CN220041281U - Cabin cover take-off and landing device for full-size airplane model dynamic display - Google Patents
Cabin cover take-off and landing device for full-size airplane model dynamic display Download PDFInfo
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- CN220041281U CN220041281U CN202321345585.1U CN202321345585U CN220041281U CN 220041281 U CN220041281 U CN 220041281U CN 202321345585 U CN202321345585 U CN 202321345585U CN 220041281 U CN220041281 U CN 220041281U
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Abstract
The utility model relates to the technical field of horizontal boring machines, in particular to a hatch cover take-off and landing device for dynamic display of a full-sized airplane model, which comprises a positioning assembly, wherein the front part of the upper end of the positioning assembly is fixedly connected with a rotating assembly, the rear part of the upper end of the positioning assembly is fixedly connected with a supporting frame, the upper end of the supporting frame is fixedly connected with an electric push rod, the output end of the electric push rod is fixedly connected with a connecting plate, the upper end of the connecting plate is fixedly connected with a supporting block, and the outer surface of the supporting block is sleeved with a positioning frame; the positioning assembly comprises a supporting plate, two supporting rods are fixedly connected to the left end and the right end of the supporting plate, extension rods are connected to the non-opposite ends of the two transverse supporting rods in a penetrating mode, and connecting blocks are fixedly connected to the non-opposite ends of the two transverse extension rods. According to the hatch cover take-off and landing device for the full-size airplane model dynamic display, the stability of the hatch cover in the take-off and landing process can be enhanced through the supporting frame and the rotating assembly.
Description
Technical Field
The utility model relates to the technical field of hatch cover take-off and landing, in particular to a hatch cover take-off and landing device for dynamic display of a full-size airplane model.
Background
The hatch cover take-off and landing device is a mechanical device for lifting the hatch cover when the rolling hatch cover is opened and closed, and has at least the following disadvantages in the use process of the existing hatch cover take-off and landing device for dynamic display of an airplane model: 1. the existing hatch cover take-off and landing device for dynamic display of the airplane model is poor in stability and troublesome to install and detach; 2. the existing hatch cover take-off and landing device for dynamic display of the airplane model is easy to shake in the process of taking off and landing the hatch cover, so that a new hatch cover take-off and landing device for dynamic display of the full-size airplane model is provided.
Disclosure of Invention
The utility model mainly aims to provide a hatch cover take-off and landing device for dynamic display of a full-size airplane model, which can effectively solve the problems in the background technology.
In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:
the cabin cover take-off and landing device for the full-size airplane model dynamic display comprises a positioning assembly, wherein the front part of the upper end of the positioning assembly is fixedly connected with a rotating assembly, the rear part of the upper end of the positioning assembly is fixedly connected with a supporting frame, the upper end of the supporting frame is fixedly connected with an electric push rod, the output end of the electric push rod is fixedly connected with a connecting plate, the upper end of the connecting plate is fixedly connected with a supporting block, and the outer surface of the supporting block is sleeved with a positioning frame;
the positioning assembly comprises a supporting plate, two supporting rods are fixedly connected to the left end and the right end of the supporting plate, extension rods are connected to the non-opposite ends of the supporting rods in a penetrating mode, connecting blocks are fixedly connected to the non-opposite ends of the extension rods, and the supporting plate is fixedly connected with the rotating assembly.
Preferably, the rotating assembly comprises a supporting plate, the right end of the supporting plate is fixedly connected with a U-shaped frame, the inner frame wall of the U-shaped frame is movably connected with a supporting block through a bearing, the upper end of the supporting block is connected with a fixed inserting block in a penetrating mode, the upper end of the supporting plate is fixedly connected with a motor, the output end of the motor penetrates through the U-shaped frame and is fixedly connected with the supporting block, and the supporting plate is fixedly connected with the positioning assembly.
Preferably, the supporting frame comprises a second U-shaped frame, a second supporting plate is fixedly connected to the middle of the right end of the second U-shaped frame, a second motor is fixedly connected to the upper end of the second supporting plate, a rotating plate is fixedly connected to the output end of the second motor, which penetrates through the part of the second U-shaped frame, and the second U-shaped frame is fixedly connected with the positioning assembly.
Preferably, the rotating plate is not contacted with the inner lower frame wall of the second U-shaped frame.
Preferably, the supporting block is not contacted with the inner lower frame wall of the first U-shaped frame.
Compared with the prior art, the utility model has the following beneficial effects:
1. through setting up the rotation subassembly, with the fixed plug on the rotation subassembly with cabin cover fixed connection, again with fixed plug with supporting shoe interlude connect to fix through the screw, can link together cabin cover and rotation subassembly, improve stability, and the connection between cabin cover and the rotation subassembly is installed and is dismantled conveniently;
2. through setting up rotation component and locating frame, come into contact with locating frame and cabin cover, support the cabin cover, with fixed insert and cabin cover fixed connection on the rotation component, can strengthen the connection between whole cabin cover and the lifting device, avoid the cabin cover to appear rocking at the lift in-process, improve stability.
Drawings
FIG. 1 is a schematic diagram of the overall structure of a hatch cover take-off and landing device for dynamic display of a full-size aircraft model;
FIG. 2 is a schematic diagram of the overall structure of a positioning assembly of a hatch cover take-off and landing device for dynamic display of a full-size aircraft model;
FIG. 3 is a schematic diagram of the overall structure of a rotating assembly of a hatch cover take-off and landing device for dynamic display of a full-size aircraft model;
fig. 4 is a schematic diagram of the overall structure of a supporting frame of a hatch cover take-off and landing device for dynamic display of a full-size aircraft model.
In the figure: 1. a positioning assembly; 2. a rotating assembly; 3. a support frame; 4. an electric push rod; 5. a connecting plate; 6. a positioning frame; 7. a support block; 11. a support plate; 12. a support rod; 13. an extension rod; 14. a connecting block; 21. a first supporting plate; 22. a motor I; 23. a U-shaped frame I; 24. a support block; 25. fixing the insert block; 31. a second U-shaped frame; 32. a second supporting plate; 33. a motor II; 34. and rotating the plate.
Detailed Description
The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.
In the description of the present utility model, it should be noted that the directions or positional relationships indicated by the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific direction, be configured and operated in the specific direction, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
Referring to fig. 1-4, the present utility model provides a technical solution:
the utility model provides a cabin cover take-off and landing device for full-size aircraft model dynamic display, includes locating component 1, locating component 1 upper end front portion fixedly connected with rotates subassembly 2, locating component 1 upper end rear portion fixedly connected with braced frame 3, braced frame 3 upper end fixedly connected with electric putter 4, electric putter 4's output fixedly connected with connecting plate 5, connecting plate 5 upper end fixedly connected with supporting shoe 7, supporting shoe 7 external surface has cup jointed locating frame 6;
in this embodiment, the positioning assembly 1 includes a supporting plate 11, two supporting rods 12 are fixedly connected to the left and right ends of the supporting plate 11, extension rods 13 are connected to the non-opposite ends of the two transverse supporting rods 12 in a penetrating manner, connecting blocks 14 are fixedly connected to the non-opposite ends of the two transverse extension rods 13, and the supporting plate 11 is fixedly connected to the rotating assembly 2; the rotating assembly 2 comprises a first supporting plate 21, the right end of the first supporting plate 21 is fixedly connected with a first U-shaped frame 23, the inner frame wall of the first U-shaped frame 23 is movably connected with a supporting block 24 through a bearing, the upper end of the supporting block 24 is connected with a fixed inserting block 25 in a penetrating way, the upper end of the first supporting plate 21 is fixedly connected with a first motor 22, the output end of the first motor 22 penetrates through the first U-shaped frame 23 and is fixedly connected with the supporting block 24, and the first supporting plate 21 is fixedly connected with the positioning assembly 1; the supporting block 24 is not contacted with the lower frame wall in the U-shaped frame 23, the whole lifting device is supported by arranging the positioning component 1, the connecting lengths of the four supporting rods 12 and the four extension rods 13 are adjusted, the positioning positions of the four connecting blocks 14 on the positioning component 1 can be adjusted by respectively fixing the connecting lengths through screws, the flexibility is improved, the hatch cover is rotated and lifted through arranging the rotating component 2, the fixed inserting block 25 is fixedly connected with the hatch cover, the fixed inserting block 25 is connected with the supporting block 24 in a penetrating manner through screws, the rotating component 2 and the hatch cover are fixedly connected together, the stability is improved, the rotating component 24 is driven to rotate through the motor 22, and the fixed inserting block 25 on the supporting block 24 can be driven to rotate in an angle manner.
In this embodiment, the supporting frame 3 includes a second U-shaped frame 31, a second supporting plate 32 is fixedly connected to the middle of the right end of the second U-shaped frame 31, a second motor 33 is fixedly connected to the upper end of the second supporting plate 32, a rotating plate 34 is fixedly connected to the output end of the second motor 33 passing through the second U-shaped frame 31, and the second U-shaped frame 31 is fixedly connected to the positioning assembly 1; the rotating plate 34 is not contacted with the lower frame wall in the second U-shaped frame 31, the lifting process of the cabin cover is supported by the supporting frame 3, the rotating plate 34 is driven to rotate by the second motor 33, the using angle of the electric push rod 4 arranged on the rotating plate 34 can be adjusted, and the flexibility is improved.
It should be noted that, the utility model relates to a full-sized aircraft model dynamic display hatch cover take-off and landing device, in the use process, the connection lengths of four support rods 12 and four extension rods 13 are adjusted, and the connection lengths are respectively fixed through screws, so that the positions of four connection blocks 14 can be adjusted, the positioning assembly 1 can be positioned in the aircraft model conveniently, the fixed plug 25 is fixedly connected with the hatch cover, the fixed plug 25 is connected with the support block 24 in a penetrating way, and the fixed plug is fixed through screws, the rotating assembly 2 can be fixedly connected with the hatch cover, the positioning frame 6 is contacted with the hatch cover, the connection plate 5 is pushed through the electric push rod 4 to push the hatch cover, the rotation plate 34 is driven to rotate through the motor 33, the pushing angle of the electric push rod 4 is adjusted, the hatch cover is conveniently opened, and when the hatch cover is opened to a certain position, the motor 22 is driven to rotate the frame 23 to rotate, the angle of the fixed plug 25 is adjusted, the hatch cover is conveniently opened further, and the stability is improved.
The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides a cabin cover take-off and landing gear for full-size aircraft model developments show, includes locating component (1), its characterized in that: the positioning device comprises a positioning assembly (1), wherein a rotating assembly (2) is fixedly connected to the front part of the upper end of the positioning assembly (1), a supporting frame (3) is fixedly connected to the rear part of the upper end of the positioning assembly (1), an electric push rod (4) is fixedly connected to the upper end of the supporting frame (3), a connecting plate (5) is fixedly connected to the output end of the electric push rod (4), a supporting block (7) is fixedly connected to the upper end of the connecting plate (5), and a positioning frame (6) is sleeved on the outer surface of the supporting block (7);
the positioning assembly (1) comprises a supporting plate (11), two supporting rods (12) are fixedly connected to the left end and the right end of the supporting plate (11), extension rods (13) are connected to the non-opposite ends of the two transverse supporting rods (12) in a penetrating mode, connecting blocks (14) are fixedly connected to the non-opposite ends of the two transverse extension rods (13), and the supporting plate (11) is fixedly connected with the rotating assembly (2).
2. The full-size aircraft model dynamic display hatch cover take-off and landing device according to claim 1, wherein: the rotating assembly (2) comprises a supporting plate (21), the right end of the supporting plate (21) is fixedly connected with a U-shaped frame (23), the inner frame wall of the U-shaped frame (23) is movably connected with a supporting block (24) through a bearing, the upper end of the supporting block (24) is connected with a fixed inserting block (25) in a penetrating mode, the upper end of the supporting plate (21) is fixedly connected with a motor (22), the output end of the motor (22) penetrates through the U-shaped frame (23) and is fixedly connected with the supporting block (24), and the supporting plate (21) is fixedly connected with the positioning assembly (1).
3. The full-size aircraft model dynamic display hatch cover take-off and landing device according to claim 1, wherein: the supporting frame (3) comprises a second U-shaped frame (31), a second supporting plate (32) is fixedly connected to the middle of the right end of the second U-shaped frame (31), a second motor (33) is fixedly connected to the upper end of the second supporting plate (32), a rotating plate (34) is fixedly connected to the output end of the second motor (33) through the part of the second U-shaped frame (31), and the second U-shaped frame (31) is fixedly connected with the positioning assembly (1).
4. A full-size aircraft model dynamic display hatch landing gear according to claim 3, characterized in that: the rotating plate (34) is not contacted with the inner lower frame wall of the second U-shaped frame (31).
5. The full-size aircraft model dynamic display hatch cover take-off and landing device according to claim 2, wherein: the supporting block (24) is not contacted with the inner lower frame wall of the first U-shaped frame (23).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321345585.1U CN220041281U (en) | 2023-05-30 | 2023-05-30 | Cabin cover take-off and landing device for full-size airplane model dynamic display |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321345585.1U CN220041281U (en) | 2023-05-30 | 2023-05-30 | Cabin cover take-off and landing device for full-size airplane model dynamic display |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220041281U true CN220041281U (en) | 2023-11-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321345585.1U Active CN220041281U (en) | 2023-05-30 | 2023-05-30 | Cabin cover take-off and landing device for full-size airplane model dynamic display |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220041281U (en) |
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2023
- 2023-05-30 CN CN202321345585.1U patent/CN220041281U/en active Active
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