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CN203946234U - A kind of hydrofoil of surface band pit - Google Patents

A kind of hydrofoil of surface band pit Download PDF

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Publication number
CN203946234U
CN203946234U CN201420164072.5U CN201420164072U CN203946234U CN 203946234 U CN203946234 U CN 203946234U CN 201420164072 U CN201420164072 U CN 201420164072U CN 203946234 U CN203946234 U CN 203946234U
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hydrofoil
dimples
plate
drag
surface according
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李超
王化明
屠璐琼
杨秀勇
陈俊宏
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Zhejiang Ocean University ZJOU
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Zhejiang Ocean University ZJOU
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Abstract

The utility model provides a kind of hydrofoil of surface band pit, this hydrofoil comprises hydrofoil plate and hydrofoil pillar, hydrofoil plate water flowing cabane strut is fixedly mounted on naval vessels below, and the outside face of hydrofoil plate is provided with the drag reduction structure being made up of rough strip, groove, pit or texture structure.Possesses the hydrofoil plate of this drag reduction structure in the time of underwater exercise, possesses higher 1ift-drag ratio, can reduce friction drag and the viscous resistance of hydrofoil to water, increase the energy efficiency that drives the means of deliverys such as hydrofoil boat, in improving ship speed, reach the beneficial effect of energy-saving and emission-reduction.

Description

一种表面带凹坑的水翼A hydrofoil with dimples on the surface

技术领域technical field

本实用新型涉及水翼装置,更具体地说,涉及一种表面带凹坑的水翼。The utility model relates to a hydrofoil device, in particular to a hydrofoil with dimples on the surface.

背景技术Background technique

水翼船或水翼艇是可以进行高速航行的水中交通工具。船身的底部装有支架,支架下方安装有水翼板,水翼板完全或部分浸没在水中。根据流体力学的原理,流速越大的位置,压强越小。当船舶在水中航行时,水相对于水翼板快速流动,并且经过其上表面的水流速度大,下表面的水流速度小,这样水翼板的上下表面就形成了压强差,当压强差强到一定程度时,船身就会被抬高,甚至高出水面。船身浸没在水中的体积减小,所受到的水的阻力也相应大幅度减小,这样,在相同的推进力下,安装了水翼的船舶可以达到更高的速度。跟其他的高速舰艇技术相比,水翼艇(主要是全浸型)的主要优点是能够在较为恶劣的海情下航行,艇身的巅簸较少。而且高速航行时所产生的兴波较为少,对岸边的影响较低。Hydrofoil boats or hydrofoil boats are water vehicles that can navigate at high speeds. The bottom of the hull is equipped with a support, and a hydrofoil is installed under the support, and the hydrofoil is completely or partially submerged in water. According to the principles of fluid mechanics, the greater the flow velocity, the lower the pressure. When the ship sails in the water, the water flows quickly relative to the hydrofoil, and the velocity of the water flow passing through its upper surface is large, while the velocity of the water flow on the lower surface is small, so that a pressure difference is formed between the upper and lower surfaces of the hydrofoil. When the pressure difference is strong To a certain extent, the hull will be raised, even higher than the water surface. The volume of the hull submerged in water is reduced, and the resistance of the water is also greatly reduced accordingly. In this way, under the same propulsion force, the ship with hydrofoils can reach a higher speed. Compared with other high-speed ship technologies, the main advantage of hydrofoil boats (mainly fully submerged) is that they can sail in harsher sea conditions with less bumping of the hull. Moreover, the waves generated during high-speed navigation are relatively small, and the impact on the shore is relatively low.

由于现在节能减排的要求,整个航运界和造船界对于能耗指标的要求达到了新的高度。对于船舶制造来说如何减小航行的阻力一直也是很多研究院校研究的一个方向,船舶阻力的减小能够在额定功率下达到更快的速度,达到节能减排的目的。安装水翼虽然可以有效提高船舶的航行速度,但是目前仍有许多问题有待解决。比如水翼在水中运动时,上下翼面都与水接触。当水流过水翼的时候,由于水本身的粘性,会在水翼表面形成一个边界层。边界层是一个薄层,它紧靠水翼表面,沿水翼表面法线方向存在着很大的速度梯度和旋度的流动区域。粘性应力对边界层的水体来说是阻力,所以随着水体沿物面向后流动,边界层内的水体会逐渐减速,增压。由于水体流动的连续性,边界层会变厚以在同一时间内流过更多的低速水体。因此边界层内存在着逆压梯度,流动在逆压梯度作用下,会进一步减速,最后整个边界层内的水体的动能都不足以长久的维持流动一直向下游进行,以致在物体表面某处其速度会与势流的速度方向相反,即产生逆流。该逆流会把边界层向势流中排挤,造成边界层突然变厚或分离。边界层分离会使得阻力上升,特别是因为位在水翼前后水体的压强差上升,使得压差阻力变大。阻力上升就会引起速度下降,起不到水翼应该起到的作用。Due to the current requirements for energy saving and emission reduction, the entire shipping industry and shipbuilding industry have reached new heights in terms of energy consumption indicators. For shipbuilding, how to reduce the resistance of navigation has always been a research direction of many research institutes. The reduction of ship resistance can achieve faster speed under rated power and achieve the purpose of energy saving and emission reduction. Although the installation of hydrofoils can effectively improve the navigation speed of ships, there are still many problems to be solved. For example, when a hydrofoil moves in water, the upper and lower surfaces of the wing are in contact with the water. When water flows over the hydrofoil, a boundary layer is formed on the surface of the hydrofoil due to the viscosity of the water itself. The boundary layer is a thin layer, which is close to the surface of the hydrofoil, and there is a flow region with a large velocity gradient and curl along the normal direction of the surface of the hydrofoil. Viscous stress is resistance to the water body in the boundary layer, so as the water body flows backward along the object surface, the water body in the boundary layer will gradually slow down and pressurize. Due to the continuum of water flow, the boundary layer thickens to allow more low-velocity water to flow at the same time. Therefore, there is a reverse pressure gradient in the boundary layer, and the flow will further decelerate under the action of the reverse pressure gradient. Finally, the kinetic energy of the water body in the entire boundary layer is not enough to maintain the flow downstream for a long time, so that somewhere on the surface of the object The velocity will be in the opposite direction to the velocity of the potential flow, ie countercurrent. This countercurrent will push the boundary layer into the potential flow, causing the boundary layer to suddenly thicken or separate. The separation of the boundary layer will increase the drag, especially because the pressure difference of the water body before and after the hydrofoil increases, so that the pressure difference drag becomes larger. The increase in resistance will cause the speed to decrease, which will not play the role that the hydrofoil should play.

此外,水翼与来流有一定攻角,翼截面有拱度,因而产生升力。水翼的运动速度不断提高,翼面上的负压强便不断下降,当负压强降至低于水在当时温度下的饱和蒸汽压强时,局部翼面上的水出现气泡,当气泡随水流运动到高压区的时候,气泡收到挤压收缩甚至发生溃灭,伴随着气泡的产生、发展和溃灭的循环过程,是空化的过程。空化是一种非常有害的现象,它会早成机械破坏、增大噪声等后果,并且会引起阻力增大和升力不稳定,甚至引发灾难事故。In addition, the hydrofoil has a certain angle of attack with the incoming flow, and the section of the wing has a camber, thus generating lift. As the movement speed of the hydrofoil continues to increase, the negative pressure on the surface of the airfoil will continue to decrease. When the negative pressure drops below the saturated vapor pressure of water at the current temperature, bubbles will appear on the water on the local surface of the airfoil. When the water flow moves to the high-pressure zone, the bubbles are squeezed, shrink or even collapse, and the cycle process of bubble generation, development and collapse is the process of cavitation. Cavitation is a very harmful phenomenon. It will cause mechanical damage, increase noise and other consequences, and it will cause increased resistance and unstable lift, and even cause disasters.

实用新型内容Utility model content

本实用新型所要解决的技术问题是提供一种性能更加优异的水翼,这种水翼可以避免现有技术中低阻力水翼的困难,降低水翼对水的摩擦阻力和粘滞阻力,增加驱动水翼艇等运载工具的能量效率,在提高船舶航速的同时达到节能减排的有益效果。The technical problem to be solved by the utility model is to provide a hydrofoil with more excellent performance, which can avoid the difficulties of the low-resistance hydrofoil in the prior art, reduce the frictional resistance and viscous resistance of the hydrofoil to the water, increase Driving the energy efficiency of vehicles such as hydrofoil boats can achieve the beneficial effects of energy saving and emission reduction while increasing the speed of ships.

相应地,本实用新型在不具限制性的实施例中提供了一种表面带凹坑的水翼以解决上述技术问题,这种水翼包括水翼板和水翼支柱,水翼板固定安装在水翼支柱的下端,水翼支柱的上端固定安装在舰艇的船身下方,水翼板的外表面上设有减阻结构,水翼板的翼截面(平行于水翼运动时前进方向的截面)为机翼形或弓形或月牙形,减阻结构可以是是分布在水翼板表面的粗糙带,粗糙带可以是连续的一整片,也可以是断续的几片,多片粗糙带可以是横向或者纵向平行分布或者称阵列形式规则分布,也可以是无序分布在水翼板的外表面上,根据试验表明粗糙带在位于距离水翼板前缘的10%~30%弦长处,其宽度为5%~20%弦长,高度为0.05mm~0.2mm可以取到较好的实用新型效果。Correspondingly, in a non-limiting embodiment, the utility model provides a hydrofoil with dimples on the surface to solve the above-mentioned technical problems. The lower end of the hydrofoil strut, the upper end of the hydrofoil strut is fixedly installed under the hull of the ship, and the outer surface of the hydrofoil plate is provided with a drag reducing structure. ) is wing-shaped or bow-shaped or crescent-shaped, and the drag reduction structure can be a rough strip distributed on the surface of the hydrofoil. It can be horizontally or vertically parallel distributed or regularly distributed in the form of an array, or it can be distributed randomly on the outer surface of the hydrofoil. According to the test, the rough zone is located at a distance of 10% to 30% of the chord length from the leading edge of the hydrofoil. The width is 5% to 20% of the chord length, and the height is 0.05mm to 0.2mm, which can achieve better utility model effects.

除了粗糙带以外,减阻结构还可以采用设置在水翼板表面的凹槽和纵横交错的网格状纹理结构。凹槽和纹理结构可以是直线型也可以是曲线型,或者是无规则线条形状,凹槽和纹理结构在水翼板表面的分布可以是横向、纵向平行分布,也可以是无序地分布在水翼板的外表面上。In addition to rough strips, the drag reduction structure can also use grooves and criss-cross grid-like texture structures arranged on the surface of the hydrofoil. The grooves and texture structures can be linear or curved, or in the shape of random lines, and the distribution of grooves and texture structures on the surface of the hydrofoil can be horizontally and vertically parallel, or randomly distributed on the surface of the hydrofoil. on the outer surface of the hydrofoil.

在本实用新型的众多实施例中,作为最优化选择,减阻结构宜采用分布在水翼板表面的凹坑结构。凹坑的数量可以是一个,也可以是多个。这些凹坑的形状为圆形凹坑、椭圆形凹坑、多边形凹坑和不规则形状凹坑中的一种或多种的组合。多个凹坑时,凹坑在水翼板的外表面的排列方式可以是如下的几种:纵横对齐排列、纵横交错排列、不规则排列。凹坑的深度范围在10mm~40mm时可以取得比较理想的减阻效果。凹坑在水翼板表面的面积率可以在5%~60%范围内进行选择。In many embodiments of the present utility model, as an optimal choice, the drag reducing structure should adopt the structure of dimples distributed on the surface of the hydrofoil. The number of pits may be one or more. The shape of these pits is one or a combination of circular pits, oval pits, polygonal pits and irregular pits. When there are multiple dimples, the dimples can be arranged in the following ways on the outer surface of the hydrofoil: vertically and horizontally aligned, vertically and horizontally staggered, and irregularly arranged. When the depth of the pits ranges from 10 mm to 40 mm, a relatively ideal drag reduction effect can be obtained. The area ratio of dimples on the surface of the hydrofoil can be selected within the range of 5% to 60%.

水翼在水体中运动时的边界层,根据局部流场的雷诺数不同,边界层内的流体可以分为层流或紊流。光滑的水翼板表面的边界层内通常是层流,而不光滑水翼板的边界层内的水流是紊流。紊流的边界层受逆压梯度的影响较小,所以不光滑的水翼板表面的边界层的分离点相对靠后,其粘性阻力反而较光滑的水翼板更低,压差阻力更是可以大幅度减小。The boundary layer when the hydrofoil moves in the water body, according to the Reynolds number of the local flow field, the fluid in the boundary layer can be divided into laminar flow or turbulent flow. The flow in the boundary layer of a smooth foil surface is usually laminar, while the flow in the boundary layer of a rough foil is turbulent. The boundary layer of turbulent flow is less affected by the adverse pressure gradient, so the separation point of the boundary layer on the surface of the rough hydrofoil is relatively behind, and its viscous resistance is lower than that of the smooth hydrofoil, and the pressure difference resistance is even greater. can be greatly reduced.

此外在水翼板表面设置减阻结构,可以增大水翼板表面的流畅湍流,使转捩点提前,显著提升水翼板表面的流场压力,延缓空化发生,并且对水翼的升力影响较小。In addition, setting a drag-reducing structure on the surface of the hydrofoil can increase the smooth turbulent flow on the surface of the hydrofoil, advance the transition point, significantly increase the flow field pressure on the surface of the hydrofoil, delay the occurrence of cavitation, and have a relatively small influence on the lift of the hydrofoil. Small.

与现有技术相比,本实用新型的有益之处在于:Compared with the prior art, the utility model is beneficial in that:

1.可以有效地推后边界分离点,减小阻力,通常情况下,水翼艇航行时,雷诺数Re能够达到105以上,远远大于发生边界层分离的Re=60的要求,所以当水翼艇正常航行时,会发生边界层的分离现象,而水翼上的减阻结构能够起到推迟边界层分离点的作用,减小水翼上的粘性阻力,降低了水翼艇航行时的能耗;1. It can effectively push back the boundary separation point and reduce resistance. Usually, when the hydrofoil sails, the Reynolds number Re can reach more than 105, which is far greater than the requirement of Re=60 for boundary layer separation. When the wing boat sails normally, the separation of the boundary layer will occur, and the drag reduction structure on the hydrofoil can delay the separation point of the boundary layer, reduce the viscous resistance on the hydrofoil, and reduce the pressure of the hydrofoil boat when it is sailing. energy consumption;

2.显著提升水翼板表面的流场压力,延缓空化发生,有效降低了机械破坏、阻力增大、升力不稳定和噪音增大等不良后果。2. Significantly increase the flow field pressure on the surface of the hydrofoil, delay the occurrence of cavitation, and effectively reduce the adverse consequences such as mechanical damage, increased resistance, unstable lift and increased noise.

附图说明Description of drawings

图1是本实用新型具体实施例一的结构示意图;Fig. 1 is the structural representation of the specific embodiment one of the utility model;

图2是水翼升力随攻角变化柱状图(横坐标为攻角角度);Figure 2 is a histogram of hydrofoil lift changing with the angle of attack (the abscissa is the angle of attack);

图3是水翼阻力随攻角变化柱状图(横坐标为攻角角度);Figure 3 is a histogram of hydrofoil resistance changing with the angle of attack (the abscissa is the angle of attack);

图4是水翼阻力随攻角变化折线图(横坐标为攻角角度);Figure 4 is a line diagram of hydrofoil resistance changing with the angle of attack (the abscissa is the angle of attack);

图5是水翼升阻比随攻角变化折线图(横坐标为攻角角度);Figure 5 is a broken line diagram of the lift-drag ratio of the hydrofoil with the angle of attack (the abscissa is the angle of attack);

图6是固定攻角条件下水翼阻力随航速变化折线图(横坐标为航速);Fig. 6 is a broken-line diagram of the hydrofoil resistance changing with the speed at a fixed angle of attack (the abscissa is the speed);

图7是固定攻角条件下水翼升阻比随航速变化折线图(横坐标为航速);Figure 7 is a broken line diagram of the lift-drag ratio of the hydrofoil changing with the speed at a fixed angle of attack (the abscissa is the speed);

图8是具体实施例二结构示意图;Fig. 8 is a schematic structural diagram of a second embodiment;

图9是具体实施例三结构示意图;Fig. 9 is a schematic structural view of the third embodiment;

图10是具体实施例四结构示意图。Fig. 10 is a schematic structural diagram of Embodiment 4.

具体实施方式Detailed ways

下面根据具体实施例和附图本本实用新型做进一步的说明。The utility model will be further described below according to specific embodiments and accompanying drawings.

如图1和图2所示的低阻力水翼,包括水翼支柱1和水翼板2,水翼板2的翼截面形状为机翼型,水翼板的翼展为15m,弦长为3m,在水翼板2的表面,纵横对齐排列着圆形凹坑3。这些凹坑3的深度为30mm,凹坑3在水翼板2表面的面积率为50%。The low-resistance hydrofoil shown in Figure 1 and Figure 2 includes a hydrofoil strut 1 and a hydrofoil plate 2. The wing section shape of the hydrofoil plate 2 is an airfoil shape, the wingspan of the hydrofoil plate is 15m, and the chord length is 3m, on the surface of the hydrofoil 2, circular pits 3 are aligned vertically and horizontally. The depth of these dimples 3 is 30 mm, and the area ratio of the dimples 3 on the surface of the hydrofoil 2 is 50%.

由于传统习惯,人们认为越光滑的表面的摩擦阻力越小,而好的材料如钛合金材料等抗空化的效果会较好,因此传统的研发方向多集中在通过改进水翼的外形来降低其受到的阻力,采用更好的材料来对抗空化效应,但是效果要么不理想,要么提高了水翼的制作成本。本实用新型的发明人克服了传统的技术偏见----粗糙的表面会增大摩擦阻力,将水翼板2的表面上设置了减阻结构,产生紊流的边界层,推迟边界分离点,提前了转捩点,无论在减少水翼受到的阻力方面,还是减少空化的危害方面,都取得了良好的效果,并且在实验中得到了证实。Due to traditional habits, people think that the smoother the surface, the smaller the frictional resistance, and good materials such as titanium alloy materials will have a better anti-cavitation effect. Therefore, the traditional research and development direction is mostly focused on reducing For the resistance it receives, better materials are used to resist the cavitation effect, but the effect is either unsatisfactory, or the production cost of the hydrofoil is increased. The inventor of the utility model has overcome the traditional technical prejudice that a rough surface will increase the frictional resistance, and a drag-reducing structure is set on the surface of the hydrofoil 2 to generate a turbulent boundary layer and delay the boundary separation point , the turning point is brought forward, no matter in terms of reducing the drag on the hydrofoil or reducing the harm of cavitation, good results have been achieved, and it has been confirmed in the experiment.

在固定航速V=20m/s的条件下,对本实用新型所提供的水翼和同样尺寸和外形的光滑水翼在不同攻角下所受到的升力(L,单位:牛顿)、阻力(R,单位:牛顿)、升阻比(K)进行测试,可以得到如下的实验结果:Under the condition of fixed speed V=20m/s, the lift (L, unit: Newton), resistance (R, R, Unit: Newton) and lift-to-drag ratio (K), the following experimental results can be obtained:

表1-1传统光滑水翼的升力(L)、阻力(R)、升阻比(K)实验数据Table 1-1 Experimental data of lift (L), drag (R), and lift-to-drag ratio (K) of traditional smooth hydrofoils

攻角Angle of attack L(N)L(N) R(N)R(N) KK 00 2826.1943922826.194392 7222.0735747222.073574 0.391330.39133 33 45115.4223345115.42233 8589.4389428589.438942 5.252435.25243 55 76782.8578776782.85787 8668.6964988668.696498 8.857498.85749 66 93015.7057493015.70574 8687.208538687.20853 10.9983910.99839 77 109047.414109047.414 8770.4769498770.476949 12.4334612.43346 88 125011.2142125011.2142 8815.9574618815.957461 14.1801114.18011

表1-2本实用新型水翼的升力(L)、阻力(R)、升阻比(K)实验数据Table 1-2 Experimental data of lift (L), drag (R) and lift-to-drag ratio (K) of the utility model hydrofoil

攻角Angle of attack L(N)L(N) R(N)R(N) KK 00 2228.870362228.87036 5574.071285574.07128 0.399860.39986 33 45164.7051545164.70515 6815.782736815.78273 6.626486.62648 55 76742.9286276742.92862 6964.774176964.77417 11.018711.0187 66 92942.2053892942.20538 6979.536396979.53639 13.316313.3163 77 109126.79475109126.79475 7006.836287006.83628 15.574315.5743 88 120997.89375120997.89375 7048.740477048.74047 17.165817.1658

由表1-1和图2和图3可知,水翼板2表面的凹坑3对水翼的升力几乎没有产生影响,但是水翼所受到的阻力却明显减小。再把水翼所受到的阻力和升阻比进行单独研究。由图4和图5可以看出,随着攻角的变大,本具体实施例和传统光滑水翼所受到的阻力都相应增大,但是传统光滑水翼所受到的阻力始终比本具体实施例要大。图5更加清晰地显示出本具体实施例的升阻比始终比传统光滑表面水翼要大,更加有利于安装了本实用新型所提供的水翼的舰艇的航行。It can be seen from Table 1-1 and Figures 2 and 3 that the dimples 3 on the surface of the hydrofoil plate 2 have almost no effect on the lift of the hydrofoil, but the resistance suffered by the hydrofoil is significantly reduced. Then the drag and lift-to-drag ratio of the hydrofoil are studied separately. As can be seen from Fig. 4 and Fig. 5, as the angle of attack increases, the resistance of this specific embodiment and the traditional smooth hydrofoil increases accordingly, but the resistance of the traditional smooth hydrofoil is always higher than that of this specific embodiment. The example should be large. Fig. 5 shows more clearly that the lift-to-drag ratio of this specific embodiment is always larger than that of the traditional smooth surface hydrofoil, which is more conducive to the navigation of ships equipped with the hydrofoil provided by the utility model.

为了进一步验证本实用新型的有益效果,在固定攻角(6°)条件下改变流体速度(模拟航速)进行进一步模拟实验。可以得到如下的实验数据:In order to further verify the beneficial effect of the utility model, a further simulation experiment was carried out by changing the fluid speed (simulated speed) under the condition of a fixed angle of attack (6°). The following experimental data can be obtained:

表1-3传统光滑水翼的升力、阻力和升阻比随流体速度变化数据Table 1-3 The lift, drag and lift-to-drag ratio of traditional smooth hydrofoil change data with fluid velocity

速度(m/s)Speed (m/s) L(N)L(N) R(N)R(N) KK 1515 52449.51452449.514 3088.62343088.6234 16.9815116.98151 2020 93015.70593015.705 8687.20858687.2085 10.9983910.99839 22.522.5 118261.114118261.114 5066.25985066.2598 23.3428823.34288 2525 121008.691121008.691 7220.42457220.4245 16.7592216.75922

表1-4本实用新型水翼的升力、阻力和升阻比随流体速度变化数据Table 1-4 The lift, drag and lift-to-drag ratio of the utility model hydrofoil change data with fluid velocity

速度(m/s)Speed (m/s) L(N)L(N) R(N)R(N) KK 1515 51145.98351145.983 2447.58822447.5882 20.810820.8108 2020 92942.2053892942.20538 6979.536396979.53639 13.316313.3163

22.522.5 116806.026116806.026 4153.4614153.461 28.3145328.31453 2525 120510.251120510.251 4782.54314782.5431 25.1979325.19793

结合图6和图7可知,流体速度在15~25m/s(接近水翼艇常规的航行速度)范围内,本实用新型的水翼的整体升阻比都大于常规光滑水翼的升阻比。Combining Figures 6 and 7, it can be known that the overall lift-to-drag ratio of the hydrofoil of the utility model is greater than that of the conventional smooth hydrofoil within the range of 15-25m/s (close to the conventional sailing speed of the hydrofoil) when the fluid velocity is within the range .

因此可以得出结论,本实用新型使得水翼的整体升阻比得到了明显提高,优化了水翼板的性能,取得了预期的效果。Therefore, it can be concluded that the utility model significantly improves the overall lift-to-drag ratio of the hydrofoil, optimizes the performance of the hydrofoil, and achieves expected effects.

在本具体实施例中,凹坑3的深度可以在10~40mm范围内进行选择,分别取凹坑深度为10mm、15mm、20mm、30mm、35mm、40mm进行测试,均可以取得理想的提高升阻比的技术效果。In this specific embodiment, the depth of the pit 3 can be selected within the range of 10-40mm, and the depth of the pit 3 is 10mm, 15mm, 20mm, 30mm, 35mm, and 40mm for testing, and an ideal increase in lift resistance can be obtained. Compared with the technical effect.

此外,凹坑3的形状也可以采用圆形凹坑、椭圆形凹坑、多边形凹坑和不规则形状凹坑中的一种或多种的组形式,可以采用规则或者不规则排列,均可以得到理想的提高升阻比的技术效果。In addition, the shape of the pit 3 can also be in the form of one or more groups of circular pits, elliptical pits, polygonal pits and irregular pits, and can be arranged regularly or irregularly. The ideal technical effect of increasing the lift-to-drag ratio is obtained.

凹坑在水翼板表面的面积率在5%~60%之间,取5%、10%、20%、30%、45%、50%、55%、60%进行测试,效果均十分理想。The area ratio of dimples on the surface of the hydrofoil is between 5% and 60%, and 5%, 10%, 20%, 30%, 45%, 50%, 55%, and 60% are used for testing, and the results are very satisfactory .

如图8所示的具体实施例二,与具体实施例一的区别仅在于其水翼板2表面的减阻结构是一片粗糙带4,该粗糙带在位于距离水翼板前缘的10%~30%弦长处,其宽度为20%弦长,高度为0.1mm。经测试,其也可以取得理想的提高升阻比,减少空化现象的技术效果。The specific embodiment 2 shown in Figure 8 differs from the specific embodiment 1 only in that the drag reduction structure on the surface of the hydrofoil 2 is a rough strip 4, which is located at a distance of 10% to 10% from the leading edge of the hydrofoil. At 30% of the chord length, its width is 20% of the chord length and its height is 0.1mm. After testing, it can also achieve ideal technical effects of increasing lift-to-drag ratio and reducing cavitation.

如图9所示的具体实施例三,与具体实施例一的区别仅在于其水翼板2表面的减阻结构是几条平行设置的凹槽5,这些凹槽的深度为30mm,平行于水翼前缘设置。The specific embodiment three shown in Figure 9 differs from the specific embodiment one only in that the drag reducing structure on the surface of the hydrofoil 2 is several parallel grooves 5, the depth of these grooves is 30mm, parallel to Foil leading edge setting.

如图10所示的具体实施例四,与具体实施例一的区别仅在于其水翼板2表面的减阻结构是一片交错的纹理结构6,这些纹理结构的深度为5mm。The fourth embodiment shown in Fig. 10 differs from the first embodiment only in that the drag reduction structure on the surface of the hydrofoil 2 is a piece of interlaced textured structure 6, and the depth of these textured structures is 5 mm.

以上实施例是供理解本实用新型之用,并非是对本实用新型的限制,有关领域的普通技术人员,在权利要求所述技术方案的基础上,还可以做出多种变化或造型,比如上述具体实施例的各种减阻结构可以是具体实施例所示地规则排列,也可以是不规则排列,还可以是多种减阻结构组合,例如凹坑和粗糙带、凹坑和槽、凹坑和纹理结构等等,这些变化或变型应当理解为仍属于本实用新型的保护范围。The above embodiments are for the purpose of understanding the utility model, and are not limitations to the utility model. Those of ordinary skill in the related art can also make various changes or shapes on the basis of the technical solution described in the claims, such as the above-mentioned The various drag reducing structures in the specific embodiments can be arranged regularly or irregularly as shown in the specific embodiments, and can also be a combination of various drag reducing structures, such as pits and rough strips, pits and grooves, and grooves. Pit and texture structure, etc., these changes or modifications should be understood as still belonging to the protection scope of the present utility model.

Claims (10)

1.一种表面带凹坑的水翼,包括水翼板和水翼支柱,水翼板固定安装在水翼支柱的下端,水翼支柱的上端固定安装在舰艇的船身下方,其特征在于:所述水翼板的外表面上设有减阻结构,所述减阻结构为分布在水翼板表面的粗糙带、凹槽、纹理结构或者凹坑中的一种或多种组合,所述粗糙带、凹槽、纹理结构或者凹坑的数量最少是一个。1. A hydrofoil with dimples on the surface, comprising a hydrofoil plate and a hydrofoil strut, the hydrofoil plate is fixedly mounted on the lower end of the hydrofoil strut, and the upper end of the hydrofoil strut is fixedly mounted below the hull of the ship, characterized in that : the outer surface of the hydrofoil is provided with a drag reducing structure, and the drag reducing structure is one or more combinations of rough bands, grooves, textured structures or pits distributed on the surface of the hydrofoil, so The minimum number of rough bands, grooves, textures or pits is one. 2.根据权利要求1所述的表面带凹坑的水翼,其特征在于:所述凹坑为圆形凹坑、椭圆形凹坑、多边形凹坑和不规则形状凹坑中的一种或多种组合。2. The hydrofoil with dimples on the surface according to claim 1, wherein the dimples are one of circular dimples, elliptical dimples, polygonal dimples and irregular dimples or Various combinations. 3.根据权利要求2所述的表面带凹坑的水翼,其特征在于:所述凹坑的数量有多个,并在水翼板的外表面纵横对齐整齐排列。3. The hydrofoil with dimples on the surface according to claim 2, characterized in that: the number of the dimples is multiple, and they are aligned vertically and horizontally on the outer surface of the hydrofoil. 4.根据权利要求2所述的表面带凹坑的水翼,其特征在于:所述凹坑的数量有多个,并在水翼板的外表面纵横交错排列。4. The hydrofoil with dimples on the surface according to claim 2, characterized in that there are multiple dimples arranged in a criss-cross pattern on the outer surface of the hydrofoil. 5.根据权利要求2所述的表面带凹坑的水翼,其特征在于:所述凹坑的数量有多个,并在水翼板的外表面不规则排列。5. The hydrofoil with dimples on the surface according to claim 2, characterized in that: there are multiple dimples arranged irregularly on the outer surface of the hydrofoil. 6.根据权利要求1至5任一项所述的表面带凹坑的水翼,其特征在于:所述凹坑的深度为10mm~40mm。6. The hydrofoil with dimples on the surface according to any one of claims 1 to 5, characterized in that: the depth of the dimples is 10mm-40mm. 7.根据权利要求6所述的表面带凹坑的水翼,其特征在于:所述凹坑的面积率为5%~20%。7. The hydrofoil with dimples on the surface according to claim 6, characterized in that: the area ratio of the dimples is 5%-20%. 8.根据权利要求1所述的表面带凹坑的水翼,其特征在于:所述水翼板的平行于舰艇前进方向的截面外轮廓为机翼型,所述粗糙带位于距离水翼板前缘的10%~30%弦长处,粗糙带的宽度为5%~20%弦长,高度0.05mm~0.2mm。8. The hydrofoil with dimples on the surface according to claim 1, characterized in that: the profile of the section of the hydrofoil plate parallel to the forward direction of the ship is an airfoil shape, and the rough strip is located at a distance from the hydrofoil plate. At 10% to 30% of the chord length of the edge, the width of the rough belt is 5% to 20% of the chord length, and the height is 0.05mm to 0.2mm. 9.根据权利要求1所述的表面带凹坑的水翼,其特征在于:所述凹槽位于所述水翼板的表面且平行于所述水翼板的前缘。9. The hydrofoil with dimples on the surface according to claim 1, wherein the grooves are located on the surface of the hydrofoil plate and parallel to the leading edge of the hydrofoil plate. 10.根据权利要求1所述的表面带凹坑的水翼,其特征在于:所述纹理结构为纵横交错的网格状纹理结构,分布于所述水翼板的表面。10 . The hydrofoil with dimples on the surface according to claim 1 , wherein the texture structure is a criss-cross grid-like texture structure distributed on the surface of the hydrofoil plate. 11 .
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103910023A (en) * 2014-04-04 2014-07-09 浙江海洋学院 Novel efficient hydrofoil
RU182684U1 (en) * 2017-10-29 2018-08-28 Виталий Алексеевич Пелешенко Hydrofoil
CN110562420A (en) * 2019-09-30 2019-12-13 重庆前卫科技集团有限公司 aerofoil plate and processing technology thereof
CN112373619A (en) * 2020-11-24 2021-02-19 天津小鲨鱼智能科技有限公司 Hydrofoil
FR3153073A1 (en) * 2023-09-20 2025-03-21 Evosea Hydrofoil-type appendage device for a boat and watercraft comprising such a device

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103910023A (en) * 2014-04-04 2014-07-09 浙江海洋学院 Novel efficient hydrofoil
CN103910023B (en) * 2014-04-04 2016-12-07 浙江海洋学院 A kind of hydrofoil
RU182684U1 (en) * 2017-10-29 2018-08-28 Виталий Алексеевич Пелешенко Hydrofoil
CN110562420A (en) * 2019-09-30 2019-12-13 重庆前卫科技集团有限公司 aerofoil plate and processing technology thereof
CN112373619A (en) * 2020-11-24 2021-02-19 天津小鲨鱼智能科技有限公司 Hydrofoil
CN112373619B (en) * 2020-11-24 2023-01-31 天津小鲨鱼智能科技有限公司 Hydrofoil
FR3153073A1 (en) * 2023-09-20 2025-03-21 Evosea Hydrofoil-type appendage device for a boat and watercraft comprising such a device

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