|Publication number||CN102213638 B|
|Application number||CN 201010142621|
|Publication date||24 Apr 2013|
|Filing date||9 Apr 2010|
|Priority date||9 Apr 2010|
|Also published as||CN102213638A|
|Publication number||201010142621.5, CN 102213638 B, CN 102213638B, CN 201010142621, CN-B-102213638, CN102213638 B, CN102213638B, CN201010142621, CN201010142621.5|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (4), Classifications (1), Legal Events (3)|
|External Links: SIPO, Espacenet|
具有内外腔的闭式循环的风洞系统 Inside and outside the cavity with a closed loop wind tunnel system
 在提交本发明申请的同时，申请人还提交了与本发明申请相对应的实用新型申请。  In the present invention, while filing, the applicant also submitted with the application of the present invention corresponding to Utility Model Application.
 本发明涉及用于运动娱乐的风洞，尤其涉及具有内外腔的闭式循环的风洞系统。  The present invention relates to a wind tunnel for sports and entertainment, and more particularly to systems having inner and outer chambers of the wind tunnel in a closed cycle. 背景技术 BACKGROUND
 风洞是能人工产生和控制气流的实验设备，用于空气动力学方面的研发。  The wind tunnel is capable of artificial flow generation and control laboratory equipment for research and development of aerodynamics. 垂直风洞可以产生垂直向上的气流，主要用于航空器研发、跳伞模拟训练。 Vertical wind tunnel can produce a vertical upward flow, mainly for aircraft development, skydiving simulation training. 上世纪九十年代以来，随着极限运动的兴起，跳伞模拟训练开始演化成一种新型的体育娱乐运动：利用垂直风洞产生的竖直方向的气流平衡人体重力达到飞翔的目的，实现人体空中自由飞行，利用现代高科技给普通大众带来空中极限运动的体验。 Since the 1990s, with the rise of extreme sports, skydiving simulation training start evolved into a new kind of sports entertainment sport: the use of a vertical direction perpendicular to the wind tunnel airflow generated by gravity to achieve the balance of the body to fly the purpose of achieving human freedom air flight, the use of modern high-tech experience to the general public to bring the air of extreme sports. 用于体育娱乐的垂直风洞，因此又称为娱乐风洞。 Vertical wind tunnel used for sports and entertainment, so-called entertainment wind tunnel. 进入二十一世纪，这项体育娱乐运动在全世界范围内迅速兴起，投资建设的娱乐风洞项目也迅速增加。 Into the twenty-first century, the rapid rise in the sports and entertainment sport worldwide entertainment wind tunnel project investment and construction is also increasing rapidly.
 传统的风洞采用气流大回合循环的方式来实现。  Traditional wind tunnel air flow by way of a large round loop to achieve. 在考察了相关娱乐风洞制造商的产品或工程后，我们发现现有的娱乐风洞普遍存在问题：投资成本高，基本上超过数千万元；施工周期长，基本上需要12个月以上。 After reviewing the relevant entertainment wind tunnel manufacturer's product or project, we found that the prevalence of current entertainment wind tunnel problem: the high cost of investment, basically more than tens of millions; long construction period, basically need 12 months or more . 因此，开发新型的、经济的、安装迅速的娱乐风洞成为市场的需求。 Therefore, the development of new, economical, quick to install wind tunnel became entertainment needs of the market.
 针对上述现有技术中存在的问题，本发明的一个目的是提供一种总占地面积较小的风洞系统。  In response to these problems of the prior art, an object of the invention is to provide a total area of small wind tunnel system.
 本发明的另一个目的是提供一种具有新型动力系统的风洞系统。  Another object of the present invention is to provide a system having a new power wind tunnel system.
 本发明的再一个目的是提供一种能够快速安装的风洞系统。  It is a further object of the present invention is to provide a system capable of rapid wind tunnel installation.
 本发明的再一个目的是提供一种具有多个飞行舱的风洞系统。  It is a further object of the present invention is to provide a system having a plurality of wind tunnel flight chamber.
 为实现本发明的目的，依照本发明的一个方面，提供了一种闭式循环的风洞系统，包括：闭式气流循环系统，它包括内腔和包围内腔的外腔，其中外腔在其两端与内腔相连通；动力系统，用于提供动力，使气体在闭式气流循环系统中循环。  For the purpose of the present invention, in accordance with one aspect of the present invention, there is provided a closed cycle wind tunnel system, comprising: a closed air circulation system, which includes a lumen and an outer lumen surrounding the cavity, wherein external cavity communicates with the cavity at its ends; power system, used to power the gas circulating in a closed air circulation system.
 上述闭式循环的风洞系统可以是垂直风洞系统，内腔为气流上升流动区，外腔为气流下降流动区。  The tunnel system is a closed loop system can be a vertical wind tunnel, the cavity of air rising flow area, outside the chamber for flow decreased flow area.
 上述闭式循环的风洞系统，其动力系统可以包括多个动力子系统，每个动力子系统可以根据动力需要被设置在外腔内的不同位置。  The closed loop wind tunnel system, the power system may include a plurality of power subsystems, each power subsystems may need to be set according to different positions of the outer cavity power.
 上述闭式循环的风洞系统，其动力子系统中的至少一个可以被设置在外腔的中部，并且动力子系统中的至少一个可以被设置在外腔的一端。  Wind tunnel above the closed-cycle system, the power subsystem of the at least one cavity may be provided in the outer middle, and at least one end of the outer chamber may be provided a power subsystem.
 上述闭式循环的风洞系统，其内腔可以包括至少一个收缩整流段和至少一个飞行舱。  The above-described tunnel closed cycle system, which comprises at least one lumen may shrink rectifying section and at least one flight chamber.  上述闭式循环的风洞系统，其外腔可以设置有进气门或进气窗，用于通过增压方式增加气流循环系统内的气体密度。  the above-mentioned closed cycle wind tunnel system, the outer chamber may be provided with an intake valve or the air intake window, methods for increasing the density of the gas through the pressurized air circulation within the system.
 上述闭式循环的风洞系统，在其一端可以设有第一回风装置，引导内腔的气流转入外腔，并且在其另一端可以设有第二回风装置，引导外腔的气流转入内腔。  the above-mentioned closed cycle wind tunnel system, in which one end of the return air can be provided with a first means for guiding the air flow into the lumen of the external cavity, and at its other end can be provided with a second return air apparatus, an outer guide flow into the chamber cavity.
 上述闭式循环的风洞系统，其内腔可以由横截面为圆形或多边形的内腔壁限定，且其外腔可以由内腔壁和横截面为圆形或多边形的外腔壁限定。  The closed loop wind tunnel system, which cavity may be formed circular or polygonal cross-section defining an inner cavity wall, the inner and outer walls and the cavity may be formed as a circular or polygonal cross-section of the outer chamber wall limiting.
 上述闭式循环的风洞系统，其外腔的截面面积与内腔的截面面积之比较佳地大于2。  The closed-loop wind tunnel system, cross-sectional area of the cross-sectional area of the lumen of the outer chamber of the relatively good greater than 2.
 上述闭式循环的风洞系统，其闭式气流循环系统可以包括：主体结构，该主体结构可以是筒状的框架结构，由多根短杆拼接而成，或者由至少一根长杆和多根短杆拼接而成。  The closed loop wind tunnel system, which can be closed air circulation system comprising: a main body structure, the body structure may be a tubular frame structure, composed of a plurality of short rods splicing, or by at least a length a plurality of short rods and rod splicing. 其中，筒状的框架结构的内侧可以用于覆盖内腔壁，且外侧可以用于覆盖外腔壁。 Wherein, inside the cylindrical frame structure may be used to cover the inner cavity wall, and can be used to cover the outside of the outer chamber wall.
 上述闭式循环的风洞系统，其主体结构可以包括沿该主体结构的横截面的周边重复、或者沿该主体结构的纵向重复的多个单元结构。  closed loop wind tunnel system of the above, the main structure may include a cross-section along the periphery of the main structure of the repeat, repeat or multiple unit structure longitudinally along the main structure.
 上述闭式循环的风洞系统，其中每个单元结构可以是横截面为梯形、扇环、矩形、六边形或其它多边形的柱体结构。  The closed-cycle wind tunnel system, wherein each unit structure may be trapezoidal in cross section, the fan ring, rectangular, hexagonal or other polygonal column structure.
 上述闭式循环的风洞系统，其中每个单元结构可以是由12根短杆拼接而成的横截面为梯形的垂直柱体。  Wind tunnel above the closed-cycle system, wherein each unit structure 12 may be comprised of a concatenation of short rods trapezoidal vertical cross-section cylinder.
 上述闭式循环的风洞系统，还可以包括：气密通道，其连通内腔壁和外腔壁，供人从风洞系统外进入内腔中的飞行舱；气密门，设置在气密通道与外腔壁和内腔壁的连接处。  The closed-cycle wind tunnel system, may further include: pressurizing passage, which communicates the inner bore and outer walls, for human flight chamber into the lumen from the outside wind tunnel system; airtight doors, provided In connection with the outer walls and airtight passageway within the walls of.
 上述闭式循环的风洞系统，其中气密通道可以被固定在单元结构内。  Wind tunnel above the closed-cycle system, wherein the pressurizing passage can be secured within the cell structure.
附图说明 Brief Description
 图1为依照本发明一实施例的闭式气流循环系统的正视示意图；  Figure 1 is a front view of a closed gas stream in accordance with an embodiment of the invention is a schematic diagram of the circulatory system;
 图2为依照本发明实施例的闭式气流循环系统的俯视示意图；  Figure 2 is a closed gas stream in accordance with an embodiment of the present invention is a schematic plan view of the circulatory system;
 图3为依照本发明一实施例的动力子系统的安置示意图；  Figure 3 is a schematic diagram in accordance with the placement of one embodiment of the invention the power subsystem;
 图4为依照本发明一实施例的用于构造闭式气流循环系统的基本构件、组合构件、单元结构和主体结构的示意图；  FIG. 4 is a combination of components, a schematic view of the main structure of the cell structure and the basic building blocks for the construction of closed air circulation system according to an embodiment of the invention in accordance with;
 图5为依照本发明一实施例的具有多重飞行舱的风洞的结构示意图；以及  Figure 5 is in accordance with multiple wind tunnel flight chamber to an embodiment of the present invention is a schematic view of the structure; and
 图6为依照本发明一实施例的内外腔气密通道的结构示意图。  FIG. 6 is an embodiment of the present invention in accordance with the structure of the inner and outer chamber of the pressurizing passage example of a schematic diagram.
具体实施方式 DETAILED DESCRIPTION
 下面结合附图对本发明所提供的娱乐风洞的具体实施作进一步的说明。  The following specific embodiments with reference to the wind tunnel of the entertainment provided by the present invention is further illustrated. 在所有附图中，用相同或相似的标号表不相同或相似的部件。 Throughout the drawings, same or similar reference numerals with the table is not the same or like parts.
 图1为依照本发明一实施例的闭式气流循环系统的正视示意图。  Figure 1 is a closed gas stream in accordance with an embodiment of the invention a front schematic view of the circulatory system. 在该实施例中，本发明的风洞的闭式气流循环系统包括紧密相连的内腔I与外腔2，其中外腔2包围内腔I并在其两端与外腔相连通，形成一个闭式的气流可循环流动的结构。 In this embodiment, the airflow wind tunnel closed circulation system of the present invention includes a lumen I closely connected with the outer chamber 2, wherein the outer chamber surrounds the inner chamber I and 2 at both ends thereof communicating with the outer chamber, forming a The gas stream may flow closed loop structure. 在动力系统的气流推动下，本系统的内腔I为相对地面的气体上升流动区，其外腔2为相对地面的气体下降流动区。 In the airflow pushing power system, the lumen of the system relative to the ground I was rising gas flow area, the outer surface of the cavity 2 is relatively decreased gas flow area. 气流沿内腔I向上经过系统的上回风段装置4流向外腔2，再沿外腔2向下经过系统的下回风段装置5重新进入内腔1，从而形成气流的闭式循环流动。 I pass up the airflow along the lumen of the return air system unit 4 to the outer chamber section 2, and then down along the outer chamber 2 through the system the next time the wind segment unit 5 re-enter the cavity 1, thus forming a closed circulation flow .  图2示出了依照本发明实施例的闭式气流循环系统的俯视示意图。  Figure 2 illustrates an embodiment of a closed air stream circulation system in accordance with the present invention is a schematic top view. 在本发明一实施例中，内、外腔的结构是由一组嵌套同心圆结构的内、外腔壁限定的：如图2所示，内圆是内腔壁，其内部为内腔I ;外圆是外腔壁，内圆与外圆之间的部分为外腔2。 In one embodiment of the invention, the structure of the inner and outer chamber is made within a set of nested concentric configuration, the outer walls defined by: shown in Figure 2, the inner circle is the lumen wall, the interior of the lumen I; cylindrical outer wall, the inner circle and the outer part of the external cavity between the two. 在本发明的另一实施例中，内、外腔壁采用了多边形结构。 In another embodiment of the present invention, the inner and outer walls using a polygonal configuration. 当然，本领域技术人员应该理解，在本发明中，风洞内、外腔壁的横截面可以采用各种形状，例如附图2中的圆形、多边形，并且可以采用同心结构或非同心结构，或者采用相同形状的组合或不同形状的组合，例如圆形内腔壁与多边形外腔壁的组合。 Of course, the skilled artisan will appreciate that, in the present invention, the wind tunnel, the cross-section of the outer chamber wall can take various shapes, for example, in Figure 2 the circular, polygonal, and may be concentric or non-concentric structure , or a combination of the same shape or a combination of different shapes, e.g., a combination of circular and polygonal outer walls of the cavity wall. 本发明在这一方面不受限制。 The present invention is not limited in this respect. 在较佳实施中，内、外腔壁可以采用同心圆结构，也可以采用同心正多边形，如正8、10、12边形，这样在选材与安装上可以大大降低成本费用，也可以为模块化设计提供基本条件。 In a preferred embodiment, the inner and outer wall concentric structure can also be used concentric regular polygon, such as n-gon 8,10,12, so in the selection and installation costs can be greatly reduced, but also for the module design provides the basic conditions. 此外，根据空气动力学的计算，外腔的横截面面积与内腔的横截面面积之比较佳地大于2。 In addition, based on the calculated aerodynamic cross-sectional area and cross-sectional area of the lumen of the outer chamber larger than 2 Comparative good. 与传统的风洞大回合循环的方式截然不同，本发明的风洞结构非常紧凑，能够有效地节省风洞的占地面积，为娱乐风洞的商业推广带来极大的好处。 With the traditional way different wind tunnel big round cycle, wind tunnel structure of the present invention is very compact, can effectively save the wind tunnel of the area, bring great benefits to the entertainment business promotion tunnel.
 风洞的动力装置在风洞系统的地位非常重要，直接关系到风洞的建设造价、运行效率以及运行维护成本。  the status of the power plant in the wind tunnel wind tunnel system is very important, is directly related to the construction of a wind tunnel cost, operational efficiency, and operation and maintenance costs. 传统的风洞大多采用单一的大功率电机，功率基本上大于1000KW，建安造价高，营运成本大，商业运转比较困难，这也是制约娱乐风洞市场推广的主要原因之一。 Most of the traditional wind tunnel using a single high-power motors, power is substantially greater than 1000KW, high installation cost, high operating costs, more difficult business operation, which is one of the main tunnel entertainment marketing constraints. 本发明的风洞采用多个动力子系统，即将风洞所需的动力总功率分解为多个小功率的动力子系统。 Wind tunnel present invention employs a plurality of power subsystems, i.e. the total power of the power required for the wind tunnel is decomposed into a plurality of small power power subsystem. 在本发明一实施例中，动力子系统是包括动力模块的一体式、模块化动力子系统，可以由电机和航空推进器构成。 In one embodiment of the invention, a power subsystem including a power module is integrated, modular power subsystem, may be constituted by a motor and aviation propulsion. 在一实施例中，采用多个70至120KW的高效电机，配以高效航空推进器，组成多个一体式的模块化动力子系统3。 In one embodiment, the use of more than 70 to 120KW of high-efficiency motors, together with efficient aerospace propulsion, composed of more than one type of modular power subsystem 3. 这些动力子系统3的外形几何尺寸可以控制在2*2*2米之内。 The power subsystem 3 shape geometry can be controlled within 2 * 2 * 2 meters. 如图3所示，可以根据风洞内腔的风速要求，也可以根据功率与功能的需求确定所需动力子系统3的数量，并可将这些动力子系统3设置在本发明的风洞外腔2内的任何位置，例如可以安置在外腔2的中部或底部。 3, according to the requirements of wind speed wind tunnel cavity, also according to the power demand to determine the number and function of the desired power subsystem 3, and these power subsystem 3 is provided outside of the present invention in a wind tunnel anywhere within the chamber 2, for example, may be arranged outside the middle or bottom of the chamber 2. 较佳地，本发明的动力系统可以包括6-12个分散在外腔内的动力子系统。 Preferably, the power system of the present invention may comprise the dispersion of the outer cavity of 6-12 power subsystem. 若将动力子系统3设置在本发明的风洞外腔的中部，动力推进气流的方向垂直朝下；若将动力子系统3设置在本发明的风洞外腔的底部，动力推进气流的方向平行地面并导向内腔。 If the power subsystem 3 is provided in the middle, the power of the wind tunnel of the present invention, the outer chamber perpendicular to the direction of advance downward airflow; If the power subsystem 3 is provided at the bottom of the outer chamber of the present invention, the wind tunnel, the propulsion direction of the airflow parallel to the ground and guide lumen. 这种风洞的动力系统设计灵活自由，可以完全解决由于噪音或结构支撑等因素给风洞设计带来的问题：现有风洞的电机系统大多采用一个大功率电机，并安置在风洞的顶部，而大功率电机的重量大多超过几吨甚至几十吨，这对风洞的支撑结构要求比较高，本发明将大功率的电机分解为多个小功率的电机，使得风洞的整体结构分布均匀稳定；同时，本发明的动力子系统完全处于风洞的外腔2内，风洞气流运动产生的噪音完全被阻隔在内腔I与外腔2的循环空间中，使得风洞外部的环境噪音大大降低，这与欧美一些开放式的娱乐风洞相比环境友好程度要高许多。 This wind tunnel's power system design flexibility and freedom, can be completely solved due to factors such as noise or structural support designed to bring the issue to the wind tunnel: The existing tunnel motor system mostly uses a high-power motor, and placed in the wind tunnel top, while most of the weight of the motor power more than a few tons or even tens of tons, which wind tunnel support structure is relatively high, the power of the motor of the present invention is divided into a number of small power motors, making the overall structure of the wind tunnel evenly distributed and stable; the same time, the power subsystem of the present invention is well within the wind tunnel of the outer chamber 2, the noise generated by wind tunnel of air movement completely block the lumen and outer lumen circulation space I 2, such that the external wind tunnel Environmental noise is greatly reduced, which compared with some European and American open environment friendly entertainment wind tunnel is much higher degree. 在一实施例中，我们制造了总功率达900KW的风洞，采用10组90KW的动力子系统放置在外腔的底部，内腔直径约4米。 In one embodiment, we have created a total power of 900KW wind tunnel, using 10 sets of 90KW of power subsystem is placed at the bottom of the outer chamber, lumen diameter of about 4 meters.
 在本发明一实施例中，可以采用类似晶体结构的主体结构，以实现独特的风洞结构。  In one embodiment of the invention may be employed similar to the crystal structure of the main structure, in order to achieve the unique tunnel structure. 类似晶体结构的主体结构在整体上呈现为筒状的框架结构，其中包括多个类似晶体单元的单元结构。 The main structure is similar to the crystal structure as a whole exhibits a tubular frame structure including a plurality of unit structures similar to the crystal unit. 较佳地，单元结构可以沿筒状主体结构横截面的周边重复，或者可以沿筒状主体结构的纵向重复。 Preferably, the cell structure along the periphery of the tubular body structure of the cross-section is repeated, or may be repeated longitudinally along the tubular body structure. 晶体单元结构可以呈现为各种结构，例如柱体结构、四面体结构等等。 Crystal cell structure may be presented as a variety of structures, such as the structure of the cylinder, tetrahedron structure and the like. 此外，在采用柱体单元结构的实施例中，每个单元结构可以具有各种横截面形状，例如梯形、扇环、矩形、六边形或其它多边形等。 Further, in the embodiment employs a cylindrical cell structure, the structure of each unit may have various cross-sectional shapes, such as trapezoidal, fan ring, rectangular, hexagonal or other polygonal shapes and the like.  在本发明一实施例中，类似晶体结构的主体结构可以由多个基本构件组合而成，例如可以由多根短杆拼接而成，或者可以由适当数量的长杆和短杆拼接而成。  In one embodiment of the invention, the body structure is similar to the crystal structure can be formed by a combination of a plurality of basic components, for example, can be spliced together by a plurality of studs, or may be formed by combining a suitable number of pole and short rod from. 在拼接过程中，可以将基本构件直接拼接成主体结构的框架；或者，可以先将基本构件组合成单元结构，然后采用类似搭积木的方式将多个单元结构拼接成主体结构。 In the splicing process, the basic building blocks can be spliced directly into the frame body structure; or, the basic building blocks can be combined into a unit structure first, then building-block approach similar to stitching multiple unit structure into the main structure.
 图4为依照本发明一实施例的用于构造闭式气流循环结构的基本构件10、组合构件12、单元结构14和主体结构16的示意图。  In accordance with the basic member 4 is used to construct a closed air circulation structure of an embodiment of the present invention 10, the combination member 12, a schematic diagram of the cell structure 14 and the body structure 16. 在如图4所示的实施例中，采用短杆作为基本构件10。 In the embodiment shown in Figure 4, with a short lever 10 as the basic member. 在本发明一实施例中，可以采用基本构件10直接拼接成主体结构16。 In one embodiment of the invention, the basic member 10 may be employed directly spliced into the main structure 16. 例如，采用三根短杆10拼接成组合构件12，继续进行拼接可以形成单元结构14。 For example, the use of three short rods 10 assembled into composite members 12 and continue stitching unit structure 14 can be formed. 然后，可以沿主体结构横截面的周边以及沿主体结构的纵向，在单元结构14的基础上用短杆10外延地进行拼接，得到包括多个单元结构14的主体结构16。 Then, the main structure along the periphery of the cross section and longitudinal direction of the main structure, the structure of the base unit 14 with a short lever 10 is epitaxially splicing to give the main structure 14 comprises a plurality of unit structures 16. 在本发明另一实施例中，可以先用基本构件10拼接成单元结构14，然后采用类似搭积木的方式将多个单独形成的单元结构14拼接成主体结构16。 In another embodiment of the invention, the first with the basic member 10 can be assembled into a unit structure 14, and similar building-block approach to forming a plurality of individual unit structure 14 spliced into the main structure 16. 例如，采用三根短杆10拼接成组合构件12，继续对组合构件12进行拼接可以形成单元结构14。 For example, the use of three short lever 10 splice into the combination of components 12, continued on the combination member 12 splicing unit structure 14 can be formed. 重复这一过程可以得到多个单元结构14，然后可以沿主体结构横截面的周边以及沿主体结构的纵向，采用类似搭积木的方式对已经独立形成的多个单元结构14加以堆叠以形成主体结构16。 This process is repeated a plurality of unit structures 14 can be obtained, which can then be cross-sectional structure along the periphery of the body and along the longitudinal direction of the main structure, similar building-block approach of a plurality of unit structures 14 have been formed independently be stacked to form the body structure 16. 对基本构件10、组合构件12、单元结构14的拼接可以采用焊接、螺母固定等等各种方式。 The basic member 10, the combination of components 12, 14 stitching unit structure can be used welding, nut and so on in various ways. 基本构件10 (在本实施例中是短杆）可以由金属或FRP等材料制成。 The basic member 10 (in the present embodiment is short rods) may be made of materials such as metal or FRP. 如图4所示，组合构件12可以由三根短杆10构成，每个单元结构14由4个组合构件12(即12根短杆）组成。 4, the combination member 12 may be constituted by three studs 10, each unit structure 14 by four combinations member 12 (i.e., 12 short rods) composition. 在本发明一实施例中，组合构件12的竖直短杆垂直于另两个水平短杆，并且单元结构14是横截面为梯形的垂直柱体结构。 In one embodiment of the invention, the combination of a short vertical rod member 12 is perpendicular to the other two levels of short rods, and the unit structure 14 is a cross-sectional trapezoidal vertical column structure. 在本发明的另一实施例中，单元结构14可以是横截面为扇环的柱体结构，由8根直短杆和4根弧形短杆形成。 In another embodiment of the present invention, the cell structure 14 may be cylindrical in cross section the structure of the fan ring is formed by eight straight studs and four curved short rods. 对这样的单元结构进行拼接，可以得到圆筒状的主体结构。 Such a cell structure of splicing, can be obtained in the cylindrical body structure. 在本发明的较佳实施例中，每个组合构件的几何尺寸长宽高可以控制在2米以内。 In a preferred embodiment of the present invention, the geometry of the length and breadth of each combination of components can be controlled within two meters.
 在本发明的另一实施例中，主体结构16可以由长杆和短杆的组合构成。  In another embodiment of the present invention, the body structure 16 may be composed of a combination of a short rod and a long rod. 例如，采用多根长杆形成如图4所示的主体结构16的竖直长边，然后用短杆形成该主体结构16的短边,从而拼接成主体结构16。 For example, the use of a plurality of pole form a vertical length of the main structure 16 shown in figure 4 side, then with a short rod form short edges of the body structure 16, thereby assembled into the body structure 16.
 在本发明一实施例中，风洞中除了主体结构以外的其他部件均可嵌入到单元结构14中，如动力子系统3、上回风段装置4、下回风段装置5等都可以通过预制埋件或螺栓紧固到单元结构14上。  In one embodiment of the invention, the wind tunnel, in addition to the main structure of the other components can be embedded into the cell structure 14, as the power subsystem 3, the return air segment means 4, 5 and so the next time the air section means are available through pre-embedded parts or bolted to the 14 unit structure. 在本发明一实施例中，在主体结构16的内侧，覆以表面材料如玻璃、PC板或其他板材，形成风洞的内腔壁，从而限定内腔I ;类似地，主体结构16的外侧覆以表面材料如玻璃、PC板或其他板材,形成风洞的外腔壁,主体结构的内外侧之间就成为风洞的外腔2。 In one embodiment of the present invention, the inner body structure 16, and covered with a surface material such as glass, PC board or other sheet material, forming the lumen wall of the wind tunnel, thereby defining a lumen I; outer Similarly, the main structure 16 of outer walls covered with a surface material such as glass, PC board or other sheet material, forming a wind tunnel, between the inside and outside becomes the main structure of the wind tunnel of the outer chamber 2.
 本发明的单元化主体结构设计，可将整个系统分解成许多基本构件，这样的设计利于批量制造和快速安装，这也是本发明的重要的价值所在。  unitized body structure design of the present invention, the entire system can be broken down into a number of basic components, this design is conducive to mass production and quick installation, which is an important value of the invention lies.
 本发明的风洞的内腔部分可以根据风洞设计需求，设置收缩整流段、飞行舱（即，运动娱乐段）等工作段，也可以重复设置多个工作段，例如本系统可以提供两个或两个以上的飞行舱。  lumen section of the wind tunnel of the present invention can be designed according to the needs of the wind tunnel, setting contraction rectifying section, the flight chamber (i.e., sports and entertainment segments) and the like working section to be repeated a plurality of work sections, for example, the system can providing two or more of the flight chamber. 收缩整流段是指该部分的内腔I的由下往上向内收缩，在最小收缩处连接整流装置。 Contraction rectification under section refers to the part of the cavity I shrink by up inward, connecting fairing shrink at a minimum. 如附图5，在一实施例中，我们在风洞的内腔中由下往上（相对地面）设置下收缩整流段61、下飞行舱71、上收缩整流段62、上飞行舱72等四个区域。 As Figure 5, in one embodiment, we shrink from bottom to top in the wind tunnel of the lumen (as opposed to ground) rectifying section 61, under the flight chamber 71, the contraction of the rectifying section 62, the flight chamber 72 and so on four regions. 在上压缩整流段区域61和下收缩整流段区域62中，内腔壁各自按一定比例向上收缩。 On the compression region rectifying section 61 and section area under the contraction of the rectifier 62, the inner wall of each contraction up by a certain percentage. 较佳地，收缩导风段的始末横截面的直径比例大于约1. 2，具体的收缩比例可以根据内腔的风速要求运用空气动力学方法求得。 Preferably, the shrinkage of the whole story of the wind guide section is greater than the cross-sectional diameter ratio of about 1.2, the specific shrinkage ratio can be determined by the method based on the use of the aerodynamic wind speed lumen requirements. 内腔的收缩整流段最好要保持流线形以减少气流高速通过产生湍流现象。 The best segment shrink rectified cavity to maintain streamlined to reduce airflow speed by generating turbulence. 整流装置可以采用常规的蜂窝式的整流板，整流板的厚度宜为约60-150厘米，材质可以选用金属或FRP隔栅。 Rectifying means may be used a conventional cellular rectifying plate, the rectifying plate preferably has a thickness of about 60-150 cm, a metal material can be selected or FRP grille. 上下飞行舱的横截面的直径比例较佳地小于0.8。 Diameter ratio of the vertical cross-section of the flight chamber is preferably less than 0.8. 当然，若动力系统充分，可以设计具有三个或以上的飞行舱的风洞体系。 Of course, if the power system fully, can be designed to have three or more of the flight deck of the tunnel system. 由于本发明的风洞在同一的动力系统的供应下，可提供二个或以上的飞行舱，为商业运营提供更大的利润空间。 Because of the wind tunnel of the invention under the same power supply system, providing two or more flight deck, providing greater profit margins for commercial operations.
 在一实施例中，本发明在风洞外腔部分设置了进气门或窗，通过增压方式使得本系统内的气体密度增加。  In one embodiment, the present invention is an external cavity portion is disposed in the wind tunnel of the intake valve or the window, such that by way of pressurized gas density within the system increases.
 在一实施例中，本发明的风洞还设置了气密通道8，人可以通过气密通道穿过外腔2进入内腔I内的飞行舱。  In one embodiment, the wind tunnel of the invention is also provided a gas-tight passage 8, one can enter the outer chamber 2 inside the flight chamber I through the cavity through gas-tight passage. 如附图6所示，气密通道8连接外腔壁与内腔壁，通道的宽度约在60-100厘米之间，高度约在180-200厘米之间。 As shown in Figure 6, the pressurizing passage 8 connecting the outer walls and inner walls, the width of the channel is between about 60-100 cm and a height between about 180-200 cm. 气密通道8在外腔壁与内腔壁的连接处各设置气密门，关上这两扇气密门，整个通道为密闭空间。 Channel 8 outer walls and airtight connection within the walls of each setting airtight doors, these two fan airtight doors closed, the entire channel for confined spaces. 为了减少气密通道8对外腔高速气流的阻力，可以将气密通道8的上下两段设计为圆弧形，使得整个气密通道呈胶囊状，并嵌入在风洞的外腔2内。 In order to reduce the high-speed pressurizing passage 8 external resistance to air flow chamber can be hermetically channel 8 of the vertical two-stage design is a circular arc shape, so that the entire capsule was hermetically channel and embedded within the outer chamber 2 of the wind tunnel. 例如，可以将这气密通道嵌入在一个单元结构14中。 For example, this may be embedded in a gas-tight channel 14 in the cell structure.
 尽管以上描述了本发明的较佳实施例，但本发明不仅限于此。  Although the above description of the preferred embodiments of the present invention, but the present invention is not limited thereto. 本领域的普通技术人员可以在以上描述的基础上进行各种变化和改变。 Of ordinary skill in the art can be described on the basis of the above that various changes and modifications.
 不脱离本发明精神的各种改变和变化都应落在本发明的保护范围之内。  without departing from the spirit of the invention various changes and modifications shall fall within the scope of the present invention. 本发明的保护范围由后附的权利要求书来限定。 The scope of the invention being indicated by the appended claims rights defined.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|CN1851434A||6 Jun 2006||25 Oct 2006||刘晓萌||Power system lower vertical wind tunnel|
|CN101228070A||15 Dec 2006||23 Jul 2008||沃拉尔赛公司||Improved panoramic, vertical wind tunnel|
|CA2574043A1||1 Aug 2005||2 Feb 2006||Skyventure, Llc||Recirculating vertical wind tunnel skydiving simulator and reduced drag cable for use in wind tunnels and other locations|
|US6083110||2 Jun 1999||4 Jul 2000||Sky Venture, Inc.||Vertical wind tunnel training device|
|12 Oct 2011||C06||Publication|
|30 Nov 2011||C10||Request of examination as to substance|
|24 Apr 2013||C14||Granted|