CN220478115U - Auxiliary device for manufacturing aeromodelling - Google Patents
Auxiliary device for manufacturing aeromodelling Download PDFInfo
- Publication number
- CN220478115U CN220478115U CN202321893188.8U CN202321893188U CN220478115U CN 220478115 U CN220478115 U CN 220478115U CN 202321893188 U CN202321893188 U CN 202321893188U CN 220478115 U CN220478115 U CN 220478115U
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- wing
- plate
- supporting plate
- positioning
- wing supporting
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 19
- 238000009434 installation Methods 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 239000010977 jade Substances 0.000 description 2
- 210000001503 joint Anatomy 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000000149 penetrating effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of model airplane manufacturing devices, in particular to an auxiliary model airplane manufacturing device, which comprises: the surface of the bottom plate is provided with a wing supporting plate accommodating groove, the inside of the wing supporting plate accommodating groove is provided with a wing supporting plate positioning plate accommodating groove, and the side wall of the wing supporting plate positioning plate accommodating groove is provided with a positioning groove; the wing supporting plate is arranged in the wing supporting plate accommodating groove, and the wing supporting plate positioning plate mounting frame is arranged on the surface of the wing supporting plate; the wing supporting plate positioning plate is arranged in the wing supporting plate positioning plate accommodating groove; the beneficial effects are as follows: through rotating the wing backing plate and the wing backing plate locating plate and connecting, when needing to carry out auxiliary installation to the wing, through upset wing backing plate locating plate, make wing backing plate locating plate pass through the locating ball and fix a position the constant head tank, make wing backing plate and wing backing plate locating plate form the triangle support, alright carry out auxiliary assembly to the wing through the wing backing plate this moment.
Description
Technical Field
The utility model relates to the technical field of model airplane manufacturing devices, in particular to an auxiliary model airplane manufacturing device.
Background
The aeromodelling is a generic term for various aircraft models, and comprises model aircrafts and other model aircrafts, and auxiliary assembly is needed to be carried out on model airplane components through auxiliary devices in the manufacturing process of the model airplane;
the utility model discloses a model aeroplane and model ship wing assembles auxiliary stand, through the bottom plate, inside and outside supporting plate, the support, and preceding back supporting plate is constituteed, wherein inside and outside supporting plate supports fixedly through the support, inside and outside supporting plate can accomodate the connection with inside and outside storage tank, the support can accomodate the connection with the support storage tank, when using, will inside and outside supporting plate overturn from inside and outside storage tank, will support the support and overturn out from the support storage tank, and will support inside and outside supporting plate, the model aeroplane and model ship wing is erect in the recess of preceding back supporting plate, the model aeroplane and model ship wing then is erect on inside and outside supporting plate, make model aeroplane and model ship wing form the contained angle with the fuselage relatively, be convenient for the cementing of wing and fuselage, whole support simple structure accomodates conveniently, can improve the concatenation quality of wing;
but after turning out the backing sheet from accomodating the groove, because the problem of angle, support and backing sheet are difficult to dock, need dock at specific angle, and the angle of backing sheet can't adjust after the dock, can not satisfy the auxiliary of different wing angles, and the suitability is lower.
Disclosure of Invention
The utility model aims to provide an auxiliary device for manufacturing a model airplane, which solves the problems of the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
a model airplane making aid, comprising:
the surface of the bottom plate is provided with a wing supporting plate accommodating groove, the inside of the wing supporting plate accommodating groove is provided with a wing supporting plate positioning plate accommodating groove, and the side wall of the wing supporting plate positioning plate accommodating groove is provided with a positioning groove;
the wing supporting plate is arranged in the wing supporting plate accommodating groove, and the wing supporting plate positioning plate mounting frame is arranged on the surface of the wing supporting plate;
the wing supporting plate positioning plate is arranged in the wing supporting plate positioning plate storage groove, the surface of the wing supporting plate positioning plate is provided with a telescopic groove, and the inside of the telescopic groove is provided with a positioning ball.
Preferably, the wing supporting plate storage grooves are at least provided with two groups, the side walls of the wing supporting plate storage grooves are symmetrically provided with wing supporting plate rotating shaft holes, the wing supporting plate storage grooves are symmetrically arranged in the center of the surface of the bottom plate, the surface of the bottom plate is provided with a body supporting plate storage groove, the two sides of the body supporting plate storage groove are symmetrically provided with body supporting plate rotating shaft holes, and the body supporting plate storage grooves are rotatably provided with body supporting plates through the body supporting plate rotating shaft holes.
Preferably, the wing supporting plate locating plate accommodating groove is formed in the bottom of the inner wall of the wing supporting plate accommodating groove.
Preferably, the locating grooves are at least provided with two groups, and the locating grooves are symmetrically arranged on the inner walls of the two sides of the wing supporting plate locating plate accommodating groove.
Preferably, wing supporting plate rotating shafts are fixedly arranged on two sides of the wing supporting plates, the wing supporting plate rotating shafts are rotationally inserted into the wing supporting plate rotating shaft holes, and finger grooves are formed in one ends, far away from the wing supporting plate rotating shafts, of the wing supporting plates and are used for pulling out the wing supporting plates from the inside of the wing supporting plate storage grooves.
Preferably, the wing supporting plate locating plate mounting frame is fixedly arranged on one side, close to the wing supporting plate locating plate storage groove, of the wing supporting plate, and the surface of the wing supporting plate locating plate mounting frame is provided with a locating plate rotating shaft hole in a penetrating mode.
Preferably, the two sides of the wing supporting plate locating plate are fixedly provided with locating plate rotating shafts, the locating plate rotating shafts are rotatably arranged in the locating plate rotating shaft holes, and the wing supporting plate locating plate is rotatably connected with the wing supporting plate locating plate mounting frame through the locating plate rotating shafts and the locating plate rotating shaft holes.
Preferably, the telescopic slots are symmetrically formed in two sides of one end, far away from the rotating shaft of the positioning plate, of the wing supporting plate positioning plate, and the end parts of the telescopic slots are provided with binding openings.
Preferably, the positioning ball and the inner wall of the telescopic groove are arranged in a sliding mode, and a supporting spring is arranged between the positioning ball and the inner wall of the telescopic groove.
Compared with the prior art, the utility model has the beneficial effects that:
1. through rotating the wing backing plate and the wing backing plate locating plate and being connected, when needing to carry out auxiliary installation to the wing, through upset wing backing plate locating plate, make wing backing plate locating plate pass through the locating ball and fix a position the constant head tank, make wing backing plate and wing backing plate locating plate form the triangle support, alright carry out auxiliary assembly to the wing through the wing backing plate this moment, avoided the difficult problem of docking of support and backing plate.
2. Through setting up multiunit constant head tank, when the supporting angle of wing backing plate needs to be changed, cooperates through control locating ball and different constant head tanks, has realized the multi-angle support of wing backing plate to the wing, avoids the supporting plate jade support to dock the angle of back backing plate and can't adjust, can not satisfy the supplementary problem of different wing angles
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is an exploded view of the present utility model;
FIG. 3 is a schematic view of the structure of the base plate of the present utility model;
FIG. 4 is a schematic view of the wing support panel structure of the present utility model;
FIG. 5 is a schematic view of a wing support panel positioning plate structure of the present utility model;
fig. 6 is an enlarged schematic view of the structure of fig. 5 a according to the present utility model.
In the figure: the bottom plate 1, the wing support piece accommodating groove 11, the wing support piece positioning plate accommodating groove 12, the positioning groove 13, the wing support piece rotating shaft hole 14, the body support piece accommodating groove 15, the body support piece rotating shaft hole 16, the wing support piece 2, the finger groove 21, the wing support piece rotating shaft 22, the wing support piece positioning plate mounting frame 23, the positioning plate rotating shaft hole 24, the wing support piece positioning plate 3, the positioning plate rotating shaft 31, the telescopic groove 32, the positioning ball 33, the support spring 34 and the body support piece 4.
Detailed Description
In order to more clearly illustrate the general inventive concept, reference will be made in the following detailed description, by way of example, to the accompanying drawings.
It should be noted that in the following description, numerous specific details are set forth in order to provide a thorough understanding of the present utility model, however, the present utility model may be practiced in other ways than as described herein, and therefore the scope of the present utility model is not limited by the specific embodiments disclosed below.
In addition, in the description of the present utility model, it should be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "axial", "radial", "circumferential", etc. indicate orientations or positional relationships based on the drawings, are merely for convenience in 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 orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model.
Referring to fig. 1 to 6, the present utility model provides an auxiliary device for manufacturing a model airplane, comprising:
the wing support plate comprises a bottom plate 1, wing support plate accommodating grooves 11 are formed in the surface of the bottom plate 1, wing support plate positioning plate accommodating grooves 12 are formed in the wing support plate accommodating grooves 11, positioning grooves 13 are formed in the side walls of the wing support plate positioning plate accommodating grooves 12, at least two groups of wing support plate accommodating grooves 11 are formed in the side walls of the wing support plate accommodating grooves 11, wing support plate rotating shaft holes 14 are symmetrically formed in the side walls of the wing support plate accommodating grooves 11, the wing support plate accommodating grooves 11 are symmetrically formed in the center of the surface of the bottom plate 1, fuselage support plate accommodating grooves 15 are formed in the surface of the bottom plate 1, fuselage support plate rotating shaft holes 16 are symmetrically formed in the two sides of the fuselage support plate accommodating grooves 15, fuselage support plates 4 are rotatably mounted in the interiors of the fuselage support plate accommodating grooves 15 through the fuselage support plate rotating shaft holes 16, at least two groups of the positioning grooves 13 are formed in the bottoms of the inner walls of the wing support plate accommodating grooves 11, and the positioning grooves 13 are symmetrically formed in the inner walls of the two sides of the wing support plate positioning plate accommodating grooves 12;
the wing support plate 2 is arranged in the wing support plate accommodating groove 11, a wing support plate positioning plate mounting frame 23 is arranged on the surface of the wing support plate 2, wing support plate rotating shafts 22 are fixedly arranged on two sides of the wing support plate 2, the wing support plate rotating shafts 22 are rotationally inserted into the wing support plate rotating shaft holes 14, a finger groove 21 is formed in one end, far away from the wing support plate rotating shafts 22, of the wing support plate 2 and used for pulling out the wing support plate 2 from the wing support plate accommodating groove 11, a wing support plate positioning plate mounting frame 23 is fixedly arranged on one side, close to the wing support plate positioning plate accommodating groove 12, of the wing support plate 2, and positioning plate rotating shaft holes 24 are formed in the surface of the wing support plate positioning plate mounting frame 23 in a penetrating manner;
the wing supporting plate positioning plate 3, the wing supporting plate positioning plate 3 sets up in the inside of wing supporting plate positioning plate storage tank 12, the expansion tank 32 has been seted up on the surface of wing supporting plate positioning plate 3, the inside of expansion tank 32 is provided with the locating ball 33, the both sides fixed mounting of wing supporting plate positioning plate 3 has locating plate pivot 31, locating plate pivot 31 rotates the inside of installing in locating plate pivot hole 24, wing supporting plate positioning plate 3 is rotationally connected through locating plate pivot 31 and locating plate pivot hole 24 and wing supporting plate locating plate mounting bracket 23, the expansion tank 32 symmetry is seted up in the both sides that wing supporting plate positioning plate 3 is kept away from the one end of locating plate pivot 31, the tip of expansion tank 32 is the beam mouth setting, the inner wall slip setting of locating ball 33 and expansion tank 32, be provided with supporting spring 34 between the inner wall of locating ball 33 and expansion tank 32.
Embodiment one:
in the scheme, when the wing is required to be installed in an auxiliary mode, the wing supporting plate 2 is pulled out of the wing supporting plate accommodating groove 11 through the finger groove 21, then one end, away from the wing supporting plate 2, of the wing supporting plate positioning plate 3 slides in the wing supporting plate accommodating groove 12, when the positioning ball 33 is aligned with the positioning groove 13, the positioning ball 33 is sprung into the positioning groove 13 under the action of elasticity of the supporting spring 34, one end, away from the wing supporting plate 2, of the wing supporting plate positioning plate 3 is positioned in the wing supporting plate accommodating groove 12, so that triangular supports are formed between the wing supporting plate 2 and the wing supporting plate positioning plate 3, and at the moment, auxiliary assembly of the wing is carried out through the wing supporting plate 2, and the problem that a support and the supporting plate are not easy to butt joint is avoided.
Embodiment two:
on the basis of the first embodiment, the positioning grooves 13 are arranged into a plurality of groups, when the supporting angle of the wing supporting plate 2 needs to be changed, one end, far away from the wing supporting plate 2, of the wing supporting plate positioning plate 3 is controlled to slide in the wing supporting plate accommodating groove 12, the positioning balls 33 are separated from the inner part of the current positioning groove 13 and are retracted into the inner part of the telescopic groove 32, after the wing supporting plate 2 is adjusted to a proper angle, the positioning balls 33 are clamped into the inner part of the corresponding positioning groove 13, the angles of the wing supporting plate 2 are fixed, the multi-angle support of the wing supporting plate 2 to the wing is realized, the problem that the angles of the supporting plate cannot be adjusted after the supporting plate is abutted by the supporting plate jade bracket is avoided, and the auxiliary problem of different wing angles cannot be satisfied is solved.
Working principle: in the manufacturing process of the aeromodelling, auxiliary assembly is needed to be carried out on aeromodelling components through the auxiliary device, and the aeromodelling manufacturing auxiliary device provided by the utility model is characterized in that the wing supporting plate 2 is rotationally connected with the wing supporting plate positioning plate 3, when auxiliary installation is needed to be carried out on a wing, the wing supporting plate 2 is pulled out of the wing supporting plate accommodating groove 11 through the finger groove 21, then one end of the wing supporting plate positioning plate 3, which is far away from the wing supporting plate 2, slides in the wing supporting plate accommodating groove 12, when the positioning ball 33 is aligned with the positioning groove 13, the positioning ball 33 is sprung into the positioning groove 13 under the elastic action of the supporting spring 34, so that one end of the wing supporting plate positioning plate 3, which is far away from the wing supporting plate 2, is positioned in the wing supporting plate accommodating groove 12, and therefore, the wing supporting plate 2 and the wing supporting plate positioning plate 3 form triangular support, and at the moment, auxiliary assembly can be carried out on the wing through the wing supporting plate 2, and the problem that the support and the supporting plate are not easy to butt joint is avoided.
The present utility model is intended to embrace all such alternatives, modifications and variances which fall within the broad scope of the appended claims. Therefore, any omission, modification, equivalent replacement, improvement, etc. of the present utility model should be included in the scope of the present utility model.
Claims (9)
1. A model airplane making auxiliary device, characterized by comprising:
the wing support plate comprises a bottom plate (1), wherein a wing support plate accommodating groove (11) is formed in the surface of the bottom plate (1), a wing support plate positioning plate accommodating groove (12) is formed in the wing support plate accommodating groove (11), and a positioning groove (13) is formed in the side wall of the wing support plate positioning plate accommodating groove (12);
the wing supporting plate (2), the wing supporting plate (2) is arranged in the wing supporting plate accommodating groove (11), and a wing supporting plate positioning plate mounting frame (23) is arranged on the surface of the wing supporting plate (2);
the wing supporting plate positioning plate (3), the wing supporting plate positioning plate (3) is arranged in the wing supporting plate positioning plate accommodating groove (12), the surface of the wing supporting plate positioning plate (3) is provided with a telescopic groove (32), and the inside of the telescopic groove (32) is provided with a positioning ball (33).
2. The model airplane manufacturing auxiliary device according to claim 1, wherein at least two groups of wing supporting plate accommodating grooves (11) are formed, wing supporting plate rotating shaft holes (14) are symmetrically formed in the side walls of the wing supporting plate accommodating grooves (11), the wing supporting plate accommodating grooves (11) are symmetrically formed in the center of the surface of the bottom plate (1), the body supporting plate accommodating grooves (15) are formed in the surface of the bottom plate (1), body supporting plate rotating shaft holes (16) are symmetrically formed in the two sides of the body supporting plate accommodating grooves (15), and body supporting plates (4) are rotatably mounted in the body supporting plate accommodating grooves (15) through the body supporting plate rotating shaft holes (16).
3. The model airplane manufacturing auxiliary device according to claim 2, wherein the wing supporting plate positioning plate accommodating groove (12) is formed in the bottom of the inner wall of the wing supporting plate accommodating groove (11).
4. A model airplane manufacturing auxiliary device according to claim 3, wherein the positioning grooves (13) are at least provided with two groups, and the positioning grooves (13) are symmetrically arranged on the inner walls of the two sides of the wing supporting plate positioning plate accommodating groove (12).
5. The auxiliary device for manufacturing the aeromodelling according to claim 4, wherein wing supporting plate rotating shafts (22) are fixedly arranged on two sides of the wing supporting plate (2), the wing supporting plate rotating shafts (22) are rotatably inserted into the wing supporting plate rotating shaft holes (14), and finger grooves (21) are formed in one ends, far away from the wing supporting plate rotating shafts (22), of the wing supporting plate (2) and are used for pulling out the wing supporting plate (2) from the inside of the wing supporting plate accommodating groove (11).
6. The auxiliary device for manufacturing aeromodelling according to claim 5, wherein the wing supporting plate positioning plate mounting frame (23) is fixedly mounted on one side of the wing supporting plate (2) close to the wing supporting plate positioning plate receiving groove (12), and a positioning plate rotating shaft hole (24) is formed through the surface of the wing supporting plate positioning plate mounting frame (23).
7. The model airplane manufacturing auxiliary device according to claim 6, wherein positioning plate rotating shafts (31) are fixedly arranged on two sides of the wing supporting plate positioning plate (3), the positioning plate rotating shafts (31) are rotatably arranged in the positioning plate rotating shaft holes (24), and the wing supporting plate positioning plate (3) is rotatably connected with the wing supporting plate positioning plate mounting frame (23) through the positioning plate rotating shafts (31) and the positioning plate rotating shaft holes (24).
8. The auxiliary device for manufacturing the aeromodelling according to claim 7, wherein the telescopic slots (32) are symmetrically formed on two sides of one end of the wing supporting plate locating plate (3) far away from the locating plate rotating shaft (31), and the end parts of the telescopic slots (32) are arranged for the binding openings.
9. The model airplane manufacturing auxiliary device according to claim 8, wherein the positioning ball (33) is slidably arranged with the inner wall of the telescopic groove (32), and a supporting spring (34) is arranged between the positioning ball (33) and the inner wall of the telescopic groove (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321893188.8U CN220478115U (en) | 2023-07-18 | 2023-07-18 | Auxiliary device for manufacturing aeromodelling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321893188.8U CN220478115U (en) | 2023-07-18 | 2023-07-18 | Auxiliary device for manufacturing aeromodelling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220478115U true CN220478115U (en) | 2024-02-13 |
Family
ID=89842996
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321893188.8U Active CN220478115U (en) | 2023-07-18 | 2023-07-18 | Auxiliary device for manufacturing aeromodelling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220478115U (en) |
-
2023
- 2023-07-18 CN CN202321893188.8U patent/CN220478115U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |