CN221243943U - Mechanical aircraft model - Google Patents
Mechanical aircraft model Download PDFInfo
- Publication number
- CN221243943U CN221243943U CN202323148394.9U CN202323148394U CN221243943U CN 221243943 U CN221243943 U CN 221243943U CN 202323148394 U CN202323148394 U CN 202323148394U CN 221243943 U CN221243943 U CN 221243943U
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- China
- Prior art keywords
- connecting rod
- base
- wall
- gear
- front panel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 230000005540 biological transmission Effects 0.000 claims abstract description 14
- 229920002972 Acrylic fiber Polymers 0.000 claims description 3
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Abstract
The utility model relates to the technical field of mechanical toys, in particular to a mechanical aircraft model, which comprises a base, wherein a flight model structure is arranged at the top of the base, and a circuit board is arranged at the bottom of the base; the flying model structure comprises a main rod fixedly connected to the top of a base, the outer wall of the main rod is fixedly connected with a rear panel above the base, the front panel is arranged on the outer wall of the rear panel and on the front face of the main rod, a driving motor is fixedly connected to the lower portion of the center of the front panel, a driving gear is fixedly connected to the outer wall of an output shaft of the driving motor and on the back of the front panel, a connecting gear is connected to the top of the driving gear in a meshed mode, a transmission gear is connected to the outer wall of the rear panel and above the connecting gear in a rotating mode, the ornamental value is increased by designing a mechanical aircraft model, and the problem that the existing mechanical aircraft model cannot move and is poor in ornamental value is solved.
Description
Technical Field
The utility model relates to the technical field of mechanical toys, in particular to a mechanical aircraft model.
Background
A mechanical aircraft model is a common mechanical toy, but the existing mechanical aircraft model still has the defects, specifically: the existing mechanical aircraft model cannot move and is poor in ornamental value.
Therefore, there is a need for a mechanical aircraft model that addresses the problems set forth in the background above.
Disclosure of utility model
The present utility model is directed to a mechanical aircraft model to solve the above-mentioned problems.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
The mechanical aircraft model comprises a base, wherein a flight model structure is arranged at the top of the base, and a circuit board is arranged at the bottom of the base;
The flying model structure comprises a main rod fixedly connected to the top of a base, wherein the outer wall of the main rod is fixedly connected with a rear panel above the base, the front panel is arranged on the outer wall of the rear panel and on the front surface of the main rod, a driving motor is fixedly connected to the lower part of the center of the inner part of the front panel, the outer wall of an output shaft of the driving motor is fixedly connected with a driving gear on the back surface of the front panel, the top of the driving gear is meshed with a connecting gear, the outer wall of the rear panel is rotationally connected with a transmission gear above the connecting gear, the front surface of the transmission gear is fixedly connected with a crankshaft, an inner connecting rod is arranged on the outer wall of the crankshaft, an outer connecting rod is arranged on the outer wall of the inner connecting rod and is far away from the position of the crankshaft, and a connecting rod is arranged on the outer wall of the outer connecting rod, and wing plates are fixedly connected to the tops of the inner connecting rod and the outer connecting rod.
As a preferable scheme of the utility model, the base is made of acrylic plastic, and the circuit board is provided with a USB charging interface.
As a preferable scheme of the utility model, the main rod, the rear panel, the front panel, the crankshaft, the inner connecting rod, the outer connecting rod and the wing plates are all made of aluminum alloy.
As a preferable scheme of the utility model, the inner connecting rod and the outer connecting rod are of L-shaped structural design, the rear panel and the front panel are connected through bolts, and the connecting gear is rotationally connected with the rear panel.
As the preferable scheme of the utility model, the main rod penetrates through and extends into the base, and the transmission gear, the crankshaft, the inner connecting rod, the outer connecting rod and the connecting rod are all provided with two groups.
As a preferable scheme of the utility model, the connecting rod is connected with the crankshaft through the locating pin, the driving motor is electrically connected with the circuit board, and the driving motor penetrates through and extends out of the front panel.
Compared with the prior art, the utility model has the beneficial effects that:
1. According to the mechanical aircraft model, the ornamental value is increased by utilizing the flying model structure in the device, a power line is inserted into a charging socket in a circuit board, the circuit board starts a driving motor, the driving motor drives a connecting gear to rotate through a driving gear, the rotating connecting gear drives a crankshaft to rotate through a transmission gear, the rotating crankshaft drives an outer connecting rod to rotate downwards through an inner connecting rod, the inner connecting rod and the outer connecting rod drive a wing plate to move downwards, after the crankshaft rotates for half a circle, the crankshaft drives the wing plate to move upwards through the outer connecting rod and the inner connecting rod, and the inner connecting rod and the outer connecting rod drive the wing plate to move upwards along with the rotation of the transmission gear, so that the ornamental value is improved, and the problems that the existing mechanical aircraft model cannot move and is poor in ornamental value are solved.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a side cross-sectional view of the present utility model;
fig. 3 is a partial front cross-sectional view of the present utility model at the point of attachment of gears.
In the figure: 1. a base; 2. a flight model structure; 3. a circuit board; 201. a main rod; 202. a rear panel; 203. a front panel; 204. a drive motor; 205. a drive gear; 206. a connecting gear; 207. a transmission gear; 208. a crankshaft; 209. an inner link; 210. an outer link; 211. a connecting rod; 212. wing plates.
Detailed Description
The technical solutions of the embodiments of the present utility model will be clearly and completely described below in conjunction with the embodiments of the present utility model, and it is apparent that the described embodiments are only some embodiments of the present utility model, but not all embodiments, and all other embodiments obtained by those skilled in the art without making any inventive effort based on the embodiments of the present utility model are within the scope of protection of the present utility model.
Referring to fig. 1-3, the present utility model provides a technical solution:
the mechanical aircraft model comprises a base 1, wherein a flight model structure 2 is arranged at the top of the base 1, and a circuit board 3 is arranged at the bottom of the base 1;
Wherein the base 1 is made of acrylic plastic, and the circuit board 3 is provided with a USB charging interface;
In this embodiment, referring to fig. 2 and 3, the flight model structure 2 includes a main rod 201 fixedly connected to the top of the base 1, a rear panel 202 fixedly connected to the outer wall of the main rod 201 above the base 1, a front panel 203 mounted on the front of the main rod 201, a driving motor 204 fixedly connected to the lower part of the inner center of the front panel 203, a driving gear 205 fixedly connected to the outer wall of the output shaft of the driving motor 204 and the rear of the front panel 203, a connecting gear 206 engaged to the top of the driving gear 205, a transmission gear 207 rotatably connected to the outer wall of the rear panel 202 and above the connecting gear 206, a crankshaft 208 fixedly connected to the front of the transmission gear 207, an inner link 209 mounted to the outer wall of the crankshaft 208, an outer link 210 mounted to the outer wall of the inner link 209 and at a position far from the crankshaft 208, a connecting rod 211 disposed on the outer link 210, wing plates 212 fixedly connected to the tops of the inner link 209 and the outer link 210;
The main rod 201, the rear panel 202, the front panel 203, the crankshaft 208, the inner connecting rod 209, the outer connecting rod 210 and the wing plate 212 are all made of aluminum alloy, the inner connecting rod 209 and the outer connecting rod 210 are of L-shaped structural design, the rear panel 202 and the front panel 203 are connected through bolts, the connecting gear 206 is connected with the rear panel 202 in a rotating mode, the main rod 201 penetrates through and extends into the base 1, two groups of transmission gears 207, the crankshaft 208, the inner connecting rod 209, the outer connecting rod 210 and the connecting rod 211 are arranged, the connecting rod 211 is connected with the crankshaft 208 through positioning pins, the driving motor 204 is electrically connected with the circuit board 3 in a connecting mode, the driving motor 204 penetrates through and extends to the outside of the front panel 203, the driving motor 204 drives the connecting gear 206 to rotate through the driving gear 205, the rotating connecting gear 206 drives the crankshaft 208 to rotate through the transmission gears 207, the rotating crankshaft 208 drives the outer connecting rod 210 to rotate downwards through the inner connecting rod 209, the inner connecting rod 209 and the outer connecting rod 210 drives the wing plate 212 to move downwards, after the crankshaft 208 rotates half a circle, the crankshaft 208 is connected with the connecting rod 211 and the inner connecting rod 208 drives the inner connecting rod 210 and the outer connecting rod 208 to move upwards along with the upper wing plate 212 and the lower wing plate 212.
The working flow of the utility model is as follows: when the mechanical aircraft model designed by the scheme is operated, a power line is inserted into a charging jack in the circuit board 3, the circuit board 3 starts a driving motor 204, the driving motor 204 drives a connecting gear 206 to rotate through a driving gear 205, the rotating connecting gear 206 drives a crankshaft 208 to rotate through a transmission gear 207, the rotating crankshaft 208 drives an outer connecting rod 210 to rotate downwards through an inner connecting rod 209, the inner connecting rod 209 and the outer connecting rod 210 drive a wing plate 212 to move downwards, after the crankshaft 208 rotates for half a circle, the crankshaft 208 rotates upwards through the connecting rod 211 and the outer connecting rod 210, the inner connecting rod 209 and the outer connecting rod 210 drive the wing plate 212 to move upwards, and the crankshaft 208 continuously rotates along with the rotation of the transmission gear 207 to drive the wing plate 212 to move up and down through the inner connecting rod 209 and the outer connecting rod 210.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. A mechanical aircraft model comprising a base (1), characterized in that: the top of the base (1) is provided with a flight model structure (2), and the bottom of the base (1) is provided with a circuit board (3);
The utility model discloses a flying model structure (2), including mobile jib (201) of fixed connection at base (1) top, the outer wall of mobile jib (201) just is connected with back panel (202) in the top fixedly connected with of base (1), front panel (203) are installed in the front of mobile jib (201) and are just to the outer wall of back panel (202), the below fixedly connected with driving motor (204) of front panel (203) inside center department, the outer wall of driving motor (204) output shaft just is connected with driving gear (205) at the back fixedly connected with of front panel (203), the top meshing of driving gear (205) is connected with connecting gear (206), the outer wall of back panel (202) just rotates in the top of connecting gear (206) and is connected with drive gear (207), the front fixedly connected with bent axle (208) of drive gear (207), inner connecting rod (209) are installed to the outer wall of bent axle (208), outer connecting rod (210) are installed in the outer wall of inner connecting rod (209) and are kept away from bent axle (208) position department, outer connecting rod (210) outer wall is provided with connecting rod (211) and outer wing (212), connecting rod (209) and homopter (212) are connected with top homopter.
2. A mechanical aircraft model according to claim 1, characterized in that: the base (1) is made of acrylic plastic, and the circuit board (3) is provided with a USB charging interface.
3. A mechanical aircraft model according to claim 1, characterized in that: the main rod (201), the rear panel (202), the front panel (203), the crankshaft (208), the inner connecting rod (209), the outer connecting rod (210) and the wing plates (212) are all made of aluminum alloy.
4. A mechanical aircraft model according to claim 1, characterized in that: the inner connecting rod (209) and the outer connecting rod (210) are of L-shaped structural design, the rear panel (202) and the front panel (203) are connected through bolts, and the connecting gear (206) and the rear panel (202) are connected in a rotating mode.
5. A mechanical aircraft model according to claim 1, characterized in that: the main rod (201) penetrates through and extends into the base (1), and two groups of transmission gears (207), crankshafts (208), inner connecting rods (209), outer connecting rods (210) and connecting rods (211) are arranged.
6. A mechanical aircraft model according to claim 1, characterized in that: the connecting rod (211) is connected with the crankshaft (208) through a locating pin, the driving motor (204) is electrically connected with the circuit board (3), and the driving motor (204) penetrates through and extends out of the front panel (203).
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221243943U true CN221243943U (en) | 2024-07-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant |