CN111762306A - A hybrid drive underwater glider with ring wings - Google Patents
A hybrid drive underwater glider with ring wings Download PDFInfo
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Abstract
Description
技术领域technical field
本发明属于水下滑翔机领域,具体的说是一种携带环型机翼的混合驱动水下滑翔机。The invention belongs to the field of underwater gliders, in particular to a hybrid-driven underwater glider carrying a ring-shaped wing.
背景技术Background technique
水下滑翔机平台技术作为搭载海洋物理信息传感器的重要工具得到了快速的发展,其续 航能力强、航程远、隐蔽性强的特点使得其非常适合海洋生、化、物等参数的测量工作,是 最常用的水下移动观测平台之一,而单独依靠螺旋桨推进的水下滑翔器的续航能力较为有限, 集合浮力调节系统和螺旋桨驱动的混合驱动水下滑翔机应运而生。As an important tool for carrying marine physical information sensors, underwater glider platform technology has developed rapidly. Its strong endurance, long range and strong concealment make it very suitable for the measurement of marine biological, chemical, physical and other parameters. One of the most commonly used underwater mobile observation platforms, and the underwater glider propelled solely by propellers has limited endurance. The hybrid-driven underwater glider that integrates the buoyancy adjustment system and the propeller drive emerges as the times require.
当前国内外海洋探测领域,长航程高机动性能的潜器一直是重要发展方向之一。目前国 际上提出的Tethys航行器已具有1800公里观测能力、2节航速推进能力,日后将有大范围 应用前景。目前小型航行器均存在机动能力较差,抗流能力弱等问题。寻找一种提高水下滑 翔器稳定性和机动能力的设计具有重要意义。近年来,国内一些科研单位已经开展小型水下 滑翔器运动能力改进的相关研发工作,但相关产品存在稳定性不足等问题。例如2018年公开 的“一种基于串列翼驱动的混合动力型水下滑翔机”专利号为201811045537.8混合驱动水下 滑翔机。该发明包括耐压壳体和信号装置,所述壳体内设有浮力调节装置、横滚姿态调节装置、 俯仰姿态调节装置和控制装置等。与现有技术比较,该发明所述的串列翼混合驱动滑翔机,相 较于传统水下滑翔机的机翼,不会产生额外的阻力,噪声也相对较小,但是采用这种串联翼结 构的滑翔机与传统水下滑翔机区别较小,仍较难改善水下滑翔机水下直航推进能力及运动稳 定性。At present, in the field of ocean exploration at home and abroad, submersibles with long range and high maneuverability have always been one of the important development directions. At present, the Tethys aircraft proposed internationally has an observation capability of 1,800 kilometers and a propulsion capability at a speed of 2 knots, and will have a wide range of application prospects in the future. At present, small aircraft all have problems such as poor maneuverability and weak anti-current capability. It is of great significance to find a design that can improve the stability and maneuverability of underwater gliders. In recent years, some domestic research institutes have carried out research and development work related to the improvement of the movement capability of small underwater gliders, but the related products have problems such as insufficient stability. For example, the patent number of "A Hybrid Underwater Glider Based on Tandem Wing Drive" published in 2018 is 201811045537.8 Hybrid Drive Underwater Glider. The invention includes a pressure-resistant casing and a signal device, and the casing is provided with a buoyancy adjustment device, a roll attitude adjustment device, a pitch attitude adjustment device, a control device, and the like. Compared with the prior art, the tandem-wing hybrid drive glider described in this invention does not generate additional resistance and has relatively low noise compared with the wings of traditional underwater gliders, but the tandem-wing structure is used. The difference between the glider and the traditional underwater glider is small, and it is still difficult to improve the underwater direct flight propulsion capability and motion stability of the underwater glider.
发明内容SUMMARY OF THE INVENTION
本发明的目的是为了克服现有技术中的不足,设计一款具有改善混合驱动水下滑翔机直 航推进能力及运动稳定性的机翼结构。本发明提供一种环型机翼组合结构,可使水下滑翔器 的螺旋桨推进效率提高,并一定程度提高水下滑翔机抗流能力。The purpose of the present invention is to overcome the deficiencies in the prior art, and to design a wing structure that can improve the direct flight propulsion capability and motion stability of the hybrid-driven underwater glider. The invention provides a ring-shaped wing assembly structure, which can improve the propeller propulsion efficiency of the underwater glider and improve the current resistance capability of the underwater glider to a certain extent.
本发明的目的是通过以下技术方案实现的:The purpose of this invention is to realize through the following technical solutions:
一种携带环翼的混合驱动水下滑翔机,包括依次连接的艏部总成、舯部总成、艉部总成 和环型机翼单元;艏部总成包括传感器固定连接架、应急抛载模块、前端盖、艏部导流罩; 舯部总成包括第一中舱耐压壳体、第二中舱耐压壳体、俯仰姿态调节模块、中舱连接肋环、 机载能源模块;艉部总成包括后舱耐压壳体、浮力调节系统、后端盖、推进电机模块、艉部 导流罩、尾舵调节模块、集成天线和螺旋桨;环型机翼单元位于艉部总成外侧,固连在艉部 总成上;A hybrid drive underwater glider carrying a ring wing, comprising a bow assembly, a midship assembly, a stern assembly and a ring wing unit connected in sequence; the bow assembly includes a sensor fixing connection frame, an emergency load dumping module, front end cover, bow shroud; midship assembly includes first middle cabin pressure casing, second middle cabin pressure casing, pitching attitude adjustment module, middle cabin connecting rib ring, and airborne energy module; The stern assembly includes the pressure housing of the rear cabin, the buoyancy adjustment system, the rear end cover, the propulsion motor module, the stern fairing, the rudder adjustment module, the integrated antenna and the propeller; the annular wing unit is located in the stern assembly Outside, fixed on the stern assembly;
所述艏部导流罩和前端盖分别设置于艏部总成的前端和尾端,传感器固定连接架和应急 抛载模块安装于艏部总成内;The bow shroud and the front end cover are respectively arranged at the front end and the rear end of the bow assembly, and the sensor fixing connection frame and the emergency load dumping module are installed in the bow assembly;
舯部总成的前后两端都设有中舱支撑肋环,所述第一中舱耐压壳体和第二中舱耐压壳体 之间通过中舱连接肋环连接,俯仰姿态调节模块和机载能源模块设置于舯部总成内部,机载 能源模块为水下滑翔机提供能源;俯仰姿态调节模块用于调节水下滑翔机重心浮心相对位置, 实现俯仰姿态调节;The front and rear ends of the midship assembly are provided with middle cabin support rib rings, the first middle cabin pressure shell and the second middle cabin pressure shell are connected by the middle cabin connecting rib rings, and the pitch attitude adjustment module The airborne energy module and the airborne energy module are arranged inside the midship assembly, and the airborne energy module provides energy for the underwater glider; the pitch attitude adjustment module is used to adjust the relative position of the gravity center of the underwater glider to realize the pitch attitude adjustment;
所述集成天线与后端盖固连;所述的后导流罩上安装所述尾舵调节模块,用于调整混合 驱动水下滑翔机的水平航向;所述推进电机模块安装在艉部导流罩内,并通过固定连接架与 艉部导流罩固连,用于混合驱动的水下滑翔机水下直航工作;所述的浮力调节系统通过液压 系统实现航行体浮力变化,实现水下滑翔机的上浮和下潜;所述的推进电机模块通过电机驱 动螺旋桨,为水下滑翔机提供前进前进;水下滑翔机能够通过俯仰姿态调节模块和浮力调节 系统实现水下滑翔机在工作深度下的定深巡航;环型机翼单元固连在艉部导流罩上,环型机 翼单元包括螺旋桨和环形机翼。The integrated antenna is fixedly connected with the rear end cover; the tail rudder adjustment module is installed on the rear shroud to adjust the horizontal heading of the hybrid-driven underwater glider; the propulsion motor module is installed on the stern part of the guide The buoyancy adjustment system realizes the buoyancy change of the sailing body through the hydraulic system, and realizes the underwater glider. The said propulsion motor module drives the propeller through the motor to provide the underwater glider forward and forward; the underwater glider can realize the fixed-depth cruise of the underwater glider at the working depth through the pitch attitude adjustment module and the buoyancy adjustment system The annular wing unit is fixed on the stern shroud, and the annular wing unit includes a propeller and an annular wing.
进一步的,所述推进电机模块关闭后,水下滑翔机能够进行水下滑翔机似剖面航行作业。Further, after the propulsion motor module is turned off, the underwater glider can perform the underwater glider-like profile navigation operation.
进一步的,该混合驱动水下滑翔机通过位于内部拉紧杆内部拉紧,保证艏部总成、舯部 总成、艉部总成稳定密封连接。Further, the hybrid-driven underwater glider is tensioned inside the internal tension rod to ensure stable and sealed connection of the bow assembly, the midship assembly, and the stern assembly.
进一步的,所述的尾舵调节模块由尾舵、连接轴、舵机、舵机固定架和补偿器组成;所 述的尾舵调节模块通过调整两个垂直的舵面的旋转角度实现水下滑翔机的航向控制;所述的 集成天线用于水下滑翔机与地面的通讯,环型机翼单元通过螺栓固定在艉部总成的后端盖上; 并分别与集成天线的头部和尾舵调节模块的底部胶接,环型机翼位于螺旋桨外侧。Further, the tail rudder adjustment module is composed of a tail rudder, a connecting shaft, a steering gear, a steering gear fixing frame and a compensator; the tail rudder adjustment module realizes underwater by adjusting the rotation angle of the two vertical rudder surfaces. The heading control of the glider; the integrated antenna is used for the communication between the underwater glider and the ground, and the ring-shaped wing unit is fixed on the rear end cover of the stern assembly by bolts; and the head and tail rudder of the integrated antenna are respectively connected The bottom of the adjustment module is glued and the annular wing is on the outside of the propeller.
与现有技术相比,本发明的技术方案所带来的有益效果是:Compared with the prior art, the beneficial effects brought by the technical solution of the present invention are:
取消传统水下滑翔机平板机翼设计,本发明采用独特的环形机翼设计。通过流体力学仿 真优化,将环形机翼和螺旋桨有机结合,在兼顾水下滑翔机运动稳定性的基础上,提高了推 进系统的工作能力。环形机翼迎流面采用有一定弧度的导流线型,减小机翼的局部受力不均 情况。环形机翼安装位置与传统平板机翼安装位置不同,接近水下滑翔机尾部,便于导流至 螺旋桨。环形机翼与螺旋桨位置布局遵照导管螺旋桨设计原则,保证相对流体力学特性,提 升螺旋桨的推进效率。较大的翼面积(与水下滑翔机平板形机翼相比较)和对称布局结构形 式可一定程度提高航行器运动稳定性,并有效提高水下滑翔机的抗干扰能力,降低海流等外 界因素对海洋探测设备观测的影响。The traditional underwater glider flat wing design is cancelled, and the present invention adopts a unique annular wing design. Through the optimization of fluid mechanics simulation, the annular wing and the propeller are organically combined, and the working ability of the propulsion system is improved on the basis of taking into account the movement stability of the underwater glider. The upstream surface of the annular wing adopts a deflector with a certain radian to reduce the uneven local force of the wing. The installation position of the annular wing is different from that of the traditional flat wing, and it is close to the tail of the underwater glider, which is convenient for diversion to the propeller. The positional layout of the annular wing and the propeller follows the design principles of the ducted propeller to ensure the relative hydrodynamic characteristics and improve the propulsion efficiency of the propeller. The larger wing area (compared with the flat-shaped wing of the underwater glider) and the symmetrical layout structure can improve the motion stability of the aircraft to a certain extent, and effectively improve the anti-interference ability of the underwater glider, and reduce the impact of external factors such as ocean currents on the ocean. Detecting the effects of equipment observations.
附图说明Description of drawings
图1为本发明的混合驱动水下滑翔机总体结构示意图。FIG. 1 is a schematic diagram of the overall structure of the hybrid-driven underwater glider of the present invention.
图2为本发明的艏部总成1/4剖视结构示意图。FIG. 2 is a 1/4 sectional structural schematic diagram of the bow assembly of the present invention.
图3为本发明的舯部总成1/4剖视结构示意图。FIG. 3 is a schematic diagram of a 1/4 cross-sectional structure of the midship assembly of the present invention.
图4为本发明的艉部总成1/4剖视结构示意图。Fig. 4 is a 1/4 cross-sectional structural schematic diagram of the stern assembly of the present invention.
图5为本发明的环型翼结构示意图。FIG. 5 is a schematic diagram of the structure of the annular wing of the present invention.
附图标记:1-艏部总成,2-舯部总成,3-艉部总成,4-环型机翼单元,5-艏部导流罩,6- 应急抛载模块,7-传感器固定连接架,8-前端盖,9-中舱耐压壳体,10-中舱连接肋环,11-中 舱耐压壳体,12-机载能源模块;13-俯仰姿态调节模块;14-中舱支撑肋环,15-后舱耐压壳体, 16-浮力调节系统,17-后端盖,18-推进电机模块,19-艉部导流罩,20-集成天线,21-螺旋桨, 22-环型机翼,23-尾舵调节模块。Reference numerals: 1- Bow assembly, 2- Midship assembly, 3- Stern assembly, 4- Ring wing unit, 5- Bow shroud, 6- Emergency dump module, 7- Sensor fixing connection frame, 8- front cover, 9- middle cabin pressure shell, 10- middle cabin connecting rib ring, 11- middle cabin pressure shell, 12- airborne energy module; 13- pitch attitude adjustment module; 14- middle tank support rib ring, 15- rear tank pressure shell, 16- buoyancy adjustment system, 17- rear end cover, 18- propulsion motor module, 19- stern fairing, 20- integrated antenna, 21- Propeller, 22-ring wing, 23-rudder adjustment module.
具体实施方式Detailed ways
以下结合附图和具体实施例对本发明作进一步详细说明。应当理解,此处所描述的具体 实施例仅仅用以解释本发明,并不用于限定本发明。The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.
如图1至图5所示,本发明提供一种携带环翼的混合驱动水下滑翔机,包括依次连接的 艏部总成1、舯部总成2、艉部总成3和环型机翼单元4;艏部总成1包括传感器固定连接架 7、应急抛载模块6、前端盖8、艏部导流罩5;舯部总成2包括中舱耐压壳体9、中舱耐压壳体11、俯仰姿态调节模块13、中舱连接肋环10、机载能源模块12;艉部总成3包括后舱耐 压壳体15、浮力调节系统16、后端盖17、推进电机模块18、艉部导流罩19、尾舵调节模块 23、集成天线20和螺旋桨21;环型机翼单元4位于艉部总成3外侧,固连在艉部总成3上; 包括螺旋桨21和环形机翼22。利用集成天线20上部与尾舵调节模块23下部与环型机翼22 相连,使环型机翼22与螺旋桨21组成类似导管螺旋桨结构,提高螺旋桨周围流场特性,从 而提高螺旋桨推进效率。As shown in FIGS. 1 to 5 , the present invention provides a hybrid drive underwater glider carrying a ring wing, comprising a bow assembly 1, a midship assembly 2, a
艏部总成的艏部导流罩5通过螺栓与前端盖8固定连接,连接方式为通过环向均布的螺 栓固定连接;前端盖通过与传感器固定连接架7的螺栓连接实现各种传感器单元搭载;其中 各传感器单元通过螺栓固定在传感器固定连接架上,以便水下滑翔器在水下航行时进行水中 通信、探测、目标定位、跟踪等。The
舯部总成中机载能源模块给水下滑翔器提供能源;俯仰姿态调节模块利用电机驱动电池 包在导轨上前后移动,实现水下滑翔器的俯仰姿态调节。舯部总成2通过中间拉紧杆将中舱 耐压壳体9拉紧;The airborne energy module in the midship assembly provides energy for the underwater glider; the pitch attitude adjustment module uses the motor to drive the battery pack to move back and forth on the guide rail to realize the pitch attitude adjustment of the underwater glider. The midship assembly 2 tightens the pressure-resistant shell 9 of the middle cabin through the middle tension rod;
艉部总成的集成天线通过螺栓与后端盖固连在一起;艉部导流罩安装有尾舵调节模块, 用于调整混合驱动水下滑翔机的航向;推进电机模块安装在艉部总成的艉部,用于混合驱动 水下滑翔机水下直航;浮力调节系统能够调节水下滑翔机的浮力大小,可实现水下滑翔机的 上浮和下潜,并能够实现水下滑翔机的水下浮力调节;推进电机模块,通过电机驱动螺旋桨, 开启时可实现水下滑翔机水下直航;推进器在关闭时,水下滑翔机可进行类似于水下滑翔机 式的剖面航行作业。The integrated antenna of the stern assembly is fixedly connected to the rear end cover by bolts; the stern shroud is equipped with a rudder adjustment module, which is used to adjust the heading of the hybrid-driven underwater glider; the propulsion motor module is installed in the stern assembly The stern of the hybrid drive underwater glider is used for direct underwater navigation; the buoyancy adjustment system can adjust the buoyancy of the underwater glider, realize the floating and diving of the underwater glider, and realize the underwater buoyancy adjustment of the underwater glider. ; Propulsion motor module, the propeller is driven by the motor, and the underwater glider can sail directly underwater when it is turned on; when the propeller is turned off, the underwater glider can perform profile sailing operations similar to the underwater glider.
本实施例中环形机翼是一种通过CFD计算模拟得到的环型状机翼,这种环型结构区别与 传统机翼,设计形状参数需考虑集成天线、螺旋桨、尾舵调节模块等影响。它与艉部导流罩 通过螺栓固连,并与集成天线头部、尾舵调节模块底部胶接,保证整体结构稳定性。它的形 状类似一个短粗的空心圆筒,上下圆弧部分在混合驱动滑翔机滑翔过程中产生升力,并提供方 向稳定性。环型机翼位于螺旋桨外侧,其内外部弧形设计结构可改善螺旋桨周围流场,一定 程度上改善螺旋桨性能。本设计环形型翼与后方螺旋桨组合结构类似于传统导管螺旋桨结构, 可使螺旋桨盘面处水流加速,使螺旋桨在较大速度场下工作,从而可以提高螺旋桨的效率。In this embodiment, the ring-shaped wing is a ring-shaped wing obtained by CFD calculation and simulation. This ring-shaped structure is different from the traditional wing, and the design shape parameters need to consider the effects of integrated antennas, propellers, and rudder adjustment modules. It is fixedly connected with the stern shroud by bolts, and is glued with the integrated antenna head and the bottom of the rudder adjustment module to ensure the overall structural stability. Its shape is similar to a stubby hollow cylinder, and its upper and lower arcs generate lift and provide directional stability during the gliding process of the hybrid-drive glider. The annular wing is located outside the propeller, and its inner and outer arc design structure can improve the flow field around the propeller and improve the propeller performance to a certain extent. The combined structure of the annular wing and the rear propeller designed in this design is similar to the structure of the traditional ducted propeller, which can accelerate the water flow at the propeller disc surface and make the propeller work in a larger speed field, thereby improving the efficiency of the propeller.
本发明并不限于上文描述的实施方式。以上对具体实施方式的描述旨在描述和说明本发 明的技术方案,上述的具体实施方式仅仅是示意性的,并不是限制性的。在不脱离本发明宗 旨和权利要求所保护的范围情况下,本领域的普通技术人员在本发明的启示下还可做出很多 形式的具体变换,这些均属于本发明的保护范围之内。The present invention is not limited to the embodiments described above. The above description of the specific embodiments is intended to describe and illustrate the technical solutions of the present invention, and the above-mentioned specific embodiments are only illustrative and not restrictive. Without departing from the scope of the present invention and the scope of protection of the claims, those of ordinary skill in the art can also make specific transformations in many forms under the inspiration of the present invention, and these all belong within the protection scope of the present invention.
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