CN1923618A - Double gasbag buffer unit - Google Patents
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- CN1923618A CN1923618A CN 200610032294 CN200610032294A CN1923618A CN 1923618 A CN1923618 A CN 1923618A CN 200610032294 CN200610032294 CN 200610032294 CN 200610032294 A CN200610032294 A CN 200610032294A CN 1923618 A CN1923618 A CN 1923618A
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- 239000004744 fabric Substances 0.000 description 13
- 230000003139 buffering effect Effects 0.000 description 9
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- 230000006835 compression Effects 0.000 description 2
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- 238000007789 sealing Methods 0.000 description 2
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Abstract
本发明公开了一种双气室气囊缓冲装置,它包括气囊体,所述气囊体由上至下分为各自独立的气囊顶气室和气囊底气室。气囊顶气室为封闭气室,气囊底气室上开设有底气室排气孔。气囊顶气室具有中间薄边沿厚的气室形状,气囊底气室气室较厚、容积较大。本发明是一种结构简单、操作简便、成本低廉、能够有效解决轻型精密空投设备缓冲着陆过程中的反弹、翻覆以及设备直接触地等问题的双气室气囊缓冲装置。
The invention discloses a double-chamber airbag cushioning device, which comprises an airbag body, and the airbag body is divided into independent airbag top chambers and airbag bottom chambers from top to bottom. The top air chamber of the airbag is a closed air chamber, and the bottom air chamber of the airbag is provided with vent holes for the bottom air chamber. The top air chamber of the airbag has the shape of an air chamber with a thin middle edge and thick edges, and the air chamber at the bottom of the airbag is thicker and has a larger volume. The invention is a double-chamber airbag cushioning device with simple structure, easy operation and low cost, which can effectively solve the problems of rebounding, overturning and direct contact of the equipment during the landing process of light precision airdrop equipment.
Description
技术领域technical field
本发明主要涉及到气囊式缓冲设备领域,特指一种可用来有效保护轻型精密空投设备安全着陆的双气室气囊缓冲装置。The invention mainly relates to the field of airbag buffer equipment, in particular to a double-chamber airbag buffer device that can effectively protect light precision airdrop equipment from landing safely.
背景技术Background technique
现有技术中常利用气囊式缓冲设备对空投设备安全着陆进行有效保护,例如无人驾驶侦察飞机等轻型精密设备的安全着陆常用到缓冲防护气囊,其关键技术是既要具有缓冲防护作用,又要防止出现反弹、翻覆以及空投设备直接触地的问题。现有的空降缓冲气囊中,大部分采用结构单一的单室气囊装置,此类气囊装置在缓冲过程中,总是存在空投设备直接触地或是大反弹甚至翻覆的问题,而且在设计中这些技术难点是相互制衡的。假如利用大排气来防止大反弹,就很容易导致空投设备直接触地;假如采用小排气来防止空投设备触地,则往往会降低缓冲效果和导致大反弹甚至翻覆现象。采用单一气室的气囊时,这两种矛盾往往很难协调解决。In the prior art, airbag buffer equipment is often used to effectively protect the safe landing of airdrop equipment. For example, cushioning and protective airbags are often used for the safe landing of light precision equipment such as unmanned reconnaissance aircraft. Prevent rebounding, overturning, and airdrop equipment directly touching the ground. Most of the existing airborne cushioning airbags use a single-chamber airbag device with a single structure. During the buffering process of this type of airbag device, there are always problems that the airdrop equipment directly touches the ground or rebounds or even overturns. Technical difficulties are mutual checks and balances. If a large exhaust is used to prevent a large rebound, it is easy to cause the airdrop device to touch the ground directly; if a small exhaust is used to prevent the airdrop device from touching the ground, it will often reduce the buffering effect and cause a large rebound or even overturn. When adopting the air bag of single air chamber, these two kinds of contradictions are often difficult to coordinate and solve.
发明内容Contents of the invention
本发明要解决的技术问题就在于:针对现有技术存在的技术问题,本发明提供一种结构简单、操作简便、成本低廉、能够有效解决轻型精密空投设备缓冲着陆过程中的反弹、翻覆以及设备直接触地等问题的双气室气囊缓冲装置。The technical problem to be solved by the present invention is: aiming at the technical problems existing in the prior art, the present invention provides a simple structure, easy operation, low cost, which can effectively solve the rebound, overturn and equipment during the buffer landing process of light precision airdrop equipment. Double-chamber airbag cushioning device for problems such as direct contact with the ground.
为解决上述技术问题,本发明提出的解决方案为:一种双气室气囊缓冲装置,它包括气囊体,其特征在于:所述气囊体由上至下分为各自独立的气囊顶气室和气囊底气室,气囊顶气室为封闭气室,气囊底气室上开设有底气室排气孔。In order to solve the above-mentioned technical problems, the solution proposed by the present invention is: a double-chamber airbag cushioning device, which includes an airbag body, which is characterized in that: the airbag body is divided into independent airbag top chambers and airbag top chambers from top to bottom. The bottom air chamber of the airbag and the top air chamber of the airbag are closed air chambers, and the bottom air chamber of the airbag is provided with vent holes for the bottom air chamber.
所述气囊顶气室的厚度L1小于气囊底气室的厚度L2。The thickness L 1 of the top chamber of the airbag is smaller than the thickness L 2 of the bottom chamber of the airbag.
所述气囊顶气室的形状为中间薄、边沿厚。The shape of the top air chamber of the airbag is thin in the middle and thick in the edges.
所述气囊顶气室和气囊底气室上分别设有用来调整气囊体形状的顶气室拉布和底气室拉布,顶气室拉布和底气室拉布内开设有气室连通孔。The airbag top air chamber and the air bag bottom air chamber are respectively provided with a top air chamber cloth and a bottom air chamber cloth for adjusting the shape of the air bag body, and air chamber communication holes are opened in the top air chamber cloth and the bottom air chamber cloth.
与现有技术相比,本发明的优点就在于:Compared with the prior art, the present invention has the advantages of:
1、本发明的气囊体上采用气囊顶气室和气囊底气室的双室设计,刚柔兼并,利用两个气室共同作用,两气室的体积、充气压力以及底气室的排气量和排气速度可以根据不同的空投设备和空投任务进行优化设计,能很好地满足不同的空投设备的缓冲保护要求,特别适合诸如无人驾驶侦察飞机等轻型精密设备安全着陆的防护;1. The airbag body of the present invention adopts the dual-chamber design of the top air chamber of the air bag and the bottom air chamber of the air bag, which combines rigidity and softness, and utilizes the joint action of the two air chambers. The volume of the two air chambers, the inflation pressure and the displacement and The exhaust speed can be optimized according to different airdrop equipment and airdrop tasks, which can well meet the buffer protection requirements of different airdrop equipment, especially suitable for the safe landing protection of light precision equipment such as unmanned reconnaissance aircraft;
2、本发明的双气室气囊缓冲装置结构简单、成本低廉、适合大规模生产使用,同时该装置在充气前所占空间小,着陆后方便泄气存放。气囊顶气室上非排气的密封特点是始终防止空投设备直接着地,气囊顶气室具有中间薄边沿厚的气室形状,具有防止空投设备翻覆的作用。气室较厚、容积较大的气囊底气室在缓冲过程中通过底气室排气孔向外界实现大排气并保障必要的缓冲作用时间,既起到有效的缓冲作用,又同时防止产生反弹。因此,本发明的双气室气囊缓冲装置能有效解决单一气室缓冲气囊所存在的大反弹、空投设备翻覆或直接触地的关键技术问题。2. The double-chamber airbag cushioning device of the present invention has simple structure, low cost, and is suitable for large-scale production and use. At the same time, the device occupies a small space before inflating, and is convenient for deflated storage after landing. The non-exhaust sealing feature on the top air chamber of the airbag is to always prevent the airdrop equipment from directly landing on the ground. The top air chamber of the airbag has a shape of an air chamber with a thin middle edge and a thick edge, which can prevent the airdrop equipment from overturning. The base air chamber of the airbag with a thicker air chamber and a larger volume realizes a large exhaust to the outside through the vent hole of the base air chamber during the buffering process and ensures the necessary buffering time, which not only plays an effective buffering role, but also prevents rebound. Therefore, the double-chamber airbag cushioning device of the present invention can effectively solve the key technical problems of the single-chamber cushioning airbag such as large rebound, overturning of airdrop equipment or direct ground contact.
附图说明Description of drawings
图1是本发明的结构示意图;Fig. 1 is a structural representation of the present invention;
图2是图1中A-A处的剖视示意图;Fig. 2 is a schematic cross-sectional view at A-A in Fig. 1;
图3是图1中B-B处的剖视示意图。Fig. 3 is a schematic cross-sectional view at B-B in Fig. 1 .
图例说明illustration
1、气囊顶气室 2、气囊底气室1. Airbag
3、顶气室拉布 4、底气室拉布3. Top air
5、底气室排气孔 6、气室连通孔5. Vent hole in the
7、气囊体 8、加厚边沿7.
具体实施方式Detailed ways
以下将结合附图和具体实施例对本发明做进一步详细说明。The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.
如图1、图2和图3所示,本发明双气室气囊缓冲装置,它包括气囊体7,该气囊体7采用有一定强度、密闭性好的纤维布料制做而成,无其它机械辅件或填充材料,只利用成本低廉而且环保的空气对空投设备进行全方位有效保护。根据实际工况的需要,气囊体7可以设计成圆形、方形、椭圆形或其他形状。气囊体7由上至下分为各自独立的气囊顶气室1和气囊底气室2,气囊顶气室1为封闭气室,不对外排气,气囊底气室2上开设有底气室排气孔5,底气室排气孔5处可设有单向排气阀,底气室排气孔5的个数以及孔径可根据不同的空投任务进行优化设计。气囊顶气室1的厚度L1小于气囊底气室2的厚度L2,本实施例中,气囊顶气室1的形状为中间薄、边沿厚,其结构特征具有防翻覆的作用。气囊顶气室1的气室较薄、容积较小是防止发生明显的反弹,其呈封闭状和非排气的密封特点则是始终防止空投设备直接着地。气囊底气室2的气室较厚、容积较大,其结构特征可以解决大排气和缓冲作用时间短之间的矛盾,而大排气防止发生反弹的关键技术,必要的缓冲作用时间则保障缓冲作用效果。气囊顶气室1和气囊底气室2相连但不连通,各自充气质量可根据不同的工况进行优化选择,使其满足各自任务的实际需要。气囊底气室2在缓冲过程中通过底气室排气孔5向外界排气。本实施例中,气囊顶气室1和气囊底气室2上分别设有用来调整气囊体7形状的顶气室拉布3和底气室拉布4,顶气室拉布3和底气室拉布4内开设有气室连通孔6,气室连通孔6使各自气室内的气体能够自由流动。气囊顶气室1和气囊底气室2充气后的形状分别通过顶气室拉布3和底气室拉布4进行控制,气囊顶气室1和气囊底气室2的容积大小结合实际工况进行优化设计。在空投设备的着陆缓冲过程中,由于气囊底气室2通过底气室排气孔5处的单向排气阀对外排气,在着陆瞬间,单向排气阀由于气囊压缩导致内部气压增大而开启,气囊对外排气,可迅速释放出由于气体急剧压缩而瞬间积聚的内能,起到减小气囊刚度的作用,进而可增强缓冲效果,而经优化设计的排气量和排气速度使气囊底气室2具有防止大反弹的作用。而此时封闭型的气囊顶气室1则起到联合缓冲作用,为防止空投设备翻覆而设计的结构及其经优化设计的气囊顶气室1厚度使其具有防止空投设备直接触地的作用。As shown in Figure 1, Figure 2 and Figure 3, the double-chamber airbag cushioning device of the present invention includes an airbag body 7, which is made of fiber cloth with a certain strength and good airtightness, without other mechanical Auxiliary parts or filling materials, only use low-cost and environmentally friendly air to effectively protect the airdrop equipment in all directions. According to the needs of actual working conditions, the airbag body 7 can be designed as a circle, a square, an ellipse or other shapes. The airbag body 7 is divided into independent airbag top air chamber 1 and airbag
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103448911A (en) * | 2013-09-16 | 2013-12-18 | 金陵科技学院 | Extreme low-altitude drop device |
| CN105307934A (en) * | 2013-05-29 | 2016-02-03 | 库克基金会 | Aerial delivery system |
| CN105984596A (en) * | 2015-10-14 | 2016-10-05 | 北京强度环境研究所 | Multi-air-chamber exhaust type recovery air bag |
| CN107640319A (en) * | 2017-10-31 | 2018-01-30 | 航宇救生装备有限公司 | A kind of air-drop type gravity type air bag with buffering efficiency |
| CN107813981A (en) * | 2017-12-14 | 2018-03-20 | 江苏永钢集团有限公司 | A kind of baling press weighting distribution wheel buffer unit |
| CN109250135A (en) * | 2018-09-29 | 2019-01-22 | 长光卫星技术有限公司 | A kind of unmanned plane and load guard system |
| CN113799983A (en) * | 2021-10-27 | 2021-12-17 | 江西洪都航空工业股份有限公司 | Multilayer air bag type air-drop buffering device |
| CN114852522A (en) * | 2022-04-14 | 2022-08-05 | 河北汉光重工有限责任公司 | Buffer protection device for caster of airdrop material platform |
-
2006
- 2006-09-22 CN CN 200610032294 patent/CN1923618A/en active Pending
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105307934A (en) * | 2013-05-29 | 2016-02-03 | 库克基金会 | Aerial delivery system |
| CN105307934B (en) * | 2013-05-29 | 2018-07-13 | 库克基金会 | Aerial delivery system |
| CN103448911A (en) * | 2013-09-16 | 2013-12-18 | 金陵科技学院 | Extreme low-altitude drop device |
| CN105984596A (en) * | 2015-10-14 | 2016-10-05 | 北京强度环境研究所 | Multi-air-chamber exhaust type recovery air bag |
| CN107640319A (en) * | 2017-10-31 | 2018-01-30 | 航宇救生装备有限公司 | A kind of air-drop type gravity type air bag with buffering efficiency |
| CN107813981A (en) * | 2017-12-14 | 2018-03-20 | 江苏永钢集团有限公司 | A kind of baling press weighting distribution wheel buffer unit |
| CN109250135A (en) * | 2018-09-29 | 2019-01-22 | 长光卫星技术有限公司 | A kind of unmanned plane and load guard system |
| CN113799983A (en) * | 2021-10-27 | 2021-12-17 | 江西洪都航空工业股份有限公司 | Multilayer air bag type air-drop buffering device |
| CN114852522A (en) * | 2022-04-14 | 2022-08-05 | 河北汉光重工有限责任公司 | Buffer protection device for caster of airdrop material platform |
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Open date: 20070307 |