CN203589187U - Helicopter measurement-control shelter with automatic antenna lifting apparatus - Google Patents
Helicopter measurement-control shelter with automatic antenna lifting apparatus Download PDFInfo
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- CN203589187U CN203589187U CN201320781053.2U CN201320781053U CN203589187U CN 203589187 U CN203589187 U CN 203589187U CN 201320781053 U CN201320781053 U CN 201320781053U CN 203589187 U CN203589187 U CN 203589187U
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Abstract
本实用新型涉及直升机测控方舱,特别涉及一种具有自动天线升降装置的直升机测控方舱。具有自动天线升降装置的直升机测控方舱,包括运载车和安装在运载车上的方舱,方舱内安装电子设备,所述方舱的四角竖直安装有天线及能够将天线升起降下的升降机构,所述天线与方舱内的电子设备信号连接。本实用新型中的天线升降机构,可以使天线方便地升出舱外工作,相较与以往的手摇升降,升降速度快,省时省力。
The utility model relates to a helicopter measurement and control shelter, in particular to a helicopter measurement and control shelter with an automatic antenna lifting device. Helicopter measurement and control shelter with automatic antenna lifting device, including a carrier vehicle and a shelter installed on the carrier vehicle, electronic equipment is installed in the shelter, antennas are installed vertically at the four corners of the shelter and the antenna can be raised and lowered The lifting mechanism, the antenna is connected with the electronic equipment signal in the shelter. The antenna lifting mechanism in the utility model can make the antenna conveniently lift out of the cabin to work. Compared with the previous manual lifting, the lifting speed is fast, saving time and effort.
Description
技术领域 technical field
本实用新型涉及直升机测控方舱,特别涉及一种具有自动天线升降装置的直升机测控方舱。 The utility model relates to a helicopter measurement and control shelter, in particular to a helicopter measurement and control shelter with an automatic antenna lifting device.
背景技术 Background technique
无人直升机成本低、效费比高、使用方便,在民用和军用领域有广泛的发展前景,无人直升机本身的天气适应能力强,可在不适合一般飞行条件下进行飞行,广泛应用于航拍、高空架线,线路巡查等。与无人直升机配套的——用于控制及监测直升机的测控方舱,为了能与无人直升机建立无线连接,在直升机测控方舱的四角竖直设置有天线,由于现有用于线路巡查的无人直升机主要由军用侦查遥控直升机改装而成,在设计之初考虑到军用的恶劣环境,直升机测控方舱的四角天线设置成手摇升降,比较简单实用,缺点是手摇升降较为费时费力。如今将无人直升机用于线路巡查,手摇升降天线给工作人员带来很大的麻烦。 Unmanned helicopters are low in cost, high in cost-efficiency, and easy to use. They have broad development prospects in civilian and military fields. Unmanned helicopters have strong weather adaptability and can fly under conditions that are not suitable for general flight. They are widely used in aerial photography , high-altitude stringing, line inspection, etc. Matching with the unmanned helicopter - the measurement and control cabin used to control and monitor the helicopter. In order to establish a wireless connection with the unmanned helicopter, antennas are vertically installed at the four corners of the helicopter measurement and control cabin. Manned helicopters are mainly converted from military reconnaissance remote control helicopters. Considering the harsh military environment at the beginning of the design, the four-corner antennas of the helicopter measurement and control cabin are set up to be lifted by hand, which is relatively simple and practical. The disadvantage is that the manual lift is time-consuming and laborious. Nowadays, unmanned helicopters are used for line inspections, and the manual lifting antenna brings great trouble to the staff.
实用新型内容 Utility model content
本实用新型的目的在于克服现有技术的上述不足,提供一种具有自动天线升降装置的直升机测控方舱,可有效解决直升机测控方舱的天线快速升降的问题。 The purpose of the utility model is to overcome the above-mentioned deficiencies of the prior art, and provide a helicopter measurement and control shelter with an automatic antenna lifting device, which can effectively solve the problem of rapid lifting of the antenna of the helicopter measurement and control shelter. the
为实现上述目的,本实用新型提供了以下技术方案: In order to achieve the above object, the utility model provides the following technical solutions:
具有自动天线升降装置的直升机测控方舱,包括运载车和安装在运载车上的方舱,方舱内安装电子设备,所述方舱的四角竖直安装有天线及能够将天线升起降下的升降机构,所述天线与方舱内的电子设备信号连接。 Helicopter measurement and control shelter with automatic antenna lifting device, including a carrier vehicle and a shelter installed on the carrier vehicle, electronic equipment is installed in the shelter, antennas are installed vertically at the four corners of the shelter and the antenna can be raised and lowered The lifting mechanism, the antenna is connected with the electronic equipment signal in the shelter.
上述具有自动天线升降装置的直升机测控方舱中,所述升降机构包括升降丝杆,所述升降丝杆为四个,呈长方形设置,升降丝杆之间通过三个扭力连杆驱动,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。 In the above-mentioned helicopter measurement and control shelter with an automatic antenna lifting device, the lifting mechanism includes lifting screw rods, and the lifting screw rods are four in a rectangular shape. The lifting screw rods are driven by three torsion connecting rods. A coupling is arranged between the rod and the torsion connecting rod, and one of the lifting screw rods is driven by a driving device.
上述具有自动天线升降装置的直升机测控方舱中,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吻合,驱动电机通过伞齿轮箱带动升降丝杆运动。 In the above-mentioned helicopter measurement and control shelter with an automatic antenna lifting device, the driving device includes a driving motor and a bevel gear box, the bevel gear box coincides 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.
与现有技术相比,本实用新型的有益效果:本实用新型中的天线升降机构,可以使天线方便地升出舱外工作,相较与以往的手摇升降,升降速度快,省时省力。 Compared with the prior art, the utility model has the beneficial effects: the antenna lifting mechanism in the utility model can easily lift the antenna out of the cabin to work. Compared with the previous manual lifting, the lifting speed is fast, saving time and effort .
附图说明 Description of drawings
图1为本实用新型的结构示意图。 Fig. 1 is the structural representation of the utility model.
图2为本实用新型中升降机构的结构示意图。 Fig. 2 is a structural schematic diagram of the lifting mechanism in the utility model.
图中标记:1-运载车,2-方舱,3-天线, 41-升降丝杆,42-扭力连杆,43-联轴节,51-驱动电机,52-伞齿轮箱。 Marks in the figure: 1-carrier, 2-shelter, 3-antenna, 41-lifting screw, 42-torsion connecting rod, 43-coupling, 51-drive motor, 52-bevel gearbox.
具体实施方式 Detailed ways
下面结合附图和具体实施方式对本实用新型作进一步的说明。 Below in conjunction with accompanying drawing and specific embodiment, the utility model is further described.
为了使实用新型的目的、技术方案及优点更加清楚明白,以下结合附图及实施例,对本实用新型进行进一步详细说明。应当理解,此处所描述的具体实施例仅用以解释本实用新型,并不用于限定本实用新型。 In order to make the purpose, technical solution and advantages of the utility model clearer, the utility model will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the utility model, and are not intended to limit the utility model.
实施例1Example 1
如附图1、附图2所示,本实施例具有自动天线升降装置的直升机测控方舱,包括运载车1和安装在运载车上的方舱2,方舱2内安装电子设备,所述方舱2的四角竖直安装有天线3及能够将天线升起降下的升降机构,所述天线3与方舱2内的电子设备信号连接,所述升降机构包括升降丝杆41,所述升降丝杆41为四个,呈长方形设置,升降丝杆41之间通过三个扭力连杆42驱动,升降丝杆41与扭力连杆42之间设有联轴节43,其中一个升降丝杆41通过驱动装置驱动,所述驱动装置包括驱动电机51和伞齿轮箱52,伞齿轮箱52与升降丝杆41下部吻合,驱动电机51通过伞齿轮箱52带动升降丝杆41运动。
As shown in accompanying
当天线需要升起时,驱动电机51通过伞齿轮箱52驱动其中一个升降丝杆41运动,该升降丝杆41又通过扭力连杆42带动其它三个升降丝杆41同时联动,如此保持四根升降丝杆41同步上升、下降,进而升起或降下方舱四角竖直安装的天线3,电机驱动相较与以往的手摇升降,升降速度快,省时省力。
When the antenna needs to be raised, the
以上所述仅为本实用新型的较佳实施例而已,并不用以限制本实用新型,凡在本实用新型的精神和原则之内所作的任何修改、等同替换和改进等,均应包含在本实用新型的保护范围之内。 The above descriptions are only preferred embodiments of the present utility model, and are not intended to limit the present utility model. Any modifications, equivalent replacements and improvements made within the spirit and principles of the present utility model shall be included in this utility model. within the scope of protection of utility models.
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108692860A (en) * | 2018-07-11 | 2018-10-23 | 广东省计量科学研究院 | A kind of elevating mechanism |
CN113945121A (en) * | 2021-10-28 | 2022-01-18 | 贵州航天特种车有限责任公司 | Self-propelled rocket gun with double launching devices |
-
2013
- 2013-12-03 CN CN201320781053.2U patent/CN203589187U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108692860A (en) * | 2018-07-11 | 2018-10-23 | 广东省计量科学研究院 | A kind of elevating mechanism |
CN108692860B (en) * | 2018-07-11 | 2024-05-31 | 广东省计量科学研究院 | Lifting mechanism |
CN113945121A (en) * | 2021-10-28 | 2022-01-18 | 贵州航天特种车有限责任公司 | Self-propelled rocket gun with double launching devices |
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Granted publication date: 20140507 Termination date: 20171203 |