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    • 4. 发明授权
    • Waterjet propulsion unit
    • 水刀推进装置
    • US06500035B2
    • 2002-12-31
    • US10112445
    • 2002-03-28
    • Hendrik Terlouw
    • Hendrik Terlouw
    • B63H2546
    • B63H11/103B63H11/04
    • The invention aims to increase the efficiency of a waterjet propulsion unit with a jet tube, open at its upper and lower end and accommodating a rotating water propulsion means, and with in its outflow opening a rotatable grid of essentially mutual parallel guide plates which cross the axis of the propulsion means under an acute angle, in which a great power can be handled, in that the jet tube is surrounded at the outside of the inlet end by a guide surface having a spherically curved cross-section, and ends at the inlet end in a converging chamber of which two opposite walls an acute angle include with the axis of the propulsion means, said chamber carrying at the outflow end the grid of guide plates of which the plates are parallel with the horizontal end edges of said walls, the whole being rotable together with this grid around the axis of the propulsion means.
    • 本发明旨在提高具有喷射管的水射流推进装置的效率,喷射管在其上端和下端开口并且容纳旋转的水推进装置,并且在其流出口中具有基本相互平行的引导板的可转动的格栅, 推动装置的轴线处于锐角处,其中可以处理大功率,因为​​喷射管在入口端的外侧被具有球形弯曲横截面的引导表面包围,并且在入口端部 其结合在一个会聚室中,其两个相对的壁的锐角与推进装置的轴线一起包括在内,所述腔室在流出端承载导板的格栅,板的平行于所述壁的水平端边缘, 整体可与该格栅一起围绕推进装置的轴线旋转。
    • 7. 发明授权
    • Portable dynamic positioning system with self-contained diesel hydraulic thrusters
    • 便携式动态定位系统,配备独立柴油液压推进器
    • US06799528B1
    • 2004-10-05
    • US10695105
    • 2003-10-28
    • Joannes Raymond Mari Bekker
    • Joannes Raymond Mari Bekker
    • B63H2546
    • B63H20/00B63H23/26B63H25/04B63H2020/005B63H2025/045B63J2099/006
    • The integrated and self contained diesel hydraulic thruster system integral has a dynamic positioning control system for dynamic positioning of any waterborne vessel having a hull with at least two sides and a deck connecting the sides, at least two removably mounted azimuthing thrusters, at least two self-contained diesel hydraulic power units removably secured to the deck, one for each thruster, at least one dynamic positioning computer connected to each of the self contained diesel hydraulic power units, at least one motion reference sensor connected to the dynamic positioning computer to correct reference position signals for motion of the vessel, at least one heading sensor, and at least one sensor that is either a position reference sensor connected to the dynamic positioning computer, an environmental sensor connected to the dynamic positioning computer, or a combination thereof.
    • 集成的和独立的柴油液压推进器系统集成有一个动态定位控制系统,用于动态定位任何具有至少两个侧面的船体和连接两侧的甲板的水上船舶,至少两个可移除地安装的方位推进器,至少两个自身 连接到每个推进器的至少一个动态定位计算机,连接到每个独立的柴油液压动力单元的至少一个运动参考传感器,连接到动态定位计算机以校正参考 用于船舶运动的位置信号,至少一个航向传感器,以及作为连接到动态定位计算机的位置参考传感器,连接到动态定位计算机的环境传感器或其组合的至少一个传感器。
    • 9. 发明授权
    • Turbo jet engine exhaust nozzle with masked gas jet
    • 涡轮喷气发动机排气喷嘴与掩蔽气体喷射
    • US06179225B2
    • 2001-01-30
    • US09356362
    • 1999-07-19
    • Philippe Pierre BouillerPierre-Yves BourquinDaniel KettlerJean-Pierre Ruis
    • Philippe Pierre BouillerPierre-Yves BourquinDaniel KettlerJean-Pierre Ruis
    • B63H2546
    • F02K1/825F02K1/11
    • An axially symmetric turbojet engine exhaust-nozzle includes a system for masking the exhaust jet, such system including inner hot flaps (7), hinging on a conical shell (4) and driven by a first control ring (10) powered by linear actuators (11), and outer cold flaps (20) hinging on an annular assembly (12) and driven by a second control ring (22) powered by linear actuators (23) to vary the angle of the cold flaps. The annular assembly (12) is axially displaceable by a third set of linear actuators (30). Each cold flap (20) comprises an inner skin (40) fitted with orifices (43) and hinging on the annular assembly(12) and an outer skin (41) spaced radially away of the inner skin (40) to define an air flow channel between the skins. When the annular assembly (12) is moved downstream by the third set of linear actuators (30), the outer skins (41) form a scoop introducing fresh air into the cold flaps (20), and said air is injected into the hot gas flow through the orifices (43) in the inner skin and other orifices (44) at the trailing edge (42) of the cold flaps to reduce the exhaust signature.
    • 轴向对称的涡轮喷气发动机排气喷嘴包括用于遮蔽排气射流的系统,该系统包括铰接在锥形壳体(4)上并由第一控制环(10)驱动的内部热襟翼(7),该第一控制环由线性致动器 以及铰链在环形组件(12)上并由由线性致动器(23)供电的第二控制环(22)驱动的外部冷襟翼(20),以改变冷襟翼的角度。 环形组件(12)可被第三组线性致动器(30)轴向移动。 每个冷翼(20)包括装配有孔(43)并铰接在环形组件(12)上的内表皮(40)和径向远离内表皮(40)的外表皮(41),以限定空气流 皮肤之间的通道。 当环形组件(12)由第三组线性致动器(30)向下游移动时,外表面(41)形成将新鲜空气引入冷襟翼(20)中的勺子,并将所述空气注入到热气体 流过冷皮瓣后缘(42)的内皮和其他孔(44)中的孔(43),以减少排气特征。