Unmanned aerial vehicle host plastic part correcting mechanism
By installing guide rods and connecting barrels on the bin cover and bin body of the plastic parts of the drone host, and using the cooperation of nuts and inclined shrinkage sheets, the problem of assembly deviation of the plastic parts of the drone host is solved, and a more stable and sealed connection is achieved.
Patent Information
- Application Number
- CN202422414240.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-08
- Publication Date
- 2025-07-04
- Estimated Expiration
- 2034-10-08
AI Technical Summary
The silo cover and bottom silo body of the plastic parts of the drone main unit are prone to deviations when assembling, resulting in bolt slips and affecting the stability of the connection.
A guide mechanism for plastic parts of the drone host is designed. By installing a guide rod and a connecting cylinder on the bin cover and the bin body, the nut and the inclined shrinkage sheet are used to achieve guide and lock, and the connection stability is improved.
It effectively reduces the deviation and misalignment between the bin cover and the bin body during assembly, and improves the stability and sealing of the connection.
Smart Images

Figure CN223059273U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicle manufacturing, in particular to a plastic part guide mechanism for a host of an unmanned aerial vehicle. Background Art
[0002] At present, in order to meet the lightweight demand of UAV manufacturing, the main body of the UAV is usually made of one-piece injection molded parts, which can be divided into an upper compartment cover and a bottom compartment body. In the prior art, the assembly between the upper compartment cover and the bottom compartment body is usually: using bolts to screw from the bottom compartment body into the screw holes of the upper compartment cover, but the bolts are prone to deviation when docking the screw holes, which in turn causes the bolts to damage the screw hole structure when they are twisted, causing thread slippage in the screw hole, affecting the stability of the connection.
[0003] To this end, we propose a UAV host plastic parts guiding mechanism to solve the above problems. Utility Model Content
[0004] The purpose of the utility model is to provide a plastic part guide mechanism for a drone host to solve the problems raised in the above-mentioned background technology.
[0005] In order to achieve the above purpose, the utility model provides the following technical solutions:
[0006] A guiding mechanism for a plastic part of a drone host comprises a compartment cover, a compartment body, a guide rod and a connecting tube, wherein the guide rod is connected to the lower edge of the compartment cover, and a plurality of guide rods are evenly distributed along the outer edge of the compartment cover, and the connecting tube is connected to the lower edge of the compartment body, and the connecting tube corresponds to the guide rod one by one, and when the compartment cover and the compartment body are fastened, the guide rod passes through the connecting tube, and a nut is screwed on the external thread of the connecting tube, and a plurality of inclined shrinkage sheets are provided at the lower end of the connecting tube along the circumferential direction, and an expansion joint with a narrow upper part and a wide lower part is formed between adjacent shrinkage sheets, and when the nut is tightened, the shrinkage sheet is tightly attached to the guide rod.
[0007] In a further embodiment, the lower outer edge of the bin cover is provided with an inclined connecting edge, and the upper outer edge of the bin body adopts an inclined surface structure matching the connecting edge.
[0008] In a further embodiment, a sealing gasket is embedded on the inclined inner wall of the connecting edge, and the sealing gasket fits tightly with the inclined surface of the bin body.
[0009] In a further embodiment, a connecting groove is provided on the warehouse body corresponding to each connecting tube, and the nut does not protrude from the connecting groove when being tightened.
[0010] In a further embodiment, the lower end of the guide rod is chamfered to form a tapered structure.
[0011] In a further embodiment, a ring groove is formed on the outer side wall of the guide rod, and a matching protrusion is provided at the position of the shrinkage piece corresponding to the ring groove.
[0012] In a further embodiment, a guiding body with a thinner upper part and a thicker lower part is provided inside the nut. When the nut is tightened, the guiding body is in close contact with the shrinkage piece.
[0013] Compared with the prior art, the beneficial effects of the present utility model are as follows:
[0014] When the storage cover and the storage body of the present utility model are assembled, after the guide rod is first inserted into the inside of the connecting cylinder, the nut is then tightened outside the connecting cylinder for locking and fixing, effectively reducing the deviation and dislocation during the assembly and docking of the storage cover and the storage body, guiding and correcting their connection, thereby improving the stability of the connection. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 is a schematic structural diagram of the present utility model;
[0016] Figure 2 is a schematic bottom view structural diagram of the present utility model;
[0017] Figure 3 is a schematic front sectional view structural diagram of the present utility model;
[0018] Figure 4 is a schematic partial sectional view structural diagram when the guide rod, the connecting cylinder and the nut of the present utility model are connected;
[0019] Figure 5 is a schematic structural diagram of the connecting cylinder of the present utility model.
[0020] In the figure: 1, storage cover; 11, connecting edge; 12, sealing gasket; 2, storage body; 21, connecting groove; 3, guide rod; 31, ring groove; 4, connecting cylinder; 41, shrinkage piece; 411, protrusion; 42, expansion joint; 5, nut; 51, guiding body. DETAILED DESCRIPTION OF THE EMBODIMENTS
[0021] In the description of the present utility model, it should be understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as a limitation to the present utility model. In the description of the present utility model, unless otherwise specified, the meaning of "a plurality" is two or more.
[0022] In the description of the present utility model, it should be noted that unless otherwise clearly specified and defined, the terms "installation", "connection", and "coupling" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, and it can be the communication inside two components. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.
[0023] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all of the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.
[0024] Please refer to Figures 1-3 , a guiding mechanism for a plastic part of a drone main body, including a storage cover 1, a storage body 2, a guiding rod 3, and a connecting cylinder 4. Among them, the guiding rod 3 is connected to the lower edge of the storage cover 1, and a plurality of guiding rods 3 are evenly distributed along the outer edge of the storage cover 1. The storage cover 1 and the guiding rod 3 are integrally injection-molded. The connecting cylinder 4 is connected to the lower edge of the storage body 2, and the connecting cylinder 4 corresponds to the guiding rod 3 one by one. The connecting cylinder 4 and the storage body 2 are integrally injection-molded. When the storage cover 1 and the storage body 2 are butted and fastened up and down, the guiding rod 3 penetrates through the connecting cylinder 4. Further, the lower end of the guiding rod 3 is chamfered to form a conical structure, which is convenient for inserting into the connecting cylinder 4. A nut 5 is screwed on the outer thread of the connecting cylinder 4. A plurality of inclined shrinking pieces 41 are arranged along the circumference at the lower end of the connecting cylinder 4. A shrinking gap 42 that is narrower at the top and wider at the bottom is formed between adjacent shrinking pieces 41. When the nut 5 is tightened, the shrinking pieces 41 shrink and then closely adhere to the guiding rod 3 to lock and fix the guiding rod 3.
[0025] Please refer to Figures 4-5 , in order to ensure the locking effect of the shrinking pieces 41, it is provided that the inside of the nut 5 is provided with a guiding body 51 that is thinner at the top and thicker at the bottom. When the nut 5 is tightened, the guiding body 51 gradually presses the shrinking pieces 41, so that the shrinking pieces 41 can shrink and closely adhere to the guiding rod 3. At the same time, a ring groove 31 is opened on the outer side wall of the guiding rod 3, and a matching protrusion 411 is provided at the position of the shrinking piece 41 corresponding to the ring groove 31. When the guiding rod 3 is inserted into the inside of the connecting cylinder 4, the protrusion 411 just snaps into the ring groove 31, thereby effectively preventing the problem of loosening of the guiding rod 3 and improving its connection firmness.
[0026] Please refer to Figures 3-4, an inclined connecting edge 11 is provided at the lower outer edge of the bin cover 1. The connecting edge 11 is integrally formed with the bin cover 1, and the upper outer edge of the bin body 2 adopts an inclined surface structure that matches the connecting edge 11. When the bin cover 1 and the bin body 2 are butted up and down, the connecting edge 11 is buckled on the inclined surface of the bin body 2, which is more convenient for butting and fastening compared with the traditional vertical connecting surface.
[0027] Furthermore, a sealing gasket 12 is inlaid on the inclined inner wall of the connecting edge 11, and the sealing gasket 12 is in close fit with the inclined surface of the bin body 2, so as to improve the sealing performance of the connecting edge.
[0028] Please refer to Figures 1-3 , a connecting groove 21 is provided on the bin body 2 corresponding to each connecting cylinder 4, and the nut 5 does not protrude from the connecting groove 21 when tightened, so as to facilitate the storage of the connecting cylinder 4 in the connecting groove 21 and prevent the connecting cylinder 4 from being collided during the use of the drone.
[0029] For those skilled in the art, it is obvious that the present utility model is not limited to the details of the above exemplary embodiments, and the present utility model can be implemented in other specific forms without departing from the spirit or basic characteristics of the present utility model. Therefore, from any point of view, the embodiments should be regarded as exemplary and non-restrictive. The scope of the present utility model is defined by the appended claims rather than the above description. Therefore, all changes falling within the meaning and scope of the equivalent elements of the claims are intended to be included in the present utility model. Any reference signs in the claims should not be regarded as limiting the claimed rights.
[0030] In addition, it should be understood that although this specification is described according to the embodiments, not every embodiment only contains an independent technical solution. This narrative way of the specification is only for clarity. Those skilled in the art should regard the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.
Claims
1. A guiding mechanism for plastic parts of a drone main body, comprising a warehouse cover (1), a warehouse body (2), a guide rod (3) and a connecting cylinder (4), characterized in that: The guide rods (3) are connected to the lower edge of the bin cover (1), and several guide rods (3) are evenly distributed along the outer edge of the bin cover (1). The connecting cylinders (4) are connected to the lower edge of the bin body (2), and the connecting cylinders (4) correspond to the guide rods (3) one by one. When the bin cover (1) and the bin body (2) are fastened, the guide rods (3) penetrate through the connecting cylinders (4), and nuts (5) are screwed onto the external threads of the connecting cylinders (4). A number of inclined shrinking pieces (41) are arranged circumferentially at the lower end of the connecting cylinder (4), and a telescopic gap (42) that is narrow at the top and wide at the bottom is formed between adjacent shrinking pieces (41). When the nut (5) is tightened, the shrinking piece (41) closely adheres to the guide rod (3).
2. The guiding mechanism for the plastic parts of the UAV mainframe according to claim 1, characterized in that: An inclined connecting edge (11) is provided at the outer lower edge of the bin cover (1), and the outer upper edge of the bin body (2) adopts an inclined surface structure that matches the connecting edge (11).
3. The guiding mechanism for the plastic parts of the UAV mainframe according to claim 2, wherein: A sealing gasket (12) is embedded on the inclined inner wall of the connecting edge (11), and the sealing gasket (12) is in close fit with the inclined surface of the bin body (2).
4. A guiding mechanism for a plastic part of an unmanned aerial vehicle mainframe according to claim 1, characterized in that: A connecting groove (21) is provided on the bin body (2) corresponding to each connecting cylinder (4), and when the nut (5) is tightened, it does not protrude from the connecting groove (21).
5. The guiding mechanism for the plastic parts of the UAV mainframe according to claim 1, characterized in that: The lower end of the guide rod (3) is chamfered to form a conical structure.
6. The guiding mechanism for the plastic parts of the UAV mainframe according to claim 1, characterized in that: A ring groove (31) is provided on the outer side wall of the guide rod (3), and a matching protrusion (411) is provided on the shrinking piece (41) corresponding to the ring groove (31).
7. The guiding mechanism for the plastic parts of the UAV main body according to claim 1, characterized in that: A guiding body (51) that is thin at the top and thick at the bottom is provided inside the nut (5). When the nut (5) is tightened, the guiding body (51) is in close fit with the shrinking piece (41).