CN220595516U - Model airplane main framework - Google Patents
Model airplane main framework Download PDFInfo
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- CN220595516U CN220595516U CN202322198803.XU CN202322198803U CN220595516U CN 220595516 U CN220595516 U CN 220595516U CN 202322198803 U CN202322198803 U CN 202322198803U CN 220595516 U CN220595516 U CN 220595516U
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- 230000000694 effects Effects 0.000 abstract description 10
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000004088 simulation Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Abstract
The utility model discloses a model airplane main framework, which relates to the technical field of model airplane main frameworks, in particular to a model airplane main framework, and comprises a carrying frame, wherein a supporting seat is fixedly arranged at the top of the carrying frame, a lifting groove is formed in one side of the supporting seat, a first screw rod is rotatably connected in the lifting groove, a lifting seat is connected to the outer side of the first screw rod in a transmission manner, the outer side of the lifting seat is slidably connected in the lifting groove, a supporting frame is fixedly arranged on one side of the lifting seat, a driven bevel gear is fixedly arranged below the outer side of the first screw rod, a motor seat is fixedly arranged on the other side of the supporting seat, and a first servo motor is fixedly arranged in the motor seat. This model aeroplane and model ship main frame, through the setting of support and clamping frame, make this model aeroplane and model ship main frame possess the support model aeroplane and model ship that can stabilize, the effect of accurate appearance of guarantee model aeroplane and model ship to play the effect that reduces the transport degree of difficulty, reached the purpose that reduces intensity of labour.
Description
Technical Field
The utility model relates to the technical field of model airplane main frameworks, in particular to a model airplane main framework.
Background
The simulation model is a model which reproduces the real object with a certain standard force according to the size and the structure of a real object, a complex part, a highly simulated model airplane, almost what the real airplane has, from the shape and the number of rivets on the appearance, the style of welding lines to the internal structure, the cab, the lifting frame and other various components, and the research is just like the research on a real weapon system. The main display content of the simulation model airplane for display is the appearance structure of the model airplane and the like, and the model airplane can fly without being required, so that the frame-shaped framework is usually adopted in the model airplane to support the components such as wings and landing gear of the model airplane, and the model airplane needs to be fixedly supported for ensuring the structural strength.
Traditional model aeroplane and model ship skeleton structure is complicated, heavy, and dead weight is big also to self structural strength requirement higher, leads to transport difficulty, intensity of labour are big to current in the handling generally all fix through the rope, and this kind of fixed mode takes place to rock easily, and then causes the model aeroplane and model ship skeleton to take place the appearance change, and it is comparatively inconvenient to use, and the security is lower.
Disclosure of Invention
(one) solving the technical problems
Aiming at the defects of the prior art, the utility model provides a model airplane main framework, which solves the problems in the background art.
(II) technical scheme
In order to achieve the above purpose, the utility model is realized by the following technical scheme: the utility model provides a model aeroplane and model ship owner skeleton, includes the transport frame, the top fixed mounting of transport frame has the supporting seat, the lift groove has been seted up to one side of supporting seat, the inside rotation of lift groove is connected with first lead screw, the outside transmission of first lead screw is connected with the lift seat, the outside sliding connection of lift seat is in the inside of lift groove, one side fixed mounting of lift seat has the support frame, the outside below fixed mounting of first lead screw has driven bevel gear, the opposite side fixed mounting of supporting seat has the motor cabinet, the inside fixed mounting of motor cabinet has first servo motor, the output fixed mounting of first servo motor has driving bevel gear, driving bevel gear's outside meshing is in driven bevel gear's outside, the top fixed mounting of support frame has the support, clamping groove has been seted up to top one side of support, the inside rotation of clamping groove is connected with the second lead screw, the outside transmission of second lead screw is connected with the clamping seat, the outside sliding connection of clamping seat has the inside of clamping groove.
Optionally, the top fixed mounting of clamping seat has the clamping frame, top one side fixed mounting of support has the fixing base.
Optionally, a second servo motor is fixedly installed in the fixing seat, and the output end of the second servo motor is fixedly installed at one end of a second screw rod.
Optionally, the top of support is provided with the model aeroplane and model ship body, one side butt of clamping frame is in one side of model aeroplane and model ship body.
Optionally, a fixing frame is fixedly installed on one side of the top of the carrying frame, a movable groove is formed in the fixing frame, and an electric telescopic rod is fixedly installed on the inner bottom wall of the movable groove.
Optionally, the fixed lifting plate that has of stretching out end of electric telescopic handle, the outside sliding connection of lifting plate is in the inside of movable groove, the top fixed mounting of lifting plate has straight rack.
Optionally, the top of mount rotates and is connected with the rotation axis, the outside fixed mounting of rotation axis has the spur gear, the outside meshing of spur gear is in one side of straight rack.
Optionally, a clamping limit frame is fixedly installed at one end of the rotating shaft, and a clamping limit seat is fixedly installed at one end of the clamping limit frame.
(III) beneficial effects
The utility model provides a model airplane main framework, which has the following beneficial effects:
1. this model airplane main frame, through the setting of support and clamping frame, make this model airplane main frame possess the support model airplane that can stabilize, can ensure the effect of model airplane stable, accurate appearance, through the supporting seat, the lift groove, first lead screw, clamping groove, the second lead screw, clamping seat, clamping frame, the fixing base, the cooperation setting of second servo motor and model airplane body, at first can place the model airplane body at the top of support in the in-process of using, start the second servo motor, the output of second servo motor can drive the second lead screw and rotate, the outside of second lead screw can drive clamping seat and slide in clamping groove's inside, clamping seat can drive clamping frame and slide at the top of support, make one side butt at the model airplane body of clamping frame, when needing to adjust its height, the output of first servo motor can drive driving bevel gear and rotate, driving bevel gear can drive driven bevel gear and rotate, first lead screw can drive the inside slip of lift seat at the lift groove, the support frame can drive the support frame and move, and then the support frame can drive the support frame and move in the inside of clamping groove, thereby the proper position has reached the purpose of carrier height adjustment, the carrier has been reached.
2. This model airplane main frame, through the setting of pressing from both sides tight spacing and pressing from both sides tight spacing, make this model airplane main frame possess and further fix the model airplane in handling, prevent to appear rocking, cause the effect that the model airplane skeleton appearance changed, through the movable groove, electric telescopic handle, the lifter plate, the straight rack, the rotation axis, the spur gear, press from both sides tight spacing and press from both sides the cooperation setting of tight spacing, can open electric telescopic handle when need consolidate the model airplane body in the in-process of use, electric telescopic handle's the inside upward movement of lifter plate in the movable groove can be driven to the extension end, the lifter plate can drive straight rack upward movement, the spur gear can drive the rotation axis and rotate, the rotation axis can drive and press from both sides tight spacing and move, press from both sides tight spacing one end of tight spacing can drive and press from both sides tight spacing and move, and then make one side butt at the top one side of model airplane body, thereby play comparatively convenient effect, the higher purpose of security has been reached.
Drawings
FIG. 1 is a schematic view of a three-dimensional structure of the present utility model;
FIG. 2 is a schematic illustration of the structure of the equal side of the present utility model;
FIG. 3 is a schematic cross-sectional view of the present utility model;
FIG. 4 is an enlarged schematic view of the structure of FIG. 3A according to the present utility model;
FIG. 5 is an enlarged schematic view of the structure of FIG. 2B according to the present utility model;
FIG. 6 is an enlarged schematic view of the structure of FIG. 3C according to the present utility model;
fig. 7 is an enlarged schematic view of the structure of fig. 1D according to the present utility model.
In the figure: 1. a transport rack; 2. a support base; 3. a lifting groove; 4. a first lead screw; 5. a lifting seat; 6. a support frame; 7. a driven bevel gear; 8. a motor base; 9. a first servo motor; 10. a drive bevel gear; 11. a bracket; 12. a clamping groove; 13. a second lead screw; 14. a clamping seat; 15. a clamping frame; 16. a fixing seat; 17. a second servo motor; 18. a model body; 19. a fixing frame; 20. a movable groove; 21. an electric telescopic rod; 22. a lifting plate; 23. a straight rack; 24. a rotation shaft; 25. spur gears; 26. clamping a limit frame; 27. clamping the limiting seat.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments.
Example 1
Referring to fig. 1 to 6, the present utility model provides the following technical solutions: a model airplane main framework comprises a carrying frame 1, a supporting seat 2 is fixedly arranged at the top of the carrying frame 1, a lifting groove 3 is formed in one side of the supporting seat 2, a first lead screw 4 is rotatably connected in the lifting groove 3, a lifting seat 5 is connected on the outer side of the first lead screw 4 in a transmission manner, the outer side of the lifting seat 5 is slidably connected in the lifting groove 3, a supporting frame 6 is fixedly arranged on one side of the lifting seat 5, a driven bevel gear 7 is fixedly arranged below the outer side of the first lead screw 4, a motor seat 8 is fixedly arranged on the other side of the supporting seat 2, a first servo motor 9 is fixedly arranged in the motor seat 8, a driving bevel gear 10 is fixedly arranged at the output end of the first servo motor 9, the outer side of the driving bevel gear 10 is meshed on the outer side of the driven bevel gear 7, a bracket 11 is fixedly arranged at the top of the supporting frame 6, a clamping groove 12 is formed in one side of the top of the bracket 11, the inside of the clamping groove 12 is rotationally connected with a second lead screw 13, the outside of the second lead screw 13 is in transmission connection with a clamping seat 14, the outside of the clamping seat 14 is in sliding connection with the inside of the clamping groove 12, the top of the clamping seat 14 is fixedly provided with a clamping frame 15, one side of the top of the bracket 11 is fixedly provided with a fixed seat 16, the inside of the fixed seat 16 is fixedly provided with a second servo motor 17, the output end of the second servo motor 17 is fixedly arranged at one end of the second lead screw 13, the top of the bracket 11 is provided with a model airplane body 18, one side of the clamping frame 15 is abutted to one side of the model airplane body 18, one side of the top of the carrying frame 1 is fixedly provided with a fixed frame 19, the inside of the fixed frame 19 is provided with a movable groove 20, the inner bottom wall of the movable groove 20 is fixedly provided with an electric telescopic rod 21, the extending end of the electric telescopic rod 21 is fixedly provided with a lifting plate 22, the outside of the lifting plate 22 is in sliding connection with the inside of the movable groove 20, the top fixed mounting of lifter plate 22 has straight rack 23, the top rotation of mount 19 is connected with rotation axis 24, the outside fixed mounting of rotation axis 24 has straight gear 25, the outside meshing of straight gear 25 is in one side of straight rack 23, the one end fixed mounting of rotation axis 24 has the tight spacing 26 of clamp, the one end fixed mounting of tight spacing 26 has the tight spacing seat 27 of clamp, through the setting of support 11 and clamp 15, make this model aeroplane and model ship main frame possess the support model ship that can stabilize, can ensure the effect of the stable, accurate appearance of model aeroplane and model ship, thereby play the effect of reducing the transport degree of difficulty, reached the purpose that reduces intensity of labour.
When the device is used, firstly, the model airplane body 18 is placed at the top of the bracket 11, the second servo motor 17 is started, the output end of the second servo motor 17 drives the second screw rod 13 to rotate, the outer side of the second screw rod 13 drives the clamping seat 14 to slide in the clamping groove 12, the clamping seat 14 drives the clamping frame 15 to slide at the top of the bracket 11, one side of the clamping frame 15 is abutted to one side of the model airplane body 18, when the height of the model airplane body is required to be adjusted, the first servo motor 9 is started, the output end of the first servo motor 9 drives the driving bevel gear 10 to rotate, the driving bevel gear 10 drives the driven bevel gear 7 to rotate, the driven bevel gear 7 drives the first screw rod 4 to rotate, the first screw rod 4 drives the lifting seat 5 to slide in the lifting groove 3, the lifting seat 5 drives the supporting frame 6 to move, and the supporting frame 6 drives the bracket 11 to move, so that the height of the model airplane body 18 is adjusted to a proper position, and the purposes of reducing carrying difficulty are achieved.
Example 2
Referring to fig. 1 to 7, the present utility model provides the following technical solutions: a model airplane main framework comprises a carrying frame 1, a supporting seat 2 is fixedly arranged at the top of the carrying frame 1, a lifting groove 3 is formed in one side of the supporting seat 2, a first lead screw 4 is rotatably connected in the lifting groove 3, a lifting seat 5 is connected on the outer side of the first lead screw 4 in a transmission manner, the outer side of the lifting seat 5 is slidably connected in the lifting groove 3, a supporting frame 6 is fixedly arranged on one side of the lifting seat 5, a driven bevel gear 7 is fixedly arranged below the outer side of the first lead screw 4, a motor seat 8 is fixedly arranged on the other side of the supporting seat 2, a first servo motor 9 is fixedly arranged in the motor seat 8, a driving bevel gear 10 is fixedly arranged at the output end of the first servo motor 9, the outer side of the driving bevel gear 10 is meshed on the outer side of the driven bevel gear 7, a bracket 11 is fixedly arranged at the top of the supporting frame 6, a clamping groove 12 is formed in one side of the top of the bracket 11, the inside of the clamping groove 12 is rotationally connected with a second lead screw 13, the outside of the second lead screw 13 is in transmission connection with a clamping seat 14, the outside of the clamping seat 14 is in sliding connection with the inside of the clamping groove 12, the top of the clamping seat 14 is fixedly provided with a clamping frame 15, one side of the top of the bracket 11 is fixedly provided with a fixed seat 16, the inside of the fixed seat 16 is fixedly provided with a second servo motor 17, the output end of the second servo motor 17 is fixedly arranged at one end of the second lead screw 13, the top of the bracket 11 is provided with a model airplane body 18, one side of the clamping frame 15 is abutted to one side of the model airplane body 18, one side of the top of the carrying frame 1 is fixedly provided with a fixed frame 19, the inside of the fixed frame 19 is provided with a movable groove 20, the inner bottom wall of the movable groove 20 is fixedly provided with an electric telescopic rod 21, the extending end of the electric telescopic rod 21 is fixedly provided with a lifting plate 22, the outside of the lifting plate 22 is in sliding connection with the inside of the movable groove 20, the top fixed mounting of lifter plate 22 has straight rack 23, the top rotation of mount 19 is connected with rotation axis 24, rotation axis 24's outside fixed mounting has straight gear 25, the outside meshing of straight gear 25 is in one side of straight rack 23, rotation axis 24's one end fixed mounting has the tight spacing 26 of clamp, the one end fixed mounting of tight spacing 26 has the tight spacing seat 27 of clamp, through the setting of the spacing 26 of clamp and tight spacing seat 27, make this model aeroplane and model ship main frame possess further fixed the model ship in the handling, prevent to appear rocking, cause the effect that the model aeroplane and model ship skeleton appearance changed, thereby played comparatively convenient effect, reached the higher purpose of security.
When the model airplane 18 is required to be reinforced, the electric telescopic rod 21 is opened, the extending end of the electric telescopic rod 21 can drive the lifting plate 22 to move upwards in the movable groove 20, the lifting plate 22 can drive the straight rack 23 to move upwards, the straight rack 23 can drive the straight gear 25 to rotate, the straight gear 25 can drive the rotating shaft 24 to rotate, the rotating shaft 24 can drive the clamping limiting frame 26 to move, one end of the clamping limiting frame 26 can drive the clamping limiting seat 27 to move, and then one side of the clamping limiting seat 27 is abutted to one side of the top of the model airplane 18, so that a more convenient effect is achieved, and the aim of higher safety is fulfilled.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (8)
1. The utility model provides a model aeroplane and model ship main frame, includes transport frame (1), its characterized in that: the top fixed mounting of handling frame (1) has supporting seat (2), lifting groove (3) have been seted up to one side of supporting seat (2), the inside rotation of lifting groove (3) is connected with first lead screw (4), the outside transmission of first lead screw (4) is connected with lifting seat (5), the outside sliding connection of lifting seat (5) is in the inside of lifting groove (3), one side fixed mounting of lifting seat (5) has support frame (6), the outside below fixed mounting of first lead screw (4) has driven bevel gear (7), the opposite side fixed mounting of supporting seat (2) has motor cabinet (8), the inside fixed mounting of motor cabinet (8) has first servo motor (9), the output fixed mounting of first servo motor (9) has initiative bevel gear (10), the outside meshing of initiative bevel gear (10) is in the outside of driven bevel gear (7), the top fixed mounting of support frame (6) has support frame (11), clamping groove (12) have been seted up to one side of the top of support frame (11), clamping groove (12) have the inside rotation of second lead screw (13) is connected with clamping groove (13), the outside of the clamping seat (14) is connected with the inside of the clamping groove (12) in a sliding way.
2. A model airplane main skeleton according to claim 1, characterized in that: the top of the clamping seat (14) is fixedly provided with a clamping frame (15), and one side of the top of the bracket (11) is fixedly provided with a fixing seat (16).
3. A model airplane main skeleton according to claim 2, characterized in that: the inside fixed mounting of fixing base (16) has second servo motor (17), the output fixed mounting of second servo motor (17) is in the one end of second lead screw (13).
4. A model airplane main skeleton according to claim 3, characterized in that: the top of support (11) is provided with model aeroplane and model ship body (18), one side butt of clamping frame (15) is in one side of model aeroplane and model ship body (18).
5. A model airplane main skeleton according to claim 4, characterized in that: a fixing frame (19) is fixedly arranged on one side of the top of the carrying frame (1), a movable groove (20) is formed in the fixing frame (19), and an electric telescopic rod (21) is fixedly arranged on the inner bottom wall of the movable groove (20).
6. A model airplane main skeleton according to claim 5, characterized in that: the electric telescopic device is characterized in that a lifting plate (22) is fixedly arranged at the extending end of the electric telescopic rod (21), the outer side of the lifting plate (22) is slidably connected in the movable groove (20), and a straight rack (23) is fixedly arranged at the top of the lifting plate (22).
7. A model airplane main skeleton according to claim 6, characterized in that: the top of mount (19) rotates and is connected with rotation axis (24), the outside fixed mounting of rotation axis (24) has spur gear (25), the outside meshing of spur gear (25) is in one side of spur rack (23).
8. A model airplane main skeleton according to claim 7, characterized in that: one end of the rotating shaft (24) is fixedly provided with a clamping limiting frame (26), and one end of the clamping limiting frame (26) is fixedly provided with a clamping limiting seat (27).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322198803.XU CN220595516U (en) | 2023-08-16 | 2023-08-16 | Model airplane main framework |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322198803.XU CN220595516U (en) | 2023-08-16 | 2023-08-16 | Model airplane main framework |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220595516U true CN220595516U (en) | 2024-03-15 |
Family
ID=90165801
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322198803.XU Active CN220595516U (en) | 2023-08-16 | 2023-08-16 | Model airplane main framework |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220595516U (en) |
-
2023
- 2023-08-16 CN CN202322198803.XU patent/CN220595516U/en active Active
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