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    • 5. 发明申请
    • LOW DRAG SHIP HULL
    • WO2005060552A2
    • 2005-07-07
    • PCT/US2004/040307
    • 2004-12-03
    • LANG, Thomas, G.LANG, James, T.
    • LANG, Thomas, G.LANG, James, T.
    • B63B1/04B63B1/06B63B1/10B63B1/12B63B1/18B63B1/24B63B1/32B63B1/34B63B1/38B63G8/00B63G8/18
    • B63B1/32B63B1/18B63B1/24B63B1/38B63B39/06Y02T70/12Y02T70/122
    • A low drag ship hull generally includes a side air cavity initiated by wetted bow section, bottom air cavity initiated by wetted bottom nosepiece, wetted stern section that closes a lower portion of the side cavity, wetted bottom tailpiece that closes the bottom cavity, stabilizing fin, and propulsor. The bottom of a catamaran hull cross structure includes bow impact alleviator. Optional flaps in the stabilizing fins, together with optional all-movable canard fins are used for control. Different wetted bow sections and retractable means are used for starting side cavities. A low drag hull may utilize multiple air cavities. A new low drag hull includes a new upper bottom air cavity that is initiated by an upper bottom wetted nosepiece, and closed by an upper bottom tailpiece. Alternative designs include a shortened forward hull spaced ahead of a shortened aft hull, and a hydrofoil-supported trimaran with low drag hulls.
    • 低拖船船壳通常包括由润湿的弓形部分引导的侧空气腔,由润湿的底部喷嘴启动的底部空气腔,封闭侧腔的下部的润湿船尾部分,关闭底部空腔的润湿的底部尾部,稳定翅片 ,推荐者。 双体船船体结构的底部包括弓冲击缓冲器。 稳定鳍片中的可选翼片,以及可选的全可动翼片用于控制。 不同的润湿弓形部分和伸缩装置用于起始侧腔。 低阻力船体可以利用多个空气腔。 一个新的低拖曳船体包括一个新的上部底部空气腔,由上部底部湿的鼻梁开始,并由上部底部尾端封闭。 替代设计包括在缩短的船尾前面延伸的缩短的前船体,以及具有低拖船船体的水翼支撑的三体船。
    • 6. 发明申请
    • HIGH SPEED SHIP
    • 高速船
    • WO01079057A1
    • 2001-10-25
    • PCT/RU2001/000131
    • 2001-04-02
    • B63B1/18B63B1/26B63B1/28
    • B63B1/18B63B1/286B63B2001/183B63H2011/008
    • The invention relates to shipbuilding and to the construction design of speed ships moving in a transition regime at a most optimum speed (Froud number with respect to displacement ranges from 1.0 to 3). The inventive speed ship comprises a hull with a keelbuilt bottom and active pullout elements controlling lifting force. In the aft part, the ship is fitted with projecting bearing parts having a blunt rear edge. The lower surface of each projecting bearing part is arranged on both sides of a keel and on a plane with the adjacent bottom surface forming at the deadrise angle therewith of up to 15 DEG . The length of the projecting bearing parts ranges from 0.1 to 0.5 of the ship hull length and the thickness thereof decreases away from the stern to the rostrum. The ratio of the ship's beam fitted with the projecting bearing parts to the beam of the hull ranges from 1.2 to 2.5. The active elements controlling lifting force are arranged directly behind the blunt rear edge of the projecting bearing parts. Submerged wings with a surface ranging from 3 to 20 % of a waterline area can be arranged in the forebody, in the middle and in the aft end of the ship. Said wings can be fixed directly to the ship's hull or by means of a central pillar (T-wing).
    • 本发明涉及造船和以最佳速度在过渡状态下移动的速度船的构造设计(相对于位移范围为1.0至3的弗罗批号)。 本发明的速度船包括具有龙骨底部的船体和控制提升力的主动拉出元件。 在船尾部分,船舶上安装有具有钝的后缘的突出的轴承部件。 每个突出轴承部分的下表面布置在龙骨的两侧,并且在相邻的底部表面形成与其高度相差15度的平面上。 突出轴承部件的长度范围为船体长度的0.1至0.5,其厚度从船尾延伸到主讲台。 装配有突出轴承部件的船舶梁与船体梁的比例范围为1.2至2.5。 控制提升力的活动元件直接布置在突出的轴承部分的钝的后边缘的后面。 水面面积从3%到20%的淹没翼可以排列在船体的中部和后端。 所述翼可以直接固定在船体上,也可以通过中央支柱(T翼)固定。
    • 7. 发明申请
    • HYDROPLANE
    • 水上飞机
    • WO00003914A1
    • 2000-01-27
    • PCT/RU1999/000223
    • 1999-07-09
    • B63B1/18B63B1/22B63H11/103
    • B63H11/103B63B1/18B63B1/22
    • The present invention pertains to the ship-building industry and more precisely to the construction of hydroplanes that include propulsion spoilers. This hydroplane comprises a hull with a keeled bottom as well as stern propulsion spoilers, and also includes water-jet propulsion devices mounted in the stern part of the ship. The water-intake openings of the propulsion devices are arranged at the bottom of the hull in front of the spoilers. When the ship moves with the propulsion spoilers in an expanded position, an area of increased pressure is formed immediately in front of said spoilers. This area propagates into the water-intake openings and the water intake from the area with an increased pressure increases the operation efficiency of the water-jet propulsion devices. This hydroplane can further be fitted with aft spoilers while the bottom comprises aft and stern transverse steps behind which the spoilers are arranged. In this case, the deadrise angle of the bottom ranges from 6 to 12 DEG at the aft step and from 0 to 6 DEG at the stern step.
    • 本发明涉及造船业,更准确地涉及包括推进扰流板在内的水电站的建造。 该水平面包括具有龙骨底部的船体以及船尾推进扰流板,并且还包括安装在船的船尾部分中的喷水推进装置。 推进装置的进水口布置在船体底部的扰流板前面。 当船舶在推进扰流板处于扩张位置时移动时,立即在所述扰流板的前面形成增加压力的区域。 该区域传播到进水口,并且具有增加压力的区域的进水口增加了喷水推进装置的运行效率。 该水平面还可以安装有尾部扰流板,而底部包括尾部和船尾横向台阶,扰流板布置在其后面。 在这种情况下,底部的起落角在后退阶段为6〜12°,船尾为0〜6°。