阅读说明：本技术 矩形飞行舱演艺风洞 (Rectangular flight cabin performance wind tunnel ) 是由 陈少昌 闫文涛 陈晨 于 2020-11-25 设计创作，主要内容包括：本发明涉及矩形飞行舱演艺风洞,包括飞行舱、第一扩散流道、第一拐导流板、上水平流道、轴流风机、第二扩散流道、第二拐导流板、第一垂直流道、第三拐导流板、下水平流道、第四拐导流板及收缩流道,多台轴流风机设于上水平流道内并位于第一拐导流板两侧设置形成分流,且一组第一拐导流板、一组第二拐导流板、一组第一垂直流道、一组第三拐导流板、一组下水平流道、一组第四拐导流板及收缩流道对称位于第一扩散流道两侧且沿气流方向依次连接,直至飞行舱连续循环形成回流；的飞行舱的截面长度为4m～20m、宽度为2.5m～6m,飞行舱的高度范围为3m～10m,飞行舱采用透明材料制成,该演艺风洞能够有效增强游客的使用体验,填补娱乐风洞矩形舱的空白。(The invention relates to a rectangular flight cabin performance wind tunnel which comprises a flight cabin, a first diffusion flow channel, a first turning guide plate, an upper horizontal flow channel, an axial flow fan, a second diffusion flow channel, a second turning guide plate, a first vertical flow channel, a third turning guide plate, a lower horizontal flow channel, a fourth turning guide plate and a contraction flow channel, wherein a plurality of axial flow fans are arranged in the upper horizontal flow channel and are positioned on two sides of the first turning guide plate to form shunting; the flight cabin has the cross section length of 4-20 m, the width of 2.5-6 m, the height range of the flight cabin is 3-10 m, the flight cabin is made of transparent materials, and the entertainment wind tunnel can effectively enhance the use experience of tourists and fill the blank of the entertainment wind tunnel rectangular cabin.)

1. Rectangle flight deck performance wind tunnel, its characterized in that: including flight cabin (1), first diffusion runner (2), first turning guide plate (3), go up horizontal runner (4), axial fan (5), second diffusion runner (6), second turn guide plate (7), first perpendicular runner (8), third turn guide plate (9), lower horizontal runner (10), fourth turn guide plate (11) and shrink runner (12), first diffusion runner (2) set up perpendicularly, go up horizontal runner (4) level and set up, it is many axial fan (5) are located go up horizontal runner (4) in and be located first turn guide plate (3) both sides set up and form the reposition of redundant personnel, and a set of first turn guide plate (3), a set of second turn guide plate (7), a set of first perpendicular runner (8), a set of third turn guide plate (9), a set of lower horizontal runner (10), a set of fourth turn guide plate (11) and shrink runner (12) symmetry lie in first diffusion runner (2) both sides and along first diffusion runner (2) both sides The airflow directions are sequentially connected until the flight cabin (1) continuously circulates to form double-loop backflow; the section length of the flight cabin (1) is 4-20 m, the width of the flight cabin is 2.5-6 m, the height range of the flight cabin (1) is 3-10 m, and the flight cabin (1) is made of transparent materials.

2. The rectangular flight deck performance wind tunnel according to claim 1, characterized in that: the flight cabin (1) is made of ultra-white toughened glass.

3. The rectangular flight deck performance wind tunnel according to claim 2, wherein: the airflow channel of the flight cabin (1) is made of concrete, steel plates or glass fiber reinforced plastics.

4. The rectangular flight deck performance wind tunnel according to claim 1, characterized in that: the axial flow fans (5) are arranged in an array mode on the same side of the first turning guide plate (3).

5. The rectangular flight deck performance wind tunnel according to claim 4, wherein: two sets of axial flow fans (5) are symmetrically arranged on two sides of the first turning guide plate (3) in parallel to form a flow distribution.

6. The rectangular flight deck performance wind tunnel according to claim 5, wherein: the inner diameter of the first vertical flow passage (8) gradually increases from top to bottom.

7. Rectangle flight deck performance wind tunnel, its characterized in that: comprises a flight cabin (1), a first diffusion flow channel (2), a first turning guide plate (3), an upper horizontal flow channel (4), an axial flow fan (5), a second diffusion flow channel (6), a second turning guide plate (7), a first vertical flow channel (8), a third turning guide plate (9), a lower horizontal flow channel (10), a fourth turning guide plate (11) and a contraction flow channel (12), wherein a plurality of axial flow fans (5) are arranged in the first vertical flow channel (8), a group of first turning guide plates (3), a group of second turning guide plates (7), a group of first vertical flow channels (8), a group of third turning guide plates (9), a group of lower horizontal flow channels (10), a group of fourth turning guide plates (11) and a contraction flow channel (12) are symmetrically positioned on two sides of the first diffusion flow channel (2) and are sequentially connected along the air flow direction until the flight cabin (1) continuously circulates to form double-loop backflow; the length of the section of the flight cabin (1) is 4-20 m, the width of the flight cabin is 2.5-6 m, the height range of the flight cabin (1) is 3-10 m, and the air channel material of the flight cabin (1) is made of ultra-white toughened glass.

8. The rectangular flight deck performance wind tunnel according to claim 7, wherein: the first vertical flow channel (8) is in a hemispherical shape.

9. Rectangle flight deck performance wind tunnel, its characterized in that: the air flow fan comprises a flight cabin (1), a first diffusion flow channel (2), a first turning guide plate (3), an upper horizontal flow channel (4), an axial flow fan (5), a second diffusion flow channel (6), a second turning guide plate (7), a first vertical flow channel (8), a third turning guide plate (9), a lower horizontal flow channel (10), a fourth turning guide plate (11) and a contraction flow channel (12), wherein the axial flow fan (5) is arranged in the upper horizontal flow channel (4), and the first diffusion flow channel (2), the upper horizontal flow channel (4), the second diffusion flow channel (6), the first vertical flow channel (8), the lower horizontal flow channel (10) and the contraction flow channel (12) are sequentially connected along the air flow direction until the flight cabin (1) continuously circulates to form single-loop backflow.

10. Rectangle flight deck performance wind tunnel, its characterized in that: the air flow fan comprises a flight cabin (1), a first diffusion flow channel (2), a first turning guide plate (3), an upper horizontal flow channel (4), an axial flow fan (5), a second diffusion flow channel (6), a second turning guide plate (7), a first vertical flow channel (8), a third turning guide plate (9), a lower horizontal flow channel (10), a fourth turning guide plate (11) and a contraction flow channel (12), wherein the axial flow fan (5) is arranged in the first vertical flow channel (8), and the first diffusion flow channel (2), the upper horizontal flow channel (4), the second diffusion flow channel (6), the first vertical flow channel (8), the lower horizontal flow channel (10) and the contraction flow channel (12) are sequentially connected along the air flow direction until the flight cabin (1) continuously circulates to form single-loop backflow.

Technical Field

The invention relates to the technical field of entertainment wind tunnels, in particular to a rectangular flight deck performance wind tunnel.

Background

The amusement wind tunnel is an air suspension device, and it is the project that integrates high-tech and thrill, amazing amusement and combines together, namely through artificial manufacturing and control air current, get up visitor's "blowing" in a specific space, let the people not only can experience the sensation that the space is fluttering, simultaneously, can also audio-visually know aerodynamic knowledge and wind tunnel experimental technique, play the in-process people in the amusement wind tunnel and bump with the wall body easily in the air, cause unnecessary injury to the human body, need be equipped with safety protection wall in the amusement wind tunnel.

The vertical amusement wind tunnel of current indoor parachuting, flight cabin are circular or approximate circular, and the predominant use is that entertainment experience and professional parachuting sportsman train and indoor parachuting match use, does not possess the performance function, and the reception holds the visitor volume limitedly, can not reach the multiple effect of experience training performance and sight and can not satisfy visitor's demand, leads to the place economic benefits who uses above-mentioned amusement wind tunnel to be low simultaneously, is unfavorable for the popularization and the application of amusement wind tunnel in the market.

Disclosure of Invention

The invention aims to overcome the defects in the prior art, and provides the rectangular flight deck performance wind tunnel which can effectively enhance the use experience of tourists, meet the requirements of the tourists, achieve multiple effects of training performance and appreciation, increase economic benefits, fill the blank of the rectangular flight deck of the entertainment wind tunnel, and is beneficial to popularization and application of the rectangular flight deck performance wind tunnel in the market.

In order to achieve the purpose, the invention adopts the following technical scheme: the rectangular flight cabin performance wind tunnel comprises a flight cabin, a first diffusion flow channel, a first turning guide plate, an upper horizontal flow channel, an axial flow fan, a second diffusion flow channel, a second turning guide plate, a first vertical flow channel, a third turning guide plate, a lower horizontal flow channel, a fourth turning guide plate and a contraction flow channel, wherein the first diffusion flow channel is vertically arranged, the upper horizontal flow channel is horizontally arranged, the axial flow fans are arranged in the upper horizontal flow channel and are positioned on two sides of the first turning guide plate to form shunting, and a group of first turning guide plates, a group of second turning guide plates, a group of first vertical flow channels, a group of third turning guide plates, a group of lower horizontal flow channels, a group of fourth turning guide plates and the contraction flow channel are symmetrically positioned on two sides of the first diffusion flow channel and are sequentially connected along the airflow direction until the flight cabin continuously circulates to form double-loop backflow; the length of the section of the flight cabin is 4-20 m, the width of the flight cabin is 2.5-6 m, the height range of the flight cabin is 3-10 m, and the flight cabin is made of transparent materials.

As a preferable scheme of the invention, the flight cabin is made of ultra-white toughened glass.

As a preferable scheme of the invention, the airflow channel of the flight cabin is made of concrete, steel plates or glass fiber reinforced plastics.

As a preferable scheme of the present invention, the axial flow fans are arranged in an array on the same side of the first turning guide plate.

As a preferred scheme of the invention, two groups of axial flow fans are symmetrically arranged on two sides of the first turning guide plate in parallel to form a flow distribution.

As a preferable mode of the present invention, the inner diameter of the first vertical flow passage gradually increases from top to bottom.

The rectangular flight cabin performance wind tunnel comprises a flight cabin, a first diffusion flow channel, a first turning guide plate, an upper horizontal flow channel, an axial flow fan, a second diffusion flow channel, a second turning guide plate, a first vertical flow channel, a third turning guide plate, a lower horizontal flow channel, a fourth turning guide plate and a contraction flow channel, wherein the axial flow fans are arranged in the first vertical flow channel, and a group of first turning guide plates, a group of second turning guide plates, a group of first vertical flow channels, a group of third turning guide plates, a group of lower horizontal flow channels, a group of fourth turning guide plates and the contraction flow channel are symmetrically positioned at two sides of the first diffusion flow channel and are sequentially connected along the airflow direction until the flight cabin continuously circulates to form double-loop backflow; the length of the section of the flight cabin is 4-20 m, the width of the flight cabin is 2.5-6 m, the height range of the flight cabin is 3-10 m, and the flight cabin air flow channel material is made of ultra-white toughened glass.

As a preferable aspect of the present invention, the first vertical flow channel is formed in a hemispherical shape.

The rectangular flight cabin performance wind tunnel comprises a flight cabin, a first diffusion flow channel, a first turning guide plate, an upper horizontal flow channel, an axial flow fan, a second diffusion flow channel, a second turning guide plate, a first vertical flow channel, a third turning guide plate, a lower horizontal flow channel, a fourth turning guide plate and a contraction flow channel, wherein the axial flow fan is arranged in the upper horizontal flow channel, and the first diffusion flow channel, the upper horizontal flow channel, the second diffusion flow channel, the first vertical flow channel, the lower horizontal flow channel and the contraction flow channel are sequentially connected along the air flow direction until the flight cabin continuously circulates to form single-loop backflow.

The rectangular flight cabin performance wind tunnel comprises a flight cabin, a first diffusion flow channel, a first turning guide plate, an upper horizontal flow channel, an axial flow fan, a second diffusion flow channel, a second turning guide plate, a first vertical flow channel, a third turning guide plate, a lower horizontal flow channel, a fourth turning guide plate and a contraction flow channel, wherein the axial flow fan is arranged in the first vertical flow channel, and the first diffusion flow channel, the upper horizontal flow channel, the second diffusion flow channel, the first vertical flow channel, the lower horizontal flow channel and the contraction flow channel are sequentially connected along the air flow direction until the flight cabin continuously circulates to form single-loop backflow.

Compared with the prior art, the invention has the beneficial effects that: according to the rectangular flight cabin performance wind tunnel, the vertically upward stable airflow is formed in the flight cabin, and athletes or experiencers in the flight cabin can fly freely under the action of the gravity returning to the earth and floating of the vertically upward airflow according to the change of the windward side of the body and the change of the windward side angle, so that the use experience is enhanced; and the rectangular transparent glass flight cabin is added with holographic projection, like a giant movie screen, the front and back glass projection of the flight cabin forms a 3D effect, athletes or experiencers fly in the middle of the double-layer screen to form a live-action 3D real person performance, and then the effects of lamplight and music are matched, so that the visual feast of the performance in a flying day is provided for audiences, the irreplaceable ornamental effect is achieved, and the popularization and application of the rectangular flight cabin performance wind tunnel in the market are facilitated.

Drawings

FIG. 1 is a schematic structural diagram of a rectangular flight deck performance wind tunnel in embodiment 1;

FIG. 2 is a sectional view of the structure taken along line A-A in FIG. 1;

FIG. 3 is a sectional view taken along line B-B of FIG. 1;

FIG. 4 is a schematic structural diagram of a rectangular flight deck performance wind tunnel according to embodiment 2;

FIG. 5 is a cross-sectional view of the structure taken along line E-E of FIG. 4;

FIG. 6 is a sectional view of the structure taken along line F-F in FIG. 4;

FIG. 7 is a schematic structural view of a rectangular flight deck performance wind tunnel according to embodiment 3;

FIG. 8 is a sectional view taken along line H-H in FIG. 7;

FIG. 9 is a sectional view taken along line G-G of FIG. 7;

FIG. 10 is a sectional view taken along line I-I of FIG. 7;

FIG. 11 is a schematic structural view of a rectangular flight deck performance wind tunnel according to embodiment 4;

FIG. 12 is a sectional view of the structure taken along line A-A in FIG. 11;

FIG. 13 is a sectional view taken along line B-B of FIG. 11;

FIG. 14 is a sectional view of the structure taken along line C-C of FIG. 11;

fig. 15 is a sectional view taken along line D-D in fig. 11.

Reference numerals: 1. a flight deck; 2. a first diffusion flow path; 3. a first crutch baffle; 4. an upper horizontal runner; 5. an axial flow fan; 6. a second diffusion flow path; 7. a second crutch deflector; 8. a first vertical flow channel; 9. a third crutch deflector; 10. a lower horizontal runner; 11. a fourth crutch deflector; 12. the flow passage is contracted.

Detailed Description

The following describes embodiments of the present invention in detail with reference to the accompanying drawings.

Example 1: as shown in fig. 1 to 3, the rectangular flight cabin performance wind tunnel includes a flight cabin 1, a first diffusion flow channel 2, a first turning guide plate 3, an upper horizontal flow channel 4, an axial flow fan 5, a second diffusion flow channel 6, a second turning guide plate 7, a first vertical flow channel 8, a third turning guide plate 9, a lower horizontal flow channel 10, a fourth turning guide plate 11 and a contraction flow channel 12, wherein the first diffusion flow channel 2 is vertically arranged, the upper horizontal flow channel 4 is horizontally arranged, a plurality of axial flow fans 5 are arranged in the upper horizontal flow channel 4 and positioned at two sides of the first turning guide plate 3 to form a split flow, and a group of first turning guide plates 3, a group of second turning guide plates 7, a group of first vertical flow channels 8, a group of third turning guide plates 9, a group of lower horizontal flow channels 10, a group of fourth turning guide plates 11 and contraction flow channels 12 are symmetrically positioned at two sides of the first diffusion flow channel 2 and sequentially connected along an air flow direction, until the flight cabin 1 continuously circulates to form double-loop backflow; the length of the section of the flight cabin 1 is 4 m-20 m, the width of the flight cabin 1 is 2.5 m-6 m, the height range of the flight cabin 1 is 3 m-10 m, and the flight cabin 1 is made of transparent materials. The rectangular flight cabin performance wind tunnel is mainly used for realizing real 3D (three-dimensional) aerial dance performance by combining multimedia, a mythical story is combined with the real aerial dance performance by front and back projection or holographic projection of transparent glass of the rectangular flight cabin, and as time-space shuttle, audiences are brought into scenes by visiting the scenes to feel unprecedented visual feasts. 1000 audiences can be held at every scene, and the visitor experiences several times and increases, satisfies the visitor demand, reaches the multiple effect of experience training performance and sight, increases economic benefits, fills the blank in amusement wind tunnel rectangle flight deck, fills in the blank of aerial real person 3D performance and the aerospace real person aerial dance live action of theme park with projection 3D performance.

The flight chamber 1 is made of ultra-white toughened glass, the ultra-white glass is ultra-transparent low-iron glass, also called low-iron glass and high-transparent glass, and is a novel high-grade glass variety with high quality and multiple functions, the light transmittance can reach more than 91.5%, the ultra-white glass has the characteristics of being crystal clear and high-grade and elegant, the ultra-white glass is called crystal prince of the glass family, the ultra-white glass has all the processability of high-quality float glass, has excellent physical, mechanical and optical properties, can be subjected to various deep processing like other high-quality float glass, and has incomparable excellent quality and product performance, so that the ultra-white glass has wide application space and bright market prospect, and can be applied to the manufacture of the flight chamber to further improve the quality of the flight chamber.

In order to ensure the structural strength of the flight chamber and the safety of users in the using process, the airflow channel of the flight chamber 1 is made of concrete, steel plates or glass fiber reinforced plastics.

In this embodiment, the axial flow fans 5 are arranged in an array on the same side of the first turning guide plate 3, the axial flow fans 5 are in one group, and two groups of the axial flow fans 5 are symmetrically connected in parallel to two sides of the first turning guide plate 3 to form a split flow, that is, a wind tunnel of a rectangular flight cabin in a double-loop form in this embodiment is formed, and the inner diameter of the first vertical flow channel 8 is gradually increased from top to bottom, so that the user experience is improved, and the mood is more comfortable.

The working principle of the rectangular flight cabin performance wind tunnel is as follows: the axial flow fans 5 generate air flow through the rotation of the blades, the air flow passes through a second diffusion flow channel 6, a second turning guide plate 7, a first vertical flow channel 8, a third turning guide plate 9, a lower horizontal flow channel 10, a fourth turning guide plate 11 and a contraction flow channel 12, and then passes through a first diffusion flow channel 2 and a first turning guide plate 3 upwards, and the air flow makes circular reciprocating motion.

Example 2: as shown in fig. 4 to 6, the present embodiment is different from embodiment 1 in that: the plurality of axial flow fans 5 are arranged in the first vertical flow channel 8, the rectangular flight cabin performance wind tunnel in the embodiment comprises a flight cabin 1, a first diffusion flow channel 2, a first turning guide plate 3, an upper horizontal flow channel 4, an axial flow fan 5, a second diffusion flow channel 6, a second turning guide plate 7, a first vertical flow channel 8, a third turning guide plate 9, a lower horizontal flow channel 10, a fourth turning guide plate 11 and a contraction flow channel 12, the plurality of axial flow fans 5 are arranged in the first vertical flow channel 8, a group of first turning guide plates 3, a group of second turning guide plates 7, a group of first vertical flow channels 8, a group of third turning guide plates 9, a group of lower horizontal flow channels 10, a group of fourth turning guide plates 11 and a contraction flow channel 12 are symmetrically positioned at two sides of the first diffusion flow channel 2 and are sequentially connected along the air flow direction until the flight cabin 1 continuously circulates to form double-loop backflow; the length of the section of the flight cabin 1 is 4-20 m, the width of the flight cabin 1 is 2.5-6 m, the height range of the flight cabin 1 is 3-10 m, the material of the air flow channel of the flight cabin 1 is made of super white toughened glass, and the first vertical flow channel 8 is in a hemispherical shape.

Example 3: as shown in fig. 7 to 10, the present embodiment is different from the above embodiments in that: the wind tunnel is a single-loop rectangular wind tunnel in the embodiment, and comprises a flight cabin 1, a first diffusion flow channel 2, a first turning guide plate 3, an upper horizontal flow channel 4, an axial flow fan 5, a second diffusion flow channel 6, a second turning guide plate 7, a first vertical flow channel 8, a third turning guide plate 9, a lower horizontal flow channel 10, a fourth turning guide plate 11 and a contraction flow channel 12, wherein the axial flow fan 5 is arranged in the upper horizontal flow channel 4, and the first diffusion flow channel 2, the upper horizontal flow channel 4, the second diffusion flow channel 6, the first vertical flow channel 8, the lower horizontal flow channel 10 and the contraction flow channel 12 are sequentially connected along the air flow direction until the flight cabin 1 continuously circulates to form single-loop backflow.

Example 4: as shown in fig. 11 to 15, the present embodiment is different from embodiment 3 described above in that: the axial flow fan 5 is arranged in the first vertical flow channel 8, and the rectangular flight cabin performance wind tunnel comprises a flight cabin 1, a first diffusion flow channel 2, a first turning guide plate 3, an upper horizontal flow channel 4, the axial flow fan 5, a second diffusion flow channel 6, a second turning guide plate 7, a first vertical flow channel 8, a third turning guide plate 9, a lower horizontal flow channel 10, a fourth turning guide plate 11 and a contraction flow channel 12, wherein the axial flow fan 5 is arranged in the first vertical flow channel 8, and the first diffusion flow channel 2, the upper horizontal flow channel 4, the second diffusion flow channel 6, the first vertical flow channel 8, the lower horizontal flow channel 10 and the contraction flow channel 12 are sequentially connected along the airflow direction until the flight cabin 1 continuously circulates to form single-loop backflow.

The axial flow fans 5 arranged in the rectangular wind tunnel array are symmetrically arranged in parallel, and are controlled in a variable frequency mode, so that the use effect of the axial flow fans 5 is guaranteed, and the mutual influence of the axial flow fans 5 is reduced.

In the embodiment, the rectangular flight cabin performance wind tunnel overcomes the traditional entertainment wind tunnel circular flight cabin, and a rectangular flight cabin wind tunnel is successfully designed; the design standardization is completed, the parts are modularized, the production hydration is realized, the production cost is reduced, and the product quality is ensured; the wind tunnel of the rectangular flight cabin is combined with multimedia. The vertical upward stable airflow is formed in the flight chamber, and athletes or experiencers in the flight chamber can freely fly under the action of the gravity floating of the vertical upward airflow, according to the change of the windward side of the body and the change of the windward angle. The holographic projection is added on the transparent glass of the rectangular flight cabin, like a giant movie screen, the front and back glass projections of the flight cabin form a 3D effect, athletes or experiencers fly in the middle of the double-layer screen to form a live-action 3D real person performance, and then the effects of lamplight and music are matched, so that the visual feast of the live-action performance on a flying day is provided for audiences, and the irreplaceable ornamental effect is achieved.

The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention; thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Although the reference numerals in the figures are used more here: 1. a flight deck; 2. a first diffusion flow path; 3. a first crutch baffle; 4. An upper horizontal runner; 5. an axial flow fan; 6. a second diffusion flow path; 7. a second crutch deflector; 8. a first vertical flow channel; 9. a third crutch deflector; 10. a lower horizontal runner; 11. a fourth crutch deflector; 12. constricted flow paths, etc., but does not exclude the possibility of using other terms. These terms are used merely to more conveniently describe and explain the nature of the present invention; they are to be construed as being without limitation to any additional limitations that may be imposed by the spirit of the present invention.