Multi-angle and multi-attitude flight training simulator
By designing structures such as adjustment frames, adjustment plates, universal wheels, reinforcement rods, rotating motors and rotating motors in the flight training simulator, the problems of unsmooth movement of the existing simulators are solved, and multi-angle and multi-pose flight training is achieved, which improves the training effect and safety.
Patent Information
- Application Number
- CN202421177623.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-28
- Publication Date
- 2025-03-07
- Estimated Expiration
- 2034-05-28
AI Technical Summary
When used, the existing flight training simulators are not moved smoothly and firmly enough, which poses safety risks and cannot meet the actual flight training needs, affecting the flight training effect.
A multi-angle and multi-pose flight training simulator is designed, and the multi-angle and multi-pose motion of the simulator is achieved by setting up an adjustment frame, an adjustment plate, a universal wheel, a reinforcement rod, a rotating motor and a rotating motor, combined with a driver and a controller.
It improves the smoothness and firmness of the simulator during the training process, enhances safety and practicality, can meet actual flight training needs, and improves the flight training effect.
Smart Images
Figure CN222580641U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of flight simulation training, in particular to a multi-angle and multi-attitude flight training simulator. Background Art
[0002] With the development of economy, roads are becoming more and more congested, transportation is also rapidly expanding into three-dimensional space, the demand for aircraft is increasing, which has also caused a shortage in the number of pilots. Pilot training bases are also being built simultaneously. Flight training simulators will be used for training in the constructed training bases. There are at least the following disadvantages in the use of existing flight training simulators: 1. When using existing flight training simulators, the training movement process of the simulator is not smooth enough, and the simulator is not strong enough, posing a safety hazard; 2. During use, the existing flight training simulators cannot meet the actual flight training needs, and thus cannot produce real flight postures and movements, affecting the flight training effect. Therefore, we have launched a multi-angle, multi-posture flight training simulator. Utility Model Content
[0003] The main purpose of the utility model is to provide a multi-angle and multi-attitude flight training simulator, which can effectively solve the problems in the background technology.
[0004] In order to achieve the above purpose, the technical solution adopted by the utility model is:
[0005] A multi-angle and multi-attitude flight training simulator comprises a mounting base, wherein a controller is fixedly connected to the middle of the front end of the mounting base, mounting holes are provided at the four corners of the upper end of the mounting base, guide rails are fixedly connected between the peripheries of the upper end of the mounting base, guide grooves are provided between the peripheries of the upper end of the guide rails, and a plurality of tooth grooves are provided on the outer surface of the guide rails, a fixing column is fixedly connected to the middle of the upper end of the mounting base, an adjustment frame is movably connected to the middle of the outer surface of the fixing column through a bearing, an adjustment plate is fixedly connected to the left end of the adjustment frame, universal wheels are fixedly connected to the four corners of the lower end of the adjustment plate, a reinforcement rod is fixedly connected to the front right end and the rear right end of the adjustment plate, and the right ends of the two reinforcement rods are fixedly connected to the right part of the outer surface of the adjustment frame, a fixing frame is fixedly connected to the middle of the lower end of the mounting base, and a ball bearing is movably connected to the lower part of the left frame wall and the lower part of the right frame wall of the fixing frame through a movable shaft.
[0006] Preferably, the lower left portion of the adjustment plate is fixedly connected to a fixed frame, a driver is provided at the lower portion of the lower frame wall of the fixed frame, and the upper end of the driver is fixedly connected to the lower end of the adjustment plate, and the output end of the driver passes through the lower frame wall of the fixed frame and is fixedly connected to an adjustment gear.
[0007] Preferably, the outer surface of the adjusting gear is meshed with a plurality of tooth grooves, and the upper end surface of the adjusting gear is higher than the upper end surface of the mounting base, and the lower end surface of the universal wheel is in contact with the upper end surface of the mounting base.
[0008] Preferably, a supporting frame is fixedly connected to the middle part of the upper end of the adjustment plate, a rotating motor is provided on the upper part of the right end of the supporting frame, and the output end of the rotating motor passes through the right frame wall of the supporting frame and is fixedly connected to the rotating frame, and the left and right ends of the rotating frame are movably connected to the left and right frame walls of the supporting frame through bearings, a self-rotating motor is provided in the middle part of the front end of the rotating frame, the output end of the self-rotating motor passes through the front frame wall of the rotating frame and is fixedly connected to the flight simulation cabin, and the front and rear ends of the flight simulation cabin are movably connected to the front and rear frame walls of the rotating frame through bearings.
[0009] Preferably, the supporting base is configured as a U-shaped structure, the rotating motor, the self-rotating motor and the driver are all connected to the controller wires, and the rotating frame is configured as a U-shaped structure.
[0010] Compared with the prior art, the utility model has the following beneficial effects:
[0011] 1. In the utility model, by setting the adjustment frame and the adjustment plate, the balls roll in the guide grooves, and the universal wheels move on the mounting base, the simulator can move more smoothly during the training process, and the adjustment frame is movably connected with the fixed column, and the reinforcement of the reinforcement rod can improve the firmness of the entire simulator, improve the safety, and also improve the practicality;
[0012] 2. In the utility model, by setting a rotating motor and a self-rotating motor, the flight simulation cabin can be driven by a driver to move in a circular direction, and then the rotating motor can drive the flight simulation cabin to rotate, and then the self-rotating motor can drive the flight simulation cabin to rotate, so that multi-angle and multi-attitude flight training can be carried out, thereby meeting the actual flight training needs and enhancing the flight training effect. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Figure 1 This is a schematic diagram of the overall structure of a multi-angle, multi-attitude flight training simulator of the utility model;
[0014] Figure 2 This is a schematic diagram of the connection between the adjustment plate and the adjustment frame of a multi-angle and multi-attitude flight training simulator of the utility model;
[0015] Figure 3 It is a top view of an adjustment panel of a multi-angle and multi-attitude flight training simulator of the utility model;
[0016] Figure 4The utility model is a schematic diagram of the connection between a supporting base frame and a rotating frame of a multi-angle and multi-attitude flight training simulator.
[0017] In the figure: 1. Mounting base; 2. Controller; 3. Mounting hole; 4. Guide track; 5. Guide groove; 6. Tooth groove; 7. Fixed column; 8. Adjustment frame; 9. Adjustment plate; 10. Universal wheel; 11. Reinforcement rod; 12. Fixed frame; 13. Ball bearing; 14. Fixed frame; 15. Driver; 16. Adjustment gear; 17. Support frame; 18. Rotating motor; 19. Rotating frame; 20. Rotating motor; 21. Flight simulation cabin. DETAILED DESCRIPTION
[0018] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further described below in conjunction with specific implementation methods.
[0019] In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "two ends", "one end", "the other end" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operate in a specific orientation, and therefore cannot be understood as a limitation on the present invention. In addition, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating or implying relative importance.
[0020] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "provided with", "connected", etc. should be understood in a broad sense. For example, "connected" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be an indirect connection through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.
[0021] See also Figure 1-4 , the utility model provides a technical solution:
[0022] A multi-angle and multi-posture flight training simulator, including an installation base 1. In the middle of the front end of the installation base 1, a controller 2 is fixedly connected. Installation holes 3 are opened at the four corners of the upper end of the installation base 1. A guiding track 4 is fixedly connected between the peripheries of the upper end of the installation base 1. A guiding groove 5 is opened between the peripheries of the upper end of the guiding track 4. A plurality of tooth grooves 6 are opened on the outer surface of the guiding track 4. In the middle of the upper end of the installation base 1, a fixed column 7 is fixedly connected. In the middle of the outer surface of the fixed column 7, an adjusting frame 8 is inserted and movably connected through a bearing. At the left end of the adjusting frame 8, an adjusting plate 9 is fixedly connected. At the four corners of the lower end of the adjusting plate 9, universal wheels 10 are fixedly connected. At the front part and the rear part of the right end of the adjusting plate 9, reinforcing rods 11 are fixedly connected, and the right ends of the two reinforcing rods 11 are fixedly connected to the right part of the outer surface of the adjusting frame 8. In the middle of the lower end of the installation base 1, a fixed frame 12 is fixedly connected. Between the lower part of the left frame wall and the lower part of the right frame wall of the fixed frame 12, a ball 13 is inserted and movably connected through a movable shaft.
[0023] In this embodiment, at the lower left part of the lower end of the adjusting plate 9, a fixed frame 14 is fixedly connected. At the lower part of the lower frame wall of the fixed frame 14, a driver 15 is arranged, and the upper end of the driver 15 is fixedly connected to the lower end of the adjusting plate 9. The output end of the driver 15 penetrates through the lower frame wall of the fixed frame 14 and is fixedly connected with an adjusting gear 16; the outer surface of the adjusting gear 16 meshes with a plurality of tooth grooves 6, and the adjusting plate 9 can be driven to move through the meshing transmission therebetween. Moreover, the upper end surface of the adjusting gear 16 is higher than the upper end surface of the installation base 1, so that the adjusting gear 16 does not contact the installation base 1 and does not affect the rotation of the adjusting gear 16. The lower end surface of the universal wheel 10 contacts the upper end surface of the installation base 1, so that the universal wheel 10 plays a supporting role for the adjusting plate 9, and the stability of the adjusting plate 9 during the movement can be improved.
[0024] In this embodiment, at the middle part of the upper end of the adjusting plate 9, a supporting bottom frame 17 is fixedly connected. At the upper right part of the supporting bottom frame 17, a rotating motor 18 is arranged, and the output end of the rotating motor 18 penetrates through the right frame wall of the supporting bottom frame 17 and is fixedly connected with a rotating frame 19. The left end and the right end of the rotating frame 19 are movably connected with the left frame wall and the right frame wall of the supporting bottom frame 17 through bearings. At the middle part of the front end of the rotating frame 19, a self-rotating motor 20 is arranged. The output end of the self-rotating motor 20 penetrates through the front frame wall of the rotating frame 19 and is fixedly connected with a flight simulation cabin 21. The front end and the rear end of the flight simulation cabin 21 are movably connected with the front frame wall and the rear frame wall of the rotating frame 19 through bearings; the supporting bottom frame 17 is arranged in a C-shaped structure. The rotating motor 18, the self-rotating motor 20 and the driver 15 are all electrically connected to the controller 2, and the entire simulator can be flexibly controlled through the controller 2. The rotating frame 19 is arranged in a double-square structure, which can strengthen the firmness of the rotating frame 19.
[0025] It should be noted that the utility model is a multi-angle, multi-attitude flight training simulator. During use, the trainee first enters the flight simulation cabin 21, and then flexibly controls the entire simulator through the controller 2, so that the controller 2 starts the driver 15, the rotating motor 18 and the rotating motor 20 in sequence, simultaneously, intermittently or individually, etc. When the driver 15 is started, the adjustable gear 16 can be rotated, and then the adjustment plate 9 drives the flight simulation cabin 21 to move in a circular direction through the engagement between the adjustment gear 16 and a plurality of tooth grooves 6, and during the movement, the universal wheel 10 moves on the mounting base 1, and cooperates with the roller The beads 13 roll in the guide groove 5, which can make the adjustment plate 9 move more smoothly during training. The adjustment frame 8 rotates on the fixed column 7, and cooperates with the reinforcement rod 11 to make the adjustment frame 8 reinforce the adjustment plate 9, thereby improving the firmness of the entire simulator and improving safety. When the rotating motor 18 starts to drive the rotating frame 19 to rotate, the flight simulation cabin 21 can be driven to rotate, and the self-rotating motor 20 is started to drive the flight simulation cabin 21 to rotate, so that the flight simulation cabin 21 can perform multi-angle and multi-attitude flight training, and can produce real flight attitudes and movements, thereby meeting actual flight training needs and enhancing the flight training effect.
[0026] The above shows and describes the basic principle and main features of the utility model and the advantages of the utility model. Those skilled in the art should understand that the utility model is not limited by the above embodiments. The above embodiments and descriptions are only for explaining the principle of the utility model. Without departing from the spirit and scope of the utility model, the utility model may have various changes and improvements, which fall within the scope of the utility model to be protected. The scope of protection claimed by the utility model is defined by the attached claims and their equivalents.
Claims
1. A multi-angle, multi-attitude flight training simulator, comprising a mounting base (1), characterized in that: A controller (2) is fixedly connected to the middle of the front end of the mounting base (1); mounting holes (3) are provided at four corners of the upper end of the mounting base (1); guide rails (4) are fixedly connected between the upper peripheries of the mounting base (1); guide grooves (5) are provided between the upper peripheries of the guide rails (4); a plurality of tooth grooves (6) are provided on the outer surface of the guide rails (4); a fixing column (7) is fixedly connected to the middle of the upper end of the mounting base (1); and an adjustment frame is movably connected to the middle of the outer surface of the fixing column (7) through a bearing. (8), the left end of the adjustment frame (8) is fixedly connected to an adjustment plate (9), the four corners of the lower end of the adjustment plate (9) are fixedly connected to universal wheels (10), the front right end and the rear right end of the adjustment plate (9) are fixedly connected to reinforcement rods (11), and the right ends of the two reinforcement rods (11) are fixedly connected to the right part of the outer surface of the adjustment frame (8), the middle part of the lower end of the mounting base (1) is fixedly connected to a fixing frame (12), and a ball bearing (13) is movably connected between the lower part of the left frame wall and the lower part of the right frame wall of the fixing frame (12) through a movable shaft.
2. A multi-angle, multi-attitude flight training simulator according to claim 1, characterized in that: The lower left portion of the adjusting plate (9) is fixedly connected to a fixing frame (14), a driver (15) is provided at the lower portion of the lower frame wall of the fixing frame (14), and the upper end of the driver (15) is fixedly connected to the lower end of the adjusting plate (9), and the output end of the driver (15) passes through the lower frame wall of the fixing frame (14) and is fixedly connected to an adjusting gear (16).
3. A multi-angle, multi-attitude flight training simulator according to claim 2, characterized in that: The outer surface of the adjusting gear (16) meshes with a plurality of tooth grooves (6), and the upper end surface of the adjusting gear (16) is higher than the upper end surface of the mounting base (1), and the lower end surface of the universal wheel (10) contacts the upper end surface of the mounting base (1).
4. The multi-angle, multi-attitude flight training simulator according to claim 1, characterized in that: The middle part of the upper end of the adjustment plate (9) is fixedly connected to a support frame (17), the upper part of the right end of the support frame (17) is provided with a rotating motor (18), and the output end of the rotating motor (18) passes through the right frame wall of the support frame (17) and is fixedly connected to a rotating frame (19), and the left and right ends of the rotating frame (19) are movably connected to the left and right frame walls of the support frame (17) through bearings, and the middle part of the front end of the rotating frame (19) is provided with a self-rotating motor (20), the output end of the self-rotating motor (20) passes through the front frame wall of the rotating frame (19) and is fixedly connected to a flight simulation cabin (21), and the front and rear ends of the flight simulation cabin (21) are movably connected to the front and rear frame walls of the rotating frame (19) through bearings.
5. A multi-angle, multi-attitude flight training simulator according to claim 4, characterized in that: The supporting base frame (17) is configured as a U-shaped structure, the rotating motor (18), the self-rotating motor (20) and the driver (15) are all connected to the controller (2) by wires, and the rotating frame (19) is configured as a U-shaped structure.