CN114405015A - Flight entertainment sightseeing system - Google Patents
Flight entertainment sightseeing system Download PDFInfo
- Publication number
- CN114405015A CN114405015A CN202210051842.4A CN202210051842A CN114405015A CN 114405015 A CN114405015 A CN 114405015A CN 202210051842 A CN202210051842 A CN 202210051842A CN 114405015 A CN114405015 A CN 114405015A
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- CN
- China
- Prior art keywords
- rotor
- aerial vehicle
- unmanned aerial
- sightseeing
- flight entertainment
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63G—MERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
- A63G1/00—Roundabouts
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63G—MERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
- A63G23/00—Rotating or rocking pots, e.g. by moving the whole body
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Abstract
The invention discloses a flight entertainment sightseeing system, relates to the technical field of flight entertainment, and aims to solve the problems that in the prior art, flight entertainment equipment cannot bring more exciting experience to tourists due to the fact that the flight entertainment equipment cannot rotate in multiple directions and multiple angles, and cannot view a wider range of beautiful scenery. According to the invention, the tourist sits in the unmanned aerial vehicle, and the unmanned aerial vehicle can rotate and fly in multiple directions and multiple angles through the rotating mechanism, so that more stimulating experiences can be brought to the tourist sitting in the unmanned aerial vehicle, and meanwhile, a wider range of beautiful scenery can be enjoyed for the tourist sitting in the unmanned aerial vehicle.
Description
Technical Field
The invention relates to the technical field of flight entertainment, in particular to a flight entertainment sightseeing system.
Background
With the increasing competition, people can select corresponding entertainment to relieve stress and seek stimulation, wherein the entertainment comprises watching various beauty scenes, performances and the like in amusement places such as amusement parks, theme parks and the like, and people adopt an aerial flying overlooking mode for better watching various beauty scenes, performances and the like.
In the prior art, devices such as roller coasters and the like which can overlook the surrounding environment at high altitudes such as amusement parks and theme parks are available, but the traditional mode is more inclined to the stimulation of speed, and thus tourists cannot better view the surrounding environment; for another example, a rotary trojan is used, although the rotary trojan can better view the surrounding environment relative to a roller coaster, the rotary trojan can only rotate around the support column and cannot rotate, so that the rotary trojan also cannot bring more exciting experience to tourists, and the tourists cannot view a wider range of beautiful scenery.
In summary, the flying entertainment device in the prior art cannot bring more exciting experience to tourists and cannot enjoy a wider range of beauty views because the flying entertainment device cannot rotate and fly in multiple directions and angles.
Disclosure of Invention
The invention aims to: in order to solve the problems that in the prior art, the flying entertainment equipment cannot bring more exciting experience to tourists and cannot view a wider range of beautiful scenery due to the fact that the flying entertainment equipment cannot rotate in multiple directions and multiple angles, the invention provides a flying entertainment sightseeing system to increase the more exciting experience to the tourists and view the wider range of beautiful scenery.
The invention specifically adopts the following technical scheme for realizing the purpose:
flight amusement sightseeing system, including the stand that is located vertical direction, the support arm that is located the horizontal direction is installed to the upper end of stand, the both ends of support arm all are connected with the cable wire, the end of cable wire is connected with unmanned aerial vehicle through rotary mechanism.
The preferred structure of the rotary mechanism is: the rotating mechanism comprises a rotating column connected to the tail end of the steel cable, and the lower end of the rotating column is located in the unmanned aerial vehicle and can rotate in the unmanned aerial vehicle.
Preferably, the rotary column comprises a column body, a connecting ring is integrally formed at one end of the column body, a ball head is integrally formed at the other end of the column body, the ball head is located in the unmanned aerial vehicle, and the connecting ring is connected with the steel cable.
The specific structure of unmanned aerial vehicle does: unmanned aerial vehicle includes sightseeing storehouse and rotor section of thick bamboo, along the even rotor arm that installs a plurality of sightseeing storehouse upper portion that all pass of circumference on the rotor section of thick bamboo, the rotor oar is installed to the end of rotor arm, the bulb is located the rotor section of thick bamboo.
Preferably, the rotor wing barrel comprises a barrel body and a barrel cover which are mutually connected, the rotor wing arm is installed on the barrel body, a ball socket is arranged in the barrel cover, a rotating hole communicated with the ball socket is formed in the barrel cover, the cylinder penetrates through the rotating hole, and the ball head is located in the ball socket.
Preferably, the lower part of the rotor barrel is uniformly provided with a plurality of reinforcing rods connected with the inner wall of the sightseeing cabin along the circumferential direction.
Preferably, the end of rotor arm is installed with the rotor seat, the rotor oar is installed in the rotor seat, install the bracing piece of being connected with the rotor seat on the outer wall in sightseeing storehouse.
Preferably, a plurality of foot rests are uniformly arranged on the outer wall of the sightseeing cabin.
The invention has the following beneficial effects:
(1) according to the invention, the tourist sits in the unmanned aerial vehicle, and the unmanned aerial vehicle can rotate and fly in multiple directions and multiple angles through the rotating mechanism, so that more stimulating experiences can be brought to the tourist sitting in the unmanned aerial vehicle, and meanwhile, a wider range of beautiful scenery can be enjoyed for the tourist sitting in the unmanned aerial vehicle.
(2) When the unmanned aerial vehicle flies in a rotating mode, the ball head rotates in the ball socket, the rotating resistance between the ball head and the ball socket is smaller, and therefore the unmanned aerial vehicle can fly in a rotating mode for 360 degrees more conveniently.
(3) According to the invention, the rotor barrel and the sightseeing cabin can be connected more stably through the reinforcing rods, and the rotor propeller can be more stably installed on the rotor seat through the supporting rods, so that the whole unmanned aerial vehicle is more stable.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic view of a three-dimensional structure of the rotating mechanism of the present invention installed on an unmanned aerial vehicle;
FIG. 3 is a schematic view of a top view of the rotary mechanism of the present invention mounted on an unmanned aerial vehicle;
FIG. 4 is a schematic perspective view of a rotor of the present invention mounted within a rotor barrel;
FIG. 5 is a schematic front sectional view of a rotor of the present invention installed in a rotor barrel;
FIG. 6 is a schematic perspective view of the cover of the present invention;
FIG. 7 is a schematic perspective view of a spin column of the present invention;
FIG. 8 is a schematic perspective view of the cartridge of the present invention;
reference numerals: the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a rotating mechanism 2, a steel cable 3, a supporting arm 4, a stand column 5, a foot rest 6, a rotor seat 7, a rotor paddle 8, a supporting rod 9, a rotor arm 10, a rotating column 11, a ball head 111, a column body 112, a connecting ring 113, a rotor barrel 12, a barrel body 121, a barrel cover 122, a rotating hole 1221, a ball socket 1222, a reinforcing rod 13 and a sightseeing cabin 14.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.
Example 1
As shown in fig. 1, this embodiment provides flight amusement sightseeing system, including being located vertical direction's stand 5, the support arm 4 that is located the horizontal direction is installed to the upper end of stand 5, and the both ends of support arm 4 all are connected with cable wire 3, and the end of cable wire 3 is connected with unmanned aerial vehicle 1 through rotary mechanism 2.
The working principle is as follows: the upright post 5 and the support arm 4 are fixed and have a certain height of 30 meters, the support arm 4 is 15 meters long, the middle point of the support arm 4 is connected with the upright post 5, the end points of the two ends of the support arm 4 are provided with a steel cable 3, a safety protection device such as a falling protector, and the like, one end of the steel cable 3 is provided with the falling protector and is connected with the unmanned aerial vehicle 1 through a rotating mechanism 2, the other end of the steel cable is connected with the support arm 4, wherein a power supply cable of the unmanned aerial vehicle 1 is also wound with the steel cable 3, the unmanned aerial vehicle 1 can simultaneously carry two adult visitors to carry out the experience of flying entertainment and sightseeing, a control console is arranged in a cabin of the unmanned aerial vehicle 1, the unmanned aerial vehicle 1 can be controlled by the visitors to take off and land and move in a limited space, the unmanned aerial vehicle 1 is connected with a ground power supply system through a cable to supply power, the continuity of use is ensured, the ground is provided with a ground control center which has the highest authority, when the visitors enter the cabin of the unmanned aerial vehicle 1 to sit well, and after the ground staff checks that the safety belt is fastened, the ground control center sends an instruction to supply power to the unmanned aerial vehicle 1, wherein the first mode is to allow a tourist to operate the unmanned aerial vehicle 1 to take off and a series of following flight actions by himself, when the tourist is operated by mistake, the ground control center can take over to operate the unmanned aerial vehicle 1 immediately, and the second mode is to allow the tourist not to operate, and the ground control center sends an instruction to operate the unmanned aerial vehicle 1 to take off and a series of following flight actions.
It is specific, the visitor sits in unmanned aerial vehicle 1, unmanned aerial vehicle 1 can be through the multi-direction rotatory flight of rotary mechanism 2, 3 cable wire can be along with unmanned aerial vehicle 1's take off and land and remove the extension and shorten, thereby ensure can not lead to the fact the interference to unmanned aerial vehicle 1's flight, unmanned aerial vehicle 1 installs and surveys and keep away barrier device, can guarantee unmanned aerial vehicle 1 and stand 5, support arm 4, another unmanned aerial vehicle 1's safe distance, can bring more amazing experiences for the visitor who sits in unmanned aerial vehicle 1 like this, can watch the beautiful view of wider range for the visitor who sits in unmanned aerial vehicle 1 simultaneously.
Example 2
As shown in fig. 2 to 8, on the basis of the above embodiment 1, the present embodiment provides a preferable structure of the rotating mechanism 2 and the unmanned aerial vehicle 1 as follows: rotary mechanism 2 is including connecting at 3 terminal column 11 of cable 3, the lower extreme of column 11 is located unmanned aerial vehicle 1 and can rotate in unmanned aerial vehicle 1, column 11 includes cylinder 112, the one end integrated into one piece of cylinder 112 has go-between 113, another end integrated into one piece has bulb 111, bulb 111 is located unmanned aerial vehicle 1, go-between 113 is connected with cable 3, unmanned aerial vehicle 1 includes sightseeing cabin 14 and rotor section of thick bamboo 12, along the even rotor arm 10 that all passes the sightseeing cabin upper portion of installing of circumference on rotor section of thick bamboo 12, rotor oar 8 is installed to the end of rotor arm 10, bulb 111 is located rotor section of thick bamboo 12, rotor section of thick bamboo 12 includes barrel 121 and cover 122 of interconnect, rotor arm 10 installs on barrel 121, be equipped with ball 1222 in the cover 122, open the rotatory hole 1221 with ball 1222 intercommunication on the cover 122, cylinder 112 passes rotatory hole 1221, bulb 111 is located ball 1222.
In this embodiment: the number of the rotor arms 10 is six, so that the unmanned aerial vehicle 1 adopts a six-shaft six-rotor design, the maximum takeoff weight can reach 600KG, the reasonable structural design ensures the integral strength and lightens the weight, so that the unmanned aerial vehicle 1 can carry two adult tourists simultaneously for entertainment and sightseeing, the sightseeing cabin 14 is preferably hexagonal, transparent organic glass is used around, double safety seats are installed in the sightseeing cabin, the control console is installed in the sightseeing cabin, and on the premise of ensuring the safety of the tourists, the unmanned aerial vehicle 1 can meet the requirement that tourists freely control the ascending, descending and translation actions of the entertainment sightseeing unmanned aerial vehicle 1, the unmanned aerial vehicle 1 adopts a cable for power supply, the cable extends out of the rotor cylinder 12, the steel cable 3 extends to the ground, so that the weight of a carrying power supply is reduced, the endurance time of the unmanned aerial vehicle 1 is ensured, and the unmanned aerial vehicle can be used in the maintenance time range; when unmanned aerial vehicle 1 rotatory flight, bulb 111 can universal rotation in ball 1222, and the spin resistance of bulb 111 and ball 1222 is littleer, and 360 rotatory flights of unmanned aerial vehicle of being convenient for more like this also can not influence unmanned aerial vehicle 1's flight to can let the visitor experience unmanned aerial vehicle 1's driving manipulation enjoyment, obtain amazing, nervous experience in the sense organ simultaneously, can let the visitor in the high altitude environment around sightseeing.
Preferably, a plurality of reinforcing rods 13 connected with the inner wall of the sightseeing cabin 14 are uniformly arranged at the lower part of the rotor cylinder 12 along the circumferential direction, and the connection between the rotor cylinder 12 and the sightseeing cabin 14 can be more stable through the reinforcing rods 13.
Preferably, rotor arm 10's end is installed with rotor seat 7, and rotor oar 8 is installed in rotor seat 7, installs the bracing piece 9 of being connected with rotor seat 7 on the outer wall in sightseeing storehouse 14, is triangle-shaped between bracing piece 9, rotor arm 10 and sightseeing storehouse 14, can make rotor oar 8 more stable install on rotor seat 7 through bracing piece 9 to can make whole unmanned aerial vehicle 1 more stable.
Preferably, evenly install a plurality of foot rests 6 on the outer wall of sightseeing cabin 14, foot rest 6 adopts the pneumatic spring shock attenuation design, can reduce the vibrations impact to the visitor when unmanned aerial vehicle 1 falls to the ground, can alleviate the visitor moreover because of the maloperation leads to the impact on unmanned aerial vehicle 1 tenesmus contact ground.
Claims (8)
1. The flight amusement sightseeing system which characterized in that: including stand (5) that are located vertical direction, support arm (4) that are located the horizontal direction are installed to the upper end of stand (5), the both ends of support arm (4) all are connected with cable wire (3), the end of cable wire (3) is connected with unmanned aerial vehicle (1) through rotary mechanism (2).
2. The in-flight entertainment sightseeing system of claim 1 wherein: rotary mechanism (2) are including connecting at terminal column spinner (11) of cable wire (3), the lower extreme of column spinner (11) is located unmanned aerial vehicle (1) and can rotate in unmanned aerial vehicle (1).
3. The in-flight entertainment sightseeing system of claim 2 wherein: the rotary column (11) comprises a column body (112), a connecting ring (113) is integrally formed at one end of the column body (112), a ball head (111) is integrally formed at the other end of the column body (112), the ball head (111) is located in the unmanned aerial vehicle (1), and the connecting ring (113) is connected with the steel cable (3).
4. A flying entertainment sightseeing system in accordance with claim 3 wherein: unmanned aerial vehicle (1) is including sightseeing storehouse (14) and rotor section of thick bamboo (12), along the even rotor arm (10) of installing a plurality of sightseeing storehouse (14) upper portions that all pass of circumference on rotor section of thick bamboo (12), rotor oar (8) are installed to the end of rotor arm (10), bulb (111) are located rotor section of thick bamboo (12).
5. The in-flight entertainment sightseeing system of claim 4 wherein: the rotor wing cylinder (12) comprises a cylinder body (121) and a cylinder cover (122) which are connected with each other, the rotor wing arm (10) is installed on the cylinder body (121), a ball socket (1222) is arranged in the cylinder cover (122), a rotating hole (1221) communicated with the ball socket (1222) is formed in the cylinder cover (122), the column body (112) penetrates through the rotating hole (1221), and the ball head (111) is located in the ball socket (1222).
6. The in-flight entertainment sightseeing system of claim 4 wherein: and a plurality of reinforcing rods (13) connected with the inner wall of the sightseeing cabin (14) are uniformly arranged at the lower part of the rotor wing cylinder (12) along the circumferential direction.
7. The in-flight entertainment sightseeing system of claim 4 wherein: the tail end of the rotor arm (10) is provided with a rotor seat (7), the rotor paddles (8) are arranged in the rotor seat (7), and the outer wall of the sightseeing cabin (14) is provided with a support rod (9) connected with the rotor seat (7).
8. An in-flight entertainment sightseeing system in accordance with any one of claims 4-7 wherein: a plurality of foot stands (6) are uniformly arranged on the outer wall of the sightseeing cabin (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210051842.4A CN114405015A (en) | 2022-01-17 | 2022-01-17 | Flight entertainment sightseeing system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210051842.4A CN114405015A (en) | 2022-01-17 | 2022-01-17 | Flight entertainment sightseeing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114405015A true CN114405015A (en) | 2022-04-29 |
Family
ID=81272869
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210051842.4A Pending CN114405015A (en) | 2022-01-17 | 2022-01-17 | Flight entertainment sightseeing system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114405015A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006145893A (en) * | 2004-11-19 | 2006-06-08 | Kosaku Ueda | Support structure of seesaw type advertising device or like |
| CN204671889U (en) * | 2015-06-11 | 2015-09-30 | 温州南方游乐设备工程有限公司 | Interspace battleship recreational machine |
| CN106379554A (en) * | 2016-12-08 | 2017-02-08 | 中国科学院长春光学精密机械与物理研究所 | Flight test protection device and method |
| CN107261508A (en) * | 2017-08-17 | 2017-10-20 | 镇江市丹徒区硕源材料科技有限公司 | A kind of entertainment systems |
| CN107380436A (en) * | 2017-08-17 | 2017-11-24 | 镇江皮埃纳米科技有限公司 | A kind of safe heavy－duty aircraft and its application |
| CN108721901A (en) * | 2018-08-09 | 2018-11-02 | 山东方鑫游乐设备有限公司 | Amusement facility |
| CN212680062U (en) * | 2020-07-19 | 2021-03-12 | 新道信艺术设计咨询(上海)有限公司 | Novel multi-degree-of-freedom rotating amusement equipment |
-
2022
- 2022-01-17 CN CN202210051842.4A patent/CN114405015A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006145893A (en) * | 2004-11-19 | 2006-06-08 | Kosaku Ueda | Support structure of seesaw type advertising device or like |
| CN204671889U (en) * | 2015-06-11 | 2015-09-30 | 温州南方游乐设备工程有限公司 | Interspace battleship recreational machine |
| CN106379554A (en) * | 2016-12-08 | 2017-02-08 | 中国科学院长春光学精密机械与物理研究所 | Flight test protection device and method |
| CN107261508A (en) * | 2017-08-17 | 2017-10-20 | 镇江市丹徒区硕源材料科技有限公司 | A kind of entertainment systems |
| CN107380436A (en) * | 2017-08-17 | 2017-11-24 | 镇江皮埃纳米科技有限公司 | A kind of safe heavy－duty aircraft and its application |
| CN108721901A (en) * | 2018-08-09 | 2018-11-02 | 山东方鑫游乐设备有限公司 | Amusement facility |
| CN212680062U (en) * | 2020-07-19 | 2021-03-12 | 新道信艺术设计咨询(上海)有限公司 | Novel multi-degree-of-freedom rotating amusement equipment |
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