CN111504897A - Airplane wheel arresting test system based on similar theory - Google Patents
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Abstract
一种基于相似理论的机轮拦阻测试系统。其包括加载系统、拦阻材料运送系统和电机传动系统:本发明提供的基于相似理论的机轮拦阻测试系统具有的优点和积极效果是:体积小巧,基于相似理论进行试验,与同等级真机试验相比,可极大降低研究成本;可以对不同负载及运动速度下的机轮受到的拦阻系统阻拦力进行测试,同时研究不同拦阻材料的拦阻效果。可为保障机场跑道安全提供技术测试手段,为开发出新型拦阻材料服务。
A wheel arresting test system based on similarity theory. It includes a loading system, an arresting material conveying system, and a motor drive system: the wheel arresting test system based on the similarity theory provided by the present invention has the advantages and positive effects: the volume is small, and the test based on the similarity theory is comparable to the real machine test of the same level. Compared with this, the research cost can be greatly reduced; the blocking force of the blocking system on the wheel under different loads and moving speeds can be tested, and the blocking effect of different blocking materials can be studied at the same time. It can provide technical testing means for ensuring the safety of airport runways and serve for the development of new types of arresting materials.
Description
技术领域technical field
本发明属于机场工程技术领域,特别是涉及一种基于相似理论的机轮拦阻测试系统。The invention belongs to the technical field of airport engineering, in particular to a wheel arresting test system based on similarity theory.
背景技术Background technique
随着现代航空运输业的需求逐渐增大,飞机冲出跑道的事故已有发生,因此成为航空事故中威胁较大的问题之一。特性材料拦阻系统(简称EMAS)则是一种有效的民机拦阻系统,EMAS的应用能够提供与标准跑道端安全区相同的安全保障,以节省机场用于跑道端安全区的土地面积,有利于增强机场保障能力。但是EMAS的性能、飞机的速度、飞机的重量等都对拦阻系统有着重要的影响。由于项目的特殊性,真机实验难度大,费用高,因此很难进行实际试验,目前的研究中多数是有限元模拟。中国专利公开号CN102854129A中提供了一种用于飞机阻拦系统测试的装置,采用了真实的机轮和荷载,需要的实验场地大,成本也比较高。因此目前亟需一种可应用于实验室研究的小尺度的拦阻材料测试装置。With the increasing demand of the modern air transport industry, the accident of the aircraft overrunning the runway has already occurred, so it has become one of the most threatening problems in aviation accidents. The characteristic material arresting system (EMAS for short) is an effective civil aircraft arresting system. The application of EMAS can provide the same safety guarantee as the standard runway end safety area, so as to save the land area of the airport for the runway end safety area, which is beneficial to Enhance airport security capabilities. However, the performance of EMAS, the speed of the aircraft, the weight of the aircraft, etc. have an important impact on the arresting system. Due to the particularity of the project, the real machine experiment is difficult and expensive, so it is difficult to carry out the actual experiment. Most of the current research is finite element simulation. Chinese Patent Publication No. CN102854129A provides a device for testing an aircraft arresting system, which uses real wheels and loads, requires a large test site, and has a relatively high cost. Therefore, there is an urgent need for a small-scale barrier material testing device that can be applied to laboratory research.
发明内容SUMMARY OF THE INVENTION
为了解决上述问题,本发明的目的在于提供一种基于相似理论的机轮拦阻测试系统。In order to solve the above problems, the purpose of the present invention is to provide a wheel arresting test system based on the similar theory.
为了达到上述目的,本发明提供的基于相似理论的机轮拦阻测试系统包括加载系统、拦阻材料运送系统和电机传动系统:In order to achieve the above purpose, the wheel arresting test system based on the similar theory provided by the present invention includes a loading system, an arresting material conveying system and a motor drive system:
其中,所述的电机传动系统包括:导向轮、传动支架、绞盘、减速机、电机和拉力传感器;传动支架的下端设置在地面上,上部安装有同心设置的电机、减速机和绞盘,电机的输出轴连接减速机,减速机的输出轴连接在绞盘的中心孔内;导向轮设置在传动支架上位于绞盘前侧的部位;The motor transmission system includes: a guide wheel, a transmission bracket, a winch, a reducer, a motor and a tension sensor; the lower end of the transmission bracket is set on the ground, and the upper part is installed with a concentrically arranged motor, a reducer and a winch. The output shaft is connected to the reducer, and the output shaft of the reducer is connected to the center hole of the winch; the guide wheel is arranged on the transmission bracket at the front side of the winch;
所述的拦阻材料运输系统设置在电机传动系统的前方,包括拦阻材料层、拦阻测试车和钢绞线;拦阻测试车的车体为顶面和后端呈开口状的箱体,底面两侧部位设有多个滑轮,后端设有拉环;两根钢绞线的一端通过拉环连接在车体的后端两侧,另一端同时连接拉力传感器,拉力传感器的另一端利用另一根钢绞线通过导向轮缠绕在绞盘上;拦阻材料层铺设在拦阻测试车的车体前部;The arresting material transportation system is arranged in front of the motor transmission system, and includes an arresting material layer, an arresting test vehicle and a steel strand; the vehicle body of the arresting test vehicle is a box body with an open top and a rear end, and two sides of the bottom surface. There are a plurality of pulleys in the part, and the rear end is provided with a pull ring; one end of the two steel strands is connected to both sides of the rear end of the car body through the pull ring, and the other end is connected to the tension sensor at the same time, and the other end of the tension sensor uses another The steel strand is wound on the winch through the guide wheel; the blocking material layer is laid on the front of the body of the blocking test vehicle;
所述的加载系统包括加载架、加载篮、地脚螺栓、起落架机轮、激光位移传感器和机轮竖向传动系统;所述的加载架为桌式结构,下端通过地脚螺栓固定在位于拦阻测试车两侧的地面上,顶面中部形成有一个开孔;加载篮设置在加载架的正上方,内部用于放置加载砝码;机轮竖向传动系统的上端连接在加载篮的底面中部,中部贯穿加载架上的开孔,下端与起落架机轮的中心轴相连接;激光位移传感器安装在机轮竖向传动系统的侧面上,通过向加载架发射激光来测量起落架机轮的竖向位移。The loading system includes a loading frame, a loading basket, an anchor bolt, a landing gear wheel, a laser displacement sensor and a vertical transmission system of the wheel; the loading frame is a table-type structure, and the lower end is fixed at On the ground on both sides of the blocking test vehicle, an opening is formed in the middle of the top surface; the loading basket is set right above the loading frame, and the interior is used to place loading weights; the upper end of the vertical transmission system of the wheel is connected to the bottom surface of the loading basket The middle part runs through the opening on the loading frame, and the lower end is connected with the central axis of the landing gear wheel; the laser displacement sensor is installed on the side of the vertical transmission system of the wheel, and the landing gear wheel is measured by emitting laser light to the loading frame vertical displacement.
所述的电机采用可调速电机。The motor is a speed-adjustable motor.
所述的加载篮为正方体形钢结构箱体The loading basket is a cube-shaped steel structure box
本发明提供的基于相似理论的机轮拦阻测试系统具有的优点和积极效果是:体积小巧,基于相似理论进行试验,与同等级真机试验相比,可极大降低研究成本;可以对不同负载及运动速度下的机轮受到的拦阻系统阻拦力进行测试,同时研究不同拦阻材料的拦阻效果。可为保障机场跑道安全提供技术测试手段,为开发出新型拦阻材料服务。The wheel arresting test system based on the similarity theory provided by the present invention has the advantages and positive effects as follows: the volume is small, and the test based on the similarity theory can greatly reduce the research cost compared with the real machine test of the same level; At the same time, the blocking effect of different blocking materials is studied. It can provide technical testing means for ensuring the safety of airport runways and serve for the development of new types of arresting materials.
附图说明Description of drawings
图1为本发明提供的基于相似理论的机轮拦阻测试系统结构立体图;Fig. 1 is the structural perspective view of the wheel arresting test system based on similarity theory provided by the present invention;
图2为本发明提供的基于相似理论的机轮拦阻测试系统中传动支架结构正立面图;Fig. 2 is the front elevation view of the transmission support structure in the wheel arresting test system based on the similarity theory provided by the present invention;
具体实施方式Detailed ways
为进一步了解本发明的发明内容、特点及功效,例举以下实施例,并配合附图详细说明如下:In order to further understand the content of the invention, features and effects of the present invention, the following examples are given as examples, and are described in detail as follows in conjunction with the accompanying drawings:
如图1、图2所示,本发明提供的基于相似理论的机轮拦阻测试系统包括加载系统15、拦阻材料运送系统16和电机传动系统17:As shown in FIGS. 1 and 2 , the wheel arresting test system based on the similar theory provided by the present invention includes a
其中,所述的电机传动系统17包括:导向轮9、传动支架10、绞盘11、减速机12、电机13和拉力传感器8;传动支架10的下端设置在地面上,上部安装有同心设置的电机13、减速机12和绞盘11,电机13的输出轴连接减速机12,减速机12的输出轴连接在绞盘11的中心孔内;导向轮9设置在传动支架10上位于绞盘11前侧的部位;Wherein, the motor transmission system 17 includes: a guide wheel 9, a
所述的拦阻材料运输系统16设置在电机传动系统17的前方,包括拦阻材料层6、拦阻测试车7和钢绞线14;拦阻测试车7的车体为顶面和后端呈开口状的箱体,底面两侧部位设有多个滑轮,后端设有拉环;两根钢绞线14的一端通过拉环连接在车体的后端两侧,另一端同时连接拉力传感器8,拉力传感器8的另一端利用另一根钢绞线14通过导向轮9缠绕在绞盘11上;拦阻材料层6铺设在拦阻测试车7的车体前部;The described arresting
所述的加载系统15包括加载架1、加载篮2、地脚螺栓3、起落架机轮4、激光位移传感器5和机轮竖向传动系统18;所述的加载架1为桌式结构,下端通过地脚螺栓3固定在位于拦阻测试车7两侧的地面上,顶面中部形成有一个开孔;加载篮2设置在加载架1的正上方,内部用于放置加载砝码;机轮竖向传动系统18的上端连接在加载篮2的底面中部,中部贯穿加载架1上的开孔,下端与起落架机轮4的中心轴相连接;激光位移传感器5安装在机轮竖向传动系统18的侧面上,通过向加载架1发射激光来测量起落架机轮4的竖向位移。The
所述的电机13采用可调速电机。The
所述的加载篮2为正方体形钢结构箱体。The
采用相似理论进行设计,满足模型和原型的几何相似、质量相似、力学相似。The similarity theory is used for design to meet the geometric similarity, quality similarity and mechanical similarity between the model and the prototype.
本发明提供的基于相似理论的机轮拦阻测试系统的核心为起落架机轮与拦阻材料的相互作用,因此在进行系统相似设计时,需对其中的关键参数进行考虑。在实验系统中,设计独立的物理量有7个分别为:长度l、速度v、重力加速度g、密度ρ、力F、胎压p、混凝土强度fc。The core of the wheel arresting test system based on the similarity theory provided by the present invention is the interaction between the wheel of the landing gear and the arresting material. Therefore, when designing the similar system, the key parameters need to be considered. In the experimental system, seven independent physical quantities are designed: length l, velocity v, gravitational acceleration g, density ρ, force F, tire pressure p, concrete strength f c .
根据相似第一定理(π定理)和分析模型的特点,提出四个相似判据(无量纲)如下:According to the first similarity theorem (π theorem) and the characteristics of the analytical model, four similarity criteria (dimensionless) are proposed as follows:
其背后的物理意义为轮载系数、速度因数、胎压指数以及泡沫混凝土的轮载强度比。只有当模型试验和原型试验的上述四个判据均相同时,可认为模型和原型相似。The physical meaning behind it is the wheel load factor, speed factor, tire pressure index and the wheel load strength ratio of foam concrete. The model and prototype can be considered similar only when the above four criteria are the same for both the model test and the prototype test.
定义模型和原型的相似比(模型与原型的取值之比)分别为λl,λv,λg,λρ,λF,λp,λfc。由π定理及相似判据,若模型与原型相似,则有:The similarity ratio between the model and the prototype (the ratio of the value of the model to the prototype) is defined as λ l , λ v , λ g , λ ρ , λ F , λ p , λ fc , respectively. According to the π theorem and similarity criterion, if the model is similar to the prototype, there are:
在模型试验中,一般采用和原型同种材料,且在1g下进行试验,即有:In the model test, the same material as the prototype is generally used, and the test is carried out under 1g, that is:
λρ=λg=1 (2)λ ρ =λ g =1 (2)
故可以得到各量纲相似比之间的关系如下:Therefore, the relationship between the similarity ratios of various dimensions can be obtained as follows:
现将本发明提供的基于相似理论的机理拦阻测试系统的工作原理阐述如下:The working principle of the mechanism arresting test system based on the similar theory provided by the present invention is described as follows:
1.选取适宜重量的加载砝码并放置于加载篮2内,由此通过机轮竖向传动系统18下压起落架机轮4;1. Select a loading weight of suitable weight and place it in the
2.将拦阻测试车7放置在位于起落架机轮4前方的起始点,轴线对准标记线;2. Place the arresting test vehicle 7 at the starting point in front of the landing gear wheel 4, with the axis aligned with the marking line;
3.在拦阻测试车7的前部铺设一层所需测试的拦阻材料层6,并利用游标卡尺量测阻拦材料层6的初始厚度;3. Lay a layer of blocking material layer 6 to be tested on the front of the blocking test vehicle 7, and use a vernier caliper to measure the initial thickness of the blocking material layer 6;
4.开启激光位移传感器5及拉力传感器8;4. Turn on the laser displacement sensor 5 and the tension sensor 8;
5.设定电机13的转速,启动电机13,通过减速机12带动绞盘11转动,由此通过钢绞线14拉动拦阻测试车7向后运动,直到起落架机轮4全部压过拦阻材料层6为止;5. Set the speed of the
6.在拉动拦阻测试车7运动过程中,利用激光位移传感器5及拉力传感器8分别采集起落架机轮4的竖向位移和钢绞线14的牵引力;6. During the movement of the pulling and arresting test vehicle 7, use the laser displacement sensor 5 and the tension sensor 8 to collect the vertical displacement of the landing gear wheel 4 and the traction force of the
7.关闭电机13,停止激光位移传感器5及拉力传感器8的数据采集且进行记录;7. Turn off the
8.从加载篮2内卸去加载砝码,这时加载系统15中的加载篮2、机轮竖向传动系统18和起落架机轮4将提升至拦阻测试车7的上方;8. Unload the loading weight from the
9.反转电机13而将拦阻测试车7推回到原始位置;9. Reverse the
10.测量拦阻材料层6的压实厚度,之后选取四个位置算出平均值。10. Measure the compacted thickness of the barrier material layer 6, and then select four positions to calculate the average value.
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|---|---|---|---|---|
| CN102854129A (en) * | 2012-08-06 | 2013-01-02 | 中国民航科学技术研究院 | Verification testing experiment device and experiment method for aircraft arresting systems |
| US20170356137A1 (en) * | 2016-06-10 | 2017-12-14 | Daniel Webber | Engineered Material Arrestor System |
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- 2020-05-06 CN CN202010373285.9A patent/CN111504897A/en active Pending
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| CN102854129A (en) * | 2012-08-06 | 2013-01-02 | 中国民航科学技术研究院 | Verification testing experiment device and experiment method for aircraft arresting systems |
| US20170356137A1 (en) * | 2016-06-10 | 2017-12-14 | Daniel Webber | Engineered Material Arrestor System |
| CN108362638A (en) * | 2017-12-06 | 2018-08-03 | 中国飞机强度研究所 | A kind of arresting system dynamic energy absorption characteristics experimental provision and experimental method |
| CN110078437A (en) * | 2019-04-10 | 2019-08-02 | 中国建筑材料科学研究总院有限公司 | A kind of airfield runway elastomeric material arresting system and preparation method thereof and test device |
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Application publication date: 20200807 |