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CN117227899A - Wave glider opposite-air section viewing and passing instrument - Google Patents

Wave glider opposite-air section viewing and passing instrument Download PDF

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Publication number
CN117227899A
CN117227899A CN202311522877.2A CN202311522877A CN117227899A CN 117227899 A CN117227899 A CN 117227899A CN 202311522877 A CN202311522877 A CN 202311522877A CN 117227899 A CN117227899 A CN 117227899A
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observation
communication unit
wave glider
retractable
telescope
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CN117227899B (en
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李�灿
孙秀军
王雷
马思源
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Ocean University of China
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Ocean University of China
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Abstract

The invention discloses a wave glider aeroplane section viewing and passing instrument, which comprises an observation communication unit and a retraction unit, wherein the observation communication unit can observe surrounding environment in all directions by using an imaging element and is in communication connection with external equipment by using an antenna, the observation communication unit can ascend, and the retraction unit can change the distance between the observation communication unit and the wave glider, so that the observation communication unit can ascend and descend, the observation communication unit ascends and descends, the observation effect of the imaging element on the surrounding environment is further enhanced, meanwhile, the antenna is driven to ascend and descend, the transmission distance of electromagnetic waves caused by the reasons of earth curvature, sea surface absorption and the like is effectively prevented from being shortened, and the interconnection and the intercommunication of a plurality of wave gliders are realized in a longer distance. The wave glider opposite-to-air profile viewing and passing instrument can be lifted by the observation communication unit, and can meet the requirement of eliminating the interference of the water surface targets when the ocean surface platform of the wave glider is used for acoustic underwater target detection.

Description

一种波浪滑翔机对空剖面观通仪A wave glider air profile viewing instrument

技术领域Technical field

本发明涉及海洋观测设备及其周边配套设施技术领域,特别是涉及一种波浪滑翔机对空剖面观通仪。The invention relates to the technical field of ocean observation equipment and peripheral supporting facilities, and in particular to a wave glider air profile observation instrument.

背景技术Background technique

波浪滑翔机是一种利用波浪能实现驱动的海上无人船,其具备局部海域精细化作业的功能。因其驱动力完全取决于波浪能,而波浪能的大小随海况不同,波浪滑翔机作为全被动驱动平台,其只能以较低航速进行作业,其航行速度一般为1-3节。相比于传统燃油或电力船舶作业而言,波浪滑翔机因航速而限制了作业效率。同时波浪滑翔器为小型平台,其载荷搭载能力和供电能力相比于传统燃油或电力船舶而言,也处于劣势。但是考虑到波浪滑翔机的成本低廉,可无人作业,通常考虑一次性投放多台设备开展集群作业,来弥补效率和功能上的不足。The wave glider is an unmanned maritime vessel driven by wave energy. It has the function of precise operations in local sea areas. Because its driving force depends entirely on wave energy, and the magnitude of wave energy varies with sea conditions, the wave glider, as a fully passive drive platform, can only operate at a low speed, and its sailing speed is generally 1-3 knots. Compared with traditional fuel or electric ship operations, the operating efficiency of wave gliders is limited due to their speed. At the same time, the wave glider is a small platform, and its load carrying capacity and power supply capacity are also at a disadvantage compared to traditional fuel or electric ships. However, considering that the wave glider is low-cost and can operate unmanned, it is usually considered to launch multiple devices at one time for cluster operations to make up for the lack of efficiency and functionality.

目前,波浪滑翔机集群编队通常会使用10-20台套同时作业,两两台套之间的作用距离最大可达近100km。波浪滑翔机其船体长度通常为2m-3m,宽度0.6m-0.7m,载荷能力一般为10kg-20kg,考虑到运行稳定性,其天线架设高度一般不会超过2m。受地球曲率和海洋物理环境的影响,各台波浪滑翔机之间通过无线电台通讯的距离实测可有效通讯距离为2km左右,可通讯距离也很难大于5km。另外一种可实现的通讯方式是通过卫星端进行通讯,这样就使得距离数十公里的两台设备,需要分别同数百公里外的卫星通讯,通讯的实时性、经济性、可靠性以及通讯带宽等多方面都受到极大限制。At present, wave glider cluster formations usually use 10-20 units to operate simultaneously, and the maximum operating distance between two units can reach nearly 100km. The hull length of a wave glider is usually 2m-3m, the width is 0.6m-0.7m, and the load capacity is generally 10kg-20kg. Considering the operational stability, the antenna installation height generally does not exceed 2m. Affected by the curvature of the earth and the physical environment of the ocean, the measured effective communication distance between wave gliders through radio stations is about 2km, and the communication distance is difficult to exceed 5km. Another possible communication method is to communicate through satellites. This means that two devices tens of kilometers away need to communicate with satellites hundreds of kilometers away. The real-time, economical, reliable and Bandwidth and many other aspects are greatly restricted.

另外在波浪滑翔器机集群应用过程中,利用声学手段进行水下航行平台探测是常规应用。然而目前声学探测过程中,如何有效区分水面声源与水下声源,对小型平台而言难度较大。目前的解决方式主要有两种,一种是通过波浪滑翔机自身携带的摄像头、红外镜头等进行现场判断,但是受到地球曲率和设备功耗限制,该方式的作用距离很难超过5km,这一作用距离远远无法与声学探测距离相匹配,无法完全排除远距离的水面目标。另外一种方式是通过有人飞机或无人飞机排除水面目标存在的可能,从而判断该声源为水下目标。这类方式中有人或无人飞机耗费巨大,同时又因为没有停机空间,飞机必须要从岸边临时起飞过去,其时效性与续航能力也限制了该应用场景。In addition, in the application process of wave glider cluster, the use of acoustic means to detect underwater navigation platforms is a routine application. However, in the current acoustic detection process, how to effectively distinguish water surface sound sources and underwater sound sources is more difficult for small platforms. There are currently two main solutions. One is to conduct on-site judgment through the camera and infrared lens carried by the wave glider itself. However, due to the curvature of the earth and the power consumption of the equipment, the range of this method is difficult to exceed 5km. This function The distance is far from matching the acoustic detection range, and long-distance water targets cannot be completely ruled out. Another way is to use manned or unmanned aircraft to eliminate the possibility of water targets, thereby determining that the sound source is an underwater target. This method costs a lot of money to fly manned or unmanned aircraft. At the same time, because there is no parking space, the aircraft must take off temporarily from the shore. Its timeliness and endurance also limit this application scenario.

发明内容Contents of the invention

本发明的目的是提供一种波浪滑翔机对空剖面观通仪,以解决上述现有技术存在的问题,使观通仪能够升降调整距离以实现全方位观察,同时带动天线升降,增强装置与外部设备的通信能力,在较长距离内实现多台波浪滑翔器的互联互通。The purpose of the present invention is to provide a wave glider air profile viewing instrument to solve the problems existing in the above-mentioned prior art, so that the viewing instrument can be raised and lowered to adjust the distance to achieve all-round observation, and at the same time drive the antenna to rise and lower, and enhance the connection between the device and the external The communication capabilities of the equipment enable the interconnection of multiple wave gliders over a long distance.

为实现上述目的,本发明提供了如下方案:本发明提供一种波浪滑翔机对空剖面观通仪,包括:In order to achieve the above object, the present invention provides the following solutions: The present invention provides an air profile viewing instrument for a wave glider, which includes:

观测通讯单元,所述观测通讯单元包括摄像元件和天线,所述摄像元件能够采集周边环境信息,所述观测通讯单元能够利用所述天线与外部设备通信连接;所述观测通讯单元能够上升至空中以采集周边环境信息;Observation communication unit, the observation communication unit includes a camera element and an antenna, the camera element can collect surrounding environment information, the observation communication unit can use the antenna to communicate with external equipment; the observation communication unit can rise into the air To collect surrounding environment information;

收放单元,所述收放单元与波浪滑翔机相连,所述收放单元与所述观测通讯单元相连,所述收放单元能够改变所述观测通讯单元与所述波浪滑翔机之间的间距。A retractable and retractable unit, the retractable and retractable unit is connected to the wave glider, the retractable and retractable unit is connected to the observation and communication unit, and the retractable and retractable unit can change the distance between the observation and communication unit and the wave glider.

优选地,所述观测通讯单元还包括观通仪壳体,所述观通仪壳体的顶部具有观察窗,所述观察窗由透明材质制成,所述摄像元件包括摄像头和外设镜头,所述摄像头设置于所述观通仪壳体内并正对所述观察窗设置;所述外设镜头可滑动地与所述观通仪壳体相连,所述外设镜头能够绕所述观通仪壳体的轴线做圆周运动;所述天线与所述观通仪壳体相连。Preferably, the observation communication unit further includes a telescope housing, the top of the telescope housing has an observation window, the observation window is made of transparent material, and the imaging element includes a camera and a peripheral lens, The camera is disposed in the telescope housing and faces the observation window; the peripheral lens is slidably connected to the telescope housing, and the peripheral lens can rotate around the telescope housing. The axis of the instrument housing makes circular motion; the antenna is connected to the telescope housing.

优选地,所述观测通讯单元还包括电池包、驱动器和主轴,所述主轴可转动地设置于所述观通仪壳体内,所述驱动器的输出端与所述主轴相连,所述主轴利用传动机构与所述外设镜头相连,所述电池包与所述驱动器电连接。Preferably, the observation and communication unit further includes a battery pack, a driver and a main shaft. The main shaft is rotatably arranged in the telescope housing. The output end of the driver is connected to the main shaft. The main shaft uses a transmission. The mechanism is connected to the peripheral lens, and the battery pack is electrically connected to the driver.

优选地,所述传动机构包括主动齿轮、传动齿轮和内齿齿轮,所述主动齿轮与所述主轴相连,所述主动齿轮与所述传动齿轮相啮合,所述传动齿轮以及所述内齿齿轮可转动地设置于所述观通仪壳体内,所述传动齿轮与所述内齿齿轮相啮合,所述内齿齿轮与所述观通仪壳体同轴设置,所述外设镜头与所述内齿齿轮相连。Preferably, the transmission mechanism includes a driving gear, a transmission gear and an internal gear, the driving gear is connected to the main shaft, the driving gear meshes with the transmission gear, the transmission gear and the internal gear The transmission gear is rotatably arranged in the telescope housing, the transmission gear meshes with the internal gear, the internal gear is coaxially arranged with the telescope housing, and the external lens is in contact with the telescope housing. The internal gears are connected.

优选地,所述观测通讯单元还包括用于为所述电池包充电的随动充电线圈,所述随动充电线圈与所述电池包相连;Preferably, the observation and communication unit further includes a follow-up charging coil for charging the battery pack, and the follow-up charging coil is connected to the battery pack;

所述主轴远离所述传动机构的一端还设置有紧固元件,所述紧固元件能够固定所述主轴、所述电池包、所述随动充电线圈以及所述传动机构的位置。The end of the main shaft away from the transmission mechanism is also provided with a fastening element. The fastening element can fix the positions of the main shaft, the battery pack, the follow-up charging coil and the transmission mechanism.

优选地,所述观通仪壳体具有滑动环槽,所述外设镜头可滑动地设置于所述滑动环槽内,且所述外设镜头穿过所述滑动环槽与所述内齿齿轮相连。Preferably, the telescope housing has a sliding ring groove, the peripheral lens is slidably disposed in the sliding ring groove, and the peripheral lens passes through the sliding ring groove and the inner tooth. The gears are connected.

优选地,所述外设镜头的数量为多个,所述外设镜头绕所述观测通讯单元的轴线周向均布;Preferably, there are multiple peripheral lenses, and the peripheral lenses are evenly distributed around the axis of the observation communication unit;

所述天线的数量为多组,所述天线绕所述观测通讯单元的轴线周向均布。The number of the antennas is multiple groups, and the antennas are evenly distributed around the axis of the observation communication unit.

优选地,所述观测通讯单元的内腔中填充有上升介质,所述上升介质为氢气。Preferably, the inner cavity of the observation communication unit is filled with a rising medium, and the rising medium is hydrogen.

优选地,所述收放单元包括连接光缆和绞盘,所述连接光缆的一端与所述观测通讯单元相连,所述连接光缆的另一端与所述波浪滑翔机相连,所述绞盘设置于所述波浪滑翔机的水面船体上,所述绞盘具有滚筒,且能够使所述连接光缆缠绕在所述滚筒上。Preferably, the retracting and retracting unit includes a connecting optical cable and a winch, one end of the connecting optical cable is connected to the observation communication unit, the other end of the connecting optical cable is connected to the wave glider, and the winch is arranged on the wave glider. On the water surface hull of the glider, the winch has a drum, and the connecting optical cable can be wound around the drum.

优选地,所述收放单元还包括观通仪支架,所述观通仪支架设置于所述水面船体上,所述观通仪支架为锥筒状结构,所述绞盘设置于所述观通仪支架的内腔中,所述观测通讯单元的一端能够伸入所述观通仪支架内;Preferably, the retracting and retracting unit further includes a telescope bracket, the telescope bracket is arranged on the water surface hull, the telescope bracket is a cone-shaped structure, and the winch is arranged on the telescope In the inner cavity of the instrument bracket, one end of the observation communication unit can extend into the observation instrument bracket;

所述观通仪支架内还设置有固定充电线圈,用于为所述观测通讯单元充电。The observation instrument bracket is also provided with a fixed charging coil for charging the observation communication unit.

本发明相对于现有技术取得了以下技术效果:本发明的波浪滑翔机对空剖面观通仪,包括观测通讯单元和收放单元,其中,观测通讯单元包括摄像元件和天线,摄像元件能够采集周边环境信息,观测通讯单元能够利用天线与外部设备通信连接;观测通讯单元能够上升至空中以采集周边环境信息;观测通讯单元能够上升至空中以采集周边环境信息;收放单元与波浪滑翔机相连,收放单元与观测通讯单元相连,收放单元能够改变观测通讯单元与波浪滑翔机之间的间距。Compared with the prior art, the present invention has achieved the following technical effects: the wave glider air profile viewing instrument of the present invention includes an observation communication unit and a retracting and retracting unit, wherein the observation communication unit includes a camera element and an antenna, and the camera element can collect peripheral information Environmental information, the observation communication unit can use antennas to communicate with external devices; the observation communication unit can rise into the air to collect surrounding environment information; the observation communication unit can rise into the air to collect surrounding environment information; the retraction and release unit is connected to the wave glider, and the retraction and release unit is connected to the wave glider. The retracting and retracting unit is connected to the observation and communication unit, and the retracting and retracting unit can change the distance between the observation and communication unit and the wave glider.

本发明的波浪滑翔机对空剖面观通仪,包括观测通讯单元和收放单元,观测通讯单元利用摄像元件能够全方位观察周边环境,并利用天线与外部设备通信连接,且观测通讯单元能够上升,加之,收放单元能够改变观测通讯单元与波浪滑翔机之间的间距,使得观测通讯单元能够实现升降,观测通讯单元升降,进一步增强了摄像元件对周边环境的观察效果,同时实现带动天线升降,有效避免因地球曲率和海面吸收等原因造成的电磁波的传输距离变短,从而在较长距离内实现多台波浪滑翔器的互联互通。本发明的波浪滑翔机对空剖面观通仪,可直接由波浪滑翔机自身携带,观测通讯单元能够升降,可满足波浪滑翔机类的海洋表面平台在进行声学水下目标探测时排除水面目标干扰的需求,有效的弥补当前波浪滑翔机借助其他空基手段进行水面目标排除的不足。The wave glider air profile observation instrument of the present invention includes an observation communication unit and a retracting and retracting unit. The observation communication unit uses a camera element to observe the surrounding environment in all directions, and uses an antenna to communicate with external equipment, and the observation communication unit can rise. In addition, the retractable unit can change the distance between the observation communication unit and the wave glider, so that the observation communication unit can be raised and lowered, and the observation communication unit can be raised and lowered, which further enhances the observation effect of the camera element on the surrounding environment, and at the same time drives the antenna up and down, effectively It avoids shortening the transmission distance of electromagnetic waves caused by the curvature of the earth and sea surface absorption, thereby realizing the interconnection of multiple wave gliders over a longer distance. The wave glider air profile observation instrument of the present invention can be directly carried by the wave glider itself, and the observation communication unit can be raised and lowered, which can meet the needs of wave glider-type ocean surface platforms to eliminate surface target interference when performing acoustic underwater target detection. Effectively make up for the current shortcomings of wave gliders using other air-based means to eliminate surface targets.

附图说明Description of drawings

为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to explain the embodiments of the present invention or the technical solutions in the prior art more clearly, the drawings needed to be used in the embodiments will be briefly introduced below. Obviously, the drawings in the following description are only some of the drawings of the present invention. Embodiments, for those of ordinary skill in the art, other drawings can also be obtained based on these drawings without exerting creative efforts.

图1为本发明实施例所公开的波浪滑翔机对空剖面观通仪的结构示意图;Figure 1 is a schematic structural diagram of the wave glider air profile viewing instrument disclosed in the embodiment of the present invention;

图2为本发明实施例所公开的波浪滑翔机对空剖面观通仪的观测通讯单元的剖切示意图;Figure 2 is a schematic cross-sectional view of the observation and communication unit of the wave glider air profile viewing instrument disclosed in the embodiment of the present invention;

图3为本发明实施例所公开的波浪滑翔机对空剖面观通仪的剖切示意图;Figure 3 is a schematic cross-sectional view of the wave glider air profile viewing instrument disclosed in the embodiment of the present invention;

图4为本发明实施例所公开的波浪滑翔机对空剖面观通仪的摄像元件监控角度全覆盖的示意图;Figure 4 is a schematic diagram showing the full coverage of the monitoring angle of the imaging element of the wave glider air profile viewfinder disclosed in the embodiment of the present invention;

图5为本发明实施例所公开的波浪滑翔机对空剖面观通仪的观测通讯单元的运动示意图;Figure 5 is a schematic diagram of the movement of the observation and communication unit of the wave glider air profile viewing instrument disclosed in the embodiment of the present invention;

图6为本发明实施例所公开的波浪滑翔机对空剖面观通仪的多台设备交互示意图。Figure 6 is a schematic diagram of the interaction of multiple devices of the wave glider air profile viewing instrument disclosed in the embodiment of the present invention.

其中,100为观测通讯单元,200为收放单元,300为水面船体,400为水下牵引机,500为脐带缆;Among them, 100 is the observation and communication unit, 200 is the retractable unit, 300 is the surface hull, 400 is the underwater tractor, and 500 is the umbilical cable;

1为天线,2为观通仪壳体,3为观察窗,4为摄像头,5为外设镜头,6为电池包,7为驱动器,8为主轴,9为主动齿轮,10为传动齿轮,11为随动充电线圈,12为紧固元件,13为滑动环槽,14为连接光缆,15为绞盘,16为隔离架,17为滚筒,18为观通仪支架,19为固定充电线圈,20为内齿齿轮。1 is the antenna, 2 is the telescope casing, 3 is the observation window, 4 is the camera, 5 is the peripheral lens, 6 is the battery pack, 7 is the driver, 8 is the spindle, 9 is the driving gear, and 10 is the transmission gear. 11 is the following charging coil, 12 is the fastening element, 13 is the sliding ring groove, 14 is the connecting optical cable, 15 is the winch, 16 is the isolation frame, 17 is the roller, 18 is the viewing instrument bracket, 19 is the fixed charging coil, 20 is an internal gear.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts fall within the scope of protection of the present invention.

本发明的目的是提供一种波浪滑翔机对空剖面观通仪,以解决上述现有技术存在的问题,使观通仪能够升降调整距离以实现全方位观察,同时带动天线升降,增强装置与外部设备的通信能力,在较长距离内实现多台波浪滑翔器的互联互通。The purpose of the present invention is to provide a wave glider air profile viewing instrument to solve the problems existing in the above-mentioned prior art, so that the viewing instrument can be raised and lowered to adjust the distance to achieve all-round observation, and at the same time drive the antenna to rise and lower, and enhance the connection between the device and the external The communication capabilities of the equipment enable the interconnection of multiple wave gliders over a long distance.

为使本发明的上述目的、特征和优点能够更加明显易懂,下面结合附图和具体实施方式对本发明作进一步详细的说明。In order to make the above objects, features and advantages of the present invention more obvious and understandable, the present invention will be described in further detail below with reference to the accompanying drawings and specific embodiments.

本发明提供一种波浪滑翔机对空剖面观通仪,包括观测通讯单元100和收放单元200,其中,观测通讯单元100包括摄像元件和天线1,摄像元件能够采集周边环境信息,观测通讯单元100能够利用天线1与外部设备通信连接;观测通讯单元100能够上升至空中以采集周边环境信息;观测通讯单元100能够上升至空中以采集周边环境信息;收放单元200与波浪滑翔机相连,收放单元200与观测通讯单元100相连,收放单元200能够改变观测通讯单元100与波浪滑翔机之间的间距。The invention provides an air profile observation instrument for a wave glider, which includes an observation communication unit 100 and a retractable and retractable unit 200. The observation communication unit 100 includes a camera element and an antenna 1. The camera element can collect surrounding environment information. The observation communication unit 100 The antenna 1 can be used to communicate with external devices; the observation and communication unit 100 can rise into the air to collect surrounding environment information; the observation and communication unit 100 can rise into the air to collect surrounding environment information; the retractable and retractable unit 200 is connected to the wave glider. 200 is connected to the observation communication unit 100, and the retraction unit 200 can change the distance between the observation communication unit 100 and the wave glider.

本发明的波浪滑翔机对空剖面观通仪,包括观测通讯单元100和收放单元200,观测通讯单元100利用摄像元件能够全方位观察周边环境,并利用天线1与外部设备通信连接,且观测通讯单元100能够上升,加之,收放单元200能够改变观测通讯单元100与波浪滑翔机之间的间距,使得观测通讯单元100能够实现升降,观测通讯单元100升降,进一步增强了摄像元件对周边环境的观察效果,同时实现带动天线1升降,有效避免因地球曲率和海面吸收等原因造成的电磁波的传输距离变短,从而在较长距离内实现多台波浪滑翔器的互联互通。本发明的波浪滑翔机对空剖面观通仪,可直接由波浪滑翔机自身携带,观测通讯单元100能够升降,可满足波浪滑翔机类的海洋表面平台在进行声学水下目标探测时排除水面目标干扰的需求,有效的弥补当前波浪滑翔机借助其他空基手段进行水面目标排除的不足。The wave glider air profile observation instrument of the present invention includes an observation communication unit 100 and a retractable and retractable unit 200. The observation communication unit 100 uses a camera element to observe the surrounding environment in all directions, and uses the antenna 1 to communicate with external equipment, and the observation communication unit The unit 100 can rise. In addition, the retractable unit 200 can change the distance between the observation communication unit 100 and the wave glider, so that the observation communication unit 100 can be raised and lowered. The observation communication unit 100 can be raised and lowered, further enhancing the observation of the surrounding environment by the camera element. The effect is to drive the antenna 1 up and down at the same time, effectively avoiding the shortening of the transmission distance of electromagnetic waves caused by the curvature of the earth and sea surface absorption, thereby realizing the interconnection of multiple wave gliders over a long distance. The wave glider air profile observation instrument of the present invention can be directly carried by the wave glider itself, and the observation communication unit 100 can be raised and lowered, which can meet the needs of wave glider-like ocean surface platforms to eliminate surface target interference when performing acoustic underwater target detection. , effectively making up for the current shortcomings of wave gliders using other air-based means to eliminate surface targets.

具体地,观测通讯单元100还包括观通仪壳体2,观通仪壳体2的顶部具有观察窗3,观察窗3由透明材质制成,摄像元件包括摄像头4和外设镜头5,摄像头4设置于观通仪壳体2内并正对观察窗3设置,在确保摄像头4能够进行观察的同时,利用观察窗3保护摄像头4;外设镜头5可滑动地与观通仪壳体2相连,外设镜头5能够绕观通仪壳体2的轴线做圆周运动,观通仪壳体2的轴线平行于竖直方向,外设镜头5与摄像头4相配合,从而全方位观察周边水面环境和船只信息;天线1与观通仪壳体2相连。Specifically, the observation communication unit 100 also includes a telescope housing 2. The top of the telescope housing 2 has an observation window 3. The observation window 3 is made of transparent material. The imaging element includes a camera 4 and a peripheral lens 5. The camera 4 is installed in the telescope housing 2 and facing the observation window 3. While ensuring that the camera 4 can observe, the observation window 3 is used to protect the camera 4; the peripheral lens 5 is slidably connected to the telescope housing 2. Connected, the peripheral lens 5 can make circular motion around the axis of the telescope housing 2. The axis of the telescope housing 2 is parallel to the vertical direction. The peripheral lens 5 cooperates with the camera 4 to observe the surrounding water surface in an all-round way. Environmental and ship information; the antenna 1 is connected to the telescope housing 2.

其中,观测通讯单元100还包括电池包6、驱动器7和主轴8,主轴8可转动地设置于观通仪壳体2内,驱动器7的输出端与主轴8相连,主轴8利用传动机构与外设镜头5相连,电池包6与驱动器7电连接,驱动器7利用主轴8带动外设镜头5转动,实现全方位观测,电池包6为驱动器7提供了电力来源。在本发明的其他具体实施方式中,还可以将外设镜头5设置为可调结构,以调整外设镜头5的俯仰角度,以进一步摄像元件对周边环境的观察效果。在实际应用中,摄像元件可内置电源,或将摄像元件与电池包6相连,使电池包6作为电力来源。此处还需要解释说明的是,在实际应用中,观测通讯单元100设置控制元件,摄像元件、天线1、驱动器7、电池包6等均与控制元件相连,提高观测通讯单元100的可控程度,方便观测通讯单元100与外部设备的通讯连接,设置控制元件以及控制器等属于本领域技术人员的惯用手段,因此此处不再赘述。Among them, the observation communication unit 100 also includes a battery pack 6, a driver 7 and a main shaft 8. The main shaft 8 is rotatably arranged in the observation instrument housing 2. The output end of the driver 7 is connected to the main shaft 8. The main shaft 8 uses a transmission mechanism to communicate with the outside. Assume that the lens 5 is connected, and the battery pack 6 is electrically connected to the driver 7. The driver 7 uses the spindle 8 to drive the peripheral lens 5 to rotate to achieve all-round observation. The battery pack 6 provides a power source for the driver 7. In other specific embodiments of the present invention, the peripheral lens 5 can also be provided with an adjustable structure to adjust the pitch angle of the peripheral lens 5 to further improve the observation effect of the imaging element on the surrounding environment. In practical applications, the imaging element can have a built-in power supply, or the imaging element can be connected to the battery pack 6 so that the battery pack 6 serves as the power source. What needs to be explained here is that in actual applications, the observation communication unit 100 is provided with control components, and the camera component, antenna 1, driver 7, battery pack 6, etc. are all connected to the control components to improve the controllability of the observation communication unit 100. , to facilitate the communication connection between the observation communication unit 100 and external devices, and setting control components and controllers are common methods for those skilled in the art, so they will not be described again here.

在本具体实施方式中,传动机构包括主动齿轮9、传动齿轮10和内齿齿轮20,主动齿轮9与主轴8相连,主动齿轮9与传动齿轮10相啮合,传动齿轮10以及内齿齿轮20可转动地设置于观通仪壳体2内,传动齿轮10与内齿齿轮20相啮合,内齿齿轮20与观通仪壳体2同轴设置,外设镜头5与内齿齿轮20相连,传动机构采用齿轮传动方式,结构紧凑占用空间小,传动稳定可靠,提高了外设镜头5的运动可靠性。在本发明的其他具体实施方式中,传动机构还可以采用其他传动结构,例如带传动、链条传动等方式。In this specific embodiment, the transmission mechanism includes a driving gear 9, a transmission gear 10 and an internal gear 20. The driving gear 9 is connected to the main shaft 8, and the driving gear 9 meshes with the transmission gear 10. The transmission gear 10 and the internal gear 20 can The transmission gear 10 is in mesh with the internal gear 20. The internal gear 20 is coaxially arranged with the telescope housing 2. The peripheral lens 5 is connected to the internal gear 20. The mechanism adopts gear transmission, which has a compact structure and takes up little space. The transmission is stable and reliable, which improves the movement reliability of the peripheral lens 5. In other specific embodiments of the present invention, the transmission mechanism may also adopt other transmission structures, such as belt transmission, chain transmission, etc.

需要说明的是,观测通讯单元100还包括用于为电池包6充电的随动充电线圈11,随动充电线圈11与电池包6相连,以保证观测通讯单元100的续航能力。It should be noted that the observation communication unit 100 also includes a follow-up charging coil 11 for charging the battery pack 6. The follow-up charging coil 11 is connected to the battery pack 6 to ensure the endurance of the observation communication unit 100.

另外,主轴8远离传动机构的一端还设置有紧固元件12,紧固元件12能够固定主轴8、电池包6、随动充电线圈11以及传动机构的位置,避免零部件错位滑动,保证观测通讯单元100的结构强度和稳定性。In addition, the end of the main shaft 8 away from the transmission mechanism is also provided with a fastening element 12. The fastening element 12 can fix the positions of the main shaft 8, the battery pack 6, the follower charging coil 11 and the transmission mechanism to prevent parts from dislocating and sliding, and ensures observation and communication. Structural strength and stability of unit 100.

为了进一步提高外设镜头5的转动稳定性,观通仪壳体2具有滑动环槽13,外设镜头5可滑动地设置于滑动环槽13内,滑动环槽13为外设镜头5转动提供了导向,保证了外设镜头5的运动精确度,且外设镜头5穿过滑动环槽13与内齿齿轮20相连,在实际应用中,可在滑动环槽13处设置密封元件,避免外部杂质进入观通仪壳体2内。In order to further improve the rotational stability of the peripheral lens 5, the telescope housing 2 has a sliding ring groove 13. The peripheral lens 5 is slidably disposed in the sliding ring groove 13. The sliding ring groove 13 provides a space for the rotation of the peripheral lens 5. The guidance is ensured to ensure the movement accuracy of the peripheral lens 5, and the peripheral lens 5 passes through the sliding ring groove 13 and is connected to the internal gear 20. In practical applications, sealing elements can be set at the sliding ring groove 13 to avoid external Impurities enter the housing 2 of the telescope.

在本具体实施方式中,外设镜头5的数量为多个,外设镜头5绕观测通讯单元100的轴线周向均布,进一步增强全方位观察效果。In this specific implementation, the number of peripheral lenses 5 is multiple, and the peripheral lenses 5 are evenly distributed around the axis of the observation communication unit 100 to further enhance the all-round observation effect.

相应地,天线1的数量也设置为多组,天线1绕观测通讯单元100的轴线周向均布向各个方向发射或接收电磁波。在本具体实施方式中,外设镜头5和天线1均设置四组,在实际应用中,还可以根据观测通讯单元100的规格以及观测需要调整外设镜头5和天线1的数量以及分布,以满足不同的工况,提高观测通讯单元100的灵活适应性。Correspondingly, the number of antennas 1 is also set to multiple groups, and the antennas 1 are evenly distributed around the axis of the observation communication unit 100 to transmit or receive electromagnetic waves in all directions. In this specific implementation, four groups of peripheral lenses 5 and antennas 1 are provided. In practical applications, the number and distribution of peripheral lenses 5 and antennas 1 can also be adjusted according to the specifications of the observation communication unit 100 and observation needs. Meet different working conditions and improve the flexibility and adaptability of the observation communication unit 100.

更具体地,观测通讯单元100的内腔中填充有上升介质,上升介质为氢气,使得观测通讯单元100自身具备向上升的能力,加之与收放单元200相配合实现升降。在本发明的其他具体实施方式中,观测通讯单元100可单独设置螺旋桨等机构使其能够上升,还可以采用其他较空气密度小的上升介质。另外,还需要说明的是,观测通讯单元100的内腔可设置单独的、用于容纳上升介质的仓体,或直接将上升介质填充于观通仪壳体2内,使上升介质充满观通仪壳体2内零部件的空隙间,需注意避免上升介质影响损坏零部件,另外,可在滑动环槽13周边设置密封环或密封垫片,避免介质由滑动环槽13处泄漏。More specifically, the inner cavity of the observation and communication unit 100 is filled with a rising medium, and the rising medium is hydrogen, so that the observation and communication unit 100 itself has the ability to rise, and cooperates with the retractable unit 200 to achieve lifting. In other specific embodiments of the present invention, the observation and communication unit 100 can be separately provided with a propeller or other mechanism to enable it to rise, and other rising media with a lower density than air can also be used. In addition, it should be noted that the inner cavity of the observation communication unit 100 can be provided with a separate warehouse for accommodating the ascending medium, or the ascending medium can be directly filled into the observation instrument housing 2 so that the ascending medium is filled with the observation instrument. In the gaps between the components in the instrument housing 2, care must be taken to prevent the rising medium from damaging the components. In addition, a sealing ring or sealing gasket can be set around the sliding ring groove 13 to prevent the medium from leaking from the sliding ring groove 13.

在本具体实施方式中,观测通讯单元100的轴线截面为T形,观测通讯单元100的顶部为圆盘状结构。In this specific embodiment, the axial cross-section of the observation and communication unit 100 is T-shaped, and the top of the observation and communication unit 100 is a disk-shaped structure.

更具体地,波浪滑翔机包括水面船体300和水下牵引机400,水面船体300利用脐带缆500与水下牵引机400相连。收放单元200包括连接光缆14和绞盘15,连接光缆14的一端与观测通讯单元100相连,连接光缆14的另一端与波浪滑翔机相连,从而实现观测通讯单元100将采集信息传递至波浪滑翔机,绞盘15利用隔离架16设置于波浪滑翔机的水面船体300上,绞盘15具有滚筒17,且能够使连接光缆14缠绕在滚筒17上,绞盘15利用滚筒17收卷连接光缆14时,使观测通讯单元100下降,当绞盘15放松连接光缆14时,观测通讯单元100在自身上升力作用下升高。More specifically, the wave glider includes a surface hull 300 and an underwater tractor 400 . The surface hull 300 is connected to the underwater tractor 400 using an umbilical cable 500 . The retracting and retracting unit 200 includes a connecting optical cable 14 and a winch 15. One end of the connecting optical cable 14 is connected to the observation communication unit 100, and the other end of the connecting optical cable 14 is connected to the wave glider, so that the observation communication unit 100 transmits the collected information to the wave glider, and the winch 15 is installed on the water surface hull 300 of the wave glider using an isolation frame 16. The capstan 15 has a drum 17 and can wind the connecting optical cable 14 around the drum 17. When the capstan 15 uses the drum 17 to wind up the connecting optical cable 14, the observation communication unit 100 Descending, when the winch 15 loosens the connection optical cable 14, the observation communication unit 100 rises under the action of its own lifting force.

在观测通讯单元100不工作时,收放单元200控制观测通讯单元100下降,为了支撑观测通讯单元100,收放单元200还包括观通仪支架18,观通仪支架18设置于水面船体300上,观通仪支架18为锥筒状结构,绞盘15设置于观通仪支架18的内腔中,观测通讯单元100的一端能够伸入观通仪支架18内,当观测通讯单元100不工作时,收放单元200控制观测通讯单元100下降,直至其下端伸入观通仪支架18内,对观测通讯单元100提供稳定支撑。When the observation and communication unit 100 is not working, the retractable and retractable unit 200 controls the observation and communication unit 100 to descend. In order to support the observation and communication unit 100, the retractable and retractable unit 200 also includes a telescope bracket 18. The telescope bracket 18 is arranged on the water surface hull 300. , the telescope bracket 18 is a cone-shaped structure, the winch 15 is set in the inner cavity of the telescope bracket 18, one end of the observation communication unit 100 can extend into the telescope bracket 18, when the observation communication unit 100 is not working , the retraction unit 200 controls the observation and communication unit 100 to descend until its lower end extends into the observation instrument bracket 18 to provide stable support for the observation and communication unit 100 .

另外,观通仪支架18内还设置有固定充电线圈19,用于为观测通讯单元100充电,当观测通讯单元100下降伸入观通仪支架18内时,浮动充电线圈伸入固定充电线圈19内,二者相配合为观测通讯单元100充电,为后续工作做准备。In addition, a fixed charging coil 19 is also provided in the telescope bracket 18 for charging the observation communication unit 100. When the observation communication unit 100 is lowered and extended into the telescope bracket 18, the floating charging coil extends into the fixed charging coil 19. Within, the two cooperate to charge the observation communication unit 100 and prepare for subsequent work.

本发明的波浪滑翔机对空剖面观通仪,观测通讯单元100像风筝一样,通过连接光缆14与波浪滑翔机相连,并利用收放单元200控制连接光缆14的收放卷绕,实现对观测通讯单元100升降的控制。常规数据采集模式下,观测通讯单元100不工作,降落在收放单元200的观通仪支架18的孔内;观测模式下,观测通讯单元100会在自身升力作用下起飞,可对周围同构波浪滑翔器进行数据通信,详见图6,也可进行海洋水面安全观测,监视水面目标异常。波浪滑翔器作为观通仪的运行载体。In the wave glider air profile observation instrument of the present invention, the observation communication unit 100 is connected to the wave glider through the connecting optical cable 14 like a kite, and the retracting and unwinding unit 200 is used to control the retracting and unwinding of the connecting optical cable 14 to realize the observation and communication unit 100 lift control. In the regular data collection mode, the observation communication unit 100 does not work and lands in the hole of the telescope bracket 18 of the retractable unit 200; in the observation mode, the observation communication unit 100 takes off under the action of its own lift and can isomorphically monitor the surroundings. The wave glider performs data communication, as shown in Figure 6 for details. It can also conduct safety observations on the ocean surface and monitor abnormalities in water surface targets. The wave glider serves as the operating carrier of the telescope.

本发明中应用了具体个例对本发明的原理及实施方式进行了阐述,以上实施例的说明只是用于帮助理解本发明的方法及其核心思想;同时,对于本领域的一般技术人员,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。综上所述,本说明书内容不应理解为对本发明的限制。Specific examples are used in the present invention to illustrate the principles and implementation methods of the present invention. The description of the above embodiments is only used to help understand the method of the present invention and its core idea; at the same time, for those of ordinary skill in the art, based on this The idea of the invention will be subject to change in the specific implementation and scope of application. In summary, the contents of this description should not be construed as limitations of the present invention.

Claims (10)

1.一种波浪滑翔机对空剖面观通仪,其特征在于,包括:1. A wave glider air profile viewing instrument, which is characterized in that it includes: 观测通讯单元,所述观测通讯单元包括摄像元件和天线,所述摄像元件能够采集周边环境信息,所述观测通讯单元能够利用所述天线与外部设备通信连接;所述观测通讯单元能够上升至空中以采集周边环境信息;Observation communication unit, the observation communication unit includes a camera element and an antenna, the camera element can collect surrounding environment information, the observation communication unit can use the antenna to communicate with external equipment; the observation communication unit can rise into the air To collect surrounding environment information; 收放单元,所述收放单元与波浪滑翔机相连,所述收放单元与所述观测通讯单元相连,所述收放单元能够改变所述观测通讯单元与所述波浪滑翔机之间的间距。A retractable and retractable unit, the retractable and retractable unit is connected to the wave glider, the retractable and retractable unit is connected to the observation and communication unit, and the retractable and retractable unit can change the distance between the observation and communication unit and the wave glider. 2.根据权利要求1所述的波浪滑翔机对空剖面观通仪,其特征在于:所述观测通讯单元还包括观通仪壳体,所述观通仪壳体的顶部具有观察窗,所述观察窗由透明材质制成,所述摄像元件包括摄像头和外设镜头,所述摄像头设置于所述观通仪壳体内并正对所述观察窗设置;所述外设镜头可滑动地与所述观通仪壳体相连,所述外设镜头能够绕所述观通仪壳体的轴线做圆周运动;所述天线与所述观通仪壳体相连。2. The wave glider air profile observation instrument according to claim 1, characterized in that: the observation communication unit further includes an observation instrument housing, and the top of the observation instrument housing has an observation window, and the The observation window is made of transparent material. The imaging element includes a camera and an external lens. The camera is installed in the housing of the viewing instrument and facing the observation window. The external lens is slidably connected to the observation window. The telescope housing is connected, the peripheral lens can make circular motion around the axis of the telescope housing, and the antenna is connected to the telescope housing. 3.根据权利要求2所述的波浪滑翔机对空剖面观通仪,其特征在于:所述观测通讯单元还包括电池包、驱动器和主轴,所述主轴可转动地设置于所述观通仪壳体内,所述驱动器的输出端与所述主轴相连,所述主轴利用传动机构与所述外设镜头相连,所述电池包与所述驱动器电连接。3. The wave glider air profile observation instrument according to claim 2, characterized in that: the observation communication unit further includes a battery pack, a driver and a main shaft, and the main shaft is rotatably arranged on the observation instrument housing. In the body, the output end of the driver is connected to the main shaft, the main shaft is connected to the peripheral lens through a transmission mechanism, and the battery pack is electrically connected to the driver. 4.根据权利要求3所述的波浪滑翔机对空剖面观通仪,其特征在于:所述传动机构包括主动齿轮、传动齿轮和内齿齿轮,所述主动齿轮与所述主轴相连,所述主动齿轮与所述传动齿轮相啮合,所述传动齿轮以及所述内齿齿轮可转动地设置于所述观通仪壳体内,所述传动齿轮与所述内齿齿轮相啮合,所述内齿齿轮与所述观通仪壳体同轴设置,所述外设镜头与所述内齿齿轮相连。4. The wave glider air profile viewing instrument according to claim 3, characterized in that: the transmission mechanism includes a driving gear, a transmission gear and an internal gear, the driving gear is connected to the main shaft, and the driving gear is connected to the main shaft. The gear meshes with the transmission gear. The transmission gear and the internal gear are rotatably arranged in the casing of the telescope. The transmission gear meshes with the internal gear. The internal gear Arranged coaxially with the telescope housing, the external lens is connected to the internal gear. 5.根据权利要求4所述的波浪滑翔机对空剖面观通仪,其特征在于:所述观测通讯单元还包括用于为所述电池包充电的随动充电线圈,所述随动充电线圈与所述电池包相连;5. The wave glider air profile observation instrument according to claim 4, characterized in that: the observation communication unit further includes a follow-up charging coil for charging the battery pack, and the follow-up charging coil is connected to The battery packs are connected; 所述主轴远离所述传动机构的一端还设置有紧固元件,所述紧固元件能够固定所述主轴、所述电池包、所述随动充电线圈以及所述传动机构的位置。The end of the main shaft away from the transmission mechanism is also provided with a fastening element. The fastening element can fix the positions of the main shaft, the battery pack, the follow-up charging coil and the transmission mechanism. 6.根据权利要求4所述的波浪滑翔机对空剖面观通仪,其特征在于:所述观通仪壳体具有滑动环槽,所述外设镜头可滑动地设置于所述滑动环槽内,且所述外设镜头穿过所述滑动环槽与所述内齿齿轮相连。6. The wave glider air profile viewing device according to claim 4, characterized in that: the viewing device housing has a sliding ring groove, and the peripheral lens is slidably disposed in the sliding ring groove. , and the peripheral lens passes through the sliding ring groove and is connected to the internal gear. 7.根据权利要求2所述的波浪滑翔机对空剖面观通仪,其特征在于:所述外设镜头的数量为多个,所述外设镜头绕所述观测通讯单元的轴线周向均布;7. The wave glider air profile observation instrument according to claim 2, characterized in that: there are multiple peripheral lenses, and the peripheral lenses are evenly distributed circumferentially around the axis of the observation communication unit; 所述天线的数量为多组,所述天线绕所述观测通讯单元的轴线周向均布。The number of the antennas is multiple groups, and the antennas are evenly distributed around the axis of the observation communication unit. 8.根据权利要求1-7任一项所述的波浪滑翔机对空剖面观通仪,其特征在于:所述观测通讯单元的内腔中填充有上升介质,所述上升介质为氢气。8. The wave glider air profile observation instrument according to any one of claims 1 to 7, characterized in that: the inner cavity of the observation communication unit is filled with an ascending medium, and the ascending medium is hydrogen. 9.根据权利要求1-7任一项所述的波浪滑翔机对空剖面观通仪,其特征在于:所述收放单元包括连接光缆和绞盘,所述连接光缆的一端与所述观测通讯单元相连,所述连接光缆的另一端与所述波浪滑翔机相连,所述绞盘设置于所述波浪滑翔机的水面船体上,所述绞盘具有滚筒,且能够使所述连接光缆缠绕在所述滚筒上。9. The wave glider air profile observation instrument according to any one of claims 1 to 7, characterized in that: the retracting and retracting unit includes a connecting optical cable and a winch, and one end of the connecting optical cable is connected to the observation communication unit The other end of the connecting optical cable is connected to the wave glider. The winch is arranged on the water surface hull of the wave glider. The winch has a drum and can make the connecting optical cable wind around the drum. 10.根据权利要求9所述的波浪滑翔机对空剖面观通仪,其特征在于:所述收放单元还包括观通仪支架,所述观通仪支架设置于所述水面船体上,所述观通仪支架为锥筒状结构,所述绞盘设置于所述观通仪支架的内腔中,所述观测通讯单元的一端能够伸入所述观通仪支架内;10. The wave glider air profile sighting instrument according to claim 9, characterized in that: the retractable unit further includes a sighting instrument bracket, and the sighting instrument bracket is arranged on the water surface hull, and the The telescope bracket has a cone-shaped structure, the winch is arranged in the inner cavity of the telescope bracket, and one end of the observation communication unit can extend into the telescope bracket; 所述观通仪支架内还设置有固定充电线圈,用于为所述观测通讯单元充电。The observation instrument bracket is also provided with a fixed charging coil for charging the observation communication unit.
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