CN201345408Y - Antenna lifting device - Google Patents
Antenna lifting device Download PDFInfo
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- CN201345408Y CN201345408Y CNU2008202160664U CN200820216066U CN201345408Y CN 201345408 Y CN201345408 Y CN 201345408Y CN U2008202160664 U CNU2008202160664 U CN U2008202160664U CN 200820216066 U CN200820216066 U CN 200820216066U CN 201345408 Y CN201345408 Y CN 201345408Y
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Abstract
本实用新型公开了一种天线升降装置,包括天线托盘以及用于支撑天线托盘的支撑杆,还包括一个可以将天线托盘升起降下的升降机构。所述升降机构包括升降丝杆、在天线托盘上设置的与所述升降丝杆配合的丝杆螺母以及驱动升降丝杆运动的驱动装置。本实用新型所述天线升降装置,可使较大功率雷达天线方便的被推出舱外工作,并可在高低温、最大8级风、雨天等环境条件下工作。本系统集成化程度高、承载重量大、系统线缆连接已在舱内完备,方便系统展开工作。
The utility model discloses an antenna lifting device, which comprises an antenna tray and a support rod for supporting the antenna tray, and also includes a lifting mechanism capable of raising and lowering the antenna tray. The lifting mechanism includes a lifting screw, a screw nut that is arranged on the antenna tray and cooperates with the lifting screw, and a driving device that drives the lifting screw to move. The antenna lifting device described in the utility model can make the relatively high-power radar antenna conveniently pushed out of the cabin to work, and can work under high and low temperature, maximum 8-level wind, rainy weather and other environmental conditions. The system has a high degree of integration, a large carrying capacity, and the system cable connection has been completed in the cabin, which is convenient for the system to work.
Description
技术领域 technical field
本实用新型涉及一种天线升降装置,特别是一种通讯指挥车方舱内安装的天线升降装置。The utility model relates to an antenna lifting device, in particular to an antenna lifting device installed in a shelter of a communication command vehicle.
背景技术 Background technique
无论是军用战场指挥还是民用抢险救灾等场景均瞬息万变,故对指挥系统快速反应能力提出了更高的要求,所以指挥系统要有高度的集成性和高度的机动性,而对于通讯指挥车之类的快速通讯设备而言,需要加载通讯天线。Whether it is military battlefield command or civilian emergency rescue and disaster relief, the scenes are changing rapidly, so higher requirements are put forward for the command system's rapid response capability, so the command system must be highly integrated and highly mobile. For communication command vehicles and the like For fast communication equipment, it is necessary to load a communication antenna.
现许多使用较大型雷达天线的机动指挥系统在做装车设计方案时,通常为雷达天线单独配备载车或拖车,或者在较长的载车平台上预留空间使方舱与天线并装。以上装车方案使得系统的运输能力不高,并且在搭建系统时线缆连接、调试时要花费较多时间,降低了系统的快速反应能力。Many mobile command systems that use larger radar antennas are usually equipped with vehicles or trailers for radar antennas separately when designing vehicles, or reserve space on a long vehicle platform to install shelters and antennas together. The above loading scheme makes the transportation capacity of the system not high, and it takes a lot of time to connect cables and debug when building the system, which reduces the rapid response capability of the system.
实用新型内容Utility model content
发明目的:实用新型所要解决的技术问题是针对现有技术的不足,提供了一种天线升降装置。Purpose of the invention: The technical problem to be solved by the utility model is to provide an antenna lifting device for the deficiencies of the prior art.
技术方案:本实用新型公开了一种天线升降装置,包括天线托盘以及用于支撑天线托盘的支撑杆,还包括一个可以将天线托盘升起降下的升降机构。Technical solution: The utility model discloses an antenna lifting device, which includes an antenna tray and a support rod for supporting the antenna tray, and also includes a lifting mechanism that can lift and lower the antenna tray.
本实用新型中,所述升降机构包括升降丝杆、在天线托盘上设置的与所述升降丝杆配合的丝杆螺母以及驱动升降丝杆运动的驱动装置。In the utility model, the lifting mechanism includes a lifting screw, a screw nut arranged on the antenna tray to cooperate with the lifting screw, and a driving device for driving the lifting screw to move.
本实用新型中,所述升降丝杆为四个,呈正方形设置,分别通过同步的驱动装置驱动。In the utility model, there are four lifting screw rods, which are arranged in a square shape and are respectively driven by synchronous driving devices.
本实用新型中,优选地,所述升降丝杆为四个,呈正方形设置,升降丝杆之间通过三个扭力连杆传动,升降丝杆与扭力连杆之间设有联轴节;其中一个升降丝杆通过驱动装置驱动。由此可以只用一个动力较大的驱动装置实现驱动,且升降更加平稳。In the utility model, preferably, there are four lifting screw rods, which are arranged in a square shape, and the lifting screw rods are driven by three torsion connecting rods, and a coupling is provided between the lifting screw rods and the torsion connecting rods; A lifting screw is driven by a drive unit. Therefore, only one driving device with higher power can be used to realize the driving, and the lifting is more stable.
本实用新型中,所述驱动装置包括驱动电机和伞齿轮箱;伞齿轮箱与升降丝杆下部啮合,驱动电机通过伞齿轮箱带动升降丝杆运动。In the utility model, the driving device includes a driving motor and a bevel gear box; the bevel gear box meshes with the lower part of the lifting screw rod, and the driving motor drives the lifting screw rod to move through the bevel gear box.
本实用新型中,优选地,所述驱动电机和伞齿轮箱之间设有力矩限制器。电机输出轴通过力矩限制器与传动链连接,通过设定力矩限制的最大传递扭矩来确保在升降机构出现卡滞等故障时电机打滑,达到由于机械过载而保护传动链和其它设备安全的目的。系统中设定力矩限制器的最大传递扭矩约为20Nm。In the present utility model, preferably, a torque limiter is provided between the drive motor and the bevel gearbox. The output shaft of the motor is connected to the transmission chain through a torque limiter, and the maximum transmission torque of the torque limit is set to ensure that the motor slips when the lifting mechanism is stuck or other faults, so as to protect the safety of the transmission chain and other equipment due to mechanical overload. The maximum transmission torque of the set torque limiter in the system is about 20Nm.
本实用新型中,所述天线升降装置还包括中间为开口的顶盖以及同于封闭所述开口玻璃钢罩。In the present utility model, the antenna lifting device further includes a top cover with an opening in the middle and a glass fiber reinforced plastic cover for closing the opening.
本实用新型中,所述支撑杆上段设有定位孔,在定位孔内设有定位销。通过定位孔与定位销配合将天线托盘与支撑杆紧固定位。In the utility model, the upper section of the support rod is provided with a positioning hole, and a positioning pin is provided in the positioning hole. Fasten and position the antenna tray and the support rod through the positioning hole and the positioning pin.
本实用新型中,所述扭力连杆与丝杆之间通过传动盒内的蜗轮蜗杆副传动。其中蜗轮通过键与丝杆连接同步转动。蜗轮蜗杆传动的结构特点确保具有结构自锁性能,实现升降装置在任意升降高度自锁。In the utility model, the torsion connecting rod and the lead screw are driven through the worm gear in the transmission box. Wherein the worm wheel rotates synchronously through the connection of the key and the screw rod. The structural characteristics of the worm gear drive ensure the structural self-locking performance, and realize the self-locking of the lifting device at any lifting height.
有益效果:本实用新型所述天线升降装置,可使较大功率雷达天线方便的被推出舱外工作,并可在高低温、最大8级风、雨天等环境条件下工作。本系统集成化程度高、承载重量大、系统线缆连接已在舱内完备,方便系统展开工作。Beneficial effects: the antenna lifting device described in the utility model can make the relatively high-power radar antenna be pushed out of the cabin to work conveniently, and can work under high and low temperature, maximum 8 winds, rainy days and other environmental conditions. The system has a high degree of integration, a large carrying capacity, and the system cable connection has been completed in the cabin, which is convenient for the system to work.
附图说明 Description of drawings
下面结合附图和具体实施方式对本实用新型做更进一步的具体说明。Below in conjunction with accompanying drawing and specific embodiment, the utility model is described in further detail.
图1为本实用新型所述天线升降装置结构示意图。Fig. 1 is a schematic structural diagram of the antenna lifting device described in the present invention.
图2为本实用新型所述天线升降装置优选实施例的结构示意图。Fig. 2 is a schematic structural diagram of a preferred embodiment of the antenna lifting device of the present invention.
图3为本实用新型所述天线升降装置应用示意图。Fig. 3 is a schematic diagram of the application of the antenna lifting device described in the present invention.
具体实施方式 Detailed ways
如图1和图2所示,本实用新型公开了一种天线升降装置,包括天线托盘1以及用于支撑天线托盘1的支撑杆2,其特征在于,还包括一个可以将天线托盘1升起降下的升降机构。所述升降机构包括升降丝杆3、在天线托盘1上设置的与所述升降丝杆配合的丝杆螺母4以及驱动升降丝杆3运动的驱动装置。所述升降丝杆3为四个,呈正方形设置,升降丝杆3之间通过三个扭力连杆5传动,升降丝杆3与扭力连杆5之间设有联轴节6;其中一个升降丝杆3通过驱动装置驱动。所述驱动装置包括驱动电机7和伞齿轮箱8;伞齿轮箱8与升降丝杆3下部啮合,驱动电机7通过伞齿轮箱8带动升降丝杆3运动。所述驱动电机7和伞齿轮箱8之间设有力矩限制器9。所述天线升降装置还包括中间为开口的顶盖10以及同于封闭所述开口玻璃钢罩11。所述支撑杆2上段设有定位孔12,在定位孔12内设有定位销13。所述扭力连杆5与升降丝杆3之间通过传动盒15内的蜗轮蜗杆副传动。As shown in Figure 1 and Figure 2, the utility model discloses an antenna lifting device, which includes an
本实用新型另一种实施方式,所述升降丝杆3也为四个,呈正方形设置,但是分别通过同步的驱动装置驱动。In another embodiment of the present utility model, there are also four
如图3所示,位于方舱内的天线14安装在天线托盘1上,天线托盘1在升降丝杆3的推动下上升或下降。As shown in FIG. 3 , the antenna 14 located in the shelter is installed on the
本实用新型中控制系统实现对升降机构的电动升降控制,主要由电控箱、遥控盒、6个位置检测开关和连接电缆等组成。控制系统具有完善的安全保护措施,主要工作特点:The control system in the utility model realizes the electric lifting control of the lifting mechanism, and is mainly composed of an electric control box, a remote control box, 6 position detection switches and connecting cables. The control system has perfect safety protection measures, the main working characteristics:
1)具有输入相序检测和报警功能。对外部输入的三相交流电源相序进行检测,不符合相序规定,系统则不能通电工作,同时显示灯一直亮并发“吱吱”警报,保证正确的升降动作;1) It has the functions of input phase sequence detection and alarm. Detect the phase sequence of the external input three-phase AC power supply. If the phase sequence does not meet the phase sequence requirements, the system cannot be powered on and work. At the same time, the display light is always on and a "squeak" alarm is issued to ensure the correct lifting action;
2)具有电流过载保护功能。电路中设置空气开关,当驱动负载过大导致输入电流过大时,控制器自动切断电源,保证电机不受损;2) With current overload protection function. An air switch is set in the circuit. When the input current is too large due to excessive driving load, the controller will automatically cut off the power supply to ensure that the motor is not damaged;
3)升/降终点位置、天线座下方的活动地板位置、玻璃钢罩遮盖位置和舱内壁线槽盖位置均设置限位检测开关,各检测开关形成串联关系,确保电动升降动作具有联锁保护功能;3) Limit detection switches are set at the end position of lifting/lowering, the raised floor position under the antenna base, the position covered by the glass fiber reinforced plastic cover and the position of the inner wall trunking cover, and each detection switch forms a series relationship to ensure that the electric lifting action has an interlocking protection function ;
4)遥控盒上设置对应各限位检测开关的指示灯,显示各检测开关所处状态。当指示灯亮时,控制器切断电机电源并使驱动电机不能再加电。4) The remote control box is provided with indicator lamps corresponding to each limit detection switch to display the status of each detection switch. When the indicator light is on, the controller cuts off the power supply of the motor and makes the drive motor unable to re-energize.
本实用新型提供了一种天线升降装置的思路及方法,具体实现该技术方案的方法和途径很多,以上所述仅是本实用新型的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本实用新型原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本实用新型的保护范围。本实施例中未明确的各组成部份均可用现有技术加以实现。The utility model provides an idea and method of an antenna lifting device. There are many methods and approaches for realizing the technical solution. The above description is only a preferred implementation mode of the utility model. It should be pointed out that those skilled in the art In other words, on the premise of not departing from the principle of the utility model, some improvements and modifications can also be made, and these improvements and modifications should also be regarded as the protection scope of the utility model. All components that are not specified in this embodiment can be realized by existing technologies.
Claims (9)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008202160664U CN201345408Y (en) | 2008-11-24 | 2008-11-24 | Antenna lifting device |
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| CNU2008202160664U CN201345408Y (en) | 2008-11-24 | 2008-11-24 | Antenna lifting device |
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| CNU2008202160664U Expired - Fee Related CN201345408Y (en) | 2008-11-24 | 2008-11-24 | Antenna lifting device |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101901956A (en) * | 2010-08-26 | 2010-12-01 | 衡阳泰豪通信车辆有限公司 | Antenna lifting mechanism with locking function |
| CN103512688A (en) * | 2012-06-20 | 2014-01-15 | 上海宇航系统工程研究所 | Planar-unfolding antenna cable high/low-temperature torque testing device and testing method |
| CN103840272A (en) * | 2014-03-07 | 2014-06-04 | 高山 | Method for resolving conflict between antenna height and gain of communication in moving and communication in moving |
| CN104538723A (en) * | 2015-02-04 | 2015-04-22 | 上海航天测控通信研究所 | Vertical lift device for vehicle-borne radar |
| CN104993218A (en) * | 2015-07-24 | 2015-10-21 | 江苏捷诚车载电子信息工程有限公司 | Large vehicle antenna electric lifting platform |
| WO2016028269A1 (en) * | 2014-08-19 | 2016-02-25 | Raytheon Company | Antenna lifting apparatus and related techniques |
| US9496595B2 (en) | 2014-08-19 | 2016-11-15 | Raytheon Company | Antenna lifting apparatus and related techniques |
| CN111786108A (en) * | 2020-07-14 | 2020-10-16 | 广州心蛙科技有限责任公司 | Wind-control radar antenna |
| CN114425983A (en) * | 2022-01-24 | 2022-05-03 | 重庆零壹空间航天科技有限公司 | Rocket remote-measuring control vehicle |
-
2008
- 2008-11-24 CN CNU2008202160664U patent/CN201345408Y/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101901956A (en) * | 2010-08-26 | 2010-12-01 | 衡阳泰豪通信车辆有限公司 | Antenna lifting mechanism with locking function |
| CN103512688A (en) * | 2012-06-20 | 2014-01-15 | 上海宇航系统工程研究所 | Planar-unfolding antenna cable high/low-temperature torque testing device and testing method |
| CN103512688B (en) * | 2012-06-20 | 2015-09-16 | 上海宇航系统工程研究所 | Planar development class antenna cable high/low temperature torsional moment proving installation and method of testing |
| CN103840272A (en) * | 2014-03-07 | 2014-06-04 | 高山 | Method for resolving conflict between antenna height and gain of communication in moving and communication in moving |
| WO2016028269A1 (en) * | 2014-08-19 | 2016-02-25 | Raytheon Company | Antenna lifting apparatus and related techniques |
| US9496595B2 (en) | 2014-08-19 | 2016-11-15 | Raytheon Company | Antenna lifting apparatus and related techniques |
| CN104538723A (en) * | 2015-02-04 | 2015-04-22 | 上海航天测控通信研究所 | Vertical lift device for vehicle-borne radar |
| CN104538723B (en) * | 2015-02-04 | 2018-10-12 | 上海航天测控通信研究所 | A kind of vertical lift device of trailer-mounted radar |
| CN104993218A (en) * | 2015-07-24 | 2015-10-21 | 江苏捷诚车载电子信息工程有限公司 | Large vehicle antenna electric lifting platform |
| CN111786108A (en) * | 2020-07-14 | 2020-10-16 | 广州心蛙科技有限责任公司 | Wind-control radar antenna |
| CN114425983A (en) * | 2022-01-24 | 2022-05-03 | 重庆零壹空间航天科技有限公司 | Rocket remote-measuring control vehicle |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091111 Termination date: 20141124 |
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| EXPY | Termination of patent right or utility model |