CN220656359U - Simulated flight cockpit with protection function - Google Patents

Abstract

The utility model discloses a simulated flight cockpit with a protection function, and relates to the technical field of parts, parts or accessories of chairs or stools. This possess simulation flight cockpit of safeguard function, including the cabin body, the inside of cabin body sets up to cavity, the front side surface of cabin body has been seted up the entry, the front side of cabin body is provided with the running-board, the diapire fixedly connected with seat of cabin body, the seat comprises cushion, handrail and back, wherein cushion fixed connection is at the diapire of cabin body, can make the user when using this simulation flight cockpit, can not produce the risk that the foot was fallen because of the rocking of cabin, simultaneously because spacing is soft rubber material with the fixed bolster surface, avoid making the user produce painful sense because of frequent striking that rocks the production, and because limit structure's effect need not to carry out further locking after pulling down the fixed bolster, user's operation procedure has been simplified, user's use experience has been promoted.

Description

Simulated flight cockpit with protection function

Technical Field

The utility model relates to the technical field of parts, parts or accessories of chairs or stools, in particular to a simulated flight deck with a protection function.

Background

The simulated flight may also be referred to as flight simulation, which refers to a motion of performing a flight simulation control and flight sensory feedback on various elements encountered in a real-world flight, such as aerodynamic force, weather, geographical environment, flight control system, flight electronic system, fighter flight weapon system, ground flight guidance, etc., through computer software, comprehensively in a computer. It was first applied to ground flight training for civil or military pilots, but with the development of personal computers, simulated flight platforms based on home computers are also popular.

In order to strengthen the immersion of simulated flight, the cockpit is generally arranged independently, and the cockpit is provided with three degrees of freedom or six degrees of freedom, so that more realistic experience is achieved, and the experience cabin is generally arranged in a science and technology city, a market, a recreation ground and the like, but the inner part of the existing simulated flight cockpit is only provided with a seat, when children enter the experience, the children generally shake left and right to increase the immersion due to the fact that the cockpit can shake left and right to increase the immersion, the risk of foot loss and fall in the experience process is caused, personal injury is caused to the user, and damage is caused to internal equipment.

Disclosure of Invention

The utility model aims to at least solve one of the technical problems in the prior art, provides a simulated flight cockpit with a protection function, and can solve the problem of insufficient protection of the simulated flight cockpit.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a simulation flight cockpit that possesses safeguard function, includes the cabin body, the inside of cabin body sets up to cavity, the entry has been seted up to the front side surface of cabin body, the front side of cabin body is provided with the running-board, the diapire fixedly connected with seat of cabin body, the seat comprises the cushion, the handrail and back, wherein cushion fixed connection is at the diapire of cabin body, the handrail sets up in the both sides of cushion, back fixed connection is at the upper surface of cushion, the inside of back sets up to cavity, the left side surface rotation of back is connected with the swinging boom, the right side surface rotation of swinging boom runs through the right side surface of back, the upper surface fixedly connected with fixed bolster of swinging boom, the one end fixedly connected with spacing of swinging boom is kept away from to the fixed bolster, be provided with limit structure on the back.

Preferably, the limiting structure comprises a driving motor, the driving motor is fixedly connected to the inner wall of the right side of the backrest, and the output end of the driving motor is fixedly connected with a threaded rod.

Preferably, the left end of the threaded rod is rotationally connected with the left inner wall of the backrest, and a thread plate is sleeved on the outer surface thread of the threaded rod.

Preferably, the outer surface of the rotating arm positioned inside the backrest is provided with a sliding groove, and the inside of the sliding groove is connected with a limiting block in a sliding way.

Preferably, the upper surface of the limiting block extends out of the sliding groove, the upper surface of the limiting block is fixedly connected with a driving ring, and the driving ring is in sliding connection with the outer surface of the rotating arm.

Preferably, the outer surface of the driving ring is sleeved with two ratchets, the ratchets of the two ratchets are oppositely arranged, and the thread plate is rotatably sleeved on the outer surface of the driving ring.

Preferably, the inner wall fixedly connected with expansion block of back, the inside of expansion block sets up to the cavity, and the inside sliding connection of expansion block has the locking piece.

Preferably, the front side surface of the locking block penetrates through the front side surface of the telescopic block in a sliding mode, the rear side surface of the locking block is fixedly connected with a spring, and the rear end of the spring is fixedly connected with the inner wall of the telescopic block.

Compared with the prior art, the utility model has the beneficial effects that:

this simulation flight cockpit that possesses safeguard function, when using this simulation flight cockpit, get into the inside of cabin body through the running-board, after sitting on the seat afterwards, utilize both hands to stimulate the fixed bolster, the fixed bolster is rotated around the swinging boom after being pulled, the fixed bolster rotates at the spacing that moves, the spacing rotates the back and laminating with the human body, and the fixed bolster also laminates with the shoulder this moment, under limit structure's effect, the swinging boom can only rotate to same direction this moment, so need not additionally to lock, through above-mentioned structure, can make the user when using this simulation flight cockpit, can not produce the risk that the foot falls down because of the rocking of cabin, simultaneously because the spacing is soft rubber material with the fixed bolster surface, avoid producing painful sense because of frequent striking that rocks the production makes the user, and because limit structure's effect, need not to carry out further locking after pulling down the fixed bolster, user's operation procedure has been simplified, user's use experience has been promoted.

This simulation flight cockpit that possesses safeguard function, when the swinging boom rotates forward, under the effect of sliding tray and stopper, drive the actuating ring in step and rotate, the actuating ring drives two ratchet rotations in step, locking piece and right side ratchet contact this moment, and owing to slope form and locking piece laminating on the ratchet, so when rotating, the ratchet can extrude the locking piece backward, the locking piece removes compression spring, so can not restrict the rotation of right side ratchet, the swinging boom rotates smoothly, after the user has adjusted, because the ratchet can't counter-rotate under the restriction of locking piece, so the swinging boom also can't rotate, and then accomplish the locking, when wanting the unblock, drive the threaded rod through driving motor synchronization, the threaded rod, because the top cover of threaded plate has been equipped with the movement track of drive ring restriction screw plate, so the threaded rod will drive the screw plate and carry out horizontal reverse movement when rotating, because the screw plate establishes on the actuating ring for the rotation cover, so can drive the drive ring and remove two ratchet, left side ratchet and locking piece laminating after two ratchet removal, because reverse setting up so can't rotate the limit pad, can carry out the operation with the limit pad with the user, and can't be fixed with the limit pad, and the user can carry out the operation with the limit pad when the use, and the limit pad is fixed.

Drawings

The utility model is further illustrated by the following examples in conjunction with the accompanying drawings:

FIG. 1 is a schematic view of a simulated flight deck with protection according to the present utility model;

FIG. 2 is a schematic view of a fixing pad according to the present utility model;

FIG. 3 is a schematic view of a limiting structure of the present utility model;

FIG. 4 is a schematic view of a telescopic block according to the present utility model;

FIG. 5 is a schematic cross-sectional view of a telescopic block according to the present utility model.

Reference numerals: 1. a cabin body; 2. an inlet; 3. a foot pedal; 4. a cushion; 5. an armrest; 6. a backrest; 7. a rotating arm; 8. a fixing pad; 9. a limiting frame; 10. a driving motor; 11. a threaded rod; 12. a thread plate; 13. a sliding groove; 14. a limiting block; 15. a drive ring; 16. a ratchet wheel; 17. a telescopic block; 18. a locking block; 19. and (3) a spring.

Detailed Description

Reference will now be made in detail to the present embodiments of the present utility model, examples of which are illustrated in the accompanying drawings, wherein the accompanying drawings are used to supplement the description of the written description so that one can intuitively and intuitively understand each technical feature and overall technical scheme of the present utility model, but not to limit the scope of the present utility model.

In the description of the present utility model, it should be understood that references to orientation descriptions such as upper, lower, front, rear, left, right, etc. are based on the orientation or positional relationship shown in the drawings, are merely for convenience of description of the present utility model and to simplify the description, and do not indicate or imply that the apparatus or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present utility model.

In the description of the present utility model, greater than, less than, exceeding, etc. are understood to exclude this number, and above, below, within, etc. are understood to include this number. The description of the first and second is for the purpose of distinguishing between technical features only and should not be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated or implicitly indicating the precedence of the technical features indicated.

In the description of the present utility model, unless explicitly defined otherwise, terms such as arrangement, installation, connection, etc. should be construed broadly and the specific meaning of the terms in the present utility model can be reasonably determined by a person skilled in the art in combination with the specific contents of the technical scheme.

Referring to fig. 1-5, the present utility model provides a technical solution: the utility model provides a simulated flight cockpit with protection function, cabin body 1's inside sets up to cavity, cabin body 1's front side surface has seted up entry 2, cabin body 1's front side is provided with running-board 3, cabin body 1's diapire fixedly connected with seat, the seat comprises cushion 4, handrail 5 and back 6, wherein cushion 4 fixedly connected with is in cabin body 1's diapire, handrail 5 sets up in cushion 4's both sides, back 6 fixedly connected with is at cushion 4's upper surface, back 6's inside sets up to cavity, back 6's left side surface rotates and is connected with swinging boom 7, swinging boom 7's right side surface rotates and runs through back 6's right side surface, swinging boom 7's upper surface fixedly connected with fixed bolster 8, one end fixedly connected with spacing 9 of swinging boom 7 is kept away from to fixed bolster 8, be provided with limit structure on back 6, the outer surfaces of the limiting frame 9 and the fixed pad 8 are both provided with soft rubber materials, when the simulated flight cockpit is used, the simulated flight cockpit enters the cabin body 1 through the foot pedals 3, then after sitting on a seat, the fixed pad 8 is pulled by two hands, the fixed pad 8 rotates around the rotating arm 7, the fixed pad 8 rotates while the limiting frame 9 rotates, the limiting frame 9 rotates and is attached to a human body, the fixed pad 8 is attached to the shoulder at the moment, the rotating arm 7 only rotates in the same direction under the action of the limiting structure, no extra locking is needed, by the structure, a user can not fall down due to shaking of the cabin when using the simulated flight cockpit, meanwhile, because the outer surfaces of the limiting frame 9 and the fixed pad 8 are both made of soft rubber materials, the pain of the user caused by frequent impact caused by shaking is avoided, and because of the effect of the limiting structure, the fixing pad 8 does not need to be further locked after being pulled down, so that the operation steps of a user are simplified, and the use experience of the user is improved.

Further, the limiting structure comprises a driving motor 10, the driving motor 10 is fixedly connected to the right inner wall of the backrest 6, the output end of the driving motor 10 is fixedly connected with a threaded rod 11, the left end of the threaded rod 11 is rotationally connected with the left inner wall of the backrest 6, a threaded plate 12 is sleeved on the outer surface of the threaded rod 11, a sliding groove 13 is formed in the outer surface of the rotating arm 7 positioned in the backrest 6, a limiting block 14 is slidingly connected in the sliding groove 13, the upper surface of the limiting block 14 extends out of the sliding groove 13, a driving ring 15 is fixedly connected to the upper surface of the limiting block 14, the driving ring 15 is slidingly connected with the outer surface of the rotating arm 7, two ratchet wheels 16 are sleeved on the outer surface of the driving ring 15, ratchet wheels of the two ratchet wheels 16 are oppositely arranged, the threaded plate 12 is rotationally sleeved on the outer surface of the driving ring 15, a telescopic block 17 is fixedly connected to the inner wall of the backrest 6, the telescopic block 17 is hollow, the inside of the telescopic block 17 is connected with a locking block 18 in a sliding way, the front side surface of the locking block 18 penetrates through the front side surface of the telescopic block 17 in a sliding way, the rear side surface of the locking block 18 is fixedly connected with a spring 19, the rear end of the spring 19 is fixedly connected with the inner wall of the telescopic block 17, when the rotating arm 7 rotates forwards, under the action of the sliding groove 13 and the limiting block 14, the driving ring 15 is synchronously driven to rotate, the driving ring 15 synchronously drives the two ratchets 16 to rotate, at the moment, the locking block 18 contacts with the right side ratchet 16, and the inclined shape on the ratchet 16 is attached to the locking block 18, so that the ratchet 16 can press the locking block 18 backwards during rotation, the locking block 18 moves to compress the spring 19, the rotation of the right side ratchet 16 is not limited, the rotating arm 7 rotates smoothly, after the user adjusts the rotation of the ratchet 16 cannot rotate reversely under the limitation of the locking block 18, therefore, the rotating arm 7 cannot rotate, and further locking is completed, when unlocking is required, the threaded rod 11 is synchronously driven by the driving motor 10, the threaded rod 11 is sleeved with the driving ring 15 above the threaded plate 12 to limit the movement track of the threaded plate 12, so that the threaded plate 12 is driven to horizontally reversely move when the threaded rod 11 rotates, the driving ring 15 is driven to synchronously move because the threaded plate 12 is rotationally sleeved on the driving ring 15, the driving ring 15 drives the two ratchet wheels 16 to move, the left ratchet wheels 16 are attached to the locking block 18 after the two ratchet wheels 16 move, and the rotating arm 7 can only rotate clockwise under the limit of the left ratchet wheels 16 due to reverse arrangement, so that the fixing pad 8 and the limiting frame 9 are unlocked.

Working principle: when the simulated flight cockpit is used, the pedal 3 is used for entering the cockpit body 1, then after the cockpit is seated on a seat, the fixed pad 8 is pulled by two hands, the fixed pad 8 is pulled to rotate around the rotating arm 7, the fixed pad 8 rotates and simultaneously rotates the movable limiting frame 9, the limiting frame 9 is attached to a human body after rotating, the fixed pad 8 is attached to the shoulder at the moment, the rotating arm 7 only rotates in the same direction under the action of the limiting structure, no extra locking is needed, when the rotating arm 7 rotates forwards, the driving ring 15 is synchronously driven to rotate under the action of the sliding groove 13 and the limiting block 14, the driving ring 15 synchronously drives the two ratchets 16 to rotate, at the moment, the locking block 18 contacts with the right ratchet 16, and the ratchet 16 presses the locking block 18 backwards when rotating due to the oblique shape on the ratchet 16 attached to the locking block 18, the locking block 18 moves the compression spring 19, so the rotation of the right ratchet wheel 16 is not limited, the rotating arm 7 smoothly rotates, when a user adjusts, the ratchet wheels 16 cannot reversely rotate under the limitation of the locking block 18, so the rotating arm 7 cannot rotate, further locking is finished, when unlocking is required, the threaded rod 11 is synchronously driven by the driving motor 10 to rotate, the threaded rod 11 is sleeved with the driving ring 15 above the threaded plate 12 to limit the movement track of the threaded plate 12, the threaded rod 11 drives the threaded plate 12 to horizontally reversely move when rotating, the driving ring 15 is driven to synchronously move because the threaded plate 12 is rotatably sleeved on the driving ring 15, the driving ring 15 drives the two ratchet wheels 16 to move when moving, the left ratchet wheel 16 is attached to the locking block 18 after the two ratchet wheels 16 move, under the limitation of the left ratchet wheel 16 due to reverse arrangement, the rotating arm 7 can only rotate clockwise, and then the fixed pad 8 and the limiting frame 9 are unlocked.

The embodiments of the present utility model have been described in detail with reference to the accompanying drawings, but the present utility model is not limited to the above embodiments, and various changes can be made within the knowledge of one of ordinary skill in the art without departing from the spirit of the present utility model.

Claims (8)

1. The utility model provides a simulation flight deck that possesses safeguard function which characterized in that: including cabin body (1), the inside of cabin body (1) sets up to cavity, entry (2) have been seted up to the front side surface of cabin body (1), the front side of cabin body (1) is provided with running-board (3), the diapire fixedly connected with seat of cabin body (1), the seat comprises cushion (4), handrail (5) and back (6), wherein cushion (4) fixedly connected with is at the diapire of cabin body (1), handrail (5) set up in the both sides of cushion (4), back (6) fixedly connected with is at the upper surface of cushion (4), the inside of back (6) sets up to cavity, the left side surface swivelling joint of back (6) is by swinging boom (7), the right side surface of swinging boom (7) swivelling joint runs through the right side surface of back (6), upper surface fixedly connected with fixed bolster (8) of swinging boom (7), one end fixedly connected with spacing (9) of swinging boom (7) are kept away from to fixed bolster (8), be provided with limit structure on back (6).

2. A simulated flight deck with protection as claimed in claim 1, wherein: the limiting structure comprises a driving motor (10), wherein the driving motor (10) is fixedly connected to the inner wall of the right side of the backrest (6), and the output end of the driving motor (10) is fixedly connected with a threaded rod (11).

3. A simulated flight deck with protection as claimed in claim 2, wherein: the left end of the threaded rod (11) is rotatably connected with the left inner wall of the backrest (6), and a thread plate (12) is sleeved on the outer surface of the threaded rod (11) in a threaded manner.

4. A simulated flight deck with protection as claimed in claim 1, wherein: the outer surface of the rotating arm (7) positioned inside the backrest (6) is provided with a sliding groove (13), and the inside of the sliding groove (13) is connected with a limiting block (14) in a sliding way.

5. The simulated flight deck with protection as claimed in claim 4, wherein: the upper surface of the limiting block (14) extends out of the sliding groove (13), the upper surface of the limiting block (14) is fixedly connected with a driving ring (15), and the driving ring (15) is in sliding connection with the outer surface of the rotating arm (7).

6. The simulated flight deck with protection as claimed in claim 5, wherein: the outer surface of the driving ring (15) is sleeved with two ratchets (16), ratchets of the two ratchets (16) are oppositely arranged, and the thread plate (12) is rotatably sleeved on the outer surface of the driving ring (15).

7. A simulated flight deck with protection as claimed in claim 1, wherein: the inner wall of the backrest (6) is fixedly connected with a telescopic block (17), the inside of the telescopic block (17) is hollow, and a locking block (18) is slidably connected in the telescopic block (17).

8. The simulated flight deck with protection as claimed in claim 7, wherein: the front side surface of the locking block (18) penetrates through the front side surface of the telescopic block (17) in a sliding mode, a spring (19) is fixedly connected to the rear side surface of the locking block (18), and the rear end of the spring (19) is fixedly connected with the inner wall of the telescopic block (17).