Rotary airplane model support

Abstract

The utility model discloses a rotary airplane model support, and relates to the technical field of supports. The top of the base is provided with a rotating mechanism, the top of the rotating mechanism is fixedly connected with a workbench, the left side and the right side of the top of the workbench are provided with supports arranged in a staggered mode, the tops of the supports are fixedly connected with a top plate, the top of the top plate is provided with a loop bar, and the left side and the right side of the loop bar are provided with limiting grooves. A fixing assembly is arranged at the top of the base and comprises a fixing base fixedly connected to the top of the top plate, and supporting rods are fixedly connected to the front side and the rear side of the top of the fixing base correspondingly. The sleeve rods are fixedly connected to the base of the airplane model, then the sleeve rods are placed in the sleeves, the fixing assemblies are driven to clamp the sleeve rods, the sleeve rods drive the airplane model and the top plate to be conveniently mounted and dismounted, the total time needed for dismounting the airplane model can be remarkably shortened in the mounting and dismounting process, and the dismounting efficiency is improved. Therefore, the labor cost is saved.

Description

TECHNICAL FIELD

[0001] The utility model relates to a support technical field, concretely relates to a rotary type airplane model support. BACKGROUND

[0002] The history of airplane models can be traced back to the development stage of early aviation technology, they are not only exploration tools of aviation technology, but also collections of aviation enthusiasts. With the development of science and technology, modern airplane models have made great progress in materials and technology, pay more attention to the restoration of details and authenticity, and airplane model exhibition can become a platform for people to exchange aviation culture, promote cultural exchange and understanding between different regions and different countries, through the exhibition, people can understand the development history and achievements of aviation industry in different countries, and enhance mutual understanding and friendship.

[0003] The existing airplane models are generally displayed by supports, but the general airplane models are fixed with the support through screws, the screw is passed through the hole in the bottom of the model or the reserved hole on the support, and then the nut is screwed to fix the model, but the screw fixing mode needs to be checked and maintained regularly to ensure the fastening state of the screw, which undoubtedly increases the maintenance cost and time cost, especially for the exhibition scene that needs to be frequently replaced or adjusted, which further increases the maintenance cost.

[0004] Therefore, a rotary type airplane model support is provided. UTILITY MODEL CONTENTS

[0005] The utility model aims at: for solving the problem of increasing maintenance cost of airplane model using screw fixing, the utility model provides a rotary type airplane model support.

[0006] The utility model discloses a rotary type airplane model support that realizes the above-mentioned purpose specifically adopts the following technical scheme:

[0007] A rotary type airplane model support, including the base, the top of base is provided with rotating mechanism, the top of rotating mechanism is fixedly connected with workstation, the left and right sides of workstation top are provided with the support that is staggered, the top of support is fixedly connected with top plate, the top of top plate is provided with sleeve rod, the left and right sides of sleeve rod are all provided with limit slot, the top of base is provided with fixed component.

[0008] Further, the fixed component includes the fixed seat fixedly connected at the top of the top plate, the front and rear sides of the top of the fixed seat are both fixedly connected with the support rod, the top end of the support rod is fixedly connected with the sleeve, the top of the fixed seat is fixedly connected with the side plate around, the side plate is fixedly connected with the fixed rod between, the outer wall surface of the fixed rod is movably connected with the mirror image setting movable block one, the bottom end of the mutually close side of movable block one is all provided with the arc slot, the inside of the arc slot is movably connected with the cross bar, the inside bottom end of the fixed seat is fixedly connected with the hydraulic rod one.

[0009] Furthermore, the shape and volume of the sleeve are adapted to the interior of the sleeve, and the output end of the sleeve is located inside the sleeve.

[0010] Furthermore, the sides of the tops of the movable blocks that are close to each other are located inside the limiting grooves.

[0011] Furthermore, rectangular slots are provided on the left and right sides of the top of the base, and the bottom of the bracket is located inside the rectangular slots. Stepper motors are fixedly connected to the left and right sides of the base, and the output ends of the stepper motors are fixedly connected to the rotating shafts.

[0012] Furthermore, each of the brackets has a rectangular groove 2 at its bottom, a sliding rod is fixedly connected inside the rectangular groove 2, a movable block 2 is movably connected to the outer wall of the sliding rod, a telescopic rod is hinged inside the movable block 2, rectangular groove 3 is provided on the left and right sides of the top of the base, hydraulic rod 2 is fixedly connected to the front and rear sides of the base, and a rectangular block is fixedly connected to the output end of the hydraulic rod 2.

[0013] The beneficial effects of this utility model are as follows:

[0014] 1. In this utility model, the sleeve rods are first fixedly connected to the base of the aircraft model, and then the sleeve rods are placed inside the sleeve. The driving fixing component clamps the sleeve rods, so that the sleeve rods can easily install and disassemble the aircraft model with the top plate. The installation and disassembly process can significantly reduce the total time required to disassemble the aircraft model, thereby saving labor costs.

[0015] 2. This utility model, through the setting of the fixing component, first places the sleeve rod inside the sleeve. When the hydraulic rod is activated, the output end moves downward. The hydraulic rod pulls the crossbar downward through the output end. The crossbar pulls the movable blocks downward towards their respective ends, causing the movable blocks to tilt. This causes the top ends of the movable blocks to be positioned inside the limiting grooves, which in turn fix the sleeve rod to the top of the top plate. This facilitates the installation and removal of the aircraft model from the top plate. Attached Figure Description

[0016] Fig. 1 This is a three-dimensional structural diagram of the present invention;

[0017] Fig. 2 This is a schematic diagram of the fixing component of this utility model;

[0018] Fig. 3 This is a schematic diagram of the rectangular groove of this utility model;

[0019] Reference numerals in the attached drawings: 1. Base; 2. Rotating mechanism; 3. Worktable; 4. Support; 401. Top plate; 402. Sleeve rod; 403. Limiting groove; 5. Fixing assembly; 501. Fixed seat; 502. Support rod; 503. Sleeve; 504. Side plate; 505. Fixed rod; 506. Movable block one; 507. Arc groove; 508. Crossbar; 509. Hydraulic rod one; 6. Rectangular groove one; 601. Stepper motor; 602. Rotating shaft; 7. Rectangular groove two; 701. Slide rod; 702. Movable block two; 703. Telescopic rod; 704. Rectangular groove three; 705. Rectangular block; 706. Hydraulic rod two. Detailed Implementation

[0020] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, and not all embodiments. The components of the embodiments of this utility model described and shown in the accompanying drawings can generally be arranged and designed in various different configurations.

[0021] Therefore, the following detailed description of the embodiments of the present invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely to illustrate selected embodiments of the invention. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without inventive effort are within the scope of protection of the present invention.

[0022] It should be noted that similar reference numerals and letters in the following figures indicate similar items; therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures. Furthermore, the terms "first," "second," etc., are used only to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0023] In the description of the embodiments of this utility model, it should be noted that the terms "inner", "outer", "upper", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, or the orientation or positional relationship in which the utility model product is usually placed when in use. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0024] like Figs. 1 to 3As shown, a rotating aircraft model support includes a base 1, a rotating mechanism 2 is provided on the top of the base 1, a worktable 3 is fixedly connected to the top of the rotating mechanism 2, and staggered brackets 4 are provided on the left and right sides of the top of the worktable 3. A top plate 401 is fixedly connected to the top of the brackets 4, and a sleeve rod 402 is provided on the top of the top plate 401. Limiting grooves 403 are provided on the left and right sides of the sleeve rod 402. A fixing component 5 for clamping the sleeve rod 402 is provided on the top of the base 1.

[0025] It should be noted that, firstly, the sleeve rods 402 are all fixedly connected to the base plate of the aircraft model. Then, the sleeve rods 402 are placed inside the sleeve 503, and the driving fixing component 5 clamps the sleeve rods 402, so that the sleeve rods 402 can facilitate the installation and disassembly of the aircraft model and the top plate 401. The fast installation and disassembly process can significantly reduce the total time required for disassembling the aircraft model, thereby saving labor costs.

[0026] The fixing component 5 includes a fixing seat 501 fixedly connected to the top of the top plate 401. Support rods 502 are fixedly connected to the front and rear sides of the top of the fixing seat 501. A sleeve 503 is fixedly connected to the top of the support rod 502. The output end of the sleeve 402 is located inside the sleeve 503. Side plates 504 are fixedly connected to the top of the fixing seat 501. Fixing rods 505 are fixedly connected between the side plates 504. A mirror-shaped movable block 506 is movably connected to the outer wall of the fixing rod 505. An arc-shaped groove 507 is opened at the bottom of the movable block 506 on the side closest to each other. A crossbar 508 is movably connected inside the arc-shaped groove 507. A hydraulic rod 509 is fixedly connected to the bottom of the inside of the fixing seat 501. The output end of the hydraulic rod 509 is fixedly connected to the bottom of the crossbar 508.

[0027] It should be noted that, firstly, the sleeve rod 402 is placed inside the sleeve 503. The hydraulic rod 509 is activated, which drives the output end to move downward. The hydraulic rod 509 pulls the crossbar 508 downward through the output end. The crossbar 508 pulls the movable block 506 downward toward the end that is close to each other, so that the movable block 506 is in an inclined state. This causes the top sides of the movable block 506 to be located inside the limiting groove 403, so that the limiting groove 403 drives the sleeve rod 402 to be fixed at the top of the top plate 401, thereby realizing convenient installation and disassembly between the aircraft model and the top plate 401.

[0028] The base 1 has rectangular slots 6 on the left and right sides of the top. The bottom of the bracket 4 is located inside the rectangular slots 6. The base 1 has stepper motors 601 fixedly connected to the left and right sides. The output end of the stepper motor 601 is fixedly connected to the rotating shaft 602. The output end of the rotating shaft 602 is fixedly connected inside the bracket 4.

[0029] It should be noted that when the external controller is started, the stepper motor 601 starts and drives the rotating shaft 602 to rotate in the forward or reverse direction through the output terminal. During the rotation process, the rotating shaft 602 drives the support 4 to rotate inward or outward, so that the support 4 can adjust the different heights of the aircraft model when supporting the aircraft model.

[0030] The bottom of the bracket 4 is provided with rectangular groove 2 7. A slide rod 701 is fixedly connected inside the rectangular groove 2 7. A movable block 2 702 is movably connected to the outer wall of the slide rod 701. A telescopic rod 703 is hinged inside the movable block 2 702. Rectangular groove 3 704 is provided on the left and right sides of the top of the base 1. Hydraulic rod 2 706 is fixedly connected to the front and rear sides of the base 1. A rectangular block 705 is fixedly connected to the output end of the hydraulic rod 2 706. The bottom end of the telescopic rod 703 is fixedly connected to the top of the rectangular block 705.

[0031] It should be noted that when the bracket 4 is rotated to the appropriate position, the hydraulic rod 706 drives the rectangular block 705 to move forward or backward through the output end, so that the telescopic rod 703 at the top of the rectangular block 705 is in a vertical state. The telescopic rod 703 is fixed by the movable block 702 and the movable block 702, so as to prevent the bracket 4 from shaking when supporting the aircraft model.

[0032] In summary: First, the sleeve rods 402 are all fixedly connected to the base 1 of the aircraft model. Then, the sleeve rods 402 are placed inside the sleeve 503, and the driving fixing component 5 clamps the sleeve rods 402, so that the sleeve rods 402 can facilitate the installation and disassembly of the aircraft model and the top plate 401. The fast installation and disassembly process can significantly reduce the total time required for disassembling the aircraft model, thereby saving labor costs.

[0033] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claimed utility model. The scope of protection of this utility model is defined by the appended claims and their equivalents.

Claims

1. A rotating aircraft model support, characterized in that, Includes a base (1), a rotating mechanism (2) is provided on the top of the base (1), a worktable (3) is fixedly connected to the top of the rotating mechanism (2), staggered brackets (4) are provided on the left and right sides of the top of the worktable (3), a top plate (401) is fixedly connected to the top of the brackets (4), a sleeve rod (402) is provided on the top of the top plate (401), and limit grooves (403) are provided on the left and right sides of the sleeve rod (402), and a fixing component (5) is provided on the top of the base (1).

2. The rotating aircraft model support according to claim 1, characterized in that, The fixing component (5) includes a fixing seat (501) fixedly connected to the top of the top plate (401). Support rods (502) are fixedly connected to the front and rear sides of the top of the fixing seat (501). A sleeve (503) is fixedly connected to the top of the support rod (502). Side plates (504) are fixedly connected to the top of the fixing seat (501). Fixing rods (505) are fixedly connected between the side plates (504). A mirror-image movable block (506) is movably connected to the outer wall of the fixing rod (505). An arc-shaped groove (507) is opened at the bottom of the movable block (506) on the side closest to each other. A crossbar (508) is movably connected inside the arc-shaped groove (507). A hydraulic rod (509) is fixedly connected to the bottom inside the fixing seat (501).

3. A rotating aircraft model support according to claim 2, characterized in that, The shape and volume of the sleeve (402) are adapted to the interior of the sleeve (503), and the output end of the sleeve (402) is located inside the sleeve (503).

4. A rotating aircraft model support according to claim 2, characterized in that, The top sides of the movable blocks (506) that are close to each other are located inside the limiting grooves (403).

5. A rotating aircraft model support according to claim 1, characterized in that, The base (1) has rectangular slots (6) on the left and right sides of the top, and the bottom of the bracket (4) is located inside the rectangular slots (6). The base (1) has stepper motors (601) fixedly connected to the left and right sides, and the output end of the stepper motors (601) is fixedly connected to a rotating shaft (602).

6. A rotating aircraft model support according to claim 1, characterized in that, The bottom of the bracket (4) is provided with rectangular groove 2 (7), and a slide rod (701) is fixedly connected inside the rectangular groove 2 (7). A movable block 2 (702) is movably connected to the outer wall of the slide rod (701). A telescopic rod (703) is hinged inside the movable block 2 (702). Rectangular groove 3 (704) is provided on the left and right sides of the top of the base (1). Hydraulic rod 2 (706) is fixedly connected to the front and rear sides of the base (1). A rectangular block (705) is fixedly connected to the output end of the hydraulic rod 2 (706).

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