Aircraft control simulator with good simulation effect
By setting a transmission shaft, telescopic sleeve and encoder on the rotating pull rod group of the aircraft control simulator, the problem of poor simulation effect of the existing simulator knob is solved, and a higher degree of simulation and a more realistic control experience are achieved.
Patent Information
- Application Number
- CN202422580650.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-25
- Publication Date
- 2025-09-09
- Estimated Expiration
- 2034-10-25
AI Technical Summary
Existing flight simulators cannot effectively simulate the effects of actual aircraft control when using knobs, resulting in reduced simulation and affecting the experience.
An aircraft control simulator with good simulation effect is designed. By setting a combination of a transmission shaft, a telescopic sleeve and an encoder on the rotating pull rod group, the rotation, pull-out and push-in functions of the knob can be simulated to enhance the simulation effect.
The simulation degree of the aircraft control simulator has been improved, making it closer to the experience of real aircraft control and enhancing the user experience.
Smart Images
Figure CN223320929U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of flight simulators, in particular to an aircraft control simulator with good simulation effect. Background Art
[0002] In a broad sense, a flight simulator is a machine used to simulate the flight of an aircraft. Devices that simulate the flight of airplanes, missiles, satellites, spacecraft, etc. can all be called flight simulators. They are simulation devices that can reproduce the aircraft and the air environment and can be operated. In a narrow sense, it is a device used to simulate the flight of an aircraft and has a relatively complex structure and relatively complete functions. If the flight simulation device has a relatively simple structure and fewer functions, it is called a flight trainer.
[0003] The existing flight simulator includes a shell and a control panel, wherein the control panel has buttons and knobs with various functions. Pressing the buttons directly will realize different functions, and turning the knobs can adjust different parameters.
[0004] The above technical conditions still have defects: when the knobs of the above flight simulator are used, they cannot well imitate the effects of actual aircraft control, resulting in a decrease in the simulation degree of the aircraft control simulator, which is not conducive to increasing the experience effect.
[0005] Based on this, the utility model designs an aircraft control simulator with good simulation effect to solve the above problems. Utility Model Content
[0006] The purpose of the utility model is to provide an aircraft control simulator with good simulation effect to solve the above technical problems.
[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aircraft control simulator with good simulation effect, comprising a shell, a control panel fixedly connected to one side of the shell, a digital display screen inlaid on the control panel, an automatic thrust button group arranged in the middle position of the control panel, a control rotation pull rod group also arranged on the control panel, a base fixedly connected to the inside of the shell, a transmission shaft connected to one end of the control rotation pull rod group, a telescopic sleeve connected to one end of the transmission shaft, the telescopic sleeve comprising an outer tube and a telescopic column, a cross plate fixedly connected to the base, a No. 1 encoder fixedly connected to one side of the cross plate, the telescopic column of the telescopic sleeve connected to the No. 1 encoder, a guide block rotatably connected to the outside of the outer tube of the telescopic sleeve, two groups of fixed columns fixedly connected to one side of the guide block, a seat plate fixedly connected to one end of the two groups of fixed columns, a spring arranged between the seat plate and the cross plate, a spring also arranged between the guide block and the cross plate, and both groups of springs are arranged on the outside of the fixed column.
[0008] By adopting the above technical solution, when the knob is turned, the interaction between its internal transmission structure and the encoder can improve the simulation effect of the simulator.
[0009] Preferably, a detection rod is fixedly connected to one side of the seat plate, and an infrared tube detection seat is provided on the base and located on one side of the detection rod.
[0010] By adopting the above technical solution, the pulling out and pushing in of the rotating pull rod can be monitored, thereby realizing different functions.
[0011] Preferably, the control rotation pull rod group includes a speed adjustment knob, a track selection knob, an altitude selection knob and a track angle knob.
[0012] By adopting the above technical solution, the operation mode is the same, and different functions are achieved by connecting different encoders.
[0013] Preferably, the base is also provided with a data transmission connector.
[0014] By adopting the above technical solution, data can be transmitted to an external device, such as a flight simulation device.
[0015] Preferably, two auxiliary knobs are provided at the bottom of the shell, and two No. 2 encoders are fixedly connected to the bottom of the base. A transmission rod is connected to the No. 2 encoder, and the transmission rod is fixedly connected to the inner side of the auxiliary knob.
[0016] To sum up, the present application has the following beneficial technical effects: through the setting of the rotating pull rod, it can realize different functional adjustments when pressed in or pulled out, making it close to the real aircraft control, increasing the simulation degree of the flight control simulator, and the reset mechanism with a spring inside can further enhance the experience of pulling and pressing. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the following briefly introduces the drawings required for describing the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.
[0018] Figure 1 Schematic diagram of the overall structure of this embodiment;
[0019] Figure 2 This is a schematic diagram of the front structure of this embodiment;
[0020] Figure 3 Schematic diagram of the internal transmission structure in this embodiment;
[0021] Figure 4 2 is a top view of the internal transmission structure in this embodiment;
[0022] Figure 5 Schematic diagram of the structure of encoder No. 2 in this embodiment.
[0023] In the accompanying drawings, the components represented by the reference numerals are as follows:
[0024] 1. Housing; 2. Control panel; 3. Digital display; 4. Bracket; 5. Automatic thrust button group; 6. Speed adjustment knob; 7. Track selection knob; 8. Altitude selection knob; 9. Track angle knob; 10. Auxiliary knob; 11. Base; 12. Drive shaft; 13. Telescopic sleeve; 14. Encoder No. 1; 15. Cross plate; 16. Guide block; 17. Fixed column; 18. Spring; 19. Base plate; 20. Detection rod; 21. Infrared tube detection seat; 22. Data transmission connector; 23. Encoder No. 2; 24. Drive rod. DETAILED DESCRIPTION
[0025] The following will be combined with the accompanying drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.
[0026] The following is combined with Figure 1-5 This application is described in further detail.
[0027] Reference Figure 1 、 Figure 2 and Figure 3, an aircraft control simulator with good simulation effect, including a shell 1, a control panel 2 is fixedly connected to one side of the shell 1, and a digital display screen 3 is embedded on the control panel 2, which is used to display flight data, and brackets 4 are fixedly connected to both sides of the bottom of the shell 1, and the brackets 4 are used to install the shell 1 to facilitate subsequent simulation operations, an automatic thrust button group 5 is provided in the middle position of the control panel 2, and a control rotation rod group is also provided on the control panel 2, a base 11 is fixedly connected to the inside of the shell 1, a transmission shaft 12 is connected to one end of the control rotation rod group, and a telescopic sleeve 13 is connected to one end of the transmission shaft 12, and the telescopic sleeve 13 includes an outer tube and a telescopic column, and a horizontal plate 15 is also fixedly connected to the base 11, and one side of the horizontal plate 15 is fixedly connected It is connected to encoder No. 1 14, and the telescopic column of the telescopic sleeve 13 is connected to encoder No. 1 14. A guide block 16 is rotatably connected to the outside of the outer tube of the telescopic sleeve 13. When the telescopic sleeve 13 rotates, the guide block 16 can remain stationary, and the moving wire on the outer tube can drive the guide block 16 to move. Multiple groups of guide rods are fixedly connected between the inner side of the control panel 2 and the cross plate 15. The guide block 16 is adapted to the guide rod to make it more stable when moving. Two groups of fixed columns 17 are fixedly connected to one side of the guide block 16, and a seat plate 19 is fixedly connected to one end of the two groups of fixed columns 17. A spring 18 is provided between the seat plate 19 and the cross plate 15, and a spring 18 is also provided between the guide block 16 and the cross plate 15. Both groups of springs 18 are provided on the outside of the fixed column 17.
[0028] Further, refer to Figure 4 A detection rod 20 is also fixedly connected to one side of the seat plate 19, and an infrared tube detection seat 21 is provided on the base 11 and on one side of the detection rod 20, which is used to detect whether the detection rod 20 passes through the infrared tube.
[0029] Furthermore, the control rotation pull rod group includes a speed adjustment knob 6, a track selection knob 7, an altitude selection knob 8 and a track angle knob 9, all of which can be rotated, pressed in and pulled out to achieve different functional effects.
[0030] Furthermore, a data transmission connector 22 is provided on the base 11 for connecting a data transmission line to record the operation of the control simulator.
[0031] Furthermore, two auxiliary knobs 10 are provided at the bottom of the shell 1, and two No. 2 encoders 23 are fixedly connected to the bottom of the base 11. A transmission rod 24 is connected to the No. 2 encoder 23, and the transmission rod 24 is fixedly connected to the inner side of the auxiliary knob 10. By rotating the auxiliary knob 10, the No. 2 encoder 23 can start working.
[0032] The implementation principle of this embodiment is: when the rotating pull rod is rotated, the transmission shaft 12 drives the telescopic sleeve 13 to rotate, so that the telescopic column can transmit the rotation information to the No. 1 encoder 14, and then the numerical value can be adjusted. When the rotating pull rod is pulled out or pressed in, the position of the detection rod 20 inside the infrared tube detection seat 21 can be used to switch the function adjustment of the rotating pull rod. Multiple function adjustments can be achieved on the same rotating pull rod, making it close to real aircraft control and increasing the simulation degree of the flight control simulator.
[0033] In the description of the present invention, it should be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "the other end", "upper", "one side", "top", "inside", "front", "center", "two ends", etc., indicating the orientation or position relationship, are based on the orientation or position relationship shown in the accompanying 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 operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention.
[0034] In the present invention, unless otherwise clearly stipulated and limited, the terms "install", "set", "connect", "fix", "screw" and the like should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integrated connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium; it can be the internal connection of two elements or the interaction relationship between two elements. Unless otherwise clearly defined, ordinary technicians in this field can understand the specific meanings of the above terms in the present invention according to the specific circumstances.
[0035] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. An aircraft control simulator with good simulation effect, comprising a housing (1), characterized in that: A control panel (2) is fixedly connected to one side of the housing (1), a digital display screen (3) is embedded on the control panel (2), an automatic thrust button group (5) is provided in the middle position of the control panel (2), a control rotation pull rod group is also provided on the control panel (2), a base (11) is fixedly connected inside the housing (1), a transmission shaft (12) is connected to one end of the control rotation pull rod group, a telescopic sleeve (13) is connected to one end of the transmission shaft (12), the telescopic sleeve (13) includes an outer tube and a telescopic column, a transverse plate (15) is fixedly connected to the base (11), and a transverse plate (15) is fixedly connected to the transverse plate (15). ) is fixedly connected to a No. 1 encoder (14) on one side, a telescopic column of the telescopic sleeve (13) is connected to the No. 1 encoder (14), a guide block (16) is rotatably connected to the outer side of the outer tube of the telescopic sleeve (13), two groups of fixed columns (17) are fixedly connected to one side of the guide block (16), a seat plate (19) is fixedly connected to one end of the two groups of fixed columns (17), a spring (18) is provided between the seat plate (19) and the transverse plate (15), a spring (18) is also provided between the guide block (16) and the transverse plate (15), and both groups of springs (18) are provided on the outer side of the fixed column (17).
2. An aircraft control simulator with good simulation effect according to claim 1, characterized in that: One side of the seat plate (19) is also fixedly connected to a detection rod (20), and an infrared tube detection seat (21) is provided on the base (11) and located on one side of the detection rod (20).
3. The aircraft control simulator with good simulation effect according to claim 1, characterized in that: The control rotation pull rod group comprises a speed adjustment knob (6), a track selection knob (7), an altitude selection knob (8) and a track angle knob (9).
4. The aircraft control simulator with good simulation effect according to claim 1, characterized in that: The base (11) is also provided with a data transmission connector (22).
5. The aircraft control simulator with good simulation effect according to claim 1, characterized in that: Two auxiliary knobs (10) are also provided at the bottom of the housing (1), and two No. 2 encoders (23) are fixedly connected to the bottom of the base (11). A transmission rod (24) is connected to the No. 2 encoder (23), and the transmission rod (24) is fixedly connected to the inner side of the auxiliary knob (10).