STEAM TURBINE WITH IMPROVED AXIAL FORCE PROPERTY
    1.
    发明公开
    STEAM TURBINE WITH IMPROVED AXIAL FORCE PROPERTY 审中-公开
    蒸汽涡轮机具有改进的轴向力特性

    公开(公告)号:EP3241986A1

    公开(公告)日:2017-11-08

    申请号:EP15873443.4

    申请日:2015-08-28

    IPC分类号: F01D1/32 F01D1/14 F01D1/06

    CPC分类号: F01D1/06 F01D1/14 F01D1/32

    摘要: Disclosed is a steam turbine capable of reducing the load of a bearing supporting a turbine shaft transmitting rotational driving force of a plurality of nozzle-equipped rotary bodies arranged in multiple stages. The steam turbine includes a housing (110); a turbine shaft (120) pivotably supported by a bearing (121) in the housing; and a plurality of dish-shaped nozzle-equipped rotary bodies (130) integrally combined with the turbine shaft (120), provided with one or more nozzle holes (131) from which working fluid is ejected so that the nozzle rotations bodies (130) can be rotated, and stacked in an axial direction of the turbine shaft (120). The nozzle hole (131) is inclined with respect to a normal direction n of the periphery surface of the nozzle-equipped rotary body (130) and is inclined toward an axial direction c of the turbine shaft (120).

    摘要翻译: 本发明提供一种蒸汽涡轮机,其能够降低支承多级配置的多个带喷嘴旋转体的旋转驱动力的涡轮轴的轴承的负荷。 蒸汽涡轮机包括壳体(110); 涡轮轴(120),其由壳体中的轴承(121)可枢转地支撑; 和多个配备有一个或多个喷嘴孔(131)的与涡轮机轴(120)整体结合的碟形的装备有喷嘴的旋转体(130),工作流体从该喷嘴孔喷出以便喷嘴旋转体(130) 可以旋转,并沿涡轮轴(120)的轴向堆叠。 喷嘴孔131相对于具备喷嘴的旋转体130的周面的法线方向n倾斜,并朝向涡轮轴120的轴向c倾斜。

    A SEPARATION DEVICE
    4.
    发明授权
    A SEPARATION DEVICE 有权
    分离装置

    公开(公告)号:EP1175264B1

    公开(公告)日:2008-05-21

    申请号:EP00921228.3

    申请日:2000-03-21

    申请人: ALFA LAVAL AB

    IPC分类号: B04B11/02 B23Q11/10 F01D1/14

    CPC分类号: B04B1/00 B04B11/02 F04D1/14

    摘要: In a separation device for separating particles from a liquid, which is present in a container (1), a centrifugal rotor (7) is rotatable around a vertical rotational axis (R). The centrifugal rotor (7) has a tubular inlet member (8), which extends down into liquid to be treated and which upon rotation of the centrifugal rotor forms a pumping member adapted to pump liquid upwardly and into the centrifugal rotor. According to the invention the rotatable inlet member (8) is surrounded by a non-rotatable wall (12), a sealing device being adapted to seal between the rotatable inlet member (8) and the non-rotatable wall (12). Thereby is avoided that liquid is pumped upwardly on the outside of the inlet member. Furthermore, a smallest possible part of the outside of the inlet member (8) can be in contact with liquid, independent of the level of the liquid surface in the container (1).

    摘要翻译: 在用于从存在于容器(1)中的液体中分离颗粒的分离装置中,离心转子(7)可围绕垂直旋转轴线(R)旋转。 离心转子(7)具有管状入口构件(8),该管状入口构件向下延伸到待处理液体中,并且在离心转子旋转时形成泵送构件,该泵送构件适于将液体向上泵入并进入离心转子。 根据本发明,可旋转入口构件(8)由不可旋转壁(12)围绕,密封装置适于在可旋转入口构件(8)和不可旋转壁(12)之间密封。 由此避免液体在入口构件的外部向上泵送。 此外,入口构件(8)的外部的尽可能最小的部分可以与液体接触,而与容器(1)中液面的高度无关。

    MULTI-STAGE ROTARY FLUID HANDLING APPARATUS
    5.
    发明公开
    MULTI-STAGE ROTARY FLUID HANDLING APPARATUS 失效
    多级旋转机械用于流体

    公开(公告)号:EP0839284A4

    公开(公告)日:1998-08-05

    申请号:EP96909758

    申请日:1996-03-19

    申请人: ROTOFLOW CORP

    摘要: Rotary fluid handling apparatus employing a wheel (34) to provide multi-stage compression or expansion. A wheel (34) having a first set of vanes (36) includes a shroud (38) about those vanes with a second set of vanes (40) outwardly of the shroud. One set of vanes provides for law specific speed flow while the other set of vanes provides for high specific speed flow. A transfer passage (22) interconnects the outlet of the first stage with the inlet of the second stage. The difference in temperature between the inlet flow to the system and the outlet flow from the system may be exchanged (52) to increase efficiency. The multi-stage wheel and associated passages may be configured for either compression or turboexpansion.

    A regenerative turbomachine
    6.
    发明公开
    A regenerative turbomachine 失效
    Eine再生Turbomaschine。

    公开(公告)号:EP0353002A2

    公开(公告)日:1990-01-31

    申请号:EP89307503.6

    申请日:1989-07-24

    发明人: Moore, Alan

    IPC分类号: F04D23/00 F01D1/14

    CPC分类号: F01D1/14 F04D23/00

    摘要: A regenerative turbomachine has a rotatable bladed impeller (1) and an annular housing (3) surrounds the impeller (1) and defines a topological flow channel for a working fluid. There is also an inlet port (4) for admitting a working fluid to the housing (3) and an outlet port (5) spaced circumferentially of the impeller (1) from the inlet port (4) by which the working fluid can leave the housing (3). Guide means is also provided for guiding the working fluid entering the inlet port (4) through a slip flow path and a counter-flow path which follow respective spiral paths in opposite directions around the toroidal flow channel. Each flow path makes a number of successive passes through the impeller (1) and each successive pass is spaced circumferentially from the other passes.

    摘要翻译: 再生涡轮机具有可旋转的叶片叶轮(1),环形壳体(3)围绕叶轮(1)并且限定用于工作流体的拓扑流动通道。 还有一个用于将工作流体引入到壳体(3)的入口(4)和与进口(4)周向隔开的叶轮(1)的出口(5),工作流体可通过该出口端口离开 住房(3)。 引导装置还用于通过滑动流动路径和逆流通道引导进入入口(4)的工作流体,该流动路径和相反的螺旋路径围绕环形流动通道沿相反方向。 每个流动路径通过叶轮(1)进行多次连续的通过,并且每个相继的通道与其它通道沿周向隔开。

    REACTION-TYPE STEAM TURBINE
    8.
    发明公开

    公开(公告)号:EP3392456A1

    公开(公告)日:2018-10-24

    申请号:EP16875858.9

    申请日:2016-05-18

    摘要: The present invention relates to a reaction-type steam turbine. More specifically, the present invention relates to a reaction-type steam turbine that has guide blades mounted on a turbine shaft located between disk blades and a steam inlet tube to divert steam introduced into a housing from the steam inlet tube to the disk blades, thereby preventing a vortex phenomenon within the housing, and rotates the guide blades by means of the pressure of the introduced steam to rotate the turbine shaft, thereby reducing the initial load against the rotation of the turbine shaft and doubling the rotational output of the turbine shaft along with the rotation of the disk blades. To achieve this, provided is a reaction-type steam turbine that comprises: a housing having steam inlet and outlet tubes formed on opposite sides thereof, respectively, and having a space formed therein; and a turbine shaft installed to pass through the space of the housing and having a plurality of disk blades mounted thereon, wherein guide blades are shaft-coupled to the turbine shaft between the passage of the steam inlet tube and the disk blades to guide steam introduced into the space of the housing through the steam inlet tube to the disk blades.

    PROPULSEUR A HAUTE PERFORMANCE, INDÉPENDANT DU MILIEU EXTÉRIEUR
    9.
    发明公开
    PROPULSEUR A HAUTE PERFORMANCE, INDÉPENDANT DU MILIEU EXTÉRIEUR 审中-公开
    从外区独立强力的喷射赛艇

    公开(公告)号:EP2519712A2

    公开(公告)日:2012-11-07

    申请号:EP10819689.0

    申请日:2010-12-29

    申请人: Ly, Gilbert

    发明人: Ly, Gilbert

    摘要: The invention relates to an ecological thrusting device enabling optimum thrust independent from the outside environment. It consists of a special Francis turbine (1) from which the fluid is axially ejected at the outlet of the vane (1'), at a relative speed W
    2t , and is collected in a defined free space of a straight radial pump (2). Under the action of the centrifugal force, the limit of the current lines forms a fixed virtual barrier Y
    t , thus preventing the centrifuged fluid from reaching the bottom of the pump in the free space area MNBCPQ, thereby eliminating the antagonistic force exerted on said zone. As a result, the thrusting force exerted on the turbine by the fluid remains intact. As the fluid leaves the pump, it is axially reinjected at a relative speed W
    2p into a tank (4) for resupplying the turbine. There is therefore an energy exchange between the pumps and the turbine that form a closed circuit, the entire system being driven by a motor (10). It is shown that the thrust force P = (1/2) pπω
    2 r
    4 ; p being the density of the centrifuged fluid in en Kg/m
    3 ; ω being the angular speed of the turbine in rad/s; and r its radius in metres and P in Newtons. The calculation shows that the amount of thrust generated is very high; said thruster can be used to generate mechanical energy anywhere in space, and especially to drive the most highly efficient flying machines.