Method For System For A Water Jet Propulsion System For A Ship
    91.
    发明申请
    Method For System For A Water Jet Propulsion System For A Ship 有权
    一种用于船舶喷水推进系统的系统方法

    公开(公告)号:US20110045717A1

    公开(公告)日:2011-02-24

    申请号:US12934098

    申请日:2009-03-26

    IPC分类号: B63H11/10 B63H11/08

    CPC分类号: B63H11/10 B63H11/08

    摘要: A system and method of starting a water jet propulsion system for a ship in which the propulsion system includes a stator shell adapted to be mounted to the hull and having a nozzle ending in an outlet with a cross-sectional outlet area, an impeller housing attached to the stator shell and having an upstream inlet, and an impeller rotatably mounted in the impeller housing for receiving water from the inlet and discharging it through the nozzle of the stator shell so as to create a water jet upon rotation of the impeller. The method includes reducing the outlet area by partly closing the nozzle during a start up phase of the water jet propulsion system, wherein there is provided a back flow hindering arrangement arranged to hinder air to enter into the impeller housing via the nozzle.

    摘要翻译: 一种用于启动用于船舶的喷水推进系统的系统和方法,其中推进系统包括适于安装到船体的定子壳体,并且具有终止于具有横截面出口区域的出口的喷嘴,附接叶轮壳体 并且具有上游入口和可旋转地安装在叶轮壳体中的叶轮,用于从入口接收水并将其排出通过定子壳的喷嘴,以便在叶轮旋转时产生水射流。 该方法包括通过在喷水推进系统的启动阶段期间部分地关闭喷嘴来减小出口面积,其中提供了一个回流阻碍装置,其布置成阻止空气经由喷嘴进入叶轮壳体。

    Convergent divergent nozzle with slot cooled nozzle liner
    92.
    发明授权
    Convergent divergent nozzle with slot cooled nozzle liner 有权
    具有狭缝冷却喷嘴衬管的收敛发散喷嘴

    公开(公告)号:US07757477B2

    公开(公告)日:2010-07-20

    申请号:US11676595

    申请日:2007-02-20

    摘要: A nozzle system includes a multitude of circumferentially distributed convergent flaps and seals that circumscribe an engine centerline. A cooling liner body cooperates with a cooling liner panel attached to respective convergent flaps and convergent seals to define an annular cooling airflow passageway which is movable therewith. Each cooling liner panels includes an arcuate cooling liner leading edge with a multiple of openings to distribute cooling airflow over both the inner “cold-side” and outer “hot-side” surfaces thereof. Through this backside cooling, thermal gradients are controlled at the attachment interface between the arcuate cooling liner leading edge and the main cooling liner body.

    摘要翻译: 喷嘴系统包括大量周向分布的会聚翼片和密封件,其围绕发动机中心线。 冷却衬套主体与连接到相应的会聚翼片和会聚密封件的冷却衬套板配合,以限定可随之移动的环形冷却气流通道。 每个冷却衬板包括具有多个开口的弧形冷却衬套前缘,以在其“冷侧”和“外侧”表面之间分配冷却气流。 通过这种背面冷却,在弧形冷却衬套前缘和主冷却衬套主体之间的附接界面处控制热梯度。

    Convergent divergent nozzle with supported divergent seals
    93.
    发明申请
    Convergent divergent nozzle with supported divergent seals 有权
    具有支撑发散密封的收敛发散喷嘴

    公开(公告)号:US20070186555A1

    公开(公告)日:2007-08-16

    申请号:US11355116

    申请日:2006-02-15

    申请人: Donald Peters

    发明人: Donald Peters

    IPC分类号: B63H11/10

    CPC分类号: F02K1/1223 F02K1/12 F02K1/805

    摘要: A nozzle system includes a multitude of circumferentially distributed divergent seals that circumscribe an engine centerline. Each divergent seal includes an interface between a forward seal bridge bracket and an aft seal bridge bracket with a forward bridge support and an aft bridge support which provides axial and radial support for the divergent seals between adjacent divergent flaps. A divergent-convergent seal joint structure includes a horn and a fork. By having the forward bridge bracket retain the divergent seal in the axial direction, there is no need for axial sliding of the divergent seal relative to the divergent flap. The joint structure provides circumferential support as the axial and radial support are provided by the bridge-bracket interface. The joint interface permits the forward end section of the divergent seal and the forward end section of the divergent flap to include a radiused surface which provides a smooth interior interface between the convergent section and the divergent sections.

    摘要翻译: 喷嘴系统包括围绕发动机中心线的多个周向分布的发散密封件。 每个发散密封件包括前向密封桥架支架和具有前桥支撑件和后桥支撑件的后密封桥架支架之间的接口,所述前桥支撑件和后桥支撑件为相邻发散翼片之间的发散密封提供轴向和径向支撑。 发散收敛的密封接头结构包括喇叭和叉子。 通过使前桥支架沿轴向保持发散密封,不需要相对于发散翼片的发散密封件的轴向滑动。 当轴向和径向支撑由桥架支架接口提供时,接头结构提供周向支撑。 接合界面允许发散密封件的前端部分和发散片的前端部分包括一个圆形表面,其在收敛部分和发散部分之间提供平滑的内部界面。

    Nozzle assembly of dishwasher
    94.
    发明授权
    Nozzle assembly of dishwasher 失效
    洗碗机喷嘴总成

    公开(公告)号:US06959881B2

    公开(公告)日:2005-11-01

    申请号:US10721738

    申请日:2003-11-26

    申请人: Yong Hee Kim

    发明人: Yong Hee Kim

    CPC分类号: B05B3/026 A47L15/23

    摘要: A nozzle of a dishwasher reduces a space for installing a supplementary nozzle on a main nozzle by having first and second connectors coupled to be caught on each other between main and auxiliary nozzles. The nozzle assembly includes a main nozzle having a first coupling hole; an auxiliary nozzle, having a second coupling hole, for coupling with the main nozzle; a first interlocking device, having a first end, for coupling with the main nozzle at the first coupling hole, by being caught in the first coupling hole by the first end; and a second interlocking device, having a first end, for coupling with the auxiliary nozzle at the second coupling hole, by being caught in the second coupling hole by the first end and by having a second end to be caught on the first interlocking device.

    摘要翻译: 洗碗机的喷嘴通过将第一和第二连接器联接以在主喷嘴和辅助喷嘴之间彼此夹紧而减小了用于在主喷嘴上安装辅助喷嘴的空间。 喷嘴组件包括具有第一联接孔的主喷嘴; 辅助喷嘴,具有用于与主喷嘴联接的第二联接孔; 第一联锁装置,具有第一端,用于通过由第一端卡在第一联接孔中,与第一联接孔处的主喷嘴联接; 以及第二联锁装置,具有第一端,用于在第二联接孔处与辅助喷嘴联接,通过第一端被卡在第二联接孔中,并且具有被夹在第一联锁装置上的第二端。

    Personal watercraft
    95.
    发明授权
    Personal watercraft 失效
    个人船只

    公开(公告)号:US06948987B2

    公开(公告)日:2005-09-27

    申请号:US10660440

    申请日:2003-09-10

    申请人: Tomohiro Fuse

    发明人: Tomohiro Fuse

    摘要: A personal watercraft has a structure in which a steering nozzle is mounted onto a jet nozzle so as to be swingable vertically and in the left-right directions, upper and lower support shafts for mounting the steering nozzle include upper and lower bolts, the upper and lower bolts set such that the heads thereof are directed toward the jet nozzle, and the lengths of the upper and lower bolts are set such that the upper and lower bolts can be fastened to the steering nozzle when the heads of the upper and lower bolts come into contact with the jet nozzle.

    摘要翻译: 个人船舶具有将转向喷嘴安装在喷嘴上以便在垂直方向和左右方向上摆动的结构,用于安装转向喷嘴的上和下支撑轴包括上下螺栓, 下螺栓设置为使其头部朝向喷嘴,并且上螺栓和下螺栓的长度被设定为使得当上下螺栓的头部到达时,上下螺栓可以紧固到转向喷嘴 与喷嘴接触。

    Waterjet control system
    96.
    发明授权
    Waterjet control system 有权
    水刀控制系统

    公开(公告)号:US06865996B2

    公开(公告)日:2005-03-15

    申请号:US10140957

    申请日:2002-05-08

    摘要: A dual axis joystick control system is used intuitively for maneuvring a waterborne vessel having two or more waterjets with steering deflectors (13) and reverse ducts (14) mounted independently of the steering deflectors. The joystick (21) is operated to actuate the reverse ducts of the port and starboard waterjets for either common or differential deflections of thrust, and to actuate the steering deflectors of the port and starboard waterjets for common deflections of thrust.

    摘要翻译: 双轴操纵杆控制系统直观地用于操纵具有两个或更多个喷水器的水上船,其具有独立于转向导流板安装的转向导流板(13)和反向导管(14)。 操纵杆(21)被操作以致动端口和右舷喷水枪的反向通道用于推力的常见或差异偏转,并且致动端口和右舷喷水枪的转向导流器以产生一般的推力偏转。

    Vstovl engines
    97.
    发明授权
    Vstovl engines 失效
    Vstovl发动机

    公开(公告)号:US6105364A

    公开(公告)日:2000-08-22

    申请号:US591600

    申请日:1990-09-21

    申请人: Michael J Zdybel

    发明人: Michael J Zdybel

    IPC分类号: F02K3/02 F02K1/00 B63H11/10

    CPC分类号: F02K3/025

    摘要: A turbofan engine is provided with a conventional air by-pass duct communicating with a plenum chamber downstream of the engine core, vectoring nozzles upstream of the by-pass duct, and a non-vectoring nozzle and a jet-pipe exhausting from the plenum chamber. In conventional forward thrust mode the two sets of nozzles are closed and the jet-pipe is open. In lift thrust mode the jet-pipe is closed and the two sets of nozzles are open, the non-vectoring nozzle providing vertical thrust. The closure member for the vectoring nozzle is arranged, when open, to divert turbofan air to the vectoring nozzles which would otherwise have passed along the by-pass duct, and to divert to the vectoring nozzles exhaust gases from the plenum chamber that are constrained to flow in reverse along the by-pass duct. The non-vectoring nozzle is sized to permit a suitable split between gases exhausting there through and gases reverse flowing along the by-pass duct.

    摘要翻译: 涡轮风扇发动机设置有常规的空气旁路管道,其与发动机核心下游的增压室连通,在旁路管道上游引导喷嘴,以及非向量喷嘴和从增压室排出的喷射管 。 在常规的向前推力模式中,两组喷嘴关闭,喷射管是打开的。 在提升推力模式下,喷射管被关闭,两组喷嘴打开,非矢量喷嘴提供垂直推力。 用于向导喷嘴的关闭构件在打开时被布置成将涡轮风扇空气转移到否则将沿着旁通管道通过的向导喷嘴,并且将向上的喷嘴转移到来自增压室的废气被限制到 沿着旁路管道反向流动。 非矢量喷嘴的尺寸设计成允许在其中排出的气体和沿着旁路管道反向流动的气体之间的合适的分流。

    Seal for a variable geometry nozzle
    98.
    发明授权
    Seal for a variable geometry nozzle 失效
    可变几何喷嘴的密封

    公开(公告)号:US5676312A

    公开(公告)日:1997-10-14

    申请号:US516827

    申请日:1995-08-18

    IPC分类号: F02K1/12 F02K1/80 B63H11/10

    摘要: A variable geometry exhaust nozzle is disclosed in which the follower flaps of the first, upstream ring of flaps and the second, downstream ring of flaps have a seal to seal the gap between the upstream and downstream follower flaps throughout the range of movement of the variable nozzle flaps. The sealing device has a plate extending between the downstream edge portion of an upstream follower flap and the upstream edge portion of a downstream follower flap and across the entire circumferential width of the flaps. The plate has an upstream portion pivotally connected with the downstream edge portion of the upstream follower flap and a downstream portion which has a bead pivotally contacting an inner surface of the upstream edge portion of a downstream follower flap.

    摘要翻译: 公开了一种可变几何形状排气喷嘴,其中第一上游环襟翼和第二下游襟翼环的随动翼片具有密封件,用于在变量的整个移动范围内密封上游和下游跟随襟翼之间的间隙 喷嘴襟翼。 密封装置具有在上游从动翼的下游边缘部分和下游跟随器瓣的上游边缘部分之间延伸并跨过瓣片的整个周向宽度的板。 所述板具有与所述上游从动翼的下游边缘部分枢转连接的上游部分和具有与下游跟随器瓣的上游边缘部分的内表面枢转接触的胎圈的下游部分。

    Waterjet propulsion unit for water craft with control elements for
changing the direction of thrust of the waterjet
    99.
    发明授权
    Waterjet propulsion unit for water craft with control elements for changing the direction of thrust of the waterjet 失效
    水刀推进装置,用于改变水刀推力方向的控制元件

    公开(公告)号:US5649843A

    公开(公告)日:1997-07-22

    申请号:US525685

    申请日:1995-11-20

    申请人: Gerd Elger

    发明人: Gerd Elger

    CPC分类号: B63H11/113 B63H11/08

    摘要: Water jet propulsion unit for watercraft having a pump and stators arranged upstream and downstream of the pump for eliminating turbulence in the entering water and in the water jet generated by the pump, having coaxially arranged nozzles which are associated with the respective stator and are supported so as to be displaceable axially independently of one another, and having a switchable gear unit for driving the pump in the clockwise or counterclockwise direction in order to change the direction of motion of the watercraft, the water jet propulsion unit being supported at the watercraft so as to be swivelable by .+-.90.degree. approximately vertically to the axis of rotation of the pump rotor.

    摘要翻译: PCT No.PCT / DE95 / 00099 Sec。 371日期:1995年11月20日 102(e)1995年11月20日日期PCT提交1995年1月24日PCT公布。 公开号WO95 / 20520 日期1995年8月3日用于具有泵和定子的船舶的水轮喷气推进装置,其布置在泵的上游和下游,用于消除进水中的泵浦和由泵产生的水射流中的湍流,具有同轴布置的喷嘴, 定子并且被支撑成可彼此独立地位移,并且具有用于沿顺时针或逆时针方向驱动泵的可切换齿轮单元,以便改变船只的运动方向,水喷射推进单元被支撑 在船舶上可以大致垂直于泵转子的旋转轴线旋转+/- 90°。

    Water vehicle jet pump flow control apparatus
    100.
    发明授权
    Water vehicle jet pump flow control apparatus 失效
    水车喷射泵流量控制装置

    公开(公告)号:US5542863A

    公开(公告)日:1996-08-06

    申请号:US225451

    申请日:1994-04-06

    IPC分类号: B63H11/103 B63H11/10

    CPC分类号: B63H11/103

    摘要: In jet pump liquid flow control apparatus the combination comprising an annular body and a liquid flow passage through the body, the passage defining a longitudinal axis; an annular series of flow controlling elements spaced about the axis with successive of the elements having primary portions extending in edge overlapping relation whereby the elements define a flow controlling section of the passage; and control means extending about the axis for controllably urging the primary portions of elements toward the axis thereby to control the cross sectional area of the passage sections.

    摘要翻译: 在喷射泵液体流量控制装置中,组合包括环形体和通过本体的液体流动通道,通道限定纵向轴线; 围绕所述轴线间隔开的环形系列流量控制元件,所述元件的连续元件具有以边缘重叠关系延伸的主要部分,由此所述元件限定所述通道的流动控制部分; 以及围绕所述轴延伸的控制装置,用于可控地将元件的主要部分推向轴线,从而控制通道部分的横截面积。