Aircraft simulator with display screen adjusting mechanism

By designing a motor-driven display screen adjustment structure in the aircraft simulator, the problem that the display screen cannot be adjusted in the prior art is solved, and the use and shock absorption effects are achieved to adapt to users of different heights, which improves the practicality of the equipment.

CN222190091UActive Publication Date: 2024-12-17ZHANGZHOU SHIHUI ELECTRONIC TECH CO LTD
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Patent Information

Application Number
CN202420599390.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-03-27
Publication Date
2024-12-17
Estimated Expiration
2034-03-27

AI Technical Summary

Technical Problem

The display screen of the existing aircraft simulator cannot be adjusted in height and cannot be adapted to people of different heights for viewing, which is less practical.

Method used

An adjustment structure including a motor, rotary rod, pulley, gear, support cylinder, tooth plate and self-locking telescopic rod is designed. The rotary rod and pulley are driven by the motor, and the gears and tooth plates are driven to lift and lower, so as to realize the height adjustment of the display screen. , and achieve shock absorption effect through support rods and sliding sleeves.

Benefits of technology

The height adjustment of the display screen is realized, adapted to people of different heights, and provides shock absorption during the simulation process, improving the practicality of the equipment.

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Abstract

The utility model relates to the technical field of aircraft simulators, and discloses an aircraft simulator with a display screen adjusting mechanism, which comprises a bottom plate, the top of the bottom plate is fixedly connected with a chair cabin, the top of the chair cabin is fixedly connected with a support plate, the top of the bottom plate is fixedly connected with a support block, and the support block is fixedly connected with a display screen. An adjusting structure is fixedly connected to the top of the supporting block, a damping structure is fixedly connected to the interior of the chair bin, a seat is fixedly connected to the top of the damping structure, and the adjusting structure comprises a motor, a first rotating rod, a first belt pulley, a second rotating rod, a second belt pulley, a transmission belt, a gear, a supporting cylinder, a toothed plate, a display screen and a self-locking telescopic rod. The motor drives the first rotating rod to rotate, the transmission belt drives the first belt wheel and the second belt wheel to rotate, the gear is driven to rotate, the gear drives the toothed plate to ascend and descend, the display screen is driven to ascend and descend, and height adjustment of the display screen is achieved.
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Description

Technical Field

[0001] The utility model relates to the technical field of aircraft simulators, in particular to an aircraft simulator with a display screen adjustment mechanism. Background Art

[0002] The flight simulator uses real-time simulation technology to reproduce the cockpit and airborne flight environment on the ground. It is used for initial, modification and refresher training of pilots for takeoff, climb, turn, landing and maneuvering. It is not restricted by weather conditions and sites and can make flight personnel familiar with the driving techniques of the aircraft type in a relatively short period of time.

[0003] For example, the Chinese patent: "CN215987687U", the technical solution disclosed in this patent is as follows: an environmental simulator for simulating aircraft is disclosed, including a base assembly, a cabin assembly is arranged on the top of the base assembly, a control assembly is arranged on the right side of the cabin assembly, the base assembly includes a bottom plate, a movable boarding ladder is movably installed on the top of the bottom plate, a supporting hydraulic rod is movably installed on the top of the bottom plate, and the cabin assembly includes a fixed ring movably installed on the top of the supporting hydraulic rod. The environmental simulator for simulating aircraft can be operated by the user in the cabin, and the supporting hydraulic rod and the moving plate can be driven by the control assembly to achieve initial actions such as take-off and landing. The 3D landscape data of various parts of the world can be displayed through the map data analyzer, and the 3D map appearance of various parts of the world can be truly restored through the environmental simulation display screen, so as to enhance the user experience. At the same time, in conjunction with the meteorological data analyzer, the real weather of the location restored by the environmental simulation display screen can be displayed in real time, which is closer to reality.

[0004] However, in actual use, the simulator's display screen cannot be adjusted in height and cannot be viewed by people of different heights, making it less practical. Utility Model Content

[0005] 1. Technical issues to be solved

[0006] In view of the deficiencies of the prior art, the utility model provides an aircraft simulator with a display screen adjustment mechanism.

[0007] (II) Technical solution

[0008] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aircraft simulator with a display screen adjustment mechanism, comprising a base plate, a chair compartment fixedly connected to the top of the base plate, a support plate fixedly connected to the top of the chair compartment, a support block fixedly connected to the top of the base plate, an adjustment structure fixedly connected to the top of the support block, a shock absorbing structure fixedly connected to the inside of the chair compartment, a seat fixedly connected to the top of the shock absorbing structure, the adjustment structure comprising a motor, a first rotating rod, a first pulley, a second rotating rod, a second pulley, a transmission belt, a gear, a support cylinder, a toothed plate, a display screen, and a self-locking telescopic rod, the motor is fixedly connected to the top of the support block, the first rotating rod is fixedly connected to the output end of the motor, the first pulley is fixedly connected to the first rotating rod, the second rotating rod is rotatably connected to the inside of the support plate, the second pulley is fixedly connected to the second rotating rod, the transmission belt is wound around the outside of the first pulley and the second pulley, the motor is installed to drive the first rotating rod to rotate, the first rotating rod drives the first pulley to rotate, and the transmission belt is installed to drive the first pulley and the second pulley to rotate.

[0009] Preferably, the gear is fixedly connected to the first rotating rod, the supporting tube is fixedly connected to the top of the base plate, the tooth plate is slidably connected to the inside of the supporting tube, the tooth plate and the gear are meshed with each other, and the gear is installed to drive the tooth plate to telescopically move.

[0010] Preferably, the display screen is fixedly connected to the top of the toothed plate, the self-locking telescopic rod is fixedly connected to the top of the bottom plate, the other end of the self-locking telescopic rod is fixedly connected to the bottom of the display screen, and the toothed plate is installed to drive the display screen to move up and down.

[0011] Preferably, the shock absorbing structure includes a slide groove, which is fixedly connected to the top of the chair compartment, and the interior of the slide groove is slidably connected to a vertical plate, which is fixedly connected to the bottom of the seat.

[0012] Preferably, a cross bar is fixedly connected to the interior of the chair compartment, a first sliding sleeve is slidably connected to the left side of the cross bar, a first support rod is hinged to the top of the first sliding sleeve, the other end of the first support rod is hinged to the bottom of the seat, a second sliding sleeve is slidably connected to the cross bar, and the first support rod is installed to drive the first sliding sleeve to slide on the cross bar.

[0013] Preferably, the top of the second sliding sleeve is hinged with a second support rod, the other end of the second support rod is hinged to the bottom of the seat, the bottom of the chair compartment is fixedly connected with a first telescopic rod, a spring is wound around the outside of the first telescopic rod, the top of the first telescopic rod is fixedly connected to the bottom of the vertical plate, and the first telescopic rod and the spring are installed for shock absorption.

[0014] (III) Beneficial effects

[0015] Compared with the prior art, the utility model provides an aircraft simulator with a display screen adjustment mechanism, which has the following beneficial effects:

[0016] 1. An aircraft simulator with a display screen adjustment mechanism drives the first rotating rod to rotate through a motor, and drives the first pulley and the second pulley to rotate through a transmission belt, and drives the gear to rotate. The gear drives the toothed plate to move up and down, drives the display screen to move up and down, and realizes the height adjustment of the display screen.

[0017] 2. The aircraft simulator with a display screen adjustment mechanism drives the first sliding sleeve to slide on the cross bar through the first support rod, drives the second sliding sleeve to slide on the cross bar through the second support rod, and performs shock-absorbing treatment on the first telescopic rod and the spring to achieve a shock-absorbing effect during simulation. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The accompanying drawings are used to provide a further understanding of the present invention and constitute a part of the specification. Together with the embodiments of the present invention, they are used to explain the present invention and do not constitute a limitation of the present invention. In the accompanying drawings:

[0019] Figure 1 It is a front view of the structure of the utility model;

[0020] Figure 2 It is a first cross-sectional view of the structure of the utility model;

[0021] Figure 3 It is a second cross-sectional view of the structure of the utility model;

[0022] Figure 4 It is an enlarged view of point A of the structure of the present utility model.

[0023] In the figure: 1. bottom plate; 2. chair compartment; 3. support plate; 4. support block; 5. adjustment structure; 511. motor; 512. first rotating rod; 513. first pulley; 514. second rotating rod; 515. second pulley; 516. transmission belt; 517. gear; 518. support cylinder; 519. tooth plate; 520. display screen; 521. self-locking telescopic rod; 6. shock absorbing structure; 611. slide groove; 612. vertical plate; 613. first telescopic rod; 614. spring; 615. cross bar; 616. first sliding sleeve; 617. second sliding sleeve; 618. first support rod; 619. second support rod; 7. seat. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0025] Example 1

[0026] like Figure 1 , 3 As shown in Figure 4, the utility model provides an aircraft simulator with a display screen adjustment mechanism, including a base plate 1, a chair compartment 2 is fixedly connected to the top of the base plate 1, a support plate 3 is fixedly connected to the top of the chair compartment 2, a support block 4 is fixedly connected to the top of the base plate 1, an adjustment structure 5 is fixedly connected to the top of the support block 4, a shock absorbing structure 6 is fixedly connected to the inside of the chair compartment 2, a seat 7 is fixedly connected to the top of the shock absorbing structure 6, the adjustment structure 5 includes a motor 511, a first rotating rod 512, a first pulley 513, a second rotating rod 514, a second pulley 515, a transmission belt 516, a gear 517, a support cylinder 518, a toothed plate 519, a display screen 520, and a self-locking telescopic rod 521. The motor 511 is fixedly connected to the top of the support block 4, the first rotating rod 512 is fixedly connected to the output end of the motor 511, the first pulley 513 is fixedly connected to the first rotating rod 512, the second rotating rod 514 is rotatably connected to the inside of the support plate 3, and the second pulley 515 is fixedly connected to the second rotating rod 514, and the transmission belt 516 is wound around the outside of the first pulley 513 and the second pulley 515. The motor 511 is installed to drive the first rotating rod 512 to rotate, and the first rotating rod 512 drives the first pulley 513 to rotate. The transmission belt 516 is installed to drive the first pulley 513 and the second pulley 515 to rotate. The gear 517 is fixedly connected to the first rotating rod 512, the support cylinder 518 is fixedly connected to the top of the base plate 1, the toothed plate 519 is slidably connected to the inside of the support cylinder 518, the toothed plate 519 and the gear 517 are meshed with each other, and the gear 517 is installed to drive the toothed plate 519 to telescopically move. The display screen 520 is fixedly connected to the top of the toothed plate 519, the self-locking telescopic rod 521 is fixedly connected to the top of the base plate 1, and the other end of the self-locking telescopic rod 521 is fixedly connected to the bottom of the display screen 520, and the toothed plate 519 is installed to drive the display screen 520 to move up and down.

[0027] In this embodiment, the first rotating rod 512 is driven to rotate by the motor 511, and the first pulley 513 and the second pulley 515 are driven to rotate by the transmission belt 516, so that the gear 517 is driven to rotate and the toothed plate 519 is driven to rise and fall, thereby realizing the height adjustment of the display screen 520.

[0028] Example 2

[0029] like Figure 1 , 2As shown, on the basis of embodiment 1, the utility model provides a technical solution: the shock absorbing structure 6 includes a slide groove 611, the slide groove 611 is fixedly connected to the top of the chair compartment 2, the interior of the slide groove 611 is slidably connected to a vertical plate 612, the vertical plate 612 is fixedly connected to the bottom of the seat 7, the interior of the chair compartment 2 is fixedly connected to a cross bar 615, the left side of the cross bar 615 is slidably connected to a first sliding sleeve 616, the top of the first sliding sleeve 616 is hinged to a first support rod 618, the other end of the first support rod 618 is hinged to the bottom of the seat 7, and the cross bar 615 is fixedly connected to the bottom of the seat 7. The upper sliding part is connected with a second sliding sleeve 617, and a first support rod 618 is installed to drive the first sliding sleeve 616 to slide on the cross bar 615. The top of the second sliding sleeve 617 is hinged with a second support rod 619, and the other end of the second support rod 619 is hinged to the bottom of the seat 7. The bottom of the chair compartment 2 is fixedly connected with a first telescopic rod 613, and a spring 614 is wound around the outside of the first telescopic rod 613. The top of the first telescopic rod 613 is fixedly connected to the bottom of the vertical plate 612, and the first telescopic rod 613 and the spring 614 are installed for shock absorption.

[0030] In this embodiment, the first support rod 618 drives the first sliding sleeve 616 to slide on the cross bar 615, the second support rod 619 drives the second sliding sleeve 617 to slide on the cross bar 615, and the first telescopic rod 613 and the spring 614 are subjected to shock absorption treatment to achieve the shock absorption effect during simulation.

[0031] The working principle of the aircraft simulator with a display screen adjustment mechanism will be described in detail below.

[0032] like Figure 1 , 2 As shown in Figures 3 and 4, when in use, the motor 511 is started, the motor 511 drives the first rotating rod 512 to rotate, the first rotating rod 512 drives the first pulley 513 to rotate, and the second pulley 515 is driven to rotate through the transmission belt 516, the first rotating rod 512 drives the gear 517 to rotate, the gear 517 drives the toothed plate 519 to slide inside the supporting tube 518, so as to drive the display screen 520 to move up and down, so as to achieve the height adjustment of the display screen 520, and the seat 7 can be shock-absorbing during simulation, the first support rod 618 drives the first sliding sleeve 616 to slide on the cross bar 615, the second support rod 619 drives the second sliding sleeve 617 to slide on the cross bar 615, and the first telescopic rod 613 and the spring 614 can be shock-absorbing.

Claims

1. An aircraft simulator with a display screen adjustment mechanism, comprising a base plate (1), characterized in that: The top of the bottom plate (1) is fixedly connected to a chair compartment (2), the top of the chair compartment (2) is fixedly connected to a support plate (3), the top of the bottom plate (1) is fixedly connected to a support block (4), the top of the support block (4) is fixedly connected to an adjustment structure (5), the interior of the chair compartment (2) is fixedly connected to a shock absorbing structure (6), and the top of the shock absorbing structure (6) is fixedly connected to a seat (7); The adjustment structure (5) comprises a motor (511), a first rotating rod (512), a first pulley (513), a second rotating rod (514), a second pulley (515), a transmission belt (516), a gear (517), a support cylinder (518), a toothed plate (519), a display screen (520), and a self-locking telescopic rod (521); The motor (511) is fixedly connected to the top of the support block (4), the first rotating rod (512) is fixedly connected to the output end of the motor (511), the first pulley (513) is fixedly connected to the first rotating rod (512), the second rotating rod (514) is rotatably connected to the inside of the support plate (3), the second pulley (515) is fixedly connected to the second rotating rod (514), and the transmission belt (516) is wound around the outside of the first pulley (513) and the second pulley (515).

2. An aircraft simulator with a display screen adjustment mechanism according to claim 1, characterized in that: The gear (517) is fixedly connected to the first rotating rod (512), the support tube (518) is fixedly connected to the top of the bottom plate (1), the tooth plate (519) is slidably connected to the inside of the support tube (518), and the tooth plate (519) and the gear (517) are meshed with each other.

3. The aircraft simulator with a display screen adjustment mechanism according to claim 2, characterized in that: The display screen (520) is fixedly connected to the top of the toothed plate (519), the self-locking telescopic rod (521) is fixedly connected to the top of the bottom plate (1), and the other end of the self-locking telescopic rod (521) is fixedly connected to the bottom of the display screen (520).

4. The aircraft simulator with a display screen adjustment mechanism according to claim 1, characterized in that: The shock absorbing structure (6) comprises a slide groove (611), wherein the slide groove (611) is fixedly connected to the top of the chair compartment (2), and the interior of the slide groove (611) is slidably connected to a vertical plate (612), and the vertical plate (612) is fixedly connected to the bottom of the seat (7).

5. The aircraft simulator with a display screen adjustment mechanism according to claim 4, characterized in that: The interior of the chair compartment (2) is fixedly connected to a cross bar (615), the left side of the cross bar (615) is slidably connected to a first sliding sleeve (616), the top of the first sliding sleeve (616) is hinged to a first support rod (618), the other end of the first support rod (618) is hinged to the bottom of the seat (7), and the cross bar (615) is slidably connected to a second sliding sleeve (617).

6. The aircraft simulator with a display screen adjustment mechanism according to claim 5, characterized in that: The top of the second sliding sleeve (617) is hinged with a second support rod (619), the other end of the second support rod (619) is hinged to the bottom of the seat (7), the bottom of the chair compartment (2) is fixedly connected with a first telescopic rod (613), a spring (614) is wound around the outside of the first telescopic rod (613), and the top of the first telescopic rod (613) is fixedly connected to the bottom of the vertical plate (612).

Citation Information

Patent Citations

  • Environment simulator for simulating aircraft

    CN215987687U