Simulation cabin for civil aviation teaching

By introducing a shaking mechanism and a micro vibration motor in the civil aviation simulation cockpit, the acceleration and deceleration changes in flight are simulated, and the problem that traditional simulated cockpits cannot restore the real flight experience is solved, achieving a more realistic flight experience and more efficient training effect .

CN222190092UActive Publication Date: 2024-12-17HENAN SHENGSHI AVIATION SERVICE CO LTD
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Patent Information

Application Number
CN202421300354.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-07
Publication Date
2024-12-17
Estimated Expiration
2034-06-07

AI Technical Summary

Technical Problem

The traditional civil aviation simulation cockpit cannot restore the acceleration and deceleration changes in flight through shaking, resulting in limited training effects and the real flight experience cannot be fully simulated.

Method used

A simulated cockpit for civil aviation teaching was designed, using a base, guide chute, bracket and shaking mechanism. Through a single chip computer, a micro vibration motor and a motor-driven shaking mechanism, it can shake back and forth during flight, enhancing the immersion and realism.

Benefits of technology

Simulate acceleration and deceleration changes in flight by swaying back and forth, providing a more realistic flight experience, improving the pilot's training effect and experience, and enhancing immersion and realism.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a simulation cabin for civil aviation teaching. The simulation cabin comprises a base, a guide chute and a support. Guide grooves are formed in the left end and the right end of the upper surface of the base, supporting blocks are slidably connected to the front end and the rear end of the inner wall of each guide groove, and the upper surfaces of the uniformly-distributed supporting blocks are fixedly connected with the lower surface of a simulation cabin; the guide sliding groove is formed in the middle of the upper surface of the base, a shaking mechanism is arranged in the guide sliding groove, the front end and the rear end of the shaking mechanism extend out of the front end and the rear end of the base respectively, and the upper end of the shaking mechanism is fixedly connected with the lower surface of the simulation cabin; the supports are all located on the front side face of the base, the top ends of the supports are all provided with displayers, according to the simulation cabin for civil aviation teaching, the acceleration and deceleration changes in the movement process can be felt through front-back shaking, the actual dynamic experience can be restored more truly, and the more vivid effect is provided.
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Description

Technical Field

[0001] The utility model relates to the technical field of teaching simulation cockpits, in particular to a simulation cockpit for civil aviation teaching. Background Art

[0002] The equipment used to simulate the cockpit in civil aviation teaching is called a simulated cockpit training device or flight simulator. It is a device that replicates the cockpit of a real aircraft and is used to train and train civil aviation pilots. The simulated cockpit is usually used in conjunction with flight simulation software, which simulates the aircraft's flight dynamics, meteorological conditions, mechanical systems and other factors, allowing pilots to conduct various types of training in a simulated environment, such as takeoff, landing, flight operations and emergency procedures. In the traditional simulated cockpit, a static cockpit is used to restore the real flight scene. It usually consists of a simulated cabin and a display, and uses images and sound effects to simulate takeoff, flight, landing and other scenes. In the traditional simulated cockpit, the real flight scene can only be restored through visual, sound effects and other means, and the element of shaking is not included. Compared with the real flight experience, the training effect of this "static cockpit" is subject to certain limitations and cannot completely restore the effects of takeoff, flight, landing and other scenes. For this reason, we propose a simulated cockpit for civil aviation teaching. Utility Model Content

[0003] The technical problem to be solved by the utility model is to overcome the existing defects and provide a simulated cockpit for civil aviation teaching. By shaking back and forth, the changes in acceleration and deceleration during movement can be felt, the actual dynamic experience can be restored more realistically, a more realistic effect can be provided, and the problems in the background technology can be effectively solved.

[0004] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a simulated cockpit for civil aviation teaching, comprising a base, a guide slide and a bracket;

[0005] Base: Guide grooves are respectively provided at the left and right ends of the upper surface thereof, and support blocks are slidably connected to the front and rear ends of the inner wall of the guide grooves, and the upper surfaces of the evenly distributed support blocks are fixedly connected to the lower surface of a simulation cabin;

[0006] Guide chute: It is opened in the middle of the upper surface of the base, and a shaking mechanism is arranged inside the guide chute. The front and rear ends of the shaking mechanism extend to the outside of the front and rear ends of the base respectively, and the upper ends of the shaking mechanism are fixedly connected to the lower surface of the simulation cabin;

[0007] Bracket: They are all located on the front side of the base, and a display is provided on the top of the bracket;

[0008] Among them: it also includes a single-chip microcomputer, which is arranged on the right inner wall of the simulation cabin. The output end of the single-chip microcomputer is electrically connected to the input end of the display. By shaking back and forth, the changes in acceleration and deceleration during the movement can be felt, which can more realistically restore the actual dynamic experience and provide a more realistic effect.

[0009] Furthermore, the shaking mechanism includes a sliding column, a spring and a slider, the sliders are respectively slidably connected to the front and rear ends of the inner wall of the guide slide groove, the top ends of the two sliders are fixedly connected to the lower surface of a simulation cabin, the opposite outer side surfaces of the two sliders are respectively fixedly connected with sliding columns, the opposite outer end heads of the sliding columns are respectively slidably connected to the sliding holes at the adjacent ends of the base, the opposite outer end heads of the sliding columns extend to the outside of the front and rear ends of the base, springs are fixedly connected between the outer side surfaces of the two sliders and the inner walls of the adjacent guide slide grooves, and the springs are all mounted on the outer surfaces of the sliding columns. The characteristics of the springs can enhance the real shaking feeling of the simulated cabin when in use.

[0010] Furthermore, the shaking mechanism also includes a motor and a protrusion. The motor is installed on the upper surface of the base by bolts. The right end of the output shaft of the motor is fixedly connected with a protrusion. The protrusion is installed in cooperation with the two sliders to drive the shaking mechanism to operate.

[0011] Furthermore, seats are fixedly connected to the left and right ends of the bottom wall of the simulated cabin, respectively, to provide real seats for the simulated personnel.

[0012] Furthermore, it also includes a mounting plate, which is respectively mounted on the rear side surfaces of the two seats by bolts, so as to facilitate the maintenance or replacement of the micro vibration motor in the placement groove.

[0013] Furthermore, it also includes installation grooves, which are respectively opened on the rear sides of the two seats. The inner walls of the installation grooves are installed with micro vibration motors by bolts. The input ends of the micro vibration motors are electrically connected to the output ends of the single-chip microcomputer, which can physically enhance the immersive feeling during simulation.

[0014] Furthermore, evenly distributed perspective windows are respectively provided on the front and rear sides of the simulation cabin to provide a more realistic flying or driving experience.

[0015] Compared with the prior art, the beneficial effects of the utility model are: the simulated cockpit for civil aviation teaching has the following advantages:

[0016] 1. By controlling the operation of the display through the single-chip microcomputer and entering the flight simulation screen through the display, you can get a more realistic flight experience. The display can present realistic flight scenes, aircraft instruments, control panels, etc., making you feel as if you are in a real flight environment and enhancing the sense of immersion. Then when the simulated personnel sit in the seat in the simulation cabin for simulated flight, the simulated personnel controls the internal single-chip microcomputer to start, and the internal single-chip microcomputer sends a signal to the single-chip microcomputer, which makes a judgment and adjusts the operation of the micro-vibration motor behind the seat. By adding a micro-vibration motor behind the seat, the simulated flight personnel can be closer to the actual operation situation, so as to more realistically feel the vibration of civil aviation during flight, and improve the training effect and experience effect of the simulated personnel.

[0017] 2. At the same time, the single-chip computer makes a judgment and adjusts the operation of the motor. The output shaft of the motor drives the protrusion to rotate. When the protrusion rotates, the side with a larger arc contacts the adjacent slider, and the sliding column slides into the sliding hole in the middle of the base through the expansion and contraction of the spring, thereby driving the slider to slide forward or backward, thereby driving the simulation cabin to slide forward or backward. When the simulation cabin slides forward or backward, the support block slides forward or backward in the guide groove, which serves as a supporting component for the simulation cabin when it shakes forward or backward to keep the cabin stable. At the same time, the changes in acceleration and deceleration during the movement can be felt by shaking back and forth, which can more realistically restore the actual dynamic experience and provide a more realistic effect. The design of the perspective window can provide a very realistic flight or driving experience, allowing pilots and drivers to be trained and trained in a simulated environment. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the structure of the utility model;

[0019] Figure 2 It is a schematic diagram of the structure of the utility model in cross section;

[0020] Figure 3 It is a structural schematic diagram of a planar cross-section of the rocking mechanism of the utility model.

[0021] In the figure: 1 base, 2 guide groove, 3 support block, 4 seat, 5 simulation cabin, 6 mounting plate, 7 single chip computer, 8 display, 9 bracket, 10 perspective window, 11 guide slide groove, 12 shaking mechanism, 121 slide column, 122 spring, 123 slider, 124 motor, 125 bump, 13 micro vibration motor, 14 mounting groove. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0023] See also Figure 1-3 , This embodiment provides a technical solution: a simulated cockpit for civil aviation teaching, comprising a base 1, a guide chute 11 and a bracket 9;

[0024] Base 1: Guide grooves 2 are respectively provided at the left and right ends of its upper surface, and support blocks 3 are slidably connected to the front and rear ends of the inner wall of the guide groove 2. The upper surfaces of the evenly distributed support blocks 3 are fixedly connected to the lower surface of a simulation cabin 5. When the simulation cabin 5 slides forward or backward, the support blocks 3 slide forward or backward in the guide groove 2, and serve as a supporting component when the simulation cabin 5 shakes forward or backward to keep the cabin stable. The left and right ends of the bottom wall of the simulation cabin 5 are respectively fixedly connected with seats 4, and also include mounting plates 6, which are respectively installed on the rear sides of the two seats 4 by bolts, and also include mounting grooves 14, which are respectively opened on the rear sides of the two seats 4, and the inner walls of the mounting grooves 14 are respectively installed with micro-vibration motors 13 by bolts. The micro-vibration motors The input ends of 13 are electrically connected to the output ends of the single-chip computer 7. Then, when the simulated personnel sit in the seat 4 in the simulation cabin 5 for simulated flight, the simulated personnel controls the internal single-chip computer to start, and the internal single-chip computer sends a signal to the single-chip computer 7. The single-chip computer 7 makes a judgment to adjust the operation of the micro-vibration motor 13 behind the seat 4. By adding the micro-vibration motor 13 behind the seat 4, the simulated flight personnel can be closer to the actual operation situation, so as to feel the vibration of civil aviation during flight more realistically, and improve the training effect and experience effect of the simulated personnel. The front and rear sides of the simulation cabin 5 are respectively provided with evenly distributed perspective windows 10. The design of the perspective windows 10 can provide a very realistic flight or driving experience, so that pilots and drivers can be trained and trained in a simulated environment;

[0025] The guide slide groove 11 is opened in the middle of the upper surface of the base 1. A rocking mechanism 12 is arranged inside the guide slide groove 11. The front and rear ends of the rocking mechanism 12 extend to the outside of the front and rear ends of the base 1 respectively. The upper ends of the rocking mechanism 12 are fixedly connected to the lower surface of the simulation cabin 5. The rocking mechanism 12 includes a slide column 121, a spring 122 and a slider 123. The sliders 123 are slidably connected to the front and rear ends of the inner wall of the guide slide groove 11 respectively. The top ends of the two sliders 123 are fixedly connected to the lower surface of a simulation cabin 5. The opposite outer side surfaces of the two sliders 123 are fixedly connected with the slide columns 121 respectively. The opposite outer end heads of the slide columns 121 are respectively slidably connected with the sliding holes of the adjacent ends of the base 1. The opposite outer end heads of the slide columns 121 extend to the outside of the front and rear ends of the base 1 respectively. The outer side surfaces of the two sliders 123 are fixedly connected to the inner walls of the adjacent guide slide grooves 11 with springs 122. 2. The springs 122 are sleeved on the outer surface of the sliding column 121. The shaking mechanism 12 also includes a motor 124 and a protrusion 125. The motor 124 is installed on the upper surface of the base 1 by bolts. The right end of the output shaft of the motor 124 is fixedly connected with the protrusion 125. The protrusion 125 is installed in cooperation with the two sliders 123. At the same time, the single-chip microcomputer 7 makes a judgment to adjust the operation of the motor 124. The output shaft of the motor 124 drives the protrusion 125 to rotate. When the protrusion 125 rotates, the side with a larger arc contacts the adjacent slider 123, and the sliding column 121 is slid into the sliding hole in the middle of the base 1 through the expansion and contraction of the spring 122, thereby driving the slider 123 to slide forward or backward, thereby driving the simulation cabin 5 to slide forward or backward. At the same time, the acceleration and deceleration changes in the movement process can be felt by shaking back and forth, which can more realistically restore the actual dynamic experience and provide a more realistic effect.

[0026] Bracket 9: They are all located on the front side of the base 1. A display 8 is provided on the top of the bracket 9. The operation of the display 8 is controlled by the single-chip microcomputer 7. The flight simulation screen is entered through the display 8 to obtain a more realistic flight experience. The display 8 can present realistic flight scenes, aircraft instruments, control panels, etc., making you feel as if you are in a real flight environment, enhancing the sense of immersion.

[0027] The simulation cabin 5 further includes a single chip microcomputer 7 , which is arranged on the right inner wall of the simulation cabin 5 , and the output end of the single chip microcomputer 7 is electrically connected to the input end of the display 8 .

[0028] The working principle of a simulated cockpit for civil aviation teaching provided by the utility model is as follows: first, the display 8 is controlled to operate by the single-chip microcomputer 7, and a more realistic flight experience can be obtained by entering the flight simulation screen through the display 8. The display 8 can present realistic flight scenes, aircraft instruments, control panels, etc., making you feel as if you are in a real flight environment and enhancing the sense of immersion. Then, when the simulated personnel sits in the seat 4 in the simulation cabin 5 for simulated flight, the simulated personnel controls the internal single-chip microcomputer to start, and the internal single-chip microcomputer sends a signal to the single-chip microcomputer 7. The single-chip microcomputer 7 makes a judgment to adjust the operation of the micro-vibration motor 13 behind the seat 4. By adding the micro-vibration motor 13 behind the seat 4, the simulated flight personnel can be closer to the actual operation situation, so as to more realistically feel the vibration of civil aviation during flight, thereby improving the training effect and experience effect of the simulated personnel. At the same time, the single-chip microcomputer 7 makes The operation of the motor 124 is determined and controlled, and the output shaft of the motor 124 drives the protrusion 125 to rotate. When the protrusion 125 rotates, the larger arc side contacts the adjacent slider 123, and the slide column 121 is slid into the slide hole in the middle of the base 1 through the expansion and contraction of the spring 122, thereby driving the slider 123 to slide forward or backward, thereby driving the simulation cabin 5 to slide forward or backward. When the simulation cabin 5 slides forward or backward, the support block 3 slides in the guide groove 2 to slide forward or backward, and serves as a supporting component when the simulation cabin 5 swings forward or backward to keep the cabin stable. At the same time, the acceleration and deceleration changes in the movement process can be felt by swinging back and forth, which can more realistically restore the actual dynamic experience and provide a more realistic effect. The design of the perspective window 10 can provide a very realistic flight or driving experience, allowing pilots and drivers to be trained and trained in a simulated environment.

[0029] It is worth noting that the specific model of the single chip microcomputer 7 disclosed in the above embodiment is S7-200, the motor 124 can be selected as D180M-0160030B-E, and the micro vibration motor 13 can be selected as MVE60. The single chip microcomputer 7 controls the motor 124 and the micro vibration motor 13 to work using methods commonly used in the prior art.

[0030] The above description is only an embodiment of the present invention, and does not limit the patent scope of the present invention. Any equivalent structure or equivalent process transformation made by using the contents of the specification and drawings of the present invention, or directly or indirectly applied in other related technical fields, are also included in the patent protection scope of the present invention.

Claims

1. A simulated cockpit for civil aviation teaching, characterized in that: It comprises a base (1), a guide slide groove (11) and a bracket (9); Base (1): guide grooves (2) are respectively provided at the left and right ends of the upper surface thereof, support blocks (3) are slidably connected to the front and rear ends of the inner wall of the guide groove (2), and the upper surfaces of the evenly distributed support blocks (3) are fixedly connected to the lower surface of a simulation cabin (5); A guide slide groove (11): the guide slide groove (11) is provided in the middle of the upper surface of the base (1), a rocking mechanism (12) is provided inside the guide slide groove (11), front and rear ends of the rocking mechanism (12) respectively extend to the outside of the front and rear ends of the base (1), and the upper ends of the rocking mechanism (12) are fixedly connected to the lower surface of the simulation cabin (5); Brackets (9): They are all located on the front side of the base (1), and the top of the brackets (9) is provided with a display (8); The device further comprises a single chip microcomputer (7), wherein the single chip microcomputer (7) is arranged on the right inner wall of the simulation cabin (5), and an output end of the single chip microcomputer (7) is electrically connected to an input end of a display (8).

2. The simulated cockpit for civil aviation teaching according to claim 1, characterized in that: The rocking mechanism (12) comprises a slide column (121), a spring (122) and a slider (123); the slider (123) is slidably connected to the front and rear ends of the inner wall of the guide slide groove (11), the top ends of the two sliders (123) are fixedly connected to the lower surface of a simulation cabin (5), the opposite outer side surfaces of the two sliders (123) are fixedly connected to the slide columns (121), the opposite outer end heads of the slide columns (121) are slidably connected to the slide holes at the adjacent ends of the base (1), the opposite outer end heads of the slide columns (121) extend to the outside of the front and rear ends of the base (1), the springs (122) are fixedly connected between the outer side surfaces of the two sliders (123) and the inner walls of the adjacent guide slide grooves (11), and the springs (122) are sleeved on the outer surfaces of the slide columns (121).

3. The simulated cockpit for civil aviation teaching according to claim 2, characterized in that: The shaking mechanism (12) further comprises a motor (124) and a bump (125); the motor (124) is mounted on the upper surface of the base (1) by means of bolts; the right end of the output shaft of the motor (124) is fixedly connected with the bump (125); the bump (125) is mounted in cooperation with the two sliders (123).

4. The simulated cockpit for civil aviation teaching according to claim 1, characterized in that: The left and right ends of the bottom wall of the simulation cabin (5) are respectively fixedly connected with seats (4).

5. The simulated cockpit for civil aviation teaching according to claim 4, characterized in that: It also includes a mounting plate (6), wherein the mounting plate (6) is respectively mounted on the rear sides of the two seats (4) by means of bolts.

6. The simulated cockpit for civil aviation teaching according to claim 4, characterized in that: It also includes mounting grooves (14), the mounting grooves (14) being respectively opened on the rear side surfaces of the two seats (4), the inner walls of the mounting grooves (14) being respectively mounted with micro vibration motors (13) by means of bolts, and the input ends of the micro vibration motors (13) being respectively electrically connected to the output ends of the single chip computer (7).

7. The simulated cockpit for civil aviation teaching according to claim 1, characterized in that: The simulation cabin (5) is provided with evenly distributed perspective windows (10) on both the front and rear sides.