outer fluid channels with higher flow speeds are formed to generate pressure differences which guides the fluid pressure to the outside and serve as propelling force, thus the present invention creatively finds three propelling force sources, two lifting force or propelling force sources of helicopters or airplanes driven by propellers and two propelling force sources for sufficient burning of fuel in combustion chambers of engines.

公开(公告)号：US10508554B2

公开(公告)日：2019-12-17

申请号：US14923693

申请日：2015-10-27

Applicant: General Electric Company

Inventor： Rohit Chouhan ,  Shashwat Swami Jaiswal ,  Gunnar Leif Siden ,  Zachary James Taylor

IPC: F01D5/18 ,  F01D5/02 ,  F01D5/22 ,  F01D9/02 ,  F01D1/32

Abstract: A turbine bucket according to embodiments includes: a base; a blade coupled to base and extending radially outward from base, blade including: a body having: a pressure side; a suction side opposing pressure side; a leading edge between pressure side and suction side; and a trailing edge between pressure side and suction side on a side opposing leading edge; and a plurality of radially extending cooling passageways within body; and a shroud coupled to blade radially outboard of blade, shroud including: a plurality of radially extending outlet passageways fluidly connected with a first set of the plurality of radially extending cooling passageways within body; and an outlet path extending at least partially circumferentially through shroud and fluidly connected with all of a second, distinct set of the plurality of radially extending cooling passageways within body.

公开(公告)号：US10377475B2

公开(公告)日：2019-08-13

申请号：US15417595

申请日：2017-01-27

Applicant: David J. White

Inventor： David J. White

IPC: B64C27/18 ,  F01D1/32 ,  B64C27/46 ,  B64C27/473

Abstract: A nozzle for use with a rotor blade for a reaction drive type helicopter includes a first wall, a second wall opposing the first wall, and sidewalls extending between the first wall and the second wall enclosing a cavity having an upstream end and a downstream end. The nozzle includes an inlet section for receiving a gasflow at the upstream end. The distance between the first wall and the second wall reduces to a throat downstream of the inlet section. An expansion section extending from the throat, downstream thereof.

公开(公告)号：US10184229B2

公开(公告)日：2019-01-22

申请号：US14755245

申请日：2015-06-30

Applicant: Robert Kremer

Inventor： Robert Kremer

IPC: F01D1/32 ,  E03B11/16 ,  B01F5/04 ,  F24J3/00 ,  F28F13/06 ,  F24H4/04 ,  F01K13/00 ,  F24J3/08

Abstract: A transonic two-phase reaction turbine for use with low and high temperature fluid flow mediums includes at least two wheels that are configured to rotate in opposite directions, at least one of the at least two wheels being equipped with one or multiple kinetic energy harvesters.

公开(公告)号：US10006288B2

公开(公告)日：2018-06-26

申请号：US14349162

申请日：2012-09-27

Applicant: Hyuk Sun Choi

Inventor： Hyuk Sun Choi

IPC: F02D1/02 ,  F01D1/02 ,  F01D1/14 ,  F01D1/22 ,  F01D1/32 ,  F01D1/34

CPC classification number: F01D1/026 ,  F01D1/14 ,  F01D1/22 ,  F01D1/32 ,  F01D1/34

Abstract: The present invention relates to an improvement of an axial turbine. Thereto, the present invention includes a submerged turbine 100 in which a fluid is filled in an interior thereof. The present invention also includes a colliding turbine 200 for ejecting a fluid with a high pressure to rotate blades. The structure of the turbine according to the present invention includes a submerged turbine, a colliding turbine, or a combination type turbine (in which a submerged turbine and a colliding turbine are combined). Accordingly, quality and reliability of the product are significantly improved to satisfy the operator.

公开(公告)号：US09970296B1

公开(公告)日：2018-05-15

申请号：US15631827

申请日：2017-06-23

Applicant: James L. Richards

Inventor： James L. Richards

IPC: F04D25/04 ,  F02B37/10 ,  F01D1/32 ,  F02B33/40 ,  F02B37/04 ,  F01D1/18

CPC classification number: F01D1/32 ,  F01D1/18 ,  F02B33/40 ,  F02B37/04 ,  F02B37/10 ,  F04D25/04 ,  F05D2220/40 ,  F05D2240/60

Abstract: A fluid motor is disclosed employed in a turbocharger to spin-up the turbocharger turbine independently of the existing exhaust gas pressure on the exhaust turbine wheel. A fluid turbine wheel is fixedly attached to the rotary mounted shaft of the turbocharger. Fixedly mounted nozzles directed at the fluid turbine wheel present fluid from a controlled source of pressurized fluid. A fixedly mounted collector receiving exhausted fluid from the fluid turbine wheel. The fluid is recycled from the collector to the controlled source of pressurized fluid and then back to the fixedly mounted. The fluid turbine wheel exhausts the fluid with residual energy to the collector. The controlled source of pressurized fluid includes a gear pump with an accumulator and a solenoid valve.

公开(公告)号：US09856791B2

公开(公告)日：2018-01-02

申请号：US13969900

申请日：2013-08-19

Applicant: Board of Trustees of Michigan State University

Inventor： Norbert Müller ,  Janusz Piechna ,  Guangwei Sun ,  Pablo-Francisco Parraga

IPC: F02C3/14 ,  F01D1/32 ,  F02C3/16 ,  F02C5/04 ,  F02C5/10 ,  F02K7/04

CPC classification number: F02C3/14 ,  F01D1/32 ,  F02C3/165 ,  F02C5/04 ,  F02C5/10 ,  F02K7/04 ,  F05D2240/302 ,  F05D2250/82 ,  Y02T50/673

Abstract: A wave disc engine apparatus is provided. A further aspect employs a constricted nozzle in a wave rotor channel. A further aspect provides a sharp bend between an inlet and an outlet in a fluid pathway of a wave rotor, with the bend being spaced away from a peripheral edge of the wave rotor. A radial wave rotor for generating electricity in an automotive vehicle is disclosed in yet another aspect.

公开(公告)号：US20090220329A1

公开(公告)日：2009-09-03

申请号：US12282931

申请日：2007-03-14

Applicant: John D. Pickard

Inventor： John D. Pickard

IPC: F01D1/32 ,  F01D5/14

CPC classification number: F01D1/026 ,  F01D1/32 ,  F01D15/10

Abstract: A rotor for a radial flow turbine has an impulse chamber (51) having an inlet defined in a circumferential surface of the rotor and a reaction chamber (62) having an outlet defined in the circumferential surface of the rotor. The impulse chamber is in fluid communication with the reaction chamber, and the reaction chamber outlet is axially displaced from the impulse chamber inlet.

Abstract translation: 用于径向流动涡轮机的转子具有在转子的圆周表面上具有入口的脉冲室（51）和在转子的圆周表面中具有出口的反应室（62）。 脉冲室与反应室流体连通，并且反应室出口从脉冲室入口轴向移位。

公开(公告)号：US06997674B1

公开(公告)日：2006-02-14

申请号：US10839697

申请日：2004-05-04

Applicant: Neldon P. Johnson

Inventor： Neldon P. Johnson

IPC: F01D1/32

CPC classification number: F03B3/00 ,  F01D1/32 ,  Y02E10/223

Abstract: A bladeless pressurized fluid turbine engine having a bladeless turbine, internal, concentric or circumferential shaft fluid ways which transmit pressurized gas to the turbine, and a pressurized fluid intake assembly. The intake assembly has a fixed outer housing, two or more shaft seals sealing between the shaft and the outer housing forming fluid supply chambers between adjacent shaft seals, and a pair of shaft bearings bearing between the shaft and the outer housing. The outer housing has one or more fluid intake ports for each fluid supply chamber and each shaft fluid way has a shaft fluid intake which is hydraulically connected to a fluid supply chamber.

Abstract translation: 具有无压涡轮机，内部，同心或圆周轴流体通道的无叶加压流体涡轮发动机，其将加压气体传输到涡轮机，以及加压流体进料组件。 进气组件具有固定的外壳体，密封在轴和外壳体之间的两个或更多个轴封形成在相邻的轴密封件之间形成流体供应室，以及轴与轴与外壳之间的一对轴承。 外壳体具有用于每个流体供应室的一个或多个流体进入端口，并且每个轴流体路径具有液压地连接到流体供应室的轴流体入口。

公开(公告)号：US06899531B2

公开(公告)日：2005-05-31

申请号：US10719027

申请日：2003-11-24

Applicant: Karl-Ernst Hummel

Inventor： Karl-Ernst Hummel

IPC: F01D1/32 ,  F01D25/16 ,  F02C1/10 ,  F02C3/14 ,  F02C3/30 ,  F02C6/12 ,  F02C7/24 ,  F04D25/04 ,  F04D29/66 ,  F04B17/00 ,  F16D31/02

CPC classification number: F04D25/04 ,  F01D25/16 ,  F02C6/12 ,  F02C7/24 ,  F04D29/663 ,  F05D2220/40 ,  F05D2260/96 ,  F05D2300/43 ,  F05D2300/612

Abstract: A secondary air induction system (1) for an internal combustion engine of a motor vehicle, including a turbine (2) and a compressor (3), in which a turbine wheel (4) of the turbine (2) and a compressor wheel (5) of the compressor (3) are mounted on a rotatable common shaft (6) supported by a bearing assembly (8) including at least one roller bearing (17) inside a turbocharger housing (7). An insulating or noise damping material (9) externally encloses at least a portion of the housing (7) to provide sound insulation in the area of the bearing assembly (8).

Abstract translation: 一种用于机动车辆的内燃机的二次空气感应系统（1），包括涡轮机（2）和压缩机（3），其中涡轮机（2）的涡轮机叶轮（4）和压缩机叶轮 压缩机3的5）安装在由包括涡轮增压器壳体（7）内部的至少一个滚子轴承（17）的轴承组件（8）支撑的可旋转公共轴（6）上。 绝缘或噪声阻尼材料（9）在外部封闭壳体（7）的至少一部分，以在轴承组件（8）的区域中提供隔音。