CN204606238U - A kind of repairing dock column for aircraft maintenance - Google Patents
A kind of repairing dock column for aircraft maintenance Download PDFInfo
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- CN204606238U CN204606238U CN201520200811.6U CN201520200811U CN204606238U CN 204606238 U CN204606238 U CN 204606238U CN 201520200811 U CN201520200811 U CN 201520200811U CN 204606238 U CN204606238 U CN 204606238U
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Abstract
一种用于飞机维修的维修坞立柱,摒弃了传统封闭式的笼型结构,采用了开放式三角形结构,轨道竖直设置在基架中部,滑块导向架位于轨道上,在滑块导向架上安装有用以连接作业面平台的升降支撑架;滑块导向架上安装有若干导向轮,导向轮与轨道滚动接触配合,在基架顶端固定安装驱动电机,驱动电机与蜗轮箱相连接,丝杠竖直连接在蜗轮箱上,丝母通过安装座固装于滑块导向架的同时还套装在丝杠上,通过驱动电机带动丝杠转动,实现作业面平台的升降。本实用新型不但具有足够的支撑强度,还极大简化了升降驱动组件的拆卸及安装过程,方便了维修坞立柱的维护,同时在装卸过程中节省了大量的时间和人力成本。
A maintenance dock column for aircraft maintenance, which abandons the traditional closed cage structure and adopts an open triangular structure. The track is vertically arranged in the middle of the base frame, and the slider guide frame is located on the track. There is a lifting support frame for connecting the platform on the working surface; a number of guide wheels are installed on the slider guide frame, and the guide wheels are in rolling contact with the track. The driving motor is fixedly installed on the top of the base frame. The rod is vertically connected to the worm gear box, and the screw nut is fixed on the slider guide frame through the mounting seat and is also set on the lead screw. The drive motor drives the lead screw to rotate to realize the lifting of the working surface platform. The utility model not only has sufficient support strength, but also greatly simplifies the disassembly and installation process of the lifting drive assembly, facilitates the maintenance of the maintenance dock column, and saves a lot of time and labor costs during the loading and unloading process.
Description
技术领域 technical field
本实用新型属于飞机维修坞技术领域,特别是涉及一种用于飞机维修的维修坞立柱。 The utility model belongs to the technical field of aircraft maintenance docks, in particular to a maintenance dock column for aircraft maintenance.
背景技术 Background technique
对于固定式飞机维修坞而言,飞机维修坞的作业面平台想要实现升降动作,都是通过维修坞立柱完成的,在经过了一段时间的飞机维修作业后,由于作业面平台经历了若干次往复升降,维修坞立柱内的升降驱动组件就有可能损坏,因此就需要对升降驱动组件进行修理,但此时问题出现了,按照以往的设计经验,为了保证维修坞立柱的支撑强度,维修坞立柱的主体均被设计成了封闭式的笼型结构,而升降驱动组件设置在笼型结构内部,想要直接拆卸升降驱动组件进行修理几乎是不可能的,只能先对整体维修坞立柱进行拆卸,然后再拆卸升降驱动组件,而整个拆卸过程非常不方便,导致每次维修作业都会花费大量的时间和人力,即使升降驱动组件修理好后,还需要将升降驱动组件安装回维修坞立柱内,导致安装过程再次花去大量的时间和人力,因此,亟需设计一种全新结构的维修坞立柱,在保证维修坞立柱支撑强度的前提下,能够简化升降驱动组件的拆卸及安装过程,方便维修坞立柱的维护,节省时间和人力成本。 For the fixed aircraft maintenance dock, if the operation surface platform of the aircraft maintenance dock wants to realize the lifting action, it is all done through the maintenance dock column. After a period of aircraft maintenance operations, the operation surface platform has experienced several Reciprocating lifting, the lifting drive assembly in the maintenance dock column may be damaged, so the lifting drive assembly needs to be repaired, but at this time the problem has arisen. According to previous design experience, in order to ensure the support strength of the maintenance dock column, the maintenance dock The main body of the column is designed as a closed cage structure, and the lifting drive assembly is set inside the cage structure. It is almost impossible to directly disassemble the lifting drive assembly for repair. The only way to do it is to repair the entire maintenance dock column first. Disassembly, and then disassembly of the lifting drive assembly, and the entire disassembly process is very inconvenient, resulting in a lot of time and manpower for each repair operation, even after the lifting drive assembly is repaired, the lifting drive assembly needs to be installed back in the maintenance dock column , causing the installation process to take a lot of time and manpower again. Therefore, it is urgent to design a maintenance dock column with a new structure. On the premise of ensuring the support strength of the maintenance dock column, it can simplify the disassembly and installation process of the lifting drive assembly, which is convenient The maintenance of the dock column saves time and labor costs.
实用新型内容 Utility model content
针对现有技术存在的问题,本实用新型提供一种用于飞机维修的维修坞立柱,能够简化升降驱动组件的拆卸及安装过程,方便维修坞立柱的维护,节省时间和人力成本。 Aiming at the problems existing in the prior art, the utility model provides a maintenance dock column for aircraft maintenance, which can simplify the disassembly and installation process of the lifting drive assembly, facilitate the maintenance of the maintenance dock column, and save time and labor costs.
为了实现上述目的,本实用新型采用如下技术方案:一种用于飞机维修的维修坞立柱,包括基架、轨道、滑块导向架及升降驱动组件,所述基架采用开放式三角形结构,轨道竖直设置在基架中部,所述滑块导向架位于轨道上,在滑块导向架上安装有用以连接作业面平台的升降支撑架;所述滑块导向架通过升降驱动组件与轨道升降配合。 In order to achieve the above object, the utility model adopts the following technical scheme: a maintenance dock column for aircraft maintenance, including a base frame, a track, a slider guide frame and a lifting drive assembly, the base frame adopts an open triangular structure, and the track Vertically arranged in the middle of the base frame, the slider guide frame is located on the track, and a lifting support frame for connecting the working surface platform is installed on the slider guide frame; the slider guide frame cooperates with the rail lift through the lifting drive assembly .
所述升降驱动组件包括驱动电机、蜗轮箱、丝杠及丝母,所述驱动电机固定安装在基架顶端,驱动电机的电机轴通过联轴器与蜗轮箱相连接,所述丝杠竖直设置,且丝杠上端与蜗轮箱相连接,所述丝母通过安装座固装于滑块导向架的同时还套装在丝杠上。 The lifting drive assembly includes a drive motor, a worm gear box, a lead screw and a screw nut, the drive motor is fixedly mounted on the top of the base frame, the motor shaft of the drive motor is connected with the worm gear box through a coupling, and the lead screw is vertical Set, and the upper end of the lead screw is connected with the worm gear box, and the screw nut is fixedly mounted on the slider guide frame through the mounting seat and is also sleeved on the lead screw.
在所述滑块导向架上安装有若干导向轮,导向轮与轨道滚动接触配合。 Several guide wheels are installed on the slider guide frame, and the guide wheels are in rolling contact with the track.
本实用新型的有益效果: The beneficial effects of the utility model:
本实用新型与现有技术相比,打破了惯有的设计思路,摒弃了传统封闭式的笼型结构,维修坞立柱整体采用开放式三角形结构,不但保证了维修坞立柱具有足够的支撑强度,还极大简化了升降驱动组件的拆卸及安装过程,方便了维修坞立柱的维护,同时在装卸过程中节 省了大量的时间和人力成本。 Compared with the prior art, the utility model breaks the customary design idea, abandons the traditional closed cage structure, and adopts an open triangular structure for the maintenance dock column as a whole, which not only ensures that the maintenance dock column has sufficient supporting strength, It also greatly simplifies the disassembly and installation process of the lifting drive assembly, facilitates the maintenance of the maintenance dock column, and saves a lot of time and labor costs during the loading and unloading process.
附图说明 Description of drawings
图1为本实用新型的一种用于飞机维修的维修坞立柱立体图; Fig. 1 is a perspective view of a maintenance dock column for aircraft maintenance of the present invention;
图2为本实用新型的一种用于飞机维修的维修坞立柱正视图; Fig. 2 is a front view of a maintenance dock column for aircraft maintenance of the present invention;
图3为本实用新型的一种用于飞机维修的维修坞立柱侧视图; Fig. 3 is a side view of a maintenance dock column for aircraft maintenance of the present invention;
图4为本实用新型的滑块导向架结构示意图; Fig. 4 is the structural schematic diagram of the slider guide frame of the present utility model;
图中,1—基架,2—轨道,3—滑块导向架,4—升降支撑架,5—驱动电机,6—蜗轮箱,7—丝杠,8—丝母,9—导向轮。 Among the figure, 1—base frame, 2—track, 3—slider guide frame, 4—lifting support frame, 5—drive motor, 6—worm gear box, 7—leading screw, 8—screw nut, 9—guiding wheel.
具体实施方式 Detailed ways
下面结合附图和具体实施例对本实用新型做进一步的详细说明。 Below in conjunction with accompanying drawing and specific embodiment the utility model is described in further detail.
如图1、2、3、4所示,一种用于飞机维修的维修坞立柱,包括基架1、轨道2、滑块导向架3及升降驱动组件,所述基架1采用开放式三角形结构,轨道2竖直设置在基架1中部,所述滑块导向架3位于轨道2上,在滑块导向架3上安装有用以连接作业面平台的升降支撑架4;所述滑块导向架3通过升降驱动组件与轨道2升降配合。 As shown in Figures 1, 2, 3, and 4, a maintenance dock column for aircraft maintenance includes a base frame 1, a track 2, a slider guide frame 3 and a lifting drive assembly, and the base frame 1 adopts an open triangular shape. structure, the track 2 is vertically arranged in the middle of the base frame 1, the slider guide frame 3 is located on the track 2, and the lift support frame 4 for connecting the working surface platform is installed on the slider guide frame 3; the slider guide frame Frame 3 cooperates with track 2 lifting by lifting drive assembly. the
所述升降驱动组件包括驱动电机5、蜗轮箱6、丝杠7及丝母8,所述驱动电机5固定安装在基架1顶端,驱动电机5的电机轴通过联轴器与蜗轮箱6相连接,所述丝杠7竖直设置,且丝杠7上端与蜗轮箱6相连接,所述丝母8通过安装座固装于滑块导向架3的同时还套装在丝杠7上。 The lifting drive assembly includes a drive motor 5, a worm gear box 6, a lead screw 7 and a screw nut 8, the drive motor 5 is fixedly mounted on the top of the base frame 1, and the motor shaft of the drive motor 5 is connected to the worm gear box 6 through a coupling. Connected, the lead screw 7 is vertically arranged, and the upper end of the lead screw 7 is connected with the worm gear box 6, and the screw nut 8 is fixed on the slider guide frame 3 through the mounting seat and is also sleeved on the lead screw 7.
在所述滑块导向架3上安装有若干导向轮9,导向轮9与轨道2滚动接触配合。 A plurality of guide wheels 9 are installed on the slider guide frame 3 , and the guide wheels 9 are in rolling contact with the track 2 .
采用了本实用新型的维修坞,在作业面平台下方设置有4处维修坞立柱,作业面平台通过升降支撑架4与维修坞立柱相连,启动驱动电机5,通过蜗轮箱6带动丝杠7转动,通过丝杠7转动带动丝母8上下移动,进而带动滑块导向架3上下移动,从而实现了作业面平台的升降动作。在升降驱动组件工作过程中,由于没有了遮挡,可以清晰观察升降驱动组件的运行状态,方便了日常巡检作业,相比传统的封闭式笼型结构,一旦发现升降驱动组件损坏,特别是需要更换丝杠7时,只需先将滑块导向架3拆卸下来,便可轻松卸下整根丝杠7,安装丝杠7同样方便简单,如此节省了大量的时间和人力成本。 Adopting the maintenance dock of the utility model, there are four maintenance dock columns under the working surface platform, the working surface platform is connected with the maintenance dock column through the lifting support frame 4, the driving motor 5 is started, and the screw 7 is driven to rotate through the worm gear box 6 , the screw nut 8 is driven to move up and down by the rotation of the lead screw 7, and then the slider guide frame 3 is driven to move up and down, thereby realizing the lifting action of the working surface platform. During the working process of the lifting drive component, since there is no shelter, the running status of the lifting drive component can be clearly observed, which facilitates daily inspection operations. Compared with the traditional closed cage structure, once the lifting drive component is found to be damaged, it is especially necessary When replacing the lead screw 7, the whole lead screw 7 can be easily disassembled only by first disassembling the slider guide frame 3, and the installation of the lead screw 7 is also convenient and simple, which saves a lot of time and labor costs.
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Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520200811.6U CN204606238U (en) | 2015-04-03 | 2015-04-03 | A kind of repairing dock column for aircraft maintenance |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520200811.6U CN204606238U (en) | 2015-04-03 | 2015-04-03 | A kind of repairing dock column for aircraft maintenance |
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| CN204606238U true CN204606238U (en) | 2015-09-02 |
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| CN201520200811.6U Expired - Lifetime CN204606238U (en) | 2015-04-03 | 2015-04-03 | A kind of repairing dock column for aircraft maintenance |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482642A (en) * | 2018-03-07 | 2018-09-04 | 华北水利水电大学 | Aerial survey unmanned plane wing repairs frame and its restorative procedure |
| CN110576981A (en) * | 2019-08-19 | 2019-12-17 | 沈阳宝通门业有限公司 | Adjustable inclination angle type vertical tail dock working platform |
| CN110589013A (en) * | 2019-08-19 | 2019-12-20 | 沈阳宝通门业有限公司 | Lifting adjusting support suitable for fixed horizontal tail dock |
| CN111056038A (en) * | 2019-12-05 | 2020-04-24 | 南京熊猫电子股份有限公司 | Equipment of unmanned aerial vehicle undercarriage |
-
2015
- 2015-04-03 CN CN201520200811.6U patent/CN204606238U/en not_active Expired - Lifetime
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482642A (en) * | 2018-03-07 | 2018-09-04 | 华北水利水电大学 | Aerial survey unmanned plane wing repairs frame and its restorative procedure |
| CN110576981A (en) * | 2019-08-19 | 2019-12-17 | 沈阳宝通门业有限公司 | Adjustable inclination angle type vertical tail dock working platform |
| CN110589013A (en) * | 2019-08-19 | 2019-12-20 | 沈阳宝通门业有限公司 | Lifting adjusting support suitable for fixed horizontal tail dock |
| CN110589013B (en) * | 2019-08-19 | 2024-04-02 | 沈阳宝通门业有限公司 | Lifting adjusting bracket applicable to fixed horizontal tail dock |
| CN110576981B (en) * | 2019-08-19 | 2024-04-30 | 沈阳宝通门业有限公司 | Inclination-adjustable vertical tail dock working platform |
| CN111056038A (en) * | 2019-12-05 | 2020-04-24 | 南京熊猫电子股份有限公司 | Equipment of unmanned aerial vehicle undercarriage |
| CN111056038B (en) * | 2019-12-05 | 2021-09-21 | 南京熊猫电子股份有限公司 | Equipment of unmanned aerial vehicle undercarriage |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A maintenance depressed place stand for aircraft maintenance Effective date of registration: 20171019 Granted publication date: 20150902 Pledgee: Pudong Development Bank of Shanghai Limited by Share Ltd. Shenyang branch Pledgor: SHENYANG BAOTONG DOOR Co.,Ltd. Registration number: 2017210000020 |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20191118 Granted publication date: 20150902 Pledgee: Pudong Development Bank of Shanghai Limited by Share Ltd. Shenyang branch Pledgor: SHENYANG BAOTONG DOOR Co.,Ltd. Registration number: 2017210000020 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| CX01 | Expiry of patent term |
Granted publication date: 20150902 |
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| CX01 | Expiry of patent term |