Detachable transparent structure unmanned aerial vehicle for unmanned aerial vehicle teaching

Abstract

The utility model discloses a detachable transparent structure unmanned aerial vehicle for unmanned aerial vehicle teaching, which comprises an unmanned aerial vehicle shell and a shell cover, the shell cover is arranged on the opening end face of the unmanned aerial vehicle shell, a plurality of positioning holes are formed in the shell cover, positioning columns are arranged in the positioning holes, one end of each positioning column is installed on the inner wall face of the unmanned aerial vehicle shell, and the other end of each positioning column is installed on the outer wall face of the unmanned aerial vehicle shell. And a plurality of main plates are arranged in the unmanned aerial vehicle shell, grooves are formed in the two ends of each main plate, positioning seats are arranged in the grooves, arc-shaped grooves are formed in the opposite end faces of the positioning seats, and the positioning columns are sleeved with the arc-shaped grooves. The unmanned aerial vehicle shell is simple in structure, the installation structure of the main boards in the unmanned aerial vehicle shell can be seen clearly through the shell cover, the shell cover can be lifted and detached, after blocking of the shell cover is lost, the multiple main boards can be lifted one by one, the situation of each main board can be further known, and adaptability is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to an unmanned plane technical field, concretely relates to a detachable transparent structure unmanned plane for unmanned plane teaching. BACKGROUND

[0002] An unmanned plane is an aircraft that can fly without carrying people, and in recent years, with the promotion of technological development and application scene expansion, it has gradually become a field that attracts much attention.

[0003] Therefore, many teaching projects have appeared for unmanned planes, but there is a lack of unmanned planes for teaching, it is not possible to see the structure inside the unmanned plane, and the distribution and installation of the mainboard inside the unmanned plane are not clear, which affects the quality of teaching. SUMMARY

[0004] The utility model wants to solve the technical problem to provide a detachable transparent structure unmanned plane for unmanned plane teaching, can see the inside through the shell cover, and after the shell cover is opened, the mainboard can be lifted and inclined, and the structure and distribution of the mainboard are further seen, to solve the problem proposed in the above background technology.

[0005] The utility model is realized through the following technical scheme: a detachable transparent structure unmanned plane for unmanned plane teaching, including unmanned plane shell and shell cover, the shell cover is arranged on the opening end face of the unmanned plane shell, a plurality of positioning holes are arranged on the shell cover, positioning columns are arranged in the positioning holes, one end of the positioning column is installed on the inner wall surface of the unmanned plane shell, the other end is arranged in the outside, a plurality of mainboards are arranged in the inside of the unmanned plane shell, recesses are arranged at both ends of the mainboard, positioning seats are arranged in the recesses, arc grooves are arranged on the opposite end surfaces of the positioning seat, and the arc grooves are arranged outside the positioning column.

[0006] As a preferred technical scheme, bearings are embedded and installed on the inner wall surfaces of the recesses, shaft rods are installed in the inner rings of the bearings, the other ends of the shaft rods are installed in the positioning seats, clamping grooves with hemispherical structures are arranged on the two sides of the positioning seat, mounting grooves are arranged at the positions opposite to the clamping grooves on the two side surfaces of the recess, balls are arranged in the openings of the mounting grooves, part of the balls extends to the outside and is inserted into the clamping groove, the other part of the balls is provided with a first compression spring, and the other end of the first compression spring is installed on the inner wall surface of the mounting groove.

[0007] As a preferred technical scheme, assembly grooves with arc structures are arranged on the side surfaces of the positioning columns, friction plates with arc structures are installed in the assembly grooves, the outer ring surfaces of the friction plates are flush with the outer ring surfaces of the positioning columns, the inner wall surfaces of the arc grooves are frictionally positioned with the outer wall surfaces of the friction plates, rectangular openings are arranged on the friction plates close to the shell cover, retreat grooves are arranged at the positions opposite to the rectangular openings in the assembly grooves, and limiting plates for pressing the shell cover on the unmanned plane shell are arranged in the retreat grooves.

[0008] As a preferred technical scheme, one end of the limiting plate extends to the outside through the rectangular opening and is in contact with the outer side of the shell cover, and the other end of the limiting plate is provided with a second compression spring, and the other end of the second compression spring is installed on the inner wall surface of the retreat groove.

[0009] As a preferred technical scheme, the shell cover is made of transparent plastic material.

[0010] As a preferred technical scheme, the space for rotating the main board is formed between the groove and the positioning seat.

[0011] As a preferred technical scheme, the friction plate is made of metal material.

[0012] The utility model discloses the beneficial effect is: the utility model discloses simple structure can see the installation structure of the main board in the unmanned aerial vehicle shell body through the shell cover, and the shell cover can lift and disassemble, after losing the block of shell cover, a plurality of main boards can lift and condition one by one, further understand the condition of each main board, increase adaptability. DRAWINGS

[0013] In order to more clearly illustrate the technical scheme in the embodiment of the utility model or prior art, the following will be briefly introduced the drawing needed to be used in the embodiment or prior art description, obviously, the drawing in the following description only some embodiments of the utility model, for those skilled in the art, under the premise of not paying creative labor, still can obtain other drawings according to these drawings.

[0014] Figure 1 It is the whole structure schematic diagram of the utility model;

[0015] Figure 2 It is the structure schematic diagram of the utility model after removing the shell cover;

[0016] Figure 3 It is the structure schematic diagram of the main board of the utility model;

[0017] Figure 4 It is the structure schematic diagram of the main board of the utility model after lifting and condition.

[0018] Among them, 1, unmanned aerial vehicle shell;2, shell cover;3, positioning column;4, friction plate;5, limiting plate;6, main board;7, positioning seat;8, arc slot;9, shaft;10, ball;11, clamping groove. DETAILED DESCRIPTION

[0019] Embodiments of the present application will be described in detail below, examples of which are shown in the drawings, wherein the same or similar reference signs represent the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by reference to the drawings are exemplary and are intended to explain the present application only, and should not be understood as limiting the present application.

[0020] All features disclosed in this specification, or all steps of any methods or processes disclosed, may be combined in any combination, except combinations where at least some of such features and / or steps are mutually exclusive.

[0021] Any feature disclosed in this specification, unless stated otherwise, can be replaced by alternative features or equivalents having the same or a similar effect. That is, unless stated otherwise, each feature is one example only of a number of alternative or comparable features.

[0022] As shown in Figure 1 , Figure 2 and Figure 3 , the utility model discloses a detachable transparent structure unmanned plane for unmanned plane teaching, including unmanned plane shell 1 and shell cover 2, the shell cover 2 sets up on the open end surface of unmanned plane shell 1, be equipped with a plurality of positioning hole on shell cover 2, be equipped with positioning column 3 in positioning hole, and one end of positioning column 3 is installed on the inner wall surface of unmanned plane shell 1, and the other end is set to outside, and the inside of unmanned plane shell 1 is equipped with a plurality of mainboards 6, and both ends of mainboard 6 are equipped with recess, and recess is equipped with positioning seat 7, and the opposite end surface of positioning seat 7 is equipped with arc slot 8, and arc slot 8 is all set up in the outside of positioning column 3.

[0023] In this embodiment, the inner wall surface of the recess is embedded with a bearing, the inner ring of the bearing is installed with a shaft rod 9, the other end of the shaft rod 9 is installed in the positioning seat 7, the two sides of the positioning seat 7 are provided with a clamping groove 11 of hemispherical structure, the two side surfaces of the recess are provided with a mounting groove opposite to the clamping groove 11, the opening of the mounting groove is provided with a ball 10, part of the ball 10 extends to the outside and is inserted into the clamping groove 11, the other part is installed with a first compression spring, and the other end of the first compression spring is installed on the inner wall surface of the mounting groove.

[0024] In this embodiment, the side surface of the positioning column 3 is provided with an arc-shaped assembly groove, the arc-shaped assembly groove is installed with an arc-shaped friction plate 4, the outer ring surface of the friction plate 4 is flush with the outer ring surface of the positioning column 3, the inner wall surface of the arc-shaped slot 8 is frictionally positioned with the outer wall surface of the friction plate 4, the friction plate 4 is provided with a rectangular port near the shell cover 2, the assembly groove is provided with a retreat groove opposite to the rectangular port, and the retreat groove is provided with a limiting plate 5 for pressing the shell cover 2 on the unmanned plane shell 1.

[0025] In the embodiment, one end of the limiting plate 5 extends to the outside through the rectangular opening and is in contact with the outer side of the shell cover 2, and the other end of the limiting plate 5 is provided with a second compression spring, and the other end of the second compression spring is installed on the inner wall surface of the retreat groove. The second compression spring can push the limiting plate outward, so that the limiting plate can abut against the outer side of the shell cover, thereby positioning the shell cover.

[0026] In the embodiment, the shell cover 2 is made of transparent plastic material, so that the inside can be seen through the shell cover, and teaching can be better performed.

[0027] In the embodiment, the space for the rotation of the main plate 6 is formed between the groove and the positioning seat 7, so that the main plate can rotate smoothly around the shaft rod, and being stuck is avoided.

[0028] In the embodiment, the friction plate 4 is made of metal material, which increases the firmness, and the outer side of the friction plate is provided with friction lines, so that the main plate can be positioned by friction after the positioning seat moves along the friction plate.

[0029] When watching, the distribution of the inside of the unmanned aerial vehicle shell can be seen through the shell cover, and in the subsequent teaching process, the limiting plate can be squeezed into the retreat groove, and after losing the block of the limiting plate, the shell cover can move upward along the positioning column, so that the opening of the unmanned aerial vehicle shell is in an open state.

[0030] As shown in the accompanying drawings, Figure 4 After the above is completed, the main plate can be directly held and pushed upward along the friction plate, and after the upper main plate moves, the lower main plate can be exposed, so that the main plates can be seen more clearly in the teaching process, and the main plate can be rotated around the shaft rod after moving to a certain height. In the process of rotating the main plate, the ball enters the installation groove due to pressure, so that the ball can be smoothly separated from the clamping groove. At this time, the main plate can be smoothly rotated and inclined, so that the condition of the main plate can be more clearly seen, and the adaptability is increased.

[0031] The above is only a specific embodiment of the present application, but the protection scope of the present application is not limited thereto. Any change or replacement without creative labor should be covered in the protection scope of the present application. Therefore, the protection scope of the present application should be limited by the protection scope defined in the claims.

Claims

1. A detachable transparent structure drone for drone teaching, characterized in that: The device includes a drone housing (1) and a cover (2). The cover (2) is located on the open end face of the drone housing (1). The cover (2) has multiple positioning holes, each of which has a positioning post (3). One end of the positioning post (3) is installed on the inner wall of the drone housing (1), and the other end is located outside. The drone housing (1) has multiple main boards (6) inside. Both ends of the main boards (6) have grooves, each of which has a positioning seat (7). The opposite end face of the positioning seat (7) has an arc groove (8), which is fitted around the outside of the positioning post (3).

2. The detachable transparent structure UAV for UAV teaching according to claim 1, characterized in that: Bearings are embedded in the inner wall of the groove, and shafts (9) are installed in the inner rings of the bearings. The other end of the shafts (9) is installed in the positioning seat (7). The positioning seat (7) has a hemispherical slot (11) on both sides. The two sides of the groove are provided with mounting grooves opposite the slots (11). A ball (10) is provided in the opening of the mounting groove. A part of the ball (10) extends to the outside and is inserted into the slot (11). The other part is equipped with a first compression spring. The other end of the first compression spring is installed on the inner wall of the mounting groove.

3. The detachable transparent structure UAV for UAV teaching according to claim 1, characterized in that: The positioning post (3) is provided with an arc-shaped assembly groove on one side. An arc-shaped friction plate (4) is installed in the assembly groove. The outer ring surface of the friction plate (4) is flush with the outer ring surface of the positioning post (3). The inner wall of the arc groove (8) is rubbed and positioned with the outer wall surface of the friction plate (4). The friction plate (4) is provided with a rectangular opening near the shell cover (2). The assembly groove is provided with a back groove opposite the rectangular opening. The back groove is provided with a limiting plate (5) that presses the shell cover (2) onto the UAV shell (1).

4. The detachable transparent structure UAV for UAV teaching according to claim 3, characterized in that: One end of each limiting plate (5) extends through the rectangular opening to the outside and contacts the outer side of the shell cover (2). The other end of each limiting plate (5) is equipped with a second compression spring, and the other end of each second compression spring is installed on the inner wall of the back groove.

5. The detachable transparent structure UAV for UAV teaching according to claim 1, characterized in that: The cover (2) is made of transparent plastic material.

6. The detachable transparent structure UAV for UAV teaching according to claim 1, characterized in that: The groove and the positioning seat (7) both form a space for the main board (6) to rotate.

7. The detachable transparent structure UAV for UAV teaching according to claim 3, characterized in that: The friction plates (4) are all made of metal.

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