CN216536894U - Model airplane airborne module with protective structure - Google Patents
Model airplane airborne module with protective structure Download PDFInfo
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- CN216536894U CN216536894U CN202122994932.0U CN202122994932U CN216536894U CN 216536894 U CN216536894 U CN 216536894U CN 202122994932 U CN202122994932 U CN 202122994932U CN 216536894 U CN216536894 U CN 216536894U
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Abstract
The utility model discloses an aeromodelling airborne module with a protective structure, which comprises an airborne module body, a protective shell and a silica gel pad, wherein the top of the airborne module body is connected with the protective shell, the silica gel pad is arranged on the surface and the back of the airborne module body, a group of insertion grooves are formed in the two sides of the top of the airborne module body, a group of compression springs a are arranged on the two sides of the bottom of the protective shell, a transverse plate is arranged at the bottom end of each compression spring a, a bearing sleeve is arranged at the bottom of the transverse plate, the inner side wall of each bearing sleeve is connected with a rotating shaft, and a rotating handle is arranged at the bottom end of each rotating shaft. According to the utility model, the protective shell, the inserting groove, the compression spring a, the transverse plate, the bearing sleeve, the rotating shaft, the rotating handle, the movable rod, the extrusion plate, the baffle plate, the compression spring b and the silica gel pad are arranged, so that the model airplane is protected when accidental impact occurs, and the protective shell is convenient to disassemble and assemble after being damaged.
Description
Technical Field
The utility model relates to the technical field of airborne modules, in particular to an airborne module of an aeromodelling with a protective structure.
Background
The model airplane is an aviation model, the model airplane manufactured according to the appearance of an aircraft belongs to an aerospace model and is an unmanned aircraft for movement, the model airplane exceeds the narrow range of research of aerospace scientists, and becomes a learning and movement means of aerospace and flight enthusiasts, an aeromodelling airborne module is an important component of the model airplane, and the existing part of the aeromodelling airborne module does not have a certain protection structure when in use, so that parts of a fuselage of the model airplane are damaged and impact the airborne module when in collision in the flight process, internal parts of the fuselage are damaged, and certain limitation is realized when in use.
The model airplane airborne module with the protective structure in the prior art has the defects that:
1. the patent document CN10797062B discloses a modular model airplane, which comprises a fuselage, a left wing, a right wing, a left empennage and a right empennage, wherein the fuselage is transversely provided with a first slot and a second slot in a penetrating manner, the left wing and the right wing are respectively provided with a first jack and a second jack, and the upper end of the first slot is provided with a third jack and a fourth jack; a fifth jack and a sixth jack are respectively arranged on the left tail wing and the right tail wing, and a seventh jack and an eighth jack are arranged at the upper end of the second slot; the utility model also comprises a first inserting sheet, a second inserting sheet, a third inserting sheet and a fourth inserting sheet, wherein the first inserting sheet and the second inserting sheet can enable the left wing and the right wing to be connected with the airplane body; the third and fourth inserting pieces can connect the left and right empennages with the fuselage; meanwhile, a thread fixing structure is arranged between the machine body and the inserting piece; all parts of the utility model are in modular design, if one part is damaged, the part can be conveniently replaced, thus greatly saving the cost; meanwhile, the device is simple in connection structure and firm in connection, can realize quick assembly and disassembly, greatly facilitates the retraction and release of the transportation of the model airplane, does not relate to the protection of the airborne module when in use, prevents the parts of the model airplane damage from causing certain influence on the airborne module inside the model airplane when the model airplane is accidentally collided with a barrier in the flying process, and has certain limitation when in use.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an airborne module of an airplane model with a protective structure, so as to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme that the model airplane airborne module with the protection structure comprises an airborne module body, a protection shell and silica gel pads, wherein the protection shell is connected to the top of the airborne module body, and the silica gel pads are arranged on the surface and the back of the airborne module body;
a group of inserting grooves are formed in the two sides of the top of the airborne module body, a group of compression springs a are arranged on the two sides of the bottom of the protective shell, and transverse plates are arranged at the bottom ends of the compression springs a;
the bottom of diaphragm is provided with the bearing housing, the inside wall of bearing housing is connected with the pivot, the bottom of pivot is provided with changes the handle, the surface mounting who changes the handle has a set of fixture block, the surface of changeing the handle runs through in the inside of inserting groove.
Preferably, the bottom of the airborne module body is provided with a group of movable rods, and the surfaces of the movable rods are provided with extrusion plates.
Preferably, a compression spring b penetrates through the surface of the movable rod, and a movable cavity penetrates through the surface of the movable rod.
Preferably, the baffle is installed to the inside wall in activity chamber, and the surface of movable rod runs through in the inside of baffle.
Preferably, one side at airborne module body top is provided with the GPS module, one side at airborne module body top is provided with data transmission module.
Preferably, the other side at airborne module body top is provided with video input module, the other side at airborne module body top is provided with video output module.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the utility model, the protective shell, the inserting groove, the compression spring a, the transverse plate, the bearing sleeve, the rotating shaft, the rotating handle, the movable rod, the extrusion plate, the baffle plate, the compression spring b and the silica gel pad are arranged, so that the model airplane is protected when accidental impact occurs, and the protective shell is convenient to disassemble and assemble after being damaged.
Drawings
FIG. 1 is a perspective view of the structure of the present invention;
FIG. 2 is a schematic view of the structure of the insertion groove of the present invention;
FIG. 3 is a schematic view of the protective case of the present invention;
FIG. 4 is a schematic view of a rotating shaft structure according to the present invention;
fig. 5 is a schematic view of the movable rod structure of the present invention.
In the figure: 1. an airborne module body; 2. a protective shell; 3. a silica gel pad; 4. inserting grooves; 5. a compression spring a; 6. a rotating shaft; 7. turning a handle; 8. a movable rod; 9. a pressing plate; 10. a compression spring b; 11. a movable cavity; 12. a baffle plate; 13. a GPS module; 14. a data transmission module; 15. a video input module; 16. and a video output module.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The first embodiment is as follows:
referring to fig. 1, 2, 3, 4, and 5, in an embodiment of the present invention, an airborne module with a protective structure includes an airborne module body 1, a protective shell 2, and a silica gel pad 3, the top of the airborne module body 1 is connected to the protective shell 2, the silica gel pad 3 is disposed on both the surface and the back of the airborne module body 1, a set of insertion slots 4 are disposed on both sides of the top of the airborne module body 1, a set of compression springs a5 are disposed on both sides of the bottom of the protective shell 2, a transverse plate is disposed at the bottom of the compression springs a5, a bearing housing is disposed at the bottom of the transverse plate, a rotating shaft 6 is connected to the inner side wall of the bearing housing, a rotating handle 7 is disposed at the bottom of the rotating handle 7, a set of clamping blocks is mounted on the surface of the rotating handle 7, the surface of the rotating handle 7 penetrates through the insertion slots 4, a set of movable rods 8 is disposed at the bottom of the airborne module body 1, and a pressing plate 9 is mounted on the surface of the movable rods 8, a compression spring b10 penetrates through the surface of the movable rod 8, a movable cavity 11 penetrates through the surface of the movable rod 8, and a baffle plate 12 is arranged on the inner side wall of the movable cavity 11;
the protective shell 2, the inserting groove 4, the compression spring a5, the transverse plate, the bearing sleeve, the rotating shaft 6, the rotating handle 7, the movable rod 8, the extrusion plate 9, the baffle plate 12, the compression spring b10 and the silica gel pad 3 are arranged, because a group of inserting grooves 4 are respectively arranged on two sides of the top of the airborne module body 1, the compression spring a5 is respectively arranged on two sides of the bottom of the protective shell 2, the transverse plate is arranged at the bottom end of the compression spring a5, the bearing sleeve is arranged at the bottom of the transverse plate, the rotating shaft 6 is connected to the inner side wall of the bearing sleeve, the rotating handle 7 is arranged at the bottom end of the rotating shaft 6, because the rotating handle 7 penetrates through the inserting groove 4, when a worker attaches the protective shell 2 and the airborne module body 1, the rotating handle 7 is pulled out from the inside of the inserting groove 4 from the bottom of the airborne module body 1, so that the compression spring a5 is subjected to tensile force, and the rotating handle 7 is rotated through the rotating shaft 6, so that the clamping block on the surface of the rotating handle 7 is clamped at the edge of the inserting groove 4, therefore, the protective shell 2 is completely installed, a certain protection effect is achieved on the airborne module body 1, a group of movable rods 8 are arranged at the bottom of the airborne module body 1, movable cavities 11 penetrate through the surfaces of the movable rods 8, baffle plates 12 are installed on the inner side walls of the movable cavities 11, the surfaces of the movable rods 8 penetrate through the inner portions of the baffle plates 12, compression springs b10 penetrate through the surfaces of the movable rods 8, extrusion plates 9 are installed on the surfaces of the movable rods 8, the airborne module body 1 is prevented from falling off when being taken out for maintenance by workers, force borne by the protective shell 2 or the movable cavities 11 is applied to the compression springs b10 through the movable rods 8, the compression springs b10 move between the baffle plates 12 and the extrusion plates 9, the airborne module body 1 achieves a damping effect and plays a protection effect on the airborne module body 1, and silica gel pads 3 are arranged on the surfaces and the back of the airborne module body 1, make airborne module body 1's surface and back all obtain certain protection, through compression spring a5, change 7, fixture block, compression spring b10, movable rod 8, stripper plate 9 and silica gel pad 3's collocation use for the model aeroplane and model ship plays the effect of protection to it when taking place unexpected striking, and protective housing 2 takes place to damage back convenient to detach and installation simultaneously.
And the surface of the movable rod 8 penetrates through the inside of the baffle 12, a GPS module 13 is arranged on one side of the top of the airborne module body 1, a data transmission module 14 is arranged on one side of the top of the airborne module body 1, a video input module 15 is arranged on the other side of the top of the airborne module body 1, and a video output module 16 is arranged on the other side of the top of the airborne module body 1.
In the utility model, the working steps of the device are as follows:
through the matching work of the protective housing 2, the inserting groove 4, the compression spring a5, the transverse plate, the bearing sleeve, the rotating shaft 6, the rotating handle 7, the movable rod 8, the extrusion plate 9, the baffle plate 12, the compression spring b10 and the silica gel pad 3, because the two sides of the top of the airborne module body 1 are both provided with a group of inserting grooves 4, the two sides of the bottom of the protective housing 2 are both provided with the compression spring a5, the bottom end of the compression spring a5 is provided with the transverse plate, the bottom of the transverse plate is provided with the bearing sleeve, the inner side wall of the bearing sleeve is connected with the rotating shaft 6, the bottom end of the rotating shaft 6 is provided with the rotating handle 7, because the rotating handle 7 penetrates through the inside of the inserting groove 4, when a worker pastes the protective housing 2 and the airborne module body 1, the rotating handle 7 is pulled out of the inside of the inserting groove 4 from the bottom of the airborne module body 1, so that the compression spring a5 is subjected to tensile force, and meanwhile, the rotating handle 7 is rotated through the rotating shaft 6, so that the clamping block on the surface of the rotating handle 7 is clamped at the edge of the inserting groove 4, therefore, the protective shell 2 is completely installed, a certain protection effect is achieved on the airborne module body 1, a group of movable rods 8 are arranged at the bottom of the airborne module body 1, movable cavities 11 penetrate through the surfaces of the movable rods 8, baffle plates 12 are installed on the inner side walls of the movable cavities 11, the surfaces of the movable rods 8 penetrate through the inner portions of the baffle plates 12, compression springs b10 penetrate through the surfaces of the movable rods 8, extrusion plates 9 are installed on the surfaces of the movable rods 8, the airborne module body 1 is prevented from falling off when being taken out for maintenance by workers, force borne by the protective shell 2 or the movable cavities 11 is applied to the compression springs b10 through the movable rods 8, the compression springs b10 move between the baffle plates 12 and the extrusion plates 9, the airborne module body 1 achieves a damping effect and plays a protection effect on the airborne module body 1, and silica gel pads 3 are arranged on the surfaces and the back of the airborne module body 1, make airborne module body 1's surface and back all obtain certain protection, through compression spring a5, change 7, fixture block, compression spring b10, movable rod 8, stripper plate 9 and silica gel pad 3's collocation use for the model aeroplane and model ship plays the effect of protection to it when taking place unexpected striking, and protective housing 2 takes place to damage back convenient to detach and installation simultaneously.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides a model aeroplane and model ship machine carries module with protective structure, includes airborne module body (1), protective housing (2) and silica gel pad (3), its characterized in that: the top of the airborne module body (1) is connected with a protective shell (2), and silica gel pads (3) are arranged on the surface and the back of the airborne module body (1);
a group of inserting grooves (4) are formed in the two sides of the top of the airborne module body (1), a group of compression springs a (5) are arranged on the two sides of the bottom of the protective shell (2), and transverse plates are arranged at the bottom ends of the compression springs a (5);
the bottom of diaphragm is provided with the bearing housing, the inside wall of bearing housing is connected with pivot (6), the bottom of pivot (6) is provided with changes handle (7), the surface mounting who changes handle (7) has a set of fixture block, the surface of changeing handle (7) runs through in the inside of inserting groove (4).
2. The module on board of an aircraft model with a protective structure as claimed in claim 1, characterized in that: the bottom of airborne module body (1) is provided with a set of movable rod (8), the surface mounting of movable rod (8) has stripper plate (9).
3. The module on board of an aircraft model with a protective structure as claimed in claim 2, characterized in that: a compression spring b (10) penetrates through the surface of the movable rod (8), and a movable cavity (11) penetrates through the surface of the movable rod (8).
4. The module on board of an aircraft with a protective structure as claimed in claim 3, characterized in that: baffle (12) are installed to the inside wall in activity chamber (11), and the inside in baffle (12) is run through on the surface of movable rod (8).
5. The module on board of an aircraft model with a protective structure as claimed in claim 1, characterized in that: one side at airborne module body (1) top is provided with GPS module (13), one side at airborne module body (1) top is provided with data transmission module (14).
6. The module on board of an aircraft model with a protective structure as claimed in claim 1, characterized in that: the video input module (15) is arranged on the other side of the top of the airborne module body (1), and the video output module (16) is arranged on the other side of the top of the airborne module body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122994932.0U CN216536894U (en) | 2021-12-01 | 2021-12-01 | Model airplane airborne module with protective structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122994932.0U CN216536894U (en) | 2021-12-01 | 2021-12-01 | Model airplane airborne module with protective structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216536894U true CN216536894U (en) | 2022-05-17 |
Family
ID=81577453
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122994932.0U Active CN216536894U (en) | 2021-12-01 | 2021-12-01 | Model airplane airborne module with protective structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216536894U (en) |
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2021
- 2021-12-01 CN CN202122994932.0U patent/CN216536894U/en active Active
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