Universal fixed-wing aircraft simulation flight equipment

Abstract

The utility model discloses universal flight simulation equipment for a fixed-wing aircraft, and belongs to the technical field of flight simulation equipment. Universal fixed wing aircraft simulation flight equipment comprises a console and a seat, a vibration assembly is installed at the bottom end of the console and the bottom end of the seat, an adjusting assembly is installed between the seat and the vibration assembly, the vibration assembly comprises a first bottom plate, a telescopic cylinder is installed at the top of the first bottom plate, a second bottom plate is installed at the top of the telescopic cylinder, and the bottom plate is connected with the bottom plate. The second bottom plate is fixedly connected with the control table and the adjusting assembly, and a damping rod is installed between the first bottom plate and the second bottom plate. The vibration assembly is improved, the console and the seat are integrally connected with the vibration assembly, vibration is simulated through high-frequency stretching of the telescopic cylinder, vibration can be transmitted to the console and the seat at the same time, vibration simulation is more real, a damping rod is designed for vibration damping, and when vibration is stopped, the console and the seat can be more rapidly stabilized.

Description

Technical Field

[0001] The utility model relates to the technical field of simulated flight equipment, and more specifically to a universal fixed-wing aircraft simulated flight equipment. Background Art

[0002] Flight simulation is a system that reproduces or simulates the feeling of aircraft driving as realistically as possible. Flight simulators range from video games to same-scale simulated cockpits driven by hydraulics or electric motors and controlled by the most advanced computer technology.

[0003] The existing publication number is CN215770140U, and the patent name is a patent document of a universal fixed-wing aircraft simulation flight device, which discloses that the seat can be shaken during the simulated flight through a shaking component, and the slight rotation and shaking of the seat increases the realism of the simulated flight, improves the experience of the simulated flight of the experiencer, and increases the use effect of the device;

[0004] However, in actual operation, the vibration of the seat is not synchronized with the vibration of the simulation console, which leads to the lack of authenticity of the simulated vibration, the body shakes and the console does not move, causing unstable operation and affecting the simulation authenticity of the students. In view of this, we propose a universal fixed-wing aircraft simulation flight equipment. Utility Model Content

[0005] 1. Technical issues to be solved

[0006] The utility model aims to provide a universal fixed-wing aircraft flight simulation device to solve the problems raised in the above background technology.

[0007] 2. Technical solution

[0008] A universal fixed-wing aircraft flight simulation device comprises a control console and a seat, wherein a vibration assembly is installed at the bottom of the control console and the seat, an adjustment assembly is installed between the seat and the vibration assembly, the vibration assembly comprises a bottom plate 1, a telescopic cylinder is installed at the top of the bottom plate 1, a bottom plate 2 is installed at the top of the telescopic cylinder, the bottom plate 2 is fixedly connected to the control console and the adjustment assembly respectively, and a damping rod is installed between the bottom plates 1 and 2.

[0009] Preferably, at least four telescopic cylinders are provided, and the telescopic cylinders are located at the corner positions between the first bottom plate and the second bottom plate.

[0010] Preferably, the damping rods are symmetrically arranged in groups of two, the connection between the damping rods and the first bottom plate is close to the edge of the first bottom plate, and the connection between the damping rods and the second bottom plate is close to the middle of the second bottom plate.

[0011] Preferably, telescopic cylinders are installed in the middle of the base plate 1 and the base plate 2, and the tops of the telescopic cylinders are located at the intersection of the damping rods.

[0012] Preferably, the adjustment assembly comprises a bearing seat, a guide rail is mounted on the bearing seat, and the guide rail is in sliding contact with the seat.

[0013] Preferably, a screw rod is installed in the middle of the seat through a screw hole, and a self-locking motor is installed at the end of the screw rod.

[0014] Preferably, a pressure wheel is installed at the top edge of the bearing seat, and a slope is provided on the side of the seat close to the pressure wheel, and the pressure wheel is inclined at an angle of forty-five degrees.

[0015] 3. Beneficial effects

[0016] Compared with the prior art, the advantages of the present invention are:

[0017] 1. Through the improvement of the vibration component, the console and seat are connected to the vibration component as a whole. The vibration can be transmitted to the console and seat at the same time through the high-frequency extension and contraction simulation vibration of the telescopic cylinder. The vibration simulation is more realistic, and the damping rod is designed for vibration damping. When the vibration stops, the console and seat can be stabilized more quickly.

[0018] 2. The adjustment component is provided with a bearing seat with a guide rail to support the seat for sliding. Together with the inclined pressure wheel, it can provide horizontal clamping pressure and vertical downward pressure for the seat. The movable clamping does not affect the smooth adjustment. When vibrating, it can reduce the collision impact between the seat and the adjustment component, making it more stable to use. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a three-dimensional schematic diagram of the utility model;

[0020] Figure 2 A schematic diagram of the present invention from another angle;

[0021] Figure 3 This is a schematic diagram of the disassembly of the base of the utility model;

[0022] Figure 4 It is a structural schematic diagram of another state of the base of the utility model.

[0023] Description of the numbers in the figure:

[0024] Base plate 1; telescopic cylinder 2; damping rod 3; base plate 2 4; adjustment component 5; bearing seat 51; pressure wheel 52; inclined plane 53; guide rail 54; self-locking motor 55; seat 6; control console 7. DETAILED DESCRIPTION

[0025] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise" and the like indicate orientations or positional relationships based on the orientations or positional relationships 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 referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present invention.

[0026] In the description of the present invention, "plurality" means two or more than two, unless otherwise clearly and specifically defined.

[0027] In the description of the present utility model, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "provided with", "set / connected", "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 indirectly connected 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 utility model can be understood according to specific circumstances.

[0028] Example:

[0029] This embodiment provides a general fixed-wing aircraft flight simulation device, referring to Figure 1, including a console 7, which is a prior art, and a seat 6, which is a proportionally scaled aircraft seat, and can simulate the cockpit of a fixed-wing aircraft, wherein a vibration component is installed at the bottom of the console 7 and the seat 6, and the vibration component can vibrate disorderly and transmit it to the console 7 and the seat 6. Because the console 7 and the seat 6 are driven to vibrate synchronously, the vibration simulation is more realistic and can improve the training effect. An adjustment component 5 is installed between the seat 6 and the vibration component, and the adjustment component 5 can adjust the distance between the seat 6 and the console 7, wherein the vibration component includes a bottom plate 1, the bottom plate 1 is used to be fixed to the ground, and a telescopic cylinder 2 is installed on the top of the bottom plate 1 The telescopic cylinder 2 is vertically arranged, and the vibration can be simulated by the high-frequency extension and contraction of the telescopic cylinder 2. A bottom plate 2 4 is installed on the top of the telescopic cylinder 2. The telescopic cylinder 2 drives the bottom plate 2 4 to vibrate, and the bottom plate 2 4 is fixedly connected to the console 7 and the adjustment component 5 respectively, and the vibration can be transmitted to the console 7 and the seat 6 at the same time, so that the vibration simulation is more realistic. A damping rod 3 is installed between the bottom plate 1 and the bottom plate 2 4 to damp the vibration. When the vibration stops, the console 7 and the seat 6 can stop vibrating more quickly, and the damping rod 3 is in an extended state when not under pressure, so that the bottom plate 2 4 can be supported when the telescopic cylinder 2 is not working, and the telescopic cylinder 2 does not need to maintain the extended state continuously.

[0030] In a further embodiment, referring to Figure 3 At least four telescopic cylinders 2 are provided, and an air supply system is adopted between the four telescopic cylinders 2 to perform synchronous telescopic control. In a shorter stroke, the telescopic cylinder 2 is quickly shortened to compress the damping rod 3, and is quickly extended to reset the damping rod 3, so as to simulate the high-frequency vibration of the aircraft. The corner position between the bottom plate 1 and the bottom plate 2 4 can ensure that the support points are dispersed, thereby achieving stable force on the bottom plate 2 4.

[0031] In a further embodiment, referring to Figure 3 The damping rods 3 are symmetrically arranged in groups of two, and a total of four groups are arranged, which can be used for oblique support. This support method, combined with the vertical extension and contraction of the telescopic cylinder, can achieve triangular support, which can cope with the horizontal lateral force, and further ensure the safety and controllability of the equipment during vibration. In the oblique pull method, the connection between the damping rod 3 and the bottom plate 1 is close to the edge of the bottom plate 1, and the connection between the damping rod 3 and the bottom plate 24 is close to the middle of the bottom plate 24. In this way, the bottom of the damping rod 3 can be easily viewed from the edge.

[0032] In a further embodiment, referring to Figure 4For a console 7 with a heavier weight, the number of telescopic cylinders 2 can be increased to provide a greater vibration driving force. A telescopic cylinder 2 is installed in the middle of the bottom plate 1 and the bottom plate 2 4, and the top of the telescopic cylinder 2 is located at the intersection of the damping rod 3. The centering design of the telescopic cylinder 2 can avoid the stress points of the bottom plate 2 4 being at the edge, causing the middle overhead position to be bent due to stress, thereby ensuring the stable use of the bottom plate 2 4.

[0033] In a further embodiment, referring to Figure 2 A screw is installed in the middle of the seat 6 through a screw hole. In order to adjust the position of the seat 6, a transmission method of the screw and the screw hole can be used. A self-locking motor 55 is installed at the end of the screw, and the self-locking motor 55 is used to drive. The degree of automation is high, and the self-locking motor 55 is provided with a switch. The switch is located on the side of the seat, and the self-locking motor 55 is provided with a shaft lock. When the self-locking motor 55 does not rotate, the position of the screw is guaranteed to remain unchanged, thereby ensuring the stability of the position of the seat 6 during use.

[0034] In a further embodiment, referring to Figure 2 The adjustment component 5 includes a bearing seat 51, which can be a flat plate fixedly connected to the bottom plate 4. A guide rail 54 is installed on the bearing seat 51. There are two guide rails 54, which are symmetrically arranged on both sides of the screw to form a gap between the bottom surface of the seat 6 and the top surface of the bearing seat 51. The guide rail 54 is in sliding contact with the seat 6 to reduce sliding resistance and ensure stable support of the seat 6.

[0035] In a further embodiment, referring to Figure 2 A pressure wheel 52 is installed at the top edge of the bearing seat 51. The pressure wheels 52 also have two rows, and the pressure wheels 52 are inclined at a forty-five degree angle, which can provide horizontal clamping pressure and vertical downward pressure for the seat 6. When vibrating, the collision impact between the seat 6 and the adjustment component 5 can be reduced. A slope 53 is provided on the side of the seat 6 close to the pressure wheel 52. The slope 53 increases the contact area with the pressure wheel 52, and when adjusting the position of the seat 6, the rolling contact method has less resistance.

[0036] The motors and control consoles involved in the embodiments are existing products customized and produced by the manufacturer, and their supporting control systems, solenoid valves, control switches and circuit pipelines can also be provided by the manufacturer. In addition, the power supply modules, circuits, electronic components and control modules involved in the utility model are all existing technologies, which can be fully implemented by those skilled in the art. Needless to say, the content protected by the utility model does not involve improvements to the internal structure and methods.

[0037] The above shows and describes the basic principle, main features and 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 preferred examples of the utility model and are not used to limit 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 of the utility model is defined by the attached claims and their equivalents.

Claims

1. A general fixed-wing aircraft flight simulation device, comprising a control console (7) and a seat (6), characterized in that: A vibration assembly is installed at the bottom of the control console (7) and the seat (6), an adjustment assembly (5) is installed between the seat (6) and the vibration assembly, the vibration assembly comprises a base plate one (1), a telescopic cylinder (2) is installed on the top of the base plate one (1), a base plate two (4) is installed on the top of the telescopic cylinder (2), the base plate two (4) is fixedly connected to the control console (7) and the adjustment assembly (5), respectively, and a damping rod (3) is installed between the base plate one (1) and the base plate two (4).

2. A general fixed-wing aircraft flight simulation device according to claim 1, characterized in that: At least four telescopic cylinders (2) are provided, and the telescopic cylinders (2) are located at the corner positions between the first bottom plate (1) and the second bottom plate (4).

3. A general fixed-wing aircraft flight simulation device according to claim 2, characterized in that: The damping rods (3) are symmetrically arranged in groups of two, the connection between the damping rods (3) and the bottom plate one (1) is close to the edge of the bottom plate one (1), and the connection between the damping rods (3) and the bottom plate two (4) is close to the middle of the bottom plate two (4).

4. A general fixed-wing aircraft flight simulation device according to claim 3, characterized in that: A telescopic cylinder (2) is installed in the middle of the bottom plate one (1) and the bottom plate two (4), and the top of the telescopic cylinder (2) is located at the intersection of the damping rods (3).

5. A general fixed-wing aircraft flight simulation device according to claim 4, characterized in that: The adjustment assembly (5) comprises a bearing seat (51), a guide rail (54) is mounted on the bearing seat (51), and the guide rail (54) is in sliding contact with the seat (6).

6. A general fixed-wing aircraft flight simulation device according to claim 5, characterized in that: A screw rod is installed in the middle of the seat (6) through a screw hole, and a self-locking motor (55) is installed at the end of the screw rod.

7. A general fixed-wing aircraft flight simulation device according to claim 6, characterized in that: A pressure wheel (52) is installed at the top edge of the bearing seat (51), and a slope (53) is provided on the side of the seat (6) close to the pressure wheel (52), and the pressure wheel (52) is inclined at an angle of forty-five degrees.

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