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1.
碟形水下滑翔器作为一种优点众多的新型水下滑翔器,近年来得到广泛应用。其液压浮力调节系统、姿态控制系统以及转向控制系统必须安装在耐压壳体内部,因此,对于耐压壳体的设计来说,尽量小的重量和尽量大的有效容积是其设计时的重要技术指标。为了得到最优结构,采用尺寸优化方法,以壳体厚度、两道环肋的高度作为设计变量对耐压壳进行优化设计,以期达到强度足够高、最大变形值小于容许变形值和质量最小的轻量化目标。优化后,质量较初始设计减少了30%,轻量化效果明显,并对最终选择的结构进行屈曲分析,其临界压力远大于许用压力。  相似文献   

2.
针对某型救生钟的救生舱耐压壳体,推导出典型水下耐压结构的计算公式,建立结构优化数学模型,并编制计算程序以求解结构最优尺寸,在此基础上确定耐压结构的设计尺寸.对设计结果采用有限元计算和规范计算比对分析,结果证明采用程序计算设计的优化尺寸满足工程要求.本文提供的计算方法可为水下环肋耐压壳体结构工程设计提供参考.  相似文献   

3.
本文从可潜器总体设计角度出发,对内部设置布置原则,科研蓄电池电源选用,重量、浮力平衡,浮力材料,耐压壳体不连续结构的设计,壳体加工制造,以及动力推进系统的选择等问题,进行了较详细的论述。  相似文献   

4.
耐压球壳是载人潜水器的关键部件,对于载人潜水器的安全性、总体性能等诸多方面均有重要的影响。针对轻载作业型HOV耐压球壳的设计,确定了壳体材料、结构形式和主要尺度,完成了基于规范的耐压球壳强度校核和稳定性分析,设计了开孔加强结构,完成了基于有限元耐压球壳模型强度校核。最后,在考虑了材料非线性、初始缺陷等因素的基础上,采用弧长法完成了耐压球壳的稳定性分析。结果表明耐压球壳的设计方案满足规范要求,为深水轻载作业型载人潜水器耐压球壳的设计提供了参考。  相似文献   

5.
詹可  蒋垣腾  赵敏 《海洋工程》2022,40(6):83-96
常规耐压结构拓扑优化设计研究主要集中于静水压条件下的设计相关载荷拓扑优化理论及方法。但是,在深海环境下,耐压结构可能面临内爆所产生的冲击载荷,其载荷呈现高频率的周期性变化。为研究载荷变化对耐压结构优化设计的影响,在BILE模型的基础上,结合修正的SIMP插值模型,开展不同频率、设计相关动载荷作用下的水下耐压结构拓扑优化理论及方法研究。设计相关动载荷的难点在于不仅载荷的作用位置和方向在优化过程中发生变化,且其大小也随优化过程进行而发生变化,这是与常规设计相关静载荷本质的不同。通过经典的拱形结构优化算例验证BILE模型在动力学拓扑优化中的可行性,进而研究设计相关动载荷作用下的水下耐压结构的最佳拓扑形式。研究表明,在低频时,圆环型耐压结构无明显变化,但多球交接耐压结构在交接处会出现明显材料聚集;高频时,两者均发生明显变化,得到耐压结构新形式。关于设计相关动载荷作用下的水下耐压结构拓扑优化研究,将对新型水下耐压结构的探索具有一定的工程应用价值。  相似文献   

6.
采用分枝定界法和序列二次规划方法,对载人潜水器圆柱形耐压壳体的重量最小化进行了研究.设计变量是壳板的厚度、肋骨的型号、间距和数量,讨论了下潜深度、材料几何参数对重量以及其它特征量的影响.算例计算表明,下潜深度越大,屈服极限越高的材料重量减轻越明显.对于大深度而言,选用高屈服极限材料,可以使得材料能够充分利用.文中还对结构重量占排水量比例随深度变化的情况进行了研究.  相似文献   

7.
以微型轴向柱塞泵为核心的高压浮力驱动系统是1 000 m以深水下滑翔器和剖面浮标优先采用的重要动力单元。文中首先介绍了当前国际上水下滑翔器和剖面浮标两型剖面运动平台的浮力驱动系统的种类及应用,然后以1 000 m以深水下滑翔器为例,系统地阐述了其高压浮力驱动系统的工作原理和设计方法,以及绝对排油量测量、吸油口气锁防止和柱塞偶件精密配合等核心问题。设计制作出精密、高效而且可靠的高压浮力驱动系统,可以为我国剖面观测平台的进一步发展起到推进作用。  相似文献   

8.
张洪彬  徐会希 《海洋工程》2022,40(2):154-161
耐压舱设计是水下机器人的核心技术之一,其极限承载力研究是核心中的核心。针对球壳封盖加柱形壳体耐压舱,现行标准对于初始导入缺陷数值的确定往往过于保守,对于耐压舱体数量较多的无人潜水器来说,过大的设计质量是总体设计所无法接受的。首先采用装配体整体建模策略,建立复合屈曲的受力模型,将三大非线性影响因素同时引入到极限承载力研究中,提升了计算精度。然后分别针对确定性缺陷和非确定性缺陷结构开展极限承载力研究。最后,提出以0.23%的初始缺陷导入尺度作为球壳封盖加圆柱壳体的耐压壳体缺陷导入参数,给出了导入尺度的计算方法,并借助水压试验对上述参数的准确性进行验证。  相似文献   

9.
AUV在水下作业时浮力会受到海水温度、深度等的影响而发生变化,为了解决浮力变化引起的航行性能问题研制了浮力调节装置,它对于大航程、大潜深AUV的发展具有重要的意义。针对以上问题,设计了一套活塞缸式浮力调节装置,它利用液压系统驱动液压缸吸排海水改变浮力从而实现浮力调节的目的,浮力调节的大小是通过直线位移传感器测量油液的改变量间接计算得到的;接着利用AMESim进行液压系统仿真,重点分析了液压缸的动态特性,为实际系统的试验提供了理论的指导意义;最后为了验证液压库建模和HCD库建模的等效性,采用HCD库建模进行比较分析。  相似文献   

10.
氮化硅陶瓷具有密度小强度高的优点,在深潜浮力设备领域具有广阔发展前景。然而陶瓷材料固有的脆性以及万米深海严苛的工作环境,使得氮化硅陶瓷空心浮力球在深水环境下面临着内爆的风险。为探究氮化硅陶瓷空心浮力球在内爆临界状态下的失效问题,设计并进行了三点弯曲试验,确定了氮化硅陶瓷材料的力学性能参数,包括弹性模量和破坏应力;随后对氮化硅陶瓷空心浮力球内爆试验的过程及结果进行了回顾总结;基于标准球壳模型与浮力球实物的CT扫描几何模型,对浮力球在内爆临界状态的失效过程进行了有限元仿真分析。结果表明:氮化硅陶瓷空心浮力球的性能存在一定不稳定性;结构内表面局部过大的拉应力是造成失效的主要原因,对内表面进行预加压处理或能提高其抗内爆性能。  相似文献   

11.
海洋湍流混合过程对大洋热盐环流具有重要调控作用,因此海洋湍流混合特征量如湍动能耗散率等物理量的定量刻画,主要通过现场湍流观测来实现。为满足长期连续海洋湍流混合观测资料的迫切需求及打破国外的技术封锁,自行研制了基于水下滑翔机的湍流观测仪。为了测试滑翔机在小尺度湍流观测方面的可行性,将一个携带有剪切探头的湍流仪安装在滑翔机本体上,并在千岛湖进行了一系列的实验。滑翔机平台的主要噪声来源于浮力调节机构中的油泵,油泵会在接近剖面的底端时开启。三轴加速度谱在30 Hz左右有明显的谱峰,说明滑翔机油泵的振动频率应该是在30 Hz左右,在其他频率点上振动较小。由剖面下潜过程(开泵)的波数谱可知,开泵时虽然对湍流观测有影响,但是振动频率在波数空间中处于无效观测谱一侧,由此说明平台的振动对剪切信号影响很小。剪切探头测得的耗散率在10-7 W/kg量级上,且都与Nasymth理论谱吻合良好,验证了滑翔机在小尺度湍流观测方面的可行性。  相似文献   

12.
Underwater glider is an autonomous underwater vehicle that glides by controlling their buoyancy and attitude using internal actuators. By changing the vehicle's buoyancy intermittently, vertical motion can be achieved. Characteristics of glider motion include upward and downward movement in a saw tooth pattern, turning and gliding in a vertical spiral motion and gliding without using thrusters or propellers. This paper presents the modelling and identification on net buoyancy, depth and pitching angle of an underwater glider system. A ballast tank subsystem is considered appropriate for the identification process since it is the main parameter for the motion control. By selecting the ballast rate as the input, three aspects of the dynamics of a glider can be observed: buoyancy, depth of the glider and pitching angle. The MATLAB System Identification ToolboxTM is used to obtain a mathematical model of the glider ballast-buoyancy, ballast-depth and ballast-pitching angle conditioning system. The best three parametric estimation models are chosen, and the results of the comparison between simulated and estimated outputs are presented. The information obtained from the modelling and identification approaches are used for USM's Underwater Glider Prototype controller design. The information observed during this procedure are utilised for optimisation, stability, reliability and robustness analysis of the underwater glider.  相似文献   

13.
A hybrid underwater glider Petrel-II has been developed and field tested. It is equipped with an active buoyancy unit and a compact propeller unit. Its working modes have been expanded to buoyancy driven gliding and propeller driven level-flight, which can make the glider work in strong currents, as well as many other complicated ocean environments. Its maximal gliding speed reaches 1 knot and the propelling speed is up to 3 knots. In this paper, a 3D dynamic model of Petrel-II is derived using linear momentum and angular momentum equations. According to the dynamic model, the spiral motion in the underwater space is simulated for the gliding mode. Similarly the cycle motion on water surface and the depth-keeping motion underwater are simulated for the level-flight mode. These simulations are important to the performance analysis and parameter optimization for the Petrel-II underwater glider. The simulation results show a good agreement with field trials.  相似文献   

14.
A hybrid underwater glider Petrel-II has been developed and field tested. It is equipped with an active buoyancy unit and a compact propeller unit. Its working modes have been expanded to buoyancy driven gliding and propeller driven level-flight, which can make the glider work in strong currents, as well as many other complicated ocean environments. Its maximal gliding speed reaches 1 knot and the propelling speed is up to 3 knots. In this paper, a 3D dynamic model of Petrel-II is derived using linear momentum and angular momentum equations. According to the dynamic model, the spiral motion in the underwater space is simulated for the gliding mode. Similarly the cycle motion on water surface and the depth-keeping motion underwater are simulated for the level-flight mode. These simulations are important to the performance analysis and parameter optimization for the Petrel-II underwater glider.The simulation results show a good agreement with field trials.  相似文献   

15.
水下滑翔机是开展海洋无人移动观测的重要平台,其实际航行轨迹往往与预设路径存在较大差异,多台水下滑翔机协同观测时,难以始终保持预设的组网阵列。本研究提出一种基于牛顿力学积分的水下滑翔机群协同控制算法,根据水下滑翔机群出、入水的异步性调节水下滑翔机入水前的运动参数。基于对水下滑翔机受力分析,利用牛顿力学积分还原水下滑翔机在海洋中的运动状态,进而运用水下滑翔机群的协同控制算法同时约束多台水下滑翔机的运动,并开展仿真实验。实验结果证明该算法能够使多台水下滑翔机较好地保持预设组网阵列,从而可对目标海域进行协同观测。  相似文献   

16.
Yang  Ming  Liang  Yan  Wang  Yan-hui  Yang  Shao-qiong 《中国海洋工程》2022,36(5):697-706

Control parameter optimization is an efficient way to improve the endurance of underwater gliders (UGs), which influences their gliding efficiency and energy consumption. This paper analyzes the optimal matching between the net buoyancy and the pitching angle and proposes a segmented control strategy of Petrel-L. The optimization of this strategy is established based on the gliding range model of UG, which is solved based on the approximate model, and the variations of the optimal control parameters with the hotel load are obtained. The optimization results indicate that the segmented control strategy can significantly increase the gliding range when the optimal matching between the net buoyancy and the pitching angle is reached, and the increase rate is influenced by the hotel load. The gliding range of the underwater glider can be increased by 10.47% at a hotel load of 0.5 W. The optimal matching analysis adopted in this study can be applied to other UGs to realize endurance improvement.

  相似文献   

17.
曹守启  冯江伟 《海洋工程》2020,38(2):92-100
为满足对远洋环境进行长时间、大范围监测的实际需求,设计提出一种波浪动力滑翔机,该设备是一种无需携带能源即可实现自主航行的新型海洋监测平台,其主体结构由水面母船、水下牵引机和柔性缆绳三大部分组成。平台通过即时获取海洋中的波浪能、太阳能、风能作为行走的动力源,克服了传统海洋监测设备在能源供应上存在的短板。为进一步提升水下牵引机对波浪能的利用率,采用Ansys软件中的Fluent模块对水下牵引机进行水动力仿真研究,分析了侧翼板形状、侧翼板工作最大摆动角度以及侧翼板安装分布间距对滑翔机总体行走效率的影响。结果表明:NACA翼型侧翼板具有更好的水动力性能;随着最大摆动角度的增加,水下牵引机的推进效率先增大后减小,最大摆角在20°左右时,推进效果最佳;随着侧翼板分布间距的增大,水下牵引机的推进效率逐渐减小,分布间距在80 mm左右时,推进效果最佳。  相似文献   

18.
This paper describes analysis of steady motions for underwater gliders, a type of highly efficient underwater vehicle which uses gravity for propulsion. Underwater gliders are winged underwater vehicles which locomote by modulating their buoyancy and their attitude. Several underwater gliders have been developed and have proven their worth as efficient long-distance, long-duration ocean sampling platforms. Underwater gliders are so efficient because they spend much of their flight time in stable, steady motion. Wings-level gliding flight for underwater gliders has been well studied, but analysis of steady turning flight is more subtle. This paper presents an approximate analytical expression for steady turning motion for a realistic underwater glider model. The problem is formulated in terms of regular perturbation theory, with the vehicle turn rate as the perturbation parameter. The resulting solution exhibits a special structure that suggests an efficient approach to motion control as well as a planning strategy for energy efficient paths.   相似文献   

19.
水下滑翔器主体外形优化设计   总被引:2,自引:0,他引:2  
对水下滑翔器主体外形的优化设计问题进行研究.首先,在考虑内部机械结构限制的条件下,建立了主体外形优化数学模型,并采用CFX计算了若干主体形状的绕流阻力.在此基础上建立了映射主体外形的尺寸参数与绕流阻力的BP神经网络.然后将建立的神经网络作为优化设计问题的目标函数,采用坐标轮换法对滑翔器主体外形进行了优化设计,确定了尺寸参数的最优解.  相似文献   

20.
The sensitivity of the North Atlantic gyre circulation to high latitude buoyancy forcing is explored in a global, non-eddy resolving ocean general circulation model. Increased buoyancy forcing strengthens the deep western boundary current, the northern recirculation gyre, and the North Atlantic Current, which leads to a more realistic Gulf Stream path. High latitude density fluxes and surface water mass transformation are strongly dependent on the choice of sea ice and salinity restoring boundary conditions. Coupling the ocean model to a prognostic sea ice model results in much greater buoyancy loss in the Labrador Sea compared to simulations in which the ocean is forced by prescribed sea ice boundary conditions. A comparison of bulk flux forced hindcast simulations which differ only in their sea ice and salinity restoring forcings reveals the effects of a mixed thermohaline boundary condition transport feedback whereby small, positive temperature and salinity anomalies in subpolar regions are amplified when the gyre spins up as a result of increased buoyancy loss and convection. The primary buoyancy flux effects of the sea ice which cause the simulations to diverge are ice melt, which is less physical in the diagnostic sea ice model, and insulation of the ocean, which is less physical with the prognostic sea ice model. Increased salinity restoring ensures a more realistic net winter buoyancy loss in the Labrador Sea, but it is found that improvements in the Gulf Stream simulation can only be achieved with the excessive buoyancy loss associated with weak salinity restoring.  相似文献   

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