CN207791190U - Tripod is fixed on a kind of adjustable ground for space shuttle - Google Patents
Tripod is fixed on a kind of adjustable ground for space shuttle Download PDFInfo
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- CN207791190U CN207791190U CN201820146835.1U CN201820146835U CN207791190U CN 207791190 U CN207791190 U CN 207791190U CN 201820146835 U CN201820146835 U CN 201820146835U CN 207791190 U CN207791190 U CN 207791190U
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- 238000009434 installation Methods 0.000 description 28
- 125000006850 spacer group Chemical group 0.000 description 7
- 238000000034 method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
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Abstract
Description
技术领域technical field
本实用新型涉及航空用具技术领域,具体涉及一种用于航空飞机的可调节式地面固定脚架。The utility model relates to the technical field of aviation appliances, in particular to an adjustable ground fixed tripod for aviation aircraft.
背景技术Background technique
飞机是指具有一具或多具发动机的动力装置产生前进的推力或拉力,由机身的固定机翼产生升力,在大气层内飞行的重于空气的航空器。飞机是最常见的一种固定翼航空器。按照其使用的发动机类型又可被分为喷气飞机和螺旋桨飞机。自从飞机实用新型以后,飞机日益成为现代文明不可缺少的交通工具。它深刻的改变和影响了人们的生活,开启了人们征服蓝天历史。Aircraft refers to a heavier-than-air aircraft that has one or more engines to generate forward thrust or pull, and the fixed wings of the fuselage to generate lift, and fly in the atmosphere. Airplanes are the most common type of fixed-wing aircraft. According to the type of engine it uses, it can be divided into jet aircraft and propeller aircraft. Since the utility model of the aircraft, the aircraft has increasingly become an indispensable means of transportation for modern civilization. It has profoundly changed and influenced people's lives, and opened the history of people conquering the blue sky.
飞机在降落后通常需要定位停放,在空气流动较大时,容易将飞机移位,原有的飞机定位装置,只能够特定飞机使用专有轮胎定位设备,临时维修,如不能使用匹配的轮胎定位设备,则导致无法及时使用。The aircraft usually needs to be positioned and parked after landing. When the air flow is large, it is easy to shift the aircraft. The original aircraft positioning device can only use the special tire positioning equipment for specific aircraft. For temporary maintenance, if the matching tire positioning cannot be used equipment, it cannot be used in a timely manner.
实用新型内容Utility model content
本实用新型的目的就是为了克服上述现有技术存在的缺陷而提供一种适用范围广的用于航空飞机的可调节式地面固定脚架。The purpose of this utility model is to provide an adjustable ground fixed foot stand for aviation aircraft with a wide range of application in order to overcome the above-mentioned defects in the prior art.
本实用新型的目的可以通过以下技术方案来实现:一种用于航空飞机的可调节式地面固定脚架,该脚架包括固定在地面的安装底板、滑动连接在安装底板一侧的左限位挡板以及转动设置在安装底板另一端的右限位挡板,航天飞机固定时,航天飞机的轮胎卡设在左限位挡板、安装底板以及右限位挡板形成的限位槽中。本实用新型通过左限位挡板的滑动来调节限位槽的宽度,从而可以适用于不同尺寸的飞机轮胎。The purpose of this utility model can be achieved through the following technical proposals: an adjustable ground fixed stand for aviation aircraft, the stand includes a mounting base plate fixed on the ground, a left limiter slidingly connected to one side of the mounting base plate The baffle plate and the right spacer baffle that is installed at the other end of the bottom plate are rotated. When the space shuttle is fixed, the tires of the space shuttle are stuck in the spacer slots formed by the left spacer plate, the installation base plate and the right spacer plate. The utility model adjusts the width of the limiting groove through the sliding of the left limiting baffle, so that it can be applied to aircraft tires of different sizes.
飞机所述安装底板一端设有长条形的滑槽,沿着滑槽长度方向且位于滑槽两侧的安装底板上设有两排定位孔,所述安装底板的另一端设有收纳槽,所述收纳槽的内壁两侧设有两块定位板,所述左限位挡板滑动连接在滑槽中,所述右限位挡板转动安装在收纳槽中。One end of the mounting base plate of the aircraft is provided with a strip-shaped chute, two rows of positioning holes are arranged on the mounting base plate along the length direction of the chute and located on both sides of the chute, and the other end of the mounting base plate is provided with a storage slot. Two positioning plates are arranged on both sides of the inner wall of the storage groove, the left limit baffle is slidably connected in the chute, and the right limit baffle is rotatably installed in the storage groove.
所述左限位挡板包括底部的滑块、顶部的挡块以及设置在滑块和挡块之间的支撑板,所述滑块与滑槽相匹配且滑动连接在滑槽中,所述支撑板上设有螺孔。其中,滑块的材质优选为镀锌不锈钢,且挡块和支撑板之间可设有加强筋杆,增加结构强度。The left limit baffle includes a slider at the bottom, a stopper at the top, and a support plate arranged between the slider and the stopper, the slider matches the chute and is slidably connected in the chute, the The support plate is provided with screw holes. Wherein, the material of the slider is preferably galvanized stainless steel, and a reinforcing bar may be provided between the block and the support plate to increase the structural strength.
所述右限位挡板的厚度与两块定位板之间的距离相匹配,所述右限位挡板底边的一端设有销轴孔,并通过销轴与安装底板转动连接,所述右限位挡板底边的另一端设有限位孔,并通过螺栓与安装底板固定连接。当限位孔未通过螺栓与安装底板固定时,此时,整个右限位挡板仅通过销轴与安装底板连接,所以右限位挡板可以旋转;当限位孔通过螺栓与安装底板固定时,右限位挡板的底边有两个点与安装底板固定,所以整个右限位挡板固定。The thickness of the right limit baffle matches the distance between the two positioning plates, and one end of the bottom edge of the right limit baffle is provided with a pin hole, and is connected to the installation base plate through a pin rotation. The other end of the bottom edge of the right limit baffle is provided with a limit hole, and is fixedly connected with the installation base plate by bolts. When the limit hole is not fixed with the installation base plate through bolts, at this time, the entire right limit baffle is only connected with the installation base plate through the pin shaft, so the right limit baffle can rotate; when the limit hole is fixed with the installation base plate through bolts , the bottom edge of the right limit baffle has two points to be fixed with the installation base plate, so the whole right limit baffle is fixed.
所述右限位挡板中与底边设有销轴孔一端连接的一条侧边两侧设有限位板,所述限位板的厚度与定位板相同,且限位板上设有缓冲弹簧。In the right limit baffle, limit plates are arranged on both sides of a side connected to the end of the bottom edge with a pin hole, the thickness of the limit plate is the same as that of the positioning plate, and a buffer spring is arranged on the limit plate .
所述限位槽中左限位挡板和右限位挡板与安装底板的角度为钝角。The angle between the left limit baffle and the right limit baffle in the limit groove and the installation base plate is an obtuse angle.
与现有技术相比,本实用新型的有益效果体现在:该航空飞机用可调节式地面固定脚架,通过可调节的设计,通过调节的方式,适用于不同尺寸的轮胎固定,适用性较广,右限位挡板可以放下和抬起,方便轮胎的定位和自由移动,使用简单。Compared with the prior art, the beneficial effect of the utility model is reflected in that: the adjustable ground-fixed tripod for the aviation aircraft is suitable for fixing tires of different sizes through the adjustable design and the adjustment method, and the applicability is relatively high. The wide and right limit baffle can be lowered and lifted, which is convenient for tire positioning and free movement, and is easy to use.
附图说明Description of drawings
图1为本实用新型的总体结构示意图;Fig. 1 is the overall structural representation of the utility model;
图2为本实用新型安装底板的结构示意图;Fig. 2 is the structural representation of the installation base plate of the utility model;
图3为本实用新型左限位挡板的结构示意图;Fig. 3 is the structural representation of the left limit baffle of the utility model;
图4为本实用新型右限位挡板的结构示意图。Fig. 4 is a schematic structural view of the right limit baffle of the present invention.
其中,1为安装底板,2为滑槽,3为定位孔,4为左限位挡板,5为支撑板,6为滑块,7为收纳槽,8为定位板,9为右限位挡板,10为销轴孔,11为限位孔,12为限位板,13为缓冲弹簧,14为手柄,15为挡块,16为加强筋杆,17为限位槽。Among them, 1 is the installation bottom plate, 2 is the chute, 3 is the positioning hole, 4 is the left limit baffle, 5 is the support plate, 6 is the slider, 7 is the storage groove, 8 is the positioning plate, 9 is the right limit Baffle plate, 10 is bearing pin hole, and 11 is spacing hole, and 12 is spacing plate, and 13 is cushioning spring, and 14 is handle, and 15 is block, and 16 is rib bar, and 17 is spacing slot.
具体实施方式Detailed ways
下面对本实用新型的实施例作详细说明,本实施例在以本实用新型技术方案为前提下进行实施,给出了详细的实施方式和具体的操作过程,但本实用新型的保护范围不限于下述的实施例。The following is a detailed description of the embodiments of the present utility model. This embodiment is implemented on the premise of the technical solution of the present utility model, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present utility model is not limited to the following the described embodiment.
实施例1Example 1
一种用于航空飞机的可调节式地面固定脚架,该脚架包括固定在地面的安装底板1、滑动连接在安装底板1一侧的左限位挡板4以及转动设置在安装底板1另一端的右限位挡板9,航天飞机固定时,航天飞机的轮胎卡设在左限位挡板4、安装底板1以及右限位挡板9形成的限位槽17中,如图1所示。An adjustable ground fixed tripod for aviation aircraft, the tripod includes a mounting base plate 1 fixed on the ground, a left limit baffle 4 slidably connected to one side of the mounting base plate 1, and a left limit baffle 4 which is rotatably arranged on the other side of the mounting base plate 1 The right limit baffle 9 at one end, when the space shuttle is fixed, the tire of the space shuttle is set in the limit groove 17 formed by the left limit baffle 4, the installation base plate 1 and the right limit baffle 9, as shown in Figure 1 Show.
飞机安装底板1一端设有长条形的滑槽2,沿着滑槽2长度方向且位于滑槽2两侧的安装底板1上设有两排定位孔3,安装底板1的另一端设有收纳槽7,收纳槽7的内壁两侧设有两块定位板8,左限位挡板4滑动连接在滑槽2中,右限位挡板9转动安装在收纳槽7中,如图2所示。One end of the aircraft installation base plate 1 is provided with a strip-shaped chute 2, along the length direction of the chute 2 and located on the installation base plate 1 on both sides of the chute 2, two rows of positioning holes 3 are provided, and the other end of the installation base plate 1 is provided with Storage groove 7, two positioning plates 8 are provided on both sides of the inner wall of storage groove 7, left limit baffle 4 is slidably connected in chute 2, and right limit baffle 9 is installed in storage groove 7 by rotation, as shown in Figure 2 shown.
左限位挡板4包括底部的滑块6、顶部的挡块15以及设置在滑块6和挡块15之间的支撑板5,滑块6与滑槽2相匹配且滑动连接在滑槽2中,支撑板5上设有螺孔。其中,滑块6的材质优选为镀锌不锈钢,且挡块15和支撑板5之间可设有加强筋杆16,增加结构强度,如图3所示。The left limit baffle 4 includes a slide block 6 at the bottom, a stop block 15 at the top, and a support plate 5 arranged between the slide block 6 and the block 15. The slide block 6 matches the chute 2 and is slidably connected to the chute 2, the support plate 5 is provided with screw holes. Wherein, the material of the slider 6 is preferably galvanized stainless steel, and a reinforcing bar 16 may be provided between the stopper 15 and the support plate 5 to increase the structural strength, as shown in FIG. 3 .
右限位挡板9的厚度与两块定位板8之间的距离相匹配,右限位挡板9底边的一端设有销轴孔10,并通过销轴与安装底板1转动连接,右限位挡板9底边的另一端设有限位孔11,并通过螺栓与安装底板1固定连接。当限位孔11未通过螺栓与安装底板1固定时,此时,整个右限位挡板9仅通过销轴与安装底板1连接,所以右限位挡板9可以旋转;当限位孔11通过螺栓与安装底板1固定时,右限位挡板9的底边有两个点与安装底板1固定,所以整个右限位挡板9固定。右限位挡板9中与底边设有销轴孔10一端连接的一条侧边两侧设有限位板12,限位板12的厚度与定位板8相同,且限位板12上设有缓冲弹簧13。右限位挡板9的顶端设有手柄14,如图4所示,The thickness of the right limit baffle 9 is matched with the distance between two positioning plates 8, and one end of the bottom of the right limit baffle 9 is provided with a pin hole 10, and is connected with the installation base plate 1 by pin shaft rotation, the right The other end of the bottom edge of the limit baffle plate 9 is provided with a limit hole 11, and is fixedly connected with the installation base plate 1 by bolts. When the limit hole 11 is not fixed with the installation base plate 1 by bolts, at this moment, the whole right limit baffle 9 is only connected with the installation base 1 through the pin shaft, so the right limit baffle 9 can rotate; when the limit hole 11 When fixing with the installation base plate 1 by bolts, there are two points fixed with the installation base plate 1 on the bottom edge of the right limit baffle 9, so the whole right limit baffle 9 is fixed. In the right limit baffle plate 9, a limit plate 12 is provided on a side that is connected to one end of the pin hole 10 with the bottom edge, and the limit plate 12 has the same thickness as the positioning plate 8, and the limit plate 12 is provided with Buffer spring 13. The top of the right limit baffle 9 is provided with a handle 14, as shown in Figure 4,
限位槽17中左限位挡板4和右限位挡板9与安装底板1的角度为钝角。The angle between the left limit baffle 4 and the right limit baffle 9 in the limit groove 17 and the installation base plate 1 is an obtuse angle.
使用前,地面开设凹槽,凹槽的略小于安装底板1的尺寸,凹槽的上端边缘处环向开设较浅边槽,将安装底板1放置在凹槽上,使得安装底板1的边缘嵌入在边槽内,且安装底板1与地面保持水平,将安装底板1的四角通过固定在凹槽上端的边槽内。当飞机即将需要固定时,取下限位孔11与安装底板1之间的螺栓,在重力的作用下,右限位挡板9顺时针转动,使得限位板12支撑在定位板8板上,缓冲弹簧13起到缓冲的作用,从而限位板12与安装底板1的上表面在同一平面上,飞机的轮胎可以从右至左进入左限位挡板4与右限位挡板9之间,调整位置后,通过手柄14将右限位挡板9提起,并通过限位螺栓将限位孔11与安装底板1固定,飞机轮胎在左限位挡板4与右限位挡板9的作用下无法移动。当飞机的轮胎尺寸较大或者较小时,取下支撑板5上的螺栓,横向移动左限位挡板4,调整到合适的位置将支撑板5通过定位螺栓再次与安装底板1固定即可。Before use, a groove is opened on the ground, the groove is slightly smaller than the size of the installation base plate 1, and a shallower side groove is opened around the upper edge of the groove, and the installation base plate 1 is placed on the groove so that the edge of the installation base plate 1 is embedded In the side groove, and the installation base plate 1 is kept level with the ground, the four corners of the installation base plate 1 are fixed in the side groove at the upper end of the groove. When the aircraft is about to be fixed, remove the bolt between the spacer hole 11 and the mounting base plate 1, and under the action of gravity, the right spacer baffle 9 rotates clockwise, so that the spacer plate 12 is supported on the positioning plate 8, Buffer spring 13 plays the effect of buffering, thereby limit plate 12 and the upper surface of mounting base plate 1 are on the same plane, and the tire of aircraft can enter between left limit baffle 4 and right limit baffle 9 from right to left , after adjusting the position, the right limit baffle 9 is lifted by the handle 14, and the limit hole 11 is fixed to the installation base plate 1 by the limit bolt, and the aircraft tire is positioned between the left limit baffle 4 and the right limit baffle 9. Unable to move under the effect. When the tire size of the aircraft is larger or smaller, take off the bolts on the support plate 5, move the left limit baffle 4 laterally, adjust to a suitable position and fix the support plate 5 with the installation base plate 1 again through the positioning bolts.
Claims (6)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820146835.1U CN207791190U (en) | 2018-01-29 | 2018-01-29 | Tripod is fixed on a kind of adjustable ground for space shuttle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201820146835.1U CN207791190U (en) | 2018-01-29 | 2018-01-29 | Tripod is fixed on a kind of adjustable ground for space shuttle |
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| CN207791190U true CN207791190U (en) | 2018-08-31 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112644740A (en) * | 2020-12-31 | 2021-04-13 | 中国科学院长春光学精密机械与物理研究所 | Locking mechanism of aerospace device |
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2018
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112644740A (en) * | 2020-12-31 | 2021-04-13 | 中国科学院长春光学精密机械与物理研究所 | Locking mechanism of aerospace device |
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