Multifunctional wing operation platform

Abstract

The utility model provides a multifunctional wing operation platform, and belongs to the technical field of wing operation. Comprising an operation platform, a driving box is installed at the top end of the operation platform, a supporting frame is installed at the top end of the driving box, a rotating block is rotationally connected to the top end of the supporting frame, a sliding groove is formed in the top end of the rotating block, the interior of the rotating block is of a cavity structure, and a connecting rod is rotationally connected to the interior of the rotating block; the connecting rods are slidably connected into the sliding grooves, and wings are installed at the top ends of the connecting rods. According to the multifunctional wing operation platform, a second motor drives a second worm to rotate, the second worm is meshed with a second worm gear to rotate, the second worm gear drives a second rotating shaft to rotate, the second rotating shaft drives a second bevel gear to rotate, the second bevel gear is meshed with a first bevel gear to drive a first rotating shaft to rotate, and therefore a sleeve block and a connecting rod are driven to rotate, and wings are driven to swing in the direction of a sliding groove; and the first worm and the second worm are driven to rotate through synchronous rotation of the first motor and the second motor correspondingly, and practicability is high.

Description

Technical Field

[0001] The utility model belongs to the technical field of wing operation, and particularly relates to a multi-functional wing operation platform. Background Art

[0002] Application No. 201720149949.7 provides a display aircraft attitude control device, which is driven by a micro servo motor. Through the design and combination of delicate mechanisms, it realizes the control and adjustment of various attitudes of the aircraft. The mechanism is simple and reliable, the size is compact, and the installation is convenient; it avoids the characteristics of using servo motors in the past, as well as complex mechanisms, long programming cycles, and long running-in times; through a control joystick, the micro servo motor is controlled to complete various actions, so as to realize the synchronous control of the change of the aircraft wing and the aircraft attitude;

[0003] However, when controlling the movement of the aircraft, this device can only control the aircraft to move in the front, back, left, and right directions around the degree-of-freedom device, and cannot simulate more flight states, such as rotating the wing to make the wing present different flight angles to display more wing flight postures, so as to conduct a more comprehensive performance test on the wing. Content of the Utility Model

[0004] In order to solve the problem of being unable to simulate more wing flight states in the above-mentioned existing technology, the utility model provides a multi-functional wing operation platform, which uses a drive box combined with a rotating block to achieve the effect of rotating the wing at multiple angles. The specific technical solution is as follows: A multi-functional wing operation platform, including: an operation platform, a drive box is installed at the top end of the operation platform, a support frame is installed at the top end of the drive box, a rotating block is rotatably connected to the top end of the support frame, a chute is opened at the top end of the rotating block, the inside of the rotating block is a cavity structure, a connecting rod is rotatably connected to the inside of the rotating block, the connecting rod is slidably connected in the chute, and a wing is installed at the top end of the connecting rod.

[0005] Preferably, a rotating shaft one is rotatably connected between the inner walls on both sides of the rotating block, a sleeve block is sleeved on the outer wall of the rotating shaft one, and the bottom end of the connecting rod is connected to the sleeve block.

[0006] Preferably, a rotating cylinder is rotatably connected to the inside of the support frame, the top end of the rotating cylinder is connected to the rotating block, the bottom end of the rotating cylinder extends into the inside of the drive box, and a worm wheel one is sleeved at the bottom end of the rotating cylinder; a placing seat is installed at the inner bottom end of the drive box, a motor one is installed at the top end of the placing seat, and a worm one is installed at the output end of the motor one, and the worm one meshes with the worm wheel one.

[0007] Preferably, a first bevel gear is sleeved on the outer wall of the first rotating shaft. A second rotating shaft is rotatably connected inside the rotating cylinder. The top end of the second rotating shaft extends into the inside of the rotating block. A second bevel gear is sleeved on the top end of the second rotating shaft. The first bevel gear meshes with the second bevel gear. The bottom end of the second rotating shaft extends out of the rotating cylinder. A second worm gear is sleeved on the bottom end of the second rotating shaft. An electric motor two is installed at the inner bottom end of the driving box. A second worm is installed at the output end of the electric motor two. The second worm meshes with the second worm gear.

[0008] Preferably, a first bearing seat is sleeved on the outer wall of the first worm. A second bearing seat is sleeved on the outer wall of the second worm. The first bearing seat and the second bearing seat are respectively installed on the inner walls of both sides of the driving box.

[0009] Preferably, a support column is installed at the top end of the operation platform. A control panel is installed at the top end of the support column.

[0010] In addition, the multifunctional wing operation platform provided by the above technical solution of the present invention may also have the following features: A control surface is rotatably connected to the concave part of the wing. A steering gear is connected to the top end of the wing. A rocker is installed at the output end of the steering gear. A connecting rod is connected to the end of the rocker away from the steering gear. A rudder angle is hinged to the end of the connecting rod away from the rocker.

[0011] In the above technical solution, the rudder angle is installed at the top end of the control surface.

[0012] Compared with the prior art, the beneficial effects of a multifunctional wing operation platform of the present invention are as follows:

[0013] For this multifunctional wing operation platform, the electric motor two drives the second worm to rotate, causing the second worm to mesh with the second worm gear and rotate. The second worm gear drives the second rotating shaft to rotate, causing the second rotating shaft to drive the second bevel gear to rotate. The second bevel gear meshes with the first bevel gear, driving the first rotating shaft to rotate, thereby driving the sleeve block and the connecting rod to rotate, driving the wing to swing along the direction of the sliding groove.

[0014] By the synchronous rotation of the electric motor one and the electric motor two, the first worm and the second worm are respectively driven to rotate, synchronously meshing with the first worm gear and the second worm gear to rotate. The first worm gear drives the rotating cylinder to rotate, causing the rotating cylinder to drive the rotating block to rotate, thereby driving the wing to rotate. At the same time, the second worm gear drives the second rotating shaft to rotate, driving the second bevel gear to rotate synchronously with the rotating block, thereby causing the first bevel gear not to rotate, realizing the rotation of the wing.

[0015] The electric motor one drives the first worm to rotate. The first worm meshes with the first worm gear to rotate, causing the first worm gear to drive the rotating cylinder to rotate. The rotating cylinder drives the rotating block to rotate. While the rotating block rotates, the second bevel gear remains stationary. The rotation of the rotating block will drive the first bevel gear to rotate accordingly. Therefore, the first bevel gear meshes with the second bevel gear, causing the wing to rotate and rotate along the direction of the sliding groove while rotating, with strong practicability. Brief Description of the Drawings

[0016] Figure 1 Schematic perspective view of the multi-functional wing operation platform provided by the present utility model;

[0017] Figure 2 is Figure 1 enlarged view of part A of;

[0018] Figure 3 Schematic partial sectional front view of the multi-functional wing operation platform provided by the present utility model;

[0019] Figure 4 Schematic partial sectional side view of the multi-functional wing operation platform provided by the present utility model;

[0020] Wherein, Figures 1 to 4 The reference numerals and component names in are: 1, operation platform; 2, drive box; 3, support frame; 4, rotating block; 5, sliding groove; 6, connecting rod; 7, wing; 8, support column; 9, control panel; 10, sleeve block; 11, first rotating shaft; 12, first bevel gear; 13, second bevel gear; 14, rotating cylinder; 15, second rotating shaft; 16, first worm gear; 17, second worm gear; 18, placing seat; 19, first motor; 20, second motor; 21, first worm; 22, second worm; 23, first bearing seat; 24, second bearing seat; 71, control surface; 72, steering gear; 73, rocker; 74, connecting rod; 75, rudder angle. Detailed Description of the Preferred Embodiments

[0021] The following further illustrates the present utility model in conjunction with specific implementation cases and attached Figures 1 - 4 drawings. However, the present utility model is not limited to these embodiments. The present utility model provides a technical solution: a multi-functional wing operation platform, comprising: an operation platform 1, a drive box 2 is installed at the top of the operation platform 1, the drive box 2 is close to the rear side of the operation platform 1, a support frame 3 is installed at the top of the drive box 2, a rotating block 4 is rotatably connected to the top of the support frame 3, a sliding groove 5 is opened at the top of the rotating block 4, the inside of the rotating block 4 is of a cavity structure, the sliding groove 5 communicates with the cavity of the rotating block 4, a connecting rod 6 is rotatably connected inside the rotating block 4, the connecting rod 6 is slidably connected in the sliding groove 5, and the top of the connecting rod 6 is installed with a wing 7 through a connecting seat.

[0022] As a preferred solution, further, a first rotating shaft 11 is rotatably connected between the inner walls on both sides of the rotating block 4, a sleeve block 10 is sleeved on the outer wall of the first rotating shaft 11, and the bottom end of the connecting rod 6 is connected to the sleeve block 10.

[0023] As a preferred solution, furthermore, a rotating cylinder 14 is rotatably connected inside the support frame 3. The rotating cylinder 14 is a hollow structure in the vertical direction. The top end of the rotating cylinder 14 is fixedly connected to the rotating block 4. The bottom end of the rotating cylinder 14 extends into the interior of the drive box 2. The connection between the rotating cylinder 14 and the drive box 2 is rotatably connected. A first worm gear 16 is sleeved on the bottom end of the rotating cylinder 14. A placing seat 18 is installed at the inner bottom end of the drive box 2. A first motor 19 is installed at the top end of the placing seat 18. A first worm 21 is installed at the output end of the first motor 19. The first worm 21 meshes with the first worm gear 16. The placing seat 18 is used to raise the position of the first motor 19 so that the first worm 21 meshes with the first worm gear 16.

[0024] As a preferred solution, furthermore, a first bevel gear 12 is sleeved on the outer wall of the first rotating shaft 11. A second rotating shaft 15 is rotatably connected inside the rotating cylinder 14. The top end of the second rotating shaft 15 extends into the interior of the rotating block 4. A second bevel gear 13 is sleeved on the top end of the second rotating shaft 15. The first bevel gear 12 meshes with the second bevel gear 13. The bottom end of the second rotating shaft 15 extends out of the rotating cylinder 14. A second worm gear 17 is sleeved on the bottom end of the second rotating shaft 15. A second motor 20 is installed at the inner bottom end of the drive box 2. A second worm 22 is installed at the output end of the second motor 20. The second worm 22 meshes with the second worm gear 17.

[0025] As a preferred solution, furthermore, a first bearing seat 23 is sleeved on the outer wall of the first worm 21. A second bearing seat 24 is sleeved on the outer wall of the second worm 22. The first bearing seat 23 and the second bearing seat 24 are respectively installed on the inner walls of both sides of the drive box 2. The first worm 21 and the second worm 22 are stably rotated through the first bearing seat 23 and the second bearing seat 24.

[0026] As a preferred solution, furthermore, a support column 8 is installed at the top end of the operation platform 1. A control panel 9 is installed at the top end of the support column 8. The control panel 9 is electrically connected to the wing 7, the first motor 19 and the second motor 20.

[0027] As a preferred solution, furthermore, a control surface 71 is connected to the concave part of the wing 7 through a hinge. A steering gear 72 is connected to the top end of the wing 7. A rocker 73 is installed at the output end of the steering gear 72. One end of the rocker 73 away from the steering gear 72 is connected to a connecting rod 74. One end of the connecting rod 74 away from the rocker 73 is hinged to a rudder angle 75. The rudder angle 75 is installed at the top end of the control surface 71.

[0028] The wing, control panel, first motor, second motor and steering gear in this case are prior arts. The wing has the same structure and connection method as that in the cited document. Both the first motor and the second motor are three-phase motors. As long as the wing, control panel, first motor, second motor and steering gear meet the requirements of this case, they are all acceptable.

[0029] Working principle: All electrical components appearing in this application are externally connected to a power supply and a control switch during use. After the present utility model is installed, first check the installation and fixation as well as the safety protection of the present utility model, and then it can be used; during use, the staff controls the wing 7 to change the angle by operating the control panel 9, and moves the steering gear 72 by control, so that the steering gear 72 drives the rocker 73, the connecting rod 74 and the rudder angle 75 to move, thereby enabling the rudder surface 71 to rotate relative to the wing 7 through the hinge; first, control the motor 19 to rotate. The motor 19 drives the worm 21 to rotate. The worm 21 meshes with the worm gear 16 to rotate, so that the worm gear 16 drives the rotating cylinder 14 to rotate. The rotating cylinder 14 drives the rotating block 4 to rotate. The rotating block 4 drives the connecting rod 6 and the wing 7 to rotate; during the rotation of the rotating block 4, the bevel gear 13 inside the rotating block 4 remains stationary, while the bevel gear 12 rotates with the rotating block 4, resulting in the bevel gear 12 meshing with the bevel gear 13 to rotate, so that during the rotation of the wing 7 with the rotating block 4, it also rotates along the direction of the sliding groove 5.

[0030] Then, drive the worm 22 to rotate by the motor 20. The worm 22 meshes with the worm gear 17 to rotate, so that the worm gear 17 drives the rotating shaft 15 to rotate, and the rotating shaft 15 drives the bevel gear 13 to rotate. The bevel gear 13 meshes with the bevel gear 12 to rotate. The bevel gear 12 drives the rotating shaft 11 to rotate. The rotating shaft 11 drives the sleeve block 10 to rotate, so that the sleeve block 10 drives the connecting rod 6 to rotate in the sliding groove 5, and the wing 7 rotates along the direction of the sliding groove 5.

[0031] Finally, the motor 19 and the motor 20 rotate synchronously, so that the motor 19 drives the worm 21 to rotate, and the motor 20 drives the worm 22 to rotate. The worm 21 meshes with the worm gear 16 to rotate, and the worm 22 meshes with the worm gear 17 to rotate; the worm gear 16 drives the rotating cylinder 14 to rotate, so that the rotating cylinder 14 drives the rotating block 4 to rotate. While the rotating block 4 rotates, the worm gear 17 drives the rotating shaft 15 to rotate, and the rotating shaft 15 drives the bevel gear 13 to rotate, so that the bevel gear 13 meshes with the bevel gear 12, and in cooperation with the rotation of the rotating block 4, the bevel gear 12 and the rotating block 4 are in a relatively stationary state, realizing the state where only the wing 7 rotates.

[0032] In the description of the present utility model, the term "a plurality of" refers to two or more, unless otherwise clearly defined. The orientation or positional relationship indicated by terms such as "upper", "lower", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus cannot be construed as a limitation on the present utility model; terms such as "connection", "installation", "fixation", etc. should all be understood in a broad sense. For example, "connection" can be a fixed connection, a detachable connection, or an integral connection; it can be directly connected or indirectly connected through an intermediate medium. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.

[0033] The above are only the preferred embodiments of the present utility model, and are not used to limit the present utility model. For those skilled in the art, the present utility model can have various changes and modifications. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. A multifunctional wing operating platform, comprising: The operating platform (1) is characterized in that a drive box (2) is installed at the top of the operating platform (1), a support frame (3) is installed at the top of the drive box (2), a rotating block (4) is rotatably connected to the top of the support frame (3), a slide groove (5) is provided at the top of the rotating block (4), the interior of the rotating block (4) is a cavity structure, a connecting rod (6) is rotatably connected to the interior of the rotating block (4), the connecting rod (6) is slidably connected in the slide groove (5), and a wing (7) is installed at the top of the connecting rod (6).

2. The multifunctional wing operating platform according to claim 1, characterized in that: A rotating shaft (11) is rotatably connected between the inner walls on both sides of the rotating block (4), a sleeve block (10) is sleeved on the outer wall of the rotating shaft (11), and the bottom end of the connecting rod (6) is connected to the sleeve block (10).

3. The multifunctional wing operating platform according to claim 2, characterized in that: A rotating drum (14) is rotatably connected inside the support frame (3); the top end of the rotating drum (14) is connected to the rotating block (4); the bottom end of the rotating drum (14) extends into the interior of the driving box (2); a worm gear (16) is sleeved on the bottom end of the rotating drum (14); a placement seat (18) is installed at the inner bottom end of the driving box (2); a motor (19) is installed at the top end of the placement seat (18); a worm gear (21) is installed at the output end of the motor (19); the worm gear (21) is meshed with the worm gear (16).

4. The multifunctional wing operating platform according to claim 3, characterized in that: A bevel gear 1 (12) is mounted on the outer wall of the rotating shaft 1 (11); the interior of the rotating drum (14) is rotatably connected to a rotating shaft 2 (15); the top end of the rotating shaft 2 (15) extends into the interior of the rotating block (4); the top end of the rotating shaft 2 (15) is mounted with a bevel gear 2 (13); the bevel gear 1 (12) meshes with the bevel gear 2 (13); the bottom end of the rotating shaft 2 (15) extends out of the rotating drum (14); the bottom end of the rotating shaft 2 (15) is mounted with a worm gear 2 (17); the inner bottom end of the driving box (2) is mounted with a motor 2 (20); the output end of the motor 2 (20) is mounted with a worm gear 2 (22); the worm gear 2 (22) meshes with the worm gear 2 (17).

5. The multifunctional wing operating platform according to claim 4, characterized in that: A bearing seat 1 (23) is mounted on the outer wall of the worm gear 1 (21), and a bearing seat 2 (24) is mounted on the outer wall of the worm gear 2 (22). The bearing seat 1 (23) and the bearing seat 2 (24) are respectively mounted on the inner walls of both sides of the drive box (2).

6. The multifunctional wing operating platform according to claim 1, characterized in that: A support column (8) is installed at the top of the operating platform (1), and a control panel (9) is installed at the top of the support column (8).

7. The multifunctional wing operating platform according to claim 1, characterized in that: The inner concave portion of the wing (7) is rotatably connected to a rudder surface (71), the top end of the wing (7) is connected to a steering gear (72), a rocker (73) is installed at the output end of the steering gear (72), an end of the rocker (73) away from the steering gear (72) is connected to a connecting rod (74), an end of the connecting rod (74) away from the rocker (73) is hingedly connected to a rudder angle (75), and the rudder angle (75) is installed at the top end of the rudder surface (71).

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