CN221281637U - Triaxial simulation flight simulator actuating mechanism - Google Patents
Triaxial simulation flight simulator actuating mechanism Download PDFInfo
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- CN221281637U CN221281637U CN202322931583.7U CN202322931583U CN221281637U CN 221281637 U CN221281637 U CN 221281637U CN 202322931583 U CN202322931583 U CN 202322931583U CN 221281637 U CN221281637 U CN 221281637U
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- fixedly connected
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- movable seat
- flight simulator
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- 238000004088 simulation Methods 0.000 title claims abstract description 23
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 2
- 230000001788 irregular Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model relates to the field of flight training equipment, and particularly discloses a triaxial simulation flight simulator actuating mechanism which comprises a rotating base, wherein a connecting plate is fixedly connected above the rotating base, arc-shaped frames are fixedly connected to two sides of the connecting plate, a rotating plate is arranged in the arc-shaped frames, connecting rods are fixedly connected to two sides of the rotating plate, the connecting rods penetrate through the arc-shaped frames, rollers are rotatably connected to the front side and the rear side of the connecting rods, which are positioned on the left side and the right side of the arc-shaped frames, and a supporting mechanism is arranged below the rotating plate. According to the utility model, the connecting feet of the driving simulation cabin are arranged on the movable seat, the pitching angle of the driving cabin can be adjusted when the driving cabin moves through the inclined edge arranged on one side of the movable seat, and the plurality of protrusions are arranged on the horizontal upper surface of the movable seat, so that the scene when the water machine encounters airflow fluctuation to generate vibration can be simulated through the back and forth movement of the movable seat, and the processing capacity of a driver when encountering an emergency is improved.
Description
Technical Field
The utility model relates to the field of flight training equipment, in particular to a triaxial simulation flight simulator actuating mechanism.
Background
The three-axis simulation flight simulator executing mechanism is a main component of the three-axis simulation flight simulator, and can simulate a pilot to control the aircraft in the air by combining related flight software and a numerical control driving technology, so that the pilot's driving capacity is improved.
Aircraft also suffer from airflow fluctuations during flight, and pilots need to boost handling capacity during pilot training when emergency situations occur. Accordingly, one skilled in the art would provide a three-axis simulated flight simulator actuator that solves the problems set forth in the background above.
Disclosure of utility model
In order to solve the technical problems, the utility model provides a triaxial simulation flight simulator actuating mechanism, which comprises a rotating base, wherein a connecting plate is fixedly connected above the rotating base, arc-shaped frames are fixedly connected on two sides of the connecting plate, a rotating plate is arranged in the arc-shaped frames, connecting rods are fixedly connected on two sides of the rotating plate, the connecting rods penetrate through the arc-shaped frames, rollers are rotatably connected on the front side and the rear side of the connecting rods, which are positioned on the left side and the right side of the arc-shaped frames, and a supporting mechanism is arranged below the rotating plate;
The utility model discloses a motor, including rotating board top rear end fixedly connected with connecting seat, connecting seat top rotation is connected with driving simulation cabin, driving simulation cabin below front end fixedly connected with connecting foot, connecting foot below rotation is connected with the roller, rotating board top fixedly mounted has the motor, motor one end fixedly connected with lead screw, lead screw outside threaded connection has the removal seat, removes seat one end and is equipped with the hypotenuse, the roller is located the oblique edge, is equipped with a plurality of archs on the horizontal plane of removal seat top, is located lead screw top fixedly connected with support frame above the rotating board, removes seat and support frame sliding connection.
Preferably: and a plurality of supporting feet are fixedly connected to the periphery of the rotating base.
Preferably: the supporting mechanism comprises a plurality of telescopic rods symmetrically fixed above the connecting plate, the supporting rods are fixedly connected above the telescopic rods and located below the rotating plate.
Preferably: and a seat and a head-mounted display device are arranged in the driving simulation cabin.
Preferably: the screw rod is rotationally connected above the rotating plate.
Preferably: the rotating base may be a rotary hydraulic cylinder.
The utility model has the technical effects and advantages that:
According to the utility model, the connecting feet of the driving simulation cabin are arranged on the movable seat, the pitching angle of the driving cabin can be adjusted when the driving cabin moves through the inclined edge arranged on one side of the movable seat, and the plurality of protrusions are arranged on the horizontal upper surface of the movable seat, so that the scene when the water machine encounters airflow fluctuation to generate vibration can be simulated through the back and forth movement of the movable seat, and the processing capacity of a driver when encountering an emergency is improved.
Drawings
FIG. 1 is a schematic view of the structure provided by the present application;
FIG. 2 is a schematic structural view of a connecting plate and a rotating plate according to the present application;
FIG. 3 is a schematic view of a structure of a mobile seat according to the present application;
in the figure:
1. Rotating the base; 2. supporting feet; 3. a connecting plate; 4. a telescopic rod; 5. a support rod; 6. an arc-shaped frame; 7. a rotating plate; 8. a connecting rod; 9. a roller; 10. a connecting seat; 11. a driving simulation cabin; 12. a connecting pin; 13. a roller; 14. a support frame; 15. a motor; 16. a screw rod; 17. and a movable seat.
Detailed Description
The utility model will be described in further detail with reference to the drawings and the detailed description. The embodiments of the utility model have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the utility model in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, and to enable others of ordinary skill in the art to understand the utility model for various embodiments with various modifications as are suited to the particular use contemplated.
Referring to fig. 1 to 3, in this embodiment, a triaxial simulation flight simulator actuator is provided, including a rotating base 1, the rotating base 1 may be a rotating hydraulic cylinder, a plurality of supporting legs 2 are fixedly connected to the periphery of the rotating base 1, a connecting plate 3 is fixedly connected to the upper portion of the rotating base 1, two sides of the connecting plate 3 are fixedly connected with arc frames 6, a rotating plate 7 is arranged inside the arc frames 6, two sides of the rotating plate 7 are fixedly connected with connecting rods 8, the connecting rods 8 penetrate through the arc frames 6, the front side and the rear side of the connecting rods 8 are located at the left side and the right side of the arc frames 6 and are respectively connected with rollers 9 in a rotating manner, a supporting mechanism is arranged below the rotating plate 7, the supporting mechanism includes telescopic rods 4, a plurality of telescopic rods 4 are symmetrically fixed above the connecting plate 3, supporting rods 5 are fixedly connected to the upper portions of the telescopic rods 4, and the supporting rods 5 are located below the rotating plate 7;
The rear end fixedly connected with connecting seat 10 above the rotating plate 7, the rotation of connecting seat 10 top is connected with driving simulation cabin 11, driving simulation cabin 11 internally mounted has seat and wear display device, driving simulation cabin 11 below front end fixedly connected with connecting foot 12, and connecting foot 12 below rotates and is connected with roller 13, and rotating plate 7 top fixedly connected with motor 15, motor 15 one end fixedly connected with lead screw 16, lead screw 16 rotates and connects in rotating plate 7 top, and lead screw 16 outside threaded connection has movable seat 17, and movable seat 17 one end is equipped with the hypotenuse, and roller 13 is located the inclined edge, is equipped with a plurality of archs on the horizontal plane of movable seat 17 top, and rotating plate 7 top is located lead screw 16 top fixedly connected with support frame 14, movable seat 17 and support frame 14 sliding connection.
The working principle of the utility model is as follows:
When the device is used, a driver sits in the cockpit 11, the rotation base 1 rotates, the rotation base 1 drives the connecting plate 3 to rotate, the rotating plate 7 in the connecting plate 3 vertically rotates along with the rotation base, and the cockpit 11 on the rotating plate 7 rotates along with the rotation base, so that the steering of the aircraft during flight is simulated.
The telescopic rods 4 on one side are shortened, the telescopic rods 4 on the other side are lengthened, one side of the rotating plate 7 above the shortened telescopic rods 4 is lowered, one side of the rotating plate 7 above the lengthened telescopic rods 4 is raised, the rollers 9 connected with the connecting rods 8 on two sides of the rotating plate 7 are located on two sides of the arc-shaped frame 6, so that the rotating track of the rotating plate 7 is limited, and the rotating plate 7 also drives the square cockpit 11 to rotate during rotation, so that the overturn of the aircraft during flight is simulated.
The motor 15 is started, the motor 15 drives the screw rod 16 to rotate, the screw rod 16 rotates to drive the movable seat 17 to move forwards and backwards, the roller 13 below the connecting pin 12 below the cockpit 11 is jacked up by the movable seat 17 or loses the support of the movable seat 17 to descend, and the other end below the cockpit 11 is rotationally connected with the connecting seat 10, so that the cockpit 11 can only move up and down on one end, and the pitching angle change of the aircraft during flight is realized.
Meanwhile, when the roller 13 moves to the horizontal plane above the movable seat 17, the irregular protrusions are arranged above the movable seat 17, so that the roller 13 continuously moves up and down, irregular vibration is generated in the cockpit 11, and the situation that the aircraft encounters airflow fluctuation in flight and the aircraft vibrates can be realized.
It will be apparent that the described embodiments are only some, but not all, embodiments of the utility model. All other embodiments, which can be made by those skilled in the art and which are included in the embodiments of the present utility model without the inventive step, are intended to be within the scope of the present utility model. Structures, devices and methods of operation not specifically described and illustrated herein, unless otherwise indicated and limited, are implemented according to conventional means in the art.
Claims (6)
1. The utility model provides a triaxial emulation flight simulator actuating mechanism, includes rotation base (1), its characterized in that, rotation base (1) top fixedly connected with connecting plate (3), connecting plate (3) both sides fixedly connected with arc frame (6), arc frame (6) inside is equipped with rotation board (7), rotation board (7) both sides fixedly connected with connecting rod (8), connecting rod (8) pass arc frame (6), both sides are located arc frame (6) left and right sides all and rotate and be connected with gyro wheel (9) around connecting rod (8), rotation board (7) below is equipped with supporting mechanism;
The utility model discloses a motor, including rotating board (7), connecting seat (10) top fixedly connected with driving simulation cabin (11), driving simulation cabin (11) below front end fixedly connected with connecting foot (12), connecting foot (12) below rotation is connected with roller (13), rotating board (7) top fixedly mounted has motor (15), motor (15) one end fixedly connected with lead screw (16), lead screw (16) outside threaded connection has movable seat (17), movable seat (17) one end is equipped with the hypotenuse, roller (13) are located the oblique edge, be equipped with a plurality of archs on movable seat (17) top horizontal plane, rotating board (7) top is located lead screw (16) top fixedly connected with support frame (14), movable seat (17) and support frame (14) sliding connection.
2. The triaxial simulation flight simulator actuating mechanism according to claim 1, wherein a plurality of supporting feet (2) are fixedly connected to the periphery of the rotating base (1).
3. The triaxial simulation flight simulator actuating mechanism according to claim 1, wherein the supporting mechanism comprises telescopic rods (4), a plurality of telescopic rods (4) are symmetrically fixed above the connecting plate (3), supporting rods (5) are fixedly connected above the telescopic rods (4), and the supporting rods (5) are located below the rotating plate (7).
4. A triaxial simulation flight simulator actuator according to claim 1, characterized in that the cockpit (11) is internally mounted with a seat and head mounted display device.
5. A triaxial simulation flight simulator actuator according to claim 1, characterized in that the screw (16) is rotatably connected above the rotating plate (7).
6. A three-axis simulated flight simulator actuator as claimed in claim 1, wherein said rotating base (1) is a rotary hydraulic cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322931583.7U CN221281637U (en) | 2023-10-31 | 2023-10-31 | Triaxial simulation flight simulator actuating mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322931583.7U CN221281637U (en) | 2023-10-31 | 2023-10-31 | Triaxial simulation flight simulator actuating mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221281637U true CN221281637U (en) | 2024-07-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322931583.7U Active CN221281637U (en) | 2023-10-31 | 2023-10-31 | Triaxial simulation flight simulator actuating mechanism |
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| Country | Link |
|---|---|
| CN (1) | CN221281637U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119889130A (en) * | 2025-02-08 | 2025-04-25 | 中国民用航空飞行学院 | Auxiliary simulation device for aviation aircraft |
-
2023
- 2023-10-31 CN CN202322931583.7U patent/CN221281637U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119889130A (en) * | 2025-02-08 | 2025-04-25 | 中国民用航空飞行学院 | Auxiliary simulation device for aviation aircraft |
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