CN108545162A - Underwater spectroradiometer based on water jet driving - Google Patents
Underwater spectroradiometer based on water jet driving Download PDFInfo
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63C—LAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
- B63C11/00—Equipment for dwelling or working underwater; Means for searching for underwater objects
- B63C11/52—Tools specially adapted for working underwater, not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
- B63G8/14—Control of attitude or depth
- B63G8/16—Control of attitude or depth by direct use of propellers or jets
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Abstract
本发明属于机器人领域,具体涉及一种基于水射流驱动的水下滑翔机器人,包括机身壳、左水平翼、右水平翼、上垂直翼以及下垂直翼;机身壳前端为中央带有吸嘴的球面,中部为圆柱面,后部为自前向后半径减小的圆锥面,尾端为球面;左水平翼、右水平翼分别沿纵向水平设置于机身壳中部的左、右两侧;上垂直翼、下垂直翼分别沿纵向竖直安装于机身壳后部上、下两侧;左水平翼以及右右水平翼后端分别自内向外设置有驱动喷嘴以及转向喷嘴;上垂直翼以及下垂直翼的后端分别设置有俯仰喷嘴。本发明设计科学,结构简单,控制简易,机动性能好,使用可靠,能耗效率高,可广泛应用于水下探测、运载等领域的优点。
The invention belongs to the field of robots, and specifically relates to an underwater gliding robot driven by water jets, comprising a fuselage shell, a left horizontal wing, a right horizontal wing, an upper vertical wing and a lower vertical wing; The spherical surface of the mouth, the middle part is a cylindrical surface, the rear part is a conical surface whose radius decreases from front to rear, and the tail end is a spherical surface; the left horizontal wing and the right horizontal wing are respectively arranged longitudinally and horizontally on the left and right sides of the middle part of the fuselage shell ; The upper vertical wing and the lower vertical wing are vertically installed on the upper and lower sides of the rear part of the fuselage respectively; The rear ends of the wing and the lower vertical wing are respectively provided with pitch nozzles. The invention has the advantages of scientific design, simple structure, simple control, good maneuverability, reliable use, high energy consumption efficiency, and can be widely used in the fields of underwater detection and carrying.
Description
技术领域technical field
本发明属于机器人领域,具体涉及一种基于水射流驱动的水下滑翔机器人。The invention belongs to the field of robots, and in particular relates to an underwater gliding robot driven by water jets.
背景技术Background technique
水下滑翔机器人是一种依靠净浮力和水动力驱动的新型水下航行器,它具有水下作业时间长,续航距离远,机动性能耗,作业费用低,对母船依赖性低等优点,近年来被广泛应用于海洋的探测和观测领域。The underwater gliding robot is a new type of underwater vehicle driven by net buoyancy and hydrodynamic force. It has the advantages of long underwater operation time, long cruising distance, mobility, energy consumption, low operating cost, and low dependence on the mother ship. It has been widely used in the field of ocean detection and observation.
目前,水下滑翔机器人的驱动一般采用螺旋桨驱动,这种驱动方式动力配置数量多,重量大,能耗高,每个动力装置均需要高强度的动态密封,且易于受到水下生物干扰。At present, the drive of underwater gliding robots is generally driven by propellers. This driving method has a large number of power configurations, heavy weight, and high energy consumption. Each power device requires a high-strength dynamic seal and is easily disturbed by underwater organisms.
发明内容Contents of the invention
本发明的目的在于克服现有技术中的缺陷,提供一种基于水射流驱动的水下滑翔机器人。The purpose of the present invention is to overcome the defects in the prior art and provide an underwater gliding robot driven by water jets.
本发明为实现上述目的,采用以下技术方案:In order to achieve the above object, the present invention adopts the following technical solutions:
一种基于水射流驱动的水下滑翔机器人,包括机身壳、左水平翼、右水平翼、上垂直翼以及下垂直翼;所述的机身壳前端为中央带有吸嘴的球面,中部为圆柱面,后部为自前向后半径减小的圆锥面,尾端为球面;所述的左水平翼、右水平翼分别沿纵向水平设置于所述的机身壳中部的左、右两侧;所述的上垂直翼、下垂直翼分别沿纵向竖直安装于所述的机身壳后部上、下两侧;所述的左水平翼以及右右水平翼后端分别自内向外设置有驱动喷嘴以及转向喷嘴;所述的上垂直翼以及下垂直翼的后端分别设置有俯仰喷嘴。An underwater gliding robot driven by water jets, comprising a fuselage shell, a left horizontal wing, a right horizontal wing, an upper vertical wing, and a lower vertical wing; the front end of the fuselage shell is a spherical surface with a suction nozzle in the center, and the middle part It is a cylindrical surface, the rear part is a conical surface whose radius decreases from front to rear, and the tail end is a spherical surface; the left horizontal wing and the right horizontal wing are respectively horizontally arranged on the left and right sides of the middle part of the fuselage shell along the longitudinal direction. side; the upper vertical wing and the lower vertical wing are respectively vertically installed on the upper and lower sides of the rear part of the fuselage; There are driving nozzles and turning nozzles; the rear ends of the upper vertical wing and the lower vertical wing are respectively provided with pitching nozzles.
所述的驱动喷嘴、转向喷嘴以及所述的俯仰喷嘴的喷射方向均沿所述的机身壳轴线方向并向机身壳内侧偏斜。The jetting directions of the driving nozzle, the turning nozzle and the pitching nozzle are all along the axial direction of the fuselage shell and inclined towards the inside of the fuselage shell.
所述的左水平翼、右水平翼、上垂直翼以及下垂直翼均为菱形。Described left horizontal wing, right horizontal wing, upper vertical wing and lower vertical wing are rhombus.
所述吸嘴与设置在所述的机身壳内的水泵连接;所述的水泵分别与滑翔驱比例换向阀、左右转向比例换向阀、以及俯仰转向比例换向阀连接;所述的滑翔驱比例换向阀分别通过单向阀与设置在所述的左水平翼以及所述的右水平翼上的驱动喷嘴连接;所述的左右转向比例换向阀分别通过单向阀与设置在所述的左水平翼以及所述的右水平翼上的转向喷嘴连接;所述的俯仰转向比例换向阀分别通过单向阀与设置在所述的上垂直翼以及所述的下垂直翼上的俯仰喷嘴连接。The suction nozzle is connected with the water pump arranged in the fuselage shell; the water pump is respectively connected with the gliding drive proportional reversing valve, the left and right steering proportional reversing valve, and the pitch steering proportional reversing valve; The gliding drive proportional reversing valves are respectively connected to the driving nozzles arranged on the left horizontal wing and the right horizontal wing through check valves; The steering nozzles on the left horizontal wing and the right horizontal wing are connected; the pitch steering proportional reversing valve is respectively arranged on the upper vertical wing and the lower vertical wing through a one-way valve The pitch nozzle connection.
机身壳、左水平翼、右水平翼、上垂直翼、以及下垂直翼为整体密封壳体;水下滑翔机器人整体重量大于其潜水浮力,且其重心与浮心重合。The fuselage shell, left horizontal wing, right horizontal wing, upper vertical wing, and lower vertical wing are integrally sealed shells; the overall weight of the underwater gliding robot is greater than its diving buoyancy, and its center of gravity coincides with the center of buoyancy.
与现有技术相比,本发明的有益效果是:Compared with prior art, the beneficial effect of the present invention is:
本发明采用水射流作为滑翔机器人的驱动及转向,能耗低,控制简单;外壳为整体密封装置,动力的喷嘴及吸嘴均为静态密封,密封性能好,密封成本低;驱动部分没有螺旋桨及可转动的舵面,整机作业过程中,壳体外围所有部件保持相对静止状态,水域生物环境对其作业影响小。本发明设计科学,结构简单,控制简易,机动性能好,使用可靠,能耗效率高,可广泛应用于水下探测、运载等领域的优点。The present invention uses water jet as the drive and steering of the gliding robot, which has low energy consumption and simple control; the casing is an integral sealing device, and the power nozzle and suction nozzle are all statically sealed, with good sealing performance and low sealing cost; the driving part has no propeller and With the rotatable rudder surface, during the operation of the whole machine, all the peripheral parts of the shell remain relatively static, and the biological environment in the water area has little impact on its operation. The invention has the advantages of scientific design, simple structure, simple control, good maneuverability, reliable use, high energy consumption efficiency, and can be widely used in the fields of underwater detection and carrying.
附图说明Description of drawings
图1是基于水射流驱动的水下滑翔机器人示意图。Figure 1 is a schematic diagram of an underwater gliding robot driven by water jets.
图2是基于水射流驱动的水下滑翔机器水射流驱动系统示意图。Fig. 2 is a schematic diagram of the water jet drive system of the underwater gliding machine based on the water jet drive.
图中,1、机身壳;2、左水平翼;3、右水平翼;4、上垂直翼;5、下垂直翼;6、吸嘴;7、滑翔驱动喷嘴;8、右转向喷嘴;9、左转向喷嘴;10、下俯喷嘴;11、上仰喷嘴;12~17、单向阀;18、左右转向比例换向阀;19、滑翔驱动比例换向阀;20、俯仰转向比例换向阀;21水泵。In the figure, 1. fuselage shell; 2. left horizontal wing; 3. right horizontal wing; 4. upper vertical wing; 5. lower vertical wing; 6. suction nozzle; 7. gliding drive nozzle; 8. right steering nozzle; 9. Left steering nozzle; 10. Downward nozzle; 11. Upward nozzle; 12~17. One-way valve; 18. Left and right steering proportional reversing valve; 19. Gliding drive proportional reversing valve; 20. Pitching steering proportional reversing valve Directional valve; 21 water pumps.
具体实施方式Detailed ways
为了使本技术领域的技术人员更好地理解本发明的技术方案,下面结合附图和最佳实施例对本发明作进一步的详细说明。In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and preferred embodiments.
图1示出一种基于水射流驱动的水下滑翔机器人,包括机身壳1、左水平翼2、右水平翼3、上垂直翼4以及下垂直翼5;所述的机身壳前端为中央带有吸嘴6的球面,中部为圆柱面,后部为自前向后半径减小的圆锥面,尾端为球面;所述的左水平翼、右水平翼分别沿纵向水平设置于所述的机身壳中部的左、右两侧;所述的上垂直翼、下垂直翼分别沿纵向竖直安装于所述的机身壳后部上、下两侧;所述的左水平翼以及右右水平翼后端分别自内向外设置有驱动喷嘴7以及转向喷嘴;其中左水平翼对应右转向喷嘴8,其中右水平翼对应左转向喷嘴9;所述的上垂直翼以及下垂直翼的后端分别设置有俯仰喷嘴,其中,上垂直翼对应下俯喷嘴10,下垂直翼对应上仰喷嘴11。Fig. 1 shows a kind of underwater gliding robot driven by water jet, comprising a fuselage shell 1, a left horizontal wing 2, a right horizontal wing 3, an upper vertical wing 4 and a lower vertical wing 5; the front end of the fuselage shell is A spherical surface with a suction nozzle 6 in the center, a cylindrical surface in the middle, a conical surface with a decreasing radius from the front to the rear at the rear, and a spherical surface at the tail end; the left horizontal wing and the right horizontal wing are respectively horizontally arranged on the The left and right sides of the middle part of the fuselage shell; the upper vertical wing and the lower vertical wing are respectively vertically installed on the upper and lower sides of the rear part of the fuselage shell; the left horizontal wing and The rear ends of the right and right horizontal wings are respectively provided with driving nozzles 7 and steering nozzles from inside to outside; wherein the left horizontal wing corresponds to the right turning nozzle 8, and wherein the right horizontal wing corresponds to the left turning nozzle 9; the upper vertical wing and the lower vertical wing The rear ends are respectively provided with pitching nozzles, wherein the upper vertical wing corresponds to the downward pitching nozzle 10 , and the lower vertical wing corresponds to the upward pitching nozzle 11 .
所述的驱动喷嘴、转向喷嘴以及所述的俯仰喷嘴的喷射方向均沿所述的机身壳轴线方向并向机身壳内侧偏斜。所述的左水平翼、右水平翼、上垂直翼以及下垂直翼均为菱形。The jetting directions of the driving nozzle, the turning nozzle and the pitching nozzle are all along the axial direction of the fuselage shell and inclined towards the inside of the fuselage shell. Described left horizontal wing, right horizontal wing, upper vertical wing and lower vertical wing are rhombus.
所述吸嘴与设置在所述的机身壳内的水泵21连接;所述的水泵分别与滑翔驱比例换向阀19、左右转向比例换向阀18、以及俯仰转向比例换向阀20连接;所述的滑翔驱比例换向阀分别通过单向阀与设置在所述的左水平翼以及所述的右水平翼上的驱动喷嘴7连接;所述的左右转向比例换向阀分别通过单向阀与设置在所述的左水平翼的右转向喷嘴8以及设置在所述的右水平翼的左转向喷嘴9连接;所述的俯仰转向比例换向阀分别通过单向阀与设置在所述的上垂直翼的下俯喷嘴10以及所述的下垂直翼上的上仰喷嘴11连接。所述的机身壳、左水平翼、右水平翼、上垂直翼、以及下垂直翼为整体密封壳体;水下滑翔机器人整体重量大于其潜水浮力,且其重心与浮心重合。The suction nozzle is connected with the water pump 21 arranged in the fuselage shell; the water pump is respectively connected with the gliding drive proportional reversing valve 19, the left and right steering proportional reversing valve 18, and the pitch steering proportional reversing valve 20 The gliding drive proportional reversing valve is connected with the drive nozzle 7 arranged on the left horizontal wing and the right horizontal wing through a check valve respectively; The direction valve is connected with the right turning nozzle 8 arranged on the left horizontal wing and the left turning nozzle 9 arranged on the right horizontal wing; The downward-pitching nozzle 10 of the above-mentioned upper vertical wing and the upward-pitching nozzle 11 on the described lower vertical wing are connected. The fuselage shell, the left horizontal wing, the right horizontal wing, the upper vertical wing, and the lower vertical wing are an integral sealed shell; the overall weight of the underwater gliding robot is greater than its diving buoyancy, and its center of gravity coincides with the center of buoyancy.
在左水平翼、右水平翼后端安装驱动喷嘴7、右转向喷嘴8、左转向喷嘴9及相应的单向阀14、15、12、13;在上垂直翼、下垂直翼后端安装下俯喷嘴10、上仰喷嘴11及相应的单向阀16、17,并在各个喷嘴单向阀接口接入预留管路。在机身壳内装入水泵21、左右转向比例换向阀18、滑翔驱动比例换向阀19及俯仰转向比例换向阀20。按图2连接吸嘴6与水泵21进水口、连接水泵21出水口与左右转向比例换向阀18、滑翔驱动比例换向阀19及俯仰转向比例换向阀20的管路;将单向阀14、15上的预留管路连接至滑翔驱动比例换向阀19,将单向阀12、13上的预留管路连接至左右转向比例换向阀18,将单向阀16、17上的预留管路连接至俯仰转向比例换向阀20。在机身壳上安装左水平翼、右水平翼和上垂直翼、下垂直翼,并对水下滑翔机器人重量配平,使其重量稍大于其潜水浮力,重心与浮心位置重合,并对其整体外壳密封。Install driving nozzle 7, right turning nozzle 8, left turning nozzle 9 and corresponding one-way valves 14, 15, 12, 13 at the rear end of left horizontal wing and right horizontal wing; The downward nozzle 10, the upward nozzle 11 and the corresponding one-way valves 16, 17, and the reserved pipelines are connected to the one-way valve interfaces of each nozzle. Water pump 21, left and right steering proportional reversing valve 18, gliding drive proportional reversing valve 19 and pitch steering proportional reversing valve 20 are packed into the fuselage shell. According to Fig. 2, connect the suction nozzle 6 and the water inlet of the water pump 21, connect the water outlet of the water pump 21 and the left and right steering proportional reversing valve 18, the gliding drive proportional reversing valve 19 and the pipeline of the pitch steering proportional reversing valve 20; The reserved pipelines on 14 and 15 are connected to the gliding drive proportional reversing valve 19, the reserved pipelines on the check valves 12 and 13 are connected to the left and right steering proportional reversing valve 18, and the upper and lower check valves 16 and 17 are The reserved pipeline is connected to the pitch steering proportional reversing valve 20. Install the left horizontal wing, right horizontal wing, upper vertical wing, and lower vertical wing on the fuselage shell, and balance the weight of the underwater gliding robot so that its weight is slightly greater than its diving buoyancy, and the center of gravity coincides with the position of the center of buoyancy. The overall housing is sealed.
使用时,将水下滑翔机入水,开启滑翔驱动比例换向阀19,即电磁铁3DT通电,左、右驱动喷嘴7喷水,水下滑翔机器人向前滑翔;开启左右转向比例换向阀18右转,即电磁铁1DT通电,右转向喷嘴8喷水,实现滑翔机右转;开启左右转向比例换向阀18左转,即电磁铁2DT通电,左转向喷嘴9喷水,实现滑翔机右转;开启俯仰转向比例换向阀20下俯,即电磁铁4DT通电,下俯转向喷嘴10喷水,实现滑翔机下俯转向;开启俯仰转向比例换向阀20上仰,即电磁铁5DT通电,上仰转向喷嘴11喷水,实现滑翔机上仰转向。通过各个电磁铁电压大小,可实现相应喷嘴喷水流量的大小,从而调节滑翔及转向的快慢。During use, put the underwater glider into the water, open the gliding drive proportional reversing valve 19, that is, the electromagnet 3DT is energized, the left and right drive nozzles 7 spray water, and the underwater gliding robot glides forward; open the left and right steering proportional reversing valve 18 Turn, that is, the electromagnet 1DT is energized, the right steering nozzle 8 sprays water, and the glider turns right; the left and right steering proportional reversing valve 18 is opened to turn left, that is, the electromagnet 2DT is energized, and the left steering nozzle 9 sprays water, and the glider turns right; open The pitch steering proportional reversing valve 20 is pitched down, that is, the electromagnet 4DT is energized, and the pitching steering nozzle 10 sprays water to realize the downward steering of the glider; the pitch steering proportional reversing valve 20 is turned on, that is, the electromagnet 5DT is energized, and the pitching steering is realized. Nozzle 11 sprays water, realizes that glider turns upwards. Through the magnitude of the voltage of each electromagnet, the magnitude of the water spray flow of the corresponding nozzle can be realized, thereby adjusting the speed of gliding and turning.
以上内容仅为本发明的较佳实施例,对于本领域的普通技术人员,依据本发明的思想,在具体实施方式及应用范围上均会有改变之处,本说明书内容不应理解为对本发明的限制。The above content is only a preferred embodiment of the present invention. For those of ordinary skill in the art, according to the idea of the present invention, there will be changes in the specific implementation and application scope. limits.
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CN111572704A (en) * | 2020-06-23 | 2020-08-25 | 西北工业大学 | An open-loop active flow control device for underwater glider based on steady jet |
CN111674534A (en) * | 2020-06-23 | 2020-09-18 | 西北工业大学 | A closed-loop active flow control device for underwater glider based on steady blowing and suction flow |
CN111688892A (en) * | 2020-06-23 | 2020-09-22 | 西北工业大学 | Active flow control system for wing body fusion underwater glider |
CN116039887A (en) * | 2023-03-01 | 2023-05-02 | 西北工业大学 | Underwater vehicle fin rudder optimizing device based on steady active flow control |
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