CN111111237A - Dynamic flight experience system - Google Patents
Dynamic flight experience system Download PDFInfo
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- CN111111237A CN111111237A CN202010021048.6A CN202010021048A CN111111237A CN 111111237 A CN111111237 A CN 111111237A CN 202010021048 A CN202010021048 A CN 202010021048A CN 111111237 A CN111111237 A CN 111111237A
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- connecting rod
- seat
- cabin
- lifting
- base
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63J—DEVICES FOR THEATRES, CIRCUSES, OR THE LIKE; CONJURING APPLIANCES OR THE LIKE
- A63J25/00—Equipment specially adapted for cinemas
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Abstract
The invention discloses a dynamic flight experience system, which comprises: a base; a cabin located above the base and for carrying passengers; the swing mechanism is arranged on the base and is used for driving the cabin to rotate; the lifting mechanism is arranged on the swing mechanism and is used for driving the cabin to do lifting or falling motion. According to the invention, the rotation of the swing mechanism enables the cabin to rotate 90 degrees anticlockwise, meanwhile, the lifting mechanism lowers the cabin onto the boarding floor, the cabin is lifted upwards quickly after boarding is finished, meanwhile, the mechanical system rotates 90 degrees clockwise integrally, passengers are sent into the film watching dome screen from the boarding space, the film playing system starts playing films, the mechanical system requires real-time mechanical response according to the content of the film, the cabin can be greatly dropped and lifted quickly, the weightlessness experience of the passengers is enhanced, and the irritation obtained by the passengers is enhanced.
Description
Technical Field
The invention relates to the technical field of film watching equipment, in particular to a dynamic flight experience system.
Background
There are large rides available on the market that can watch movies, for example, dynamic flying experiences, which have more sensible pleasure than in movie theaters, and which generally include a base on which a mount for projection equipment is mounted and through which images are projected onto a screen. The passenger cabin of the existing dynamic flight experience facility has smaller lifting and falling amplitude, so that the weightlessness experience of the tourists is poorer, and the irritation acquired by the tourists is poorer.
Accordingly, the prior art is yet to be improved and developed.
Disclosure of Invention
In view of the defects of the prior art, the invention aims to provide a dynamic flight experience system to solve the problem that the passenger weightlessness experience of passengers is poor due to small lifting and falling amplitudes of a cabin of a dynamic flight experience facility, so that the thrill obtained by the tourists is also poor.
The technical scheme of the invention is as follows:
a dynamic flight experience system, comprising:
a base;
a cabin located above the base and for carrying passengers;
the swing mechanism is arranged on the base and is used for driving the cabin to rotate;
the lifting mechanism is arranged on the swing mechanism and is used for driving the cabin to do lifting or falling motion.
In a further aspect of the present invention, the swing mechanism comprises:
the rotary chassis is arranged on the base;
the rotary driving system is arranged on the base and is connected with the rotary chassis;
the main frame is arranged on the rotary chassis.
In a further aspect of the invention, the lifting mechanism comprises:
the first lifting assembly is rotationally connected with the slewing mechanism;
the lifting driving system comprises a mounting bracket and a plurality of lifting electric cylinders arranged on the mounting bracket, and the lifting electric cylinders are connected with the first lifting assembly.
In a further aspect of the present invention, the lifting mechanism further comprises:
the second lifting assembly is positioned below the first lifting assembly and arranged in parallel with the first lifting assembly, and the second lifting assembly is rotatably connected with the main frame;
the connecting rod, the connecting rod sets up first lifting unit and second lifting unit both sides, the one end of connecting rod with first lifting unit connects, the other end with second lifting unit connects.
In a further arrangement of the invention, the cabin comprises:
a plurality of seat frames;
the seat bracket is rotationally connected with the lifting mechanism and is positioned below the seat framework;
a seat support beam rotatably connected to the seat bracket and rotatably connected to the seat frame;
the left and right swing frames are rotatably connected with the seat framework and are positioned on two sides of the seat beam;
the seat left-right swinging electric cylinder is arranged on the seat bracket and is rotationally connected with the left-right swinging frame;
the front and back pitching electric cylinder of the seat is arranged on the seat bracket and connected with the seat supporting beam.
According to the invention, a seat left-right swinging pull rod is further arranged between two adjacent left-right swinging frames and is used for synchronously driving two adjacent seat frameworks to move.
According to the further arrangement of the invention, the first lifting assembly comprises a first connecting rod, a second connecting rod, a third connecting rod and a first pull rod, one end of the first connecting rod and one end of the second connecting rod are rotatably connected with the main frame, and the other end of the first connecting rod and the other end of the second connecting rod are rotatably connected with the cabin; the third connecting rods are provided with a plurality of connecting rods for connecting the first connecting rods and the second connecting rods; the first pull rod is arranged above the first connecting rod and the second connecting rod respectively, one end of the first pull rod is connected with the main frame, and the other end of the first pull rod is connected with the cabin; the second lifting assembly comprises a fourth connecting rod, a fifth connecting rod, a sixth connecting rod and a second pull rod, one end of the fourth connecting rod and one end of the fifth connecting rod are rotatably connected with the main frame, and the other end of the fourth connecting rod and the other end of the fifth connecting rod are rotatably connected with the cabin; the number of the sixth connecting rods is used for connecting the fourth connecting rods and the fifth connecting rods; the second pull rod is arranged above the fourth connecting rod and the fifth connecting rod respectively, one end of the second pull rod is connected with the main frame, and the other end of the second pull rod is connected with the cabin.
According to the further arrangement of the invention, the lifting mechanism further comprises a plurality of connecting plates, and the connecting plates are arranged on the main frame and used for connecting the main frame with the first connecting rod, the second connecting rod, the fourth connecting rod and the fifth connecting rod.
The invention further provides that the rotary driving system comprises a driving motor and a transmission gear which are oppositely arranged on two sides of the base, and a rack which is arranged around the base and connected with the rotary chassis, wherein the rack is meshed with the transmission gear.
According to the further arrangement of the invention, the dynamic flight experience system further comprises an upper and lower passenger floor slab and a ball curtain, wherein the ball curtain is positioned at one side of the upper and lower passenger floor slab, and the upper and lower passenger floor slab is positioned at one side of the cabin.
The invention provides a dynamic flight experience system, which comprises: a base; a cabin located above the base and for carrying passengers; the swing mechanism is arranged on the base and is used for driving the cabin to rotate; the lifting mechanism is arranged on the swing mechanism and is used for driving the cabin to do lifting or falling motion. According to the invention, the rotation of the swing mechanism enables the cabin to rotate 90 degrees anticlockwise, meanwhile, the lifting mechanism lowers the cabin onto the boarding floor, the cabin is lifted upwards quickly after boarding is finished, meanwhile, the mechanical system rotates 90 degrees clockwise integrally, passengers are sent into the film watching dome screen from the boarding space, the film playing system starts playing films, the mechanical system requires real-time mechanical response according to the content of the film, the cabin can be greatly dropped and lifted quickly, the weightlessness experience of the passengers is enhanced, and the irritation obtained by the passengers is enhanced.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
Fig. 1 is a schematic overall structure diagram of the dynamic flight experience system of the invention.
Fig. 2 is a partial schematic view 1 of the dynamic flight experience system of the present invention.
Fig. 3 is a partial schematic view of the dynamic flight experience system of the present invention 2.
Figure 4 is a schematic view of a part of the structure of the cabin of the present invention 1.
Figure 5 is a schematic view of a part of the cabin according to the invention 2.
Figure 6 is a schematic view of a part of the cabin according to the invention 3.
The various symbols in the drawings: 1. getting on and off the passenger floor; 2. a ball screen; 3. a base; 4. a cabin; 41. a seat frame; 42. a seat carrier; 43. a seat support beam; 44. a left and right rocking frame; 45. the seat swings left and right to drive the electric cylinder; 46. a seat front and back pitching electric cylinder; 47. a seat left-right swinging pull rod; 5. a swing mechanism; 51. a revolving chassis; 52. a rotation driving device; 521. a drive motor; 522. a transmission gear; 523. a rack; 53. a main frame; 6. a lifting mechanism; 61. a first lifting assembly; 611. a first connecting rod; 612. a second connecting rod; 613. a third connecting rod; 614. a first pull rod; 62. a lift drive; 621. mounting a bracket; 622. lifting the electric cylinder; 63. a second lifting assembly; 631. a fourth connecting rod; 632. a fifth connecting rod; 633. a sixth connecting rod; 634. a second pull rod; 64. a connecting rod; 65. a connecting plate.
Detailed Description
The invention provides a dynamic flight experience system, and in order to make the purpose, technical scheme and effect of the invention clearer and clearer, the invention is further described in detail below by referring to the attached drawings and taking examples. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
In the embodiments and claims, the terms "a" and "an" can mean "one or more" unless the article is specifically limited.
In addition, if there is a description of "first", "second", etc. in an embodiment of the present invention, the description of "first", "second", etc. is for descriptive purposes only and is not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, technical solutions between various embodiments may be combined with each other, but must be realized by a person skilled in the art, and when the technical solutions are contradictory or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present invention.
Referring to fig. 1 to 6, the present invention provides a preferred embodiment of a dynamic flight experience system.
As shown in fig. 1, the dynamic flight experience system comprises an upper passenger floor 1, a lower passenger floor 2, a base 3, a cabin 4, a swing mechanism 5 and a lifting mechanism 6. The dynamic flight experience system of the invention is divided into two levels, that is, the system has two groups of cabins 4. Specifically, the base 3 is installed on the ground, the cabin 4 is located above the base 3 and used for carrying passengers, the swing mechanism 5 is arranged on the base 3 and used for driving the cabin 4 to rotate, and the lifting mechanism 6 is arranged on the swing mechanism 5 and used for driving the cabin 4 to do lifting or falling movement.
According to the invention, the rotation of the swing mechanism 5 enables the cabin 4 to rotate 90 degrees anticlockwise, namely the whole mechanical system rotates 90 degrees anticlockwise, meanwhile, the cabin 4 is lowered onto the boarding floor through the lifting mechanism 6 so as to be convenient for passengers to get on the cabin 4, the cabin 4 is quickly lifted upwards after the boarding is finished, meanwhile, the cabin 4 rotates 90 degrees clockwise so as to send the passengers into the film watching dome screen 2 from the boarding space, at the moment, the film is played by the film watching system, and the mechanical system requires real-time mechanical response according to the film and television content. Through the swing mechanism 5 and the lifting mechanism 6, the cabin 4 can be greatly dropped and can be quickly lifted, and the weightlessness experience of passengers is enhanced, so that the irritation obtained by the passengers is enhanced, and the experience of the passengers is further improved. In addition, the mechanical system in the invention is rotated by 90 degrees integrally to get on passengers, so that an additional passenger-getting butt-joint platform is not needed, and meanwhile, the mysterious feeling of the passenger project experience is increased.
Referring to fig. 2 and 3, in a further embodiment of an embodiment, the swing mechanism 5 includes a swing chassis 51, a swing driving device 52, and a main frame 53. Specifically, the rotary chassis 51 is installed on the base 3, the rotary driving device 52 is installed on the base 3 and connected to the rotary chassis 51, the main frame 53 is disposed on the rotary chassis 51, and the rotary driving device 52 drives the rotary chassis 51 to rotate so as to drive the main frame 53 installed on the rotary chassis 51 to rotate, thereby driving the whole mechanical system to rotate.
More specifically, the rotation driving device 52 includes a driving motor 521 and a transmission gear 522 which are oppositely disposed on two sides of the base 3, and a rack 523 which is disposed around the base 3 and connected to the rotation chassis 51, where the rack 523 is engaged with the transmission gear 522, that is, two sets of driving motors 521 and transmission gears 522 are disposed and respectively mounted on two sides of the base 3, the transmission gear 522 is engaged with the rack 523, and the driving motors 521 disposed on two sides of the base 3 synchronously rotate to drive the transmission gear 522 to rotate, so that the transmission gear 522 drives the rack 523 to rotate, and the rack 523 drives the rotation turntable to rotate, thereby driving the main frame 53 mounted on the rotation chassis 51 to rotate. The driving motor 521 is driven by a servo motor, the servo motor has the advantages of fast response and high positioning precision, and can perform special effects of lifting and falling in real time according to the content of the film and television, so that the mechanical special effect experience points of the project are enriched.
In a further embodiment of an embodiment, with continued reference to fig. 2 and 3, the lifting mechanism 6 includes a first lifting assembly 61 and a lifting driving device 62. The first lifting assembly 61 is rotatably connected to the main frame 53, the lifting driving device 62 includes a mounting bracket 621 and a plurality of electric lifting cylinders 622 disposed on the mounting bracket 621, and the electric lifting cylinders 622 are connected to the first lifting assembly 61. Specifically, one end of the mounting bracket 621 is fixed on the revolving chassis 51, the other end of the mounting bracket is fixedly connected to the main frame 53, two lifting electric cylinders 622 are provided and mounted on the mounting bracket 621, and the other end of the lifting electric cylinder 622 is connected to the first lifting assembly 61.
Referring to fig. 2 and 3, more specifically, the first lifting assembly 61 includes a first connecting rod 611, a second connecting rod 612, a third connecting rod 613 and a first pull rod 614, one end of the first connecting rod 611 and one end of the second connecting rod 612 are rotatably connected to the main frame 53, the other end of the first connecting rod 611 and the other end of the second connecting rod 612 are rotatably connected to the cabin 4, a plurality of third connecting rods 613 are provided for connecting the first connecting rod 611 and the second connecting rod 612, in this embodiment, the number of the third connecting rods 613 is two, the first pull rod 614 is respectively disposed above the first connecting rod 611 and the second connecting rod 612, one end of the first pull rod 614 is connected to the main frame 53, and the other end of the first pull rod 614 is connected to the cabin 4. Therefore, a parallelogram structure can be formed by the first connecting rod 611, the second connecting rod 612, the third connecting rod 613 and the first pull rod 614. Because the two lifting electric cylinders 622 move synchronously, when the two lifting electric cylinders 622 extend, the lifting electric cylinders 622 support the first lifting assembly 61 to a horizontal position (lifting movement), at the moment, the cabin 4 is in the horizontal position, the position of the cabin 4 is right opposite to the spherical screen 2, when the lifting electric cylinders 622 contract, the first lifting assembly 61 swings downwards (falling movement), the first lifting assembly 61 is in an inclined state, and at the moment, the cabin 4 is still in the horizontal state, so that the lifting and falling amplitude of the cabin 4 is large, meanwhile, because the first lifting assembly 61 is of a parallelogram structure, the cabin 4 is in a horizontal sitting posture state at any lifting position, so that passengers are in a horizontal sitting posture state at any lifting position, the viewing comfort level of the passengers is high, and the phenomenon that the cabin 4 is lifted is avoided, When the passenger falls, the power device is used for driving the seat to pitch in a linkage manner to ensure the level of the passenger seat, so that the control difficulty of the system is reduced, and the safety is improved.
Referring to fig. 2 and 3, in a further implementation manner of an embodiment, the lifting mechanism 6 further includes a second lifting assembly 63 and a connecting rod 64, the second lifting assembly 63 is located below the first lifting assembly 61 and is parallel to the first lifting assembly 61, and the second lifting assembly 63 is rotatably connected to the main frame 53. The connecting rod 64 is disposed at two sides of the first lifting assembly 61 and the second lifting assembly 63, one end of the connecting rod 64 is connected with the first lifting assembly 61, and the other end is connected with the second lifting assembly 63, that is, the first lifting assembly 61 and the second lifting assembly 63 are connected together through the two connecting rods 64.
Specifically, the second lifting assembly 63 includes a fourth connecting rod 631, a fifth connecting rod 632, a sixth connecting rod 633 and a second pull rod 634, one end of the fourth connecting rod 631 and the fifth connecting rod 632 is rotatably connected to the main frame 53, the other end of the fourth connecting rod 631 and the fifth connecting rod 632 is rotatably connected to the cabin 4, the sixth connecting rod 633 is provided with a plurality of connecting rods 631 and the fifth connecting rod 632, the second pull rod 634 is respectively disposed above the fourth connecting rod 631 and the fifth connecting rod 632, one end of the second pull rod 634 is connected to the main frame 53, and the other end of the second pull rod 634 is connected to the cabin 4. In one embodiment of an embodiment, two sixth connecting rods 633 are provided, and similar to the first lifting assembly 61, the second lifting assembly 63 is also a parallelogram structure formed by the fourth connecting rod 631, the fifth connecting rod 632, the sixth connecting rod 633 and the second pull rod 634. During the extension or contraction of the lifting electric cylinder 622, that is, when the first lifting assembly 61 is lifted or dropped, the second lifting assembly 63 moves synchronously with the first lifting assembly 61 through the connecting rod 64, and the first lifting assembly 61 and the second lifting assembly 63 are kept parallel during the movement. Therefore, under the action of the lifting electric cylinder 622, the two groups of parallelogram structures can be driven to synchronously move, that is, the cabin 4 on the first lifting assembly 61 and the cabin 4 on the second lifting assembly 63 can be in a horizontal sitting posture state at any lifting position, the lifting and falling amplitudes are large, and the weight loss experience is strong.
In a further embodiment of an embodiment, referring to fig. 2 and fig. 3, the lifting mechanism 6 further includes a plurality of connecting plates 65, and the connecting plates 65 are disposed on the main frame 53 for connecting the main frame 53 and the first connecting rod 611, the second connecting rod 612, the fourth connecting rod 631, and the fifth connecting rod 632. The connecting plate 65 is fixed on the main frame 53, and the first connecting rod 611, the second connecting rod 612, the fourth connecting rod 631 and the fifth connecting rod 632 are hinged to the main frame 53 through the connecting plate 65, so as to complete the installation of the first lifting assembly 61 and the second lifting assembly 63.
Referring to fig. 4, 5 and 6, in a further embodiment of an embodiment, the cabin 4 includes a plurality of seat frames 41, seat brackets 42, seat support beams 43, a roll frame 44, a seat roll electric cylinder 45 and a seat pitch electric cylinder 46. Seat bracket 42 with elevating system 6 rotates to be connected and is located seat skeleton 41 below, seat supporting beam 43 with seat bracket 42 rotates to be connected and with seat skeleton 41 rotates to be connected, swing frame 44 about with seat skeleton 41 rotates to be connected and is located seat supporting beam 43 both sides, the electronic jar 45 of seat side to side swing sets up on seat bracket 42 and with swing frame 44 rotates to be connected, the electronic jar 46 of pitch sets up around the seat on seat bracket 42 and with seat supporting beam 43 connects.
It can be understood that, since the dynamic flight experience system of the present invention is divided into two levels, that is, the cockpit 4 is respectively disposed on the first lifting assembly 61 and the second lifting assembly 63, the case that the cockpit 4 is disposed on the first lifting assembly 61 will be specifically described below.
Wherein, two seat frames 41 are arranged in each passenger area, that is, a single cabin 4 has two seat frames 41, two visitors can be seated at the same time, and each seat frame 41 corresponds to one left and right rocking frame 44. Specifically, the seat bracket 42 is hinged to the first connecting rod 611, the second connecting rod 612 and the first pull rod 614, the seat support beam 43 is hinged to the seat bracket 42 and the seat hanger, two left and right rocking frames 44 are correspondingly disposed on a single seat frame 41, and the two left and right rocking frames 44 are disposed on two sides of the seat support beam 43 and are hinged to the seat hanger. Seat left and right rocking electric cylinder 45 installs seat bracket 42's bottom and with wherein with seat skeleton 41 correspond left and right rocking frame 44 rotates to be connected, works as when seat left and right rocking electric cylinder 45 stretches out or contracts, can drive left and right rocking frame 44 swings, thereby passes through seat left and right rocking electric cylinder 45 drives seat skeleton 41 swings to realize the purpose that single seat can independently the horizontal hunting, it is big to avoid many people to lead to row seat structure both ends amplitude of oscillation, middle amplitude of oscillation is little, makes the problem that the passenger did not have any sensation. Wherein, the amplitude of the left-right swing of the seat frame 41 is +/-10 degrees. More specifically, the seat frame 41 pitch electric cylinder 46 is provided on the seat bracket 42 and connected to the seat support beam 43, and when the seat pitch electric cylinder 46 is extended or contracted, the seat frame 41 can perform a pitch motion, so that a seat stunt motion is enriched. Wherein, under the action of the front and back pitching electric cylinders 46 of the seat framework 41, the swinging angle of the seat framework 41 is +/-10 degrees.
Referring to fig. 4, fig. 5 and fig. 6, in a further embodiment of an embodiment, a seat sway bar 47 is further disposed between two adjacent left and right swaying frames 44, and the seat sway bar 47 is used for driving two adjacent seat frames 41 to move synchronously. Specifically, be located two of the electronic jar 46 opposite side of seat front and back every single move the rocking frame 44 passes through the seat left and right rocking pull rod 47 articulates together, works as when the electronic jar 46 of seat front and back every single move drives the motion of the rocking frame 44 about that one of them seat skeleton 41 corresponds under the effect of seat left and right rocking pull rod 47, can drive the rocking frame 44 swing about that another seat skeleton 41 corresponds in step to realized the synchronous oscillation of two adjacent seat skeletons 41, thereby realized two sets of seat skeleton 41 synchronous motion's purpose through the electronic jar 46 of every single seat skeleton 41 front and back every single move, can make the passenger obtain same sight shadow experience, make promptly that every passenger's rocking experience feels unanimous.
In summary, the present invention provides a dynamic flight experience system, which includes: a base; a cabin located above the base and for carrying passengers; the swing mechanism is arranged on the base and is used for driving the cabin to rotate; the lifting mechanism is arranged on the swing mechanism and used for driving the cabin to move up and down. The novel dynamic flight experience system is divided into two layers for getting on passengers, the rotary driving device works when getting on passengers, the mechanical system rotates 90 degrees anticlockwise integrally, meanwhile, the lifting mechanism lowers the cabin onto the floor surface of the getting on passengers, the cabin is lifted upwards quickly after getting on passengers, meanwhile, the mechanical system rotates 90 degrees clockwise integrally, the passengers are sent into the video watching dome from the passenger space, the video system starts to play videos, the mechanical system requires real-time mechanical response according to the content of the videos, the upper and lower layers of cabins can be greatly dropped and lifted quickly, meanwhile, the seat can pitch +/-10 degrees forwards and backwards, swing +/-10 degrees leftwards and rightwards, the mechanical action is perfectly combined with the content of the videos, and the experience effect of the videos is greatly improved.
It is to be understood that the invention is not limited to the examples described above, but that modifications and variations may be effected thereto by those of ordinary skill in the art in light of the foregoing description, and that all such modifications and variations are intended to be within the scope of the invention as defined by the appended claims.
Claims (10)
1. A dynamic flight experience system, comprising:
a base;
a cabin located above the base and for carrying passengers;
the swing mechanism is arranged on the base and is used for driving the cabin to rotate;
the lifting mechanism is arranged on the swing mechanism and is used for driving the cabin to do lifting or falling motion.
2. The animated flight experience system of claim 1 wherein the slewing mechanism comprises:
the rotary chassis is arranged on the base;
the rotary driving device is arranged on the base and is connected with the rotary chassis;
the main frame is arranged on the rotary chassis.
3. The active flight experience system of claim 1, wherein the lift mechanism comprises:
the first lifting assembly is rotationally connected with the slewing mechanism;
the lifting driving device comprises a mounting support and a plurality of lifting electric cylinders arranged on the mounting support, and the lifting electric cylinders are connected with the first lifting assembly.
4. The active flight experience system of claim 3, wherein the lift mechanism further comprises:
the second lifting assembly is positioned below the first lifting assembly and arranged in parallel with the first lifting assembly, and the second lifting assembly is rotatably connected with the main frame;
the connecting rod, the connecting rod sets up first lifting unit and second lifting unit both sides, the one end of connecting rod with first lifting unit connects, the other end with second lifting unit connects.
5. The animated flight experience system of claim 1 wherein the cockpit comprises:
a plurality of seat frames;
the seat bracket is rotationally connected with the lifting mechanism and is positioned below the seat framework;
a seat support beam rotatably connected to the seat bracket and rotatably connected to the seat frame;
the left and right swing frames are rotatably connected with the seat framework and are positioned on two sides of the seat beam;
the seat left-right swinging electric cylinder is arranged on the seat bracket and is rotationally connected with the left-right swinging frame;
the front and back pitching electric cylinder of the seat is arranged on the seat bracket and connected with the seat supporting beam.
6. The dynamic flight experience system according to claim 5, wherein a seat sway bar is further arranged between each two adjacent sway brackets, and the seat sway bar is used for synchronously driving each two adjacent seat frameworks to move.
7. The active flight experience system of claim 4, wherein the first lifting assembly comprises a first connecting rod, a second connecting rod, a third connecting rod and a first pull rod, one end of the first connecting rod and one end of the second connecting rod are rotatably connected with the main frame, and the other end of the first connecting rod and the other end of the second connecting rod are rotatably connected with the cabin; the third connecting rods are provided with a plurality of connecting rods for connecting the first connecting rods and the second connecting rods; the first pull rod is arranged above the first connecting rod and the second connecting rod respectively, one end of the first pull rod is connected with the main frame, and the other end of the first pull rod is connected with the cabin; the second lifting assembly comprises a fourth connecting rod, a fifth connecting rod, a sixth connecting rod and a second pull rod, one end of the fourth connecting rod and one end of the fifth connecting rod are rotatably connected with the main frame, and the other end of the fourth connecting rod and the other end of the fifth connecting rod are rotatably connected with the cabin; the number of the sixth connecting rods is used for connecting the fourth connecting rods and the fifth connecting rods; the second pull rod is arranged above the fourth connecting rod and the fifth connecting rod respectively, one end of the second pull rod is connected with the main frame, and the other end of the second pull rod is connected with the cabin.
8. The dynamic flight experience system of claim 7, wherein the lifting mechanism further comprises a plurality of connection plates disposed on the main frame for connecting the main frame with the first, second, fourth, and fifth connection rods.
9. The dynamic flight experience system according to claim 2, wherein the rotary driving device comprises a driving motor and a transmission gear which are oppositely arranged on two sides of the base, and a rack which is arranged around the base and connected with the rotary chassis, wherein the rack is meshed with the transmission gear.
10. The dynamic flight experience system of claim 1, further comprising an upper and lower passenger floor and a ball curtain, the ball curtain being located on one side of the upper and lower passenger floors, the upper and lower passenger floors being located on one side of the cabin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010021048.6A CN111111237A (en) | 2020-01-08 | 2020-01-08 | Dynamic flight experience system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010021048.6A CN111111237A (en) | 2020-01-08 | 2020-01-08 | Dynamic flight experience system |
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| CN111111237A true CN111111237A (en) | 2020-05-08 |
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| CN202010021048.6A Pending CN111111237A (en) | 2020-01-08 | 2020-01-08 | Dynamic flight experience system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI788959B (en) * | 2021-08-19 | 2023-01-01 | 智崴資訊科技股份有限公司 | flight simulator |
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2020
- 2020-01-08 CN CN202010021048.6A patent/CN111111237A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI788959B (en) * | 2021-08-19 | 2023-01-01 | 智崴資訊科技股份有限公司 | flight simulator |
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