




技术领域technical field
本发明涉及飞机用地面设备技术领域,特别是一种辅助油箱拆装辅助装置。The invention relates to the technical field of aircraft ground equipment, in particular to an auxiliary device for disassembling and assembling an auxiliary fuel tank.
背景技术Background technique
传统的空客A318公务机ACT辅助油箱拆装方式以纯人工为主,采用多人联合方式将辅助油箱抬出,因高度仅有1米左右,空间狭小,人员拆卸难度大,强度高。且辅助油箱距离地面2米左右,再由另一部分机务人员使用升降平台2运至地面。安装时候要保证油箱安装位置正确,由于副油箱油口与飞机油口位置一致才能正确安装,在大负载下,短时间内便会造成机务人员疲劳,并且副油箱表面光滑,复合材料结构易损伤,因此拆装过程具有严重的安全隐患。The traditional method of dismantling and assembling the ACT auxiliary fuel tank of the Airbus A318 business jet is mainly manual, and the auxiliary fuel tank is lifted out by a joint method of multiple people. Because the height is only about 1 meter and the space is small, it is difficult for personnel to disassemble and the strength is high. And the auxiliary fuel tank is about 2 meters away from the ground, and then transported to the ground by another part of the crew using the
实用新型《一种飞机副油箱拆装辅助装置》(申请号:2017106783121)公开了一种辅助油箱拆装辅助装置,其托盘可旋转,实现副油箱上下俯仰角度的调整,使得副油箱可以实现多方位的姿态调节,便于副油箱的安装。但是,空客A318公务机ACT辅助油箱安装在货仓内部,上述实用新型的托盘无法进入空客A318公务机货仓内部,从而无法完成ACT辅助油箱的拆装。The utility model "An Auxiliary Device for Auxiliary Fuel Tank Disassembly of Aircraft" (Application No.: 2017106783121) discloses an auxiliary device for disassembling and assembling an auxiliary fuel tank. Adjustment is convenient for the installation of auxiliary fuel tank. However, the ACT auxiliary fuel tank of the Airbus A318 business jet is installed inside the cargo compartment, and the pallet of the utility model mentioned above cannot enter the interior of the cargo compartment of the Airbus A318 business jet, so that the disassembly and assembly of the ACT auxiliary fuel tank cannot be completed.
发明内容Contents of the invention
本发明的目的在于针对现有的拆装辅助无法进入飞机货仓内部进行拆装油箱技术的不足,提供一种辅助油箱拆装辅助装置,达到能够将托板伸入飞机货仓内部,方便拆装辅助油箱的目的。The purpose of the present invention is to provide an auxiliary fuel tank dismantling auxiliary device to solve the problem that the existing disassembly assistant cannot enter the interior of the aircraft cargo compartment to disassemble the fuel tank, so as to achieve the purpose of extending the supporting plate into the interior of the aircraft cargo compartment and facilitate disassembly. The purpose of installing the auxiliary fuel tank.
本发明所提供的一种辅助油箱拆装辅助装置,包括底座总成和升降平台;其特征在于:所述的底座总成通过升降平台与倾斜支架总成连接,所述的倾斜支架总成包括上倾斜架和下倾斜架,上倾斜架的一侧与下倾斜架铰接,下倾斜架与升降平台的上端连接,上倾斜架与下倾斜架通过伸缩装置连接;所述的倾斜支架总成的上端与油箱托架总成连接,油箱托架总成包括内托板、外托板、传动机构和动力机构,外托板与上倾斜架的上端面滑动配合;所述的外托板的中间位置设有长方形通孔,外托板的长方形通孔内安装有内托板,内托板的一端与外托板转动配合,所述的内托板通过传动机构与动力机构连接。An auxiliary device for disassembling and assembling an auxiliary oil tank provided by the present invention includes a base assembly and a lifting platform; it is characterized in that: the base assembly is connected with the tilting bracket assembly through the lifting platform, and the tilting bracket assembly includes The upper inclined frame and the lower inclined frame, one side of the upper inclined frame is hinged with the lower inclined frame, the lower inclined frame is connected with the upper end of the lifting platform, and the upper inclined frame is connected with the lower inclined frame through a telescopic device; the inclined bracket assembly The upper end is connected with the fuel tank bracket assembly, and the fuel tank bracket assembly includes an inner supporting plate, an outer supporting plate, a transmission mechanism and a power mechanism, and the outer supporting plate is slidingly matched with the upper end surface of the upper inclined frame; The position is provided with a rectangular through hole, and the inner supporting plate is installed in the rectangular through hole of the outer supporting plate, and one end of the inner supporting plate is rotatably matched with the outer supporting plate, and the inner supporting plate is connected with the power mechanism through a transmission mechanism.
进一步的,所述的底座总成包括底座支架、支撑机构和万向轮,底座支架下端的四个角位置分别安装有万向轮,底座支架的下端两侧分别安装有支撑机构。Further, the base assembly includes a base bracket, a supporting mechanism and universal wheels, the four corners of the lower end of the base bracket are respectively equipped with universal wheels, and the two sides of the lower end of the base bracket are respectively equipped with supporting mechanisms.
进一步的,所述的支撑机构包括螺杆、螺纹套筒、支脚座和摇杆,底座支架的两侧分别安装有螺纹套筒,螺纹套筒上设有螺纹通孔,螺杆与螺纹套筒的螺纹通孔相配合,螺杆的下端与支脚座连接,上端设有通孔,摇杆穿过螺杆上端的通孔,与螺杆垂直配合。Further, the support mechanism includes a screw rod, a threaded sleeve, a foot seat and a rocker. The two sides of the base bracket are respectively equipped with a threaded sleeve, and the threaded sleeve is provided with a threaded through hole. The threads of the screw rod and the threaded sleeve The through hole is matched, the lower end of the screw rod is connected with the foot seat, and the upper end is provided with a through hole, and the rocking rod passes through the through hole at the upper end of the screw rod to vertically cooperate with the screw rod.
进一步的,所述的上倾斜架的上端面上与多个滚轮转动配合,外托板放置在滚轮的上端。Further, the upper end surface of the upper inclined frame is rotatably matched with a plurality of rollers, and the outer supporting plate is placed on the upper ends of the rollers.
进一步的,所述的上倾斜架的两侧安装有导向板,两导向板将外托板夹在内侧,导向板的内侧安装有导轨,外托板的两侧边分别设有滑槽,导轨与滑槽滑动配合。Further, guide plates are installed on both sides of the upper tilting frame, and the two guide plates clamp the outer supporting plate inside, guide rails are installed on the inner side of the guiding plate, and slide grooves are respectively provided on both sides of the outer supporting plate, and the guide rails Sliding fit with the chute.
进一步的,所述的外托板的尾部下端安装有限位板,上倾斜架的前部的上端安装有定位板,限位板与定位板的位置相对应。Further, a limiting plate is installed at the lower end of the tail of the outer supporting plate, and a positioning plate is installed at the upper end of the front part of the upper inclined frame, and the position of the limiting plate corresponds to the position of the positioning plate.
进一步的,所述的外托板中间长方形通孔的两侧分别设有长条孔,长条孔内安装有多个呈线性均匀排列的滚轮。Further, the two sides of the rectangular through hole in the middle of the outer support plate are respectively provided with elongated holes, and a plurality of linearly and evenly arranged rollers are installed in the elongated holes.
进一步的,所述的传动机构包括齿轮和传动轴,内托板的一端安装有传动轴,外托板的一端设有通孔与长方形通孔相贯通,传动轴穿过外托板一端的通孔与齿轮的齿轮孔配合。Further, the transmission mechanism includes a gear and a transmission shaft, a transmission shaft is installed at one end of the inner support plate, a through hole is provided at one end of the outer support plate to communicate with the rectangular through hole, and the transmission shaft passes through the through hole at one end of the outer support plate. The hole mates with the gear hole of the gear.
进一步的,所述的外托板上设有两对称分布放置槽,放置槽的一端开口,放置槽内安装有撬板,撬板靠近放置槽开口的一端与外托板转动配合;撬板分别通过传动机构与动力机构连接,撬板的靠近开口的一端与传动轴连接,外托板的一端设有与放置槽相贯通的通孔,传动轴的一端穿过与放置槽相贯通的通孔与齿轮和齿轮孔固定配合。Further, two symmetrically distributed placement grooves are arranged on the outer support plate, one end of the placement groove is open, and a crowbar is installed in the placement groove, and the end of the crowbar close to the opening of the placement groove is rotatably matched with the outer support plate; The transmission mechanism is connected with the power mechanism, the end of the pry plate close to the opening is connected with the transmission shaft, one end of the outer support plate is provided with a through hole connected with the placement groove, and one end of the transmission shaft passes through the through hole connected with the placement groove Fixed fit with gears and gear holes.
进一步的,动力机构包括电动机、丝杠、导向杆和导向支座,上倾斜架的一端分别安装有导向杆和丝杠,丝杠的两端与上倾斜架转动配合,丝杠的一端与电动机的电机轴固定连接,导向支座上分别设有导向通孔和螺纹通孔,丝杠与导向支座的螺纹通孔相配合,导向杆穿过导向支座的导向通孔,导向支座的上端通过伸缩装置与连接杆固定连接,连接杆的两端分别安装有齿条,两齿条分别朝向各自对应的齿轮,齿条带齿的一端朝向下方。Further, the power mechanism includes a motor, a lead screw, a guide rod and a guide support. One end of the upper tilting frame is respectively equipped with a guide rod and a lead screw. The motor shaft is fixedly connected, the guide support is provided with a guide through hole and a threaded through hole respectively, the screw is matched with the threaded through hole of the guide support, the guide rod passes through the guide through hole of the guide support, and the guide support The upper end is fixedly connected with the connecting rod through the telescopic device, racks are respectively installed at both ends of the connecting rod, and the two racks face respectively corresponding gears, and the toothed end of the rack faces downward.
与现有技术相比较,本发明具有以下突出的有益效果:Compared with the prior art, the present invention has the following outstanding beneficial effects:
1、为了使辅助油箱顺利滑落到外托板上,本发明中简化了油箱托架总成的结构,为了减少外托板的厚度,使动力机构与传动机构分离,使动力机构安装在倾斜支架总成上,尽量减少安装在外托板上的零部件,从而减少其厚度;1. In order to make the auxiliary fuel tank slide down onto the outer support plate smoothly, the structure of the fuel tank bracket assembly is simplified in the present invention. In order to reduce the thickness of the outer support plate, the power mechanism is separated from the transmission mechanism, and the power mechanism is installed on the inclined bracket In the assembly, try to reduce the parts installed on the outer support plate, thereby reducing its thickness;
2、本发明的外托板的内部安装有内托板,由于飞机货舱门间隙较小,通过旋转内托板,能够改变辅助油箱的放置角度,从而避免其与舱门两侧的舱壁碰撞,从而能够顺利将辅助油箱运出。2. The inner supporting plate is installed inside the outer supporting plate of the present invention. Since the clearance of the aircraft cargo door is small, the placement angle of the auxiliary fuel tank can be changed by rotating the inner supporting plate, thereby avoiding its collision with the bulkheads on both sides of the door , so that the auxiliary fuel tank can be transported out smoothly.
附图说明Description of drawings
图1是本发明的结构示意图。Fig. 1 is a structural schematic diagram of the present invention.
图2是本发明的右侧视图。Figure 2 is a right side view of the present invention.
图3是本发明的俯视图。Figure 3 is a top view of the present invention.
图4是图1中A部分的局部放大图。Fig. 4 is a partially enlarged view of part A in Fig. 1 .
图5是图2中B部分的局部放大图。Fig. 5 is a partially enlarged view of part B in Fig. 2 .
具体实施方式Detailed ways
下面结合说明书附图和具体实施方式对本发明进一步说明。The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.
如图1所示,本发明包括底座总成1、倾斜支架总成3、升降平台2和油箱托架总成4。As shown in FIG. 1 , the present invention includes a
如图2所示,所述的底座总成1包括底座支架13、支撑机构12和万向轮11,底座支架13下端的四个角位置分别安装有万向轮11,底座支架13的下端两侧分别安装有支撑机构12,支撑机构12包括螺杆122、螺纹套筒123、支脚座124和摇杆121,底座支架13的两侧分别安装有螺纹套筒123,螺纹套筒123上设有螺纹通孔,螺杆122与螺纹套筒123的螺纹通孔相配合,螺杆122的下端与支脚座124固定连接,上端设有通孔,摇杆121穿过螺杆122上端的通孔,与螺杆122垂直配合,通过旋转摇杆121能够带动螺杆122转动,从而实现支脚座124与地面贴合,使底座总成1固定,不移动。As shown in Figure 2, the
所述的底座总成1的上端通过升降平台2与倾斜支架总成3连接,底座支架13的上端与升降平台2的下端连接,本实施例中,所述的升降平台2为液压升降平台2,液压升降平台2为现有装置,其具体结构不再赘述。The upper end of the
所述的倾斜支架总成3包括上倾斜架32和下倾斜架31,上倾斜架32的一侧与下倾斜架31铰接,下倾斜架31与升降平台2的上端固定连接,上倾斜架32与下倾斜架31通过伸缩装置连接,伸缩装置的下端与下倾斜架31铰接,伸缩装置的内杆的上端与上倾斜架32铰接。当伸缩装置伸缩时,能够带动上倾斜架32转动,从而改变上倾斜架32与下倾斜架31之间的角度。The
如图3所示,所述的倾斜支架总成3的上端与油箱托架总成4固定连接,油箱托架总成4包括内托板43、外托板41、传动机构和动力机构6,外托板41与上倾斜架32的上端面滑动配合,其具体配合方式为:上倾斜架32的上端面上与多个滚轮5转动配合,外托板41放置在滚轮5的上端。As shown in Fig. 3, the upper end of the
所述的上倾斜架32的两侧安装有导向板,两导向板将外托板41夹在内侧,导向板的内侧安装有导轨,外托板41的两侧边分别设有滑槽,导轨与滑槽滑动配合。The two sides of described upper tilting frame 32 are equipped with guide plates, two guide plates clamp the outer supporting
如图5所示,所述的外托板41的尾部下端安装有限位板44,上倾斜架32的前部的上端安装有定位板45,限位板44与定位板45的位置相对应,当外托板41的限位板44运动到定位板45位置时,定位板45能够挡住限位板44限制外托板41继续运动,防止其脱离上倾斜架32。As shown in Figure 5, the lower end of the tail portion of the outer supporting
所述的外托板41的中间位置设有长方形通孔,外托板41的长方形通孔内安装有内托板43,内托板43远离辅助油箱的一端与外托板41转动配合,且其上端安装有挡板46,挡板46能够起到阻挡辅助油箱的作用。所述的内托板43安装挡板46的一端的下方设有放置板,放置板与外托板41长方形通孔的两内侧壁固定连接,内托板43放置在放置板上,避免内托板43向外托板41的下方转动。The middle position of the outer supporting
所述的外托板41中间长方形通孔的两侧分别设有长条孔,长条孔内安装有多个呈线性均匀排列的滚轮5。The two sides of the rectangular through hole in the middle of the outer supporting
所述的外托板41上设有两对称分布放置槽,放置槽的一端开口,放置槽内安装有撬板42,撬板42靠近放置槽开口的一端与外托板41转动配合。所述的撬板42远离放置槽开口的一端的下方设有放置板,放置板与放置槽的两内侧壁固定连接,撬板42放置在放置板上,避免撬板42向外托板41的下方转动。The outer supporting
所述的撬板42的厚度小于外托板41的厚度,并且其与传动轴连接的一端的厚度大于另一端的厚度。当撬板42翻转180°后,撬板42厚度较小的一端朝向辅助油箱,其厚度低于辅助油箱滑轨的高度,从而能够使辅助油箱顺利的滑入到撬板42上。The thickness of the
如图4所示,所述的内托板43与撬板42分别通过传动机构与动力机构6连接,传动机构包括齿轮7和传动轴,内托板43的一端安装有传动轴,外托板41的一端设有通孔与长方形通孔相贯通,传动轴穿过外托板41一端的通孔与齿轮7的齿轮孔固定配合。所述的撬板42的靠近开口的一端与传动轴连接,外托板41的一端设有与放置槽相贯通的通孔,传动轴的一端穿过与放置槽相贯通的通孔与齿轮7和齿轮孔固定配合。As shown in Figure 4, described inner supporting
所述的上倾斜架32上安装有动力机构6,动力机构6包括电动机66、丝杠62、导向杆61和导向支座65,上倾斜架32的一端分别安装有导向杆61和丝杠62,丝杠62的两端与上倾斜架32转动配合,丝杠62的一端与电动机66的电机轴固定连接,导向支座65上分别设有导向通孔和螺纹通孔,丝杠62与导向支座65的螺纹通孔相配合,导向杆61穿过导向支座65的导向通孔,导向支座65的上端通过伸缩装置与连接杆64固定连接,连接杆64的两端分别安装有齿条63,两齿条63分别朝向各自对应的齿轮7,齿条63带齿的一端朝向下方。当丝杠62转动时,导向支座65能够带动齿条63运动到相对应的齿轮7位置,并与齿轮7进入啮合,带动齿轮7转动,从而能够分别带动内托板43和撬板42转动。A
本实施例中,所述的伸缩装置为液压缸、气缸或电动伸缩杆等能够伸缩的装置。In this embodiment, the telescopic device is a telescopic device such as a hydraulic cylinder, an air cylinder, or an electric telescopic rod.
操作流程如下:使用本发明时,将外托板41拖入空客A318公务机货仓内部后,传动机构的齿轮7与动力机构6的齿条63位于同一平面。调节倾斜支架总成3,使外托板41与货仓底板倾斜度相同,使外托板41放置在辅助油箱行程上,当外托板41的厚度高于辅助油箱滑轨的高度时,启动动力机构,使动力机构的齿条63带动齿轮7转动,使撬板42旋转180°,拆除辅助油箱的挡块,由于撬板42靠近辅助油箱一端的厚度较薄,低于辅助油箱的滑轨高度,辅助油箱能够靠重力滑到撬板42上,此时,启动动力机构,使撬板42反向转动,将辅助油箱的一端撬起,使其下端高于外托板41,从而能够依靠重力滑到外托板41上。当辅助油箱放置到外托板41上时,将其从飞机货仓出口拖出,由于飞机货舱门间隙较小,通过旋转内托板43,能够改变辅助油箱的放置角度,从而避免其与舱门两侧的舱壁碰撞。The operation process is as follows: when using the present invention, after the outer supporting
需要说明的是,本发明的特定实施方案已经对本发明进行了详细描述,对于本领域的技术人员来说,在不背离本发明的精神和范围的情况下对它进行的各种显而易见的改变都在本发明的保护范围之内。It should be noted that the specific embodiments of the present invention have described the present invention in detail, and for those skilled in the art, it is possible to make various obvious changes to it without departing from the spirit and scope of the present invention. Within the protection scope of the present invention.
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310129401.6ACN115924110B (en) | 2023-02-17 | 2023-02-17 | Auxiliary fuel tank disassembly and assembly auxiliary device |
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310129401.6ACN115924110B (en) | 2023-02-17 | 2023-02-17 | Auxiliary fuel tank disassembly and assembly auxiliary device |
| Publication Number | Publication Date |
|---|---|
| CN115924110Atrue CN115924110A (en) | 2023-04-07 |
| CN115924110B CN115924110B (en) | 2025-05-27 |
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310129401.6AActiveCN115924110B (en) | 2023-02-17 | 2023-02-17 | Auxiliary fuel tank disassembly and assembly auxiliary device |
| Country | Link |
|---|---|
| CN (1) | CN115924110B (en) |
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5565242A (en)* | 1992-09-21 | 1996-10-15 | The Boeing Company | Lubricant applications to a hole |
| CN103935528A (en)* | 2014-05-05 | 2014-07-23 | 沈阳飞研航空设备有限公司 | Engine demounting and mounting trailer |
| CN109383842A (en)* | 2017-08-10 | 2019-02-26 | 河南寰球航空装备科技有限公司 | A kind of auxiliary tank of aircraft dismounting auxiliary device |
| CN111169906A (en)* | 2020-03-16 | 2020-05-19 | 日照山太飞机工程股份有限公司 | Aircraft seat handling device |
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5565242A (en)* | 1992-09-21 | 1996-10-15 | The Boeing Company | Lubricant applications to a hole |
| CN103935528A (en)* | 2014-05-05 | 2014-07-23 | 沈阳飞研航空设备有限公司 | Engine demounting and mounting trailer |
| CN109383842A (en)* | 2017-08-10 | 2019-02-26 | 河南寰球航空装备科技有限公司 | A kind of auxiliary tank of aircraft dismounting auxiliary device |
| CN111169906A (en)* | 2020-03-16 | 2020-05-19 | 日照山太飞机工程股份有限公司 | Aircraft seat handling device |
| Publication number | Publication date |
|---|---|
| CN115924110B (en) | 2025-05-27 |
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|---|---|---|
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |