Mounting structure for steering engine base of unmanned aerial vehicle

Abstract

The utility model discloses an installation structure for a steering engine base of an unmanned aerial vehicle, relates to the field of steering engines of unmanned aerial vehicles, solves the problems that screw type assembly operation of an existing device is tedious, and work efficiency is low, and adopts the following scheme that the installation structure comprises a wing plate and a guide plate with the tail side rotationally arranged on the wing plate in a sleeving mode; the side wall of the wing plate is provided with a machine groove used for containing a steering engine base, a main body of the steering engine base is a motor base, an output shaft of the motor base is a rotating shaft, a guide plate is clamped at the top end of the rotating shaft, and four sets of sleeves distributed in an arrayed mode are fixedly installed on the guide plate. An adjuster is assembled in the guide plate, and a sleeve is also fixedly mounted on the adjuster; according to the mounting structure for the steering engine base of the unmanned aerial vehicle, through the arrangement of the steering engine base and the sleeve on the guide plate, the steering engine base and the sleeve can be conveniently clamped in the clamping groove and the column groove in the sleeve by pressing the pressing column and the clamping block on the bottom side of the steering engine base, threaded assembly is not needed, and it is guaranteed that rotating sleeving is stable while the tedious degree of operation is greatly reduced.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) servo technology, specifically to a mounting structure for a servo mount in a UAV. Background Technology

[0002] Fixed-wing drones fly in the air, and the aerodynamics on the control surfaces are changed by the deflection of the control surfaces through servo motors, thereby controlling the drone's pitch, yaw, roll and other maneuvers during flight, so as to change the drone's flight direction and take off and land.

[0003] A search revealed a patent application with patent number 202121544908.0, which discloses a mounting structure for a servo mount on a drone, comprising a servo mount assembly and a fuselage. The servo mount assembly includes a servo mount, an adapter, and a servo. The main body of the servo mount is cylindrical, with a limiting groove on its upper surface for mounting the servo. The cross-sectional area of ​​the limiting groove is smaller than the area of ​​the upper surface. A mounting portion is located at the bottom of the limiting groove. The servo mount is fixedly connected to the servo via the adapter at the mounting portion. The servo mount is in surface contact with the fuselage. This mounting structure, by providing a servo mount, allows the servo to be mounted on the servo mount externally to the fuselage, with no space restrictions. When the servo mount is mounted to the fuselage, the mounting direction is perpendicular to the fuselage, facilitating operation. The surface contact connection between the servo mount and the servo disperses the load borne by the servo to the fuselage, thereby improving the reliability of the servo-driven drone drive structure and enhancing the safety of drone flight.

[0004] The aforementioned application documents can ensure the reliability and safety of the UAV through the configuration of each component, but the servo motors require multiple sets of bolt components to be matched, which is cumbersome and has low overall installation efficiency.

[0005] Therefore, we propose a mounting structure for a servo mount for a UAV. Utility Model Content

[0006] To address the shortcomings of existing technologies, this utility model provides an installation structure for a servo motor mount for unmanned aerial vehicles (UAVs), solving the problems of cumbersome screw-type assembly operations and low work efficiency in existing devices.

[0007] To achieve the above objectives, this utility model is implemented through the following technical solution: a mounting structure for a servo mount for an unmanned aerial vehicle (UAV), comprising a wing plate and a guide plate rotatably mounted thereon on its tail side;

[0008] The side wall of the wing plate is provided with a slot for placing the servo mount. The main body of the servo mount is a motor mount. The output shaft of the motor mount is a rotating shaft. A guide plate is clamped at the top of the rotating shaft. Four sets of sleeves are fixedly installed on the guide plate.

[0009] An adjuster is assembled in the guide plate, and a sleeve is also fixedly installed on the adjuster. A receiving column is rotatably fitted between the guide plate and the sleeve on the adjuster.

[0010] The receiving column is U-shaped, and two sets of pressure columns are fixedly connected to the bottom end of the receiving column. The bottom ends of the two sets of pressure columns are fixedly connected to the locking blocks, and the sleeve is provided with column grooves and locking grooves that are compatible with the specifications of the pressure columns and locking blocks.

[0011] As a preferred embodiment of this utility model, a through groove is provided between the top and bottom of the center of the sleeve, and a retaining groove is provided on the inner side of the sleeve at the bottom of the groove.

[0012] The column groove and the slot are designed to facilitate the pressing of the column bottom end and the locking block into the sleeve, ensuring both rotation and assembly, and guaranteeing stability.

[0013] As a preferred embodiment of this utility model, four sets of symmetrically distributed mounting holes are provided on the side wall of the wing plate, and a mounting clip located outside the mounting hole is fixedly installed on the outer wall of the motor base in the servo mount, and the mounting clip and the mounting hole are assembled together by bolts.

[0014] The mounting holes and mounting clips facilitate the secure mounting of the servo mount on the wingplate, ensuring its installation stability.

[0015] As a preferred embodiment of the present invention, a groove is provided on the side wall of the guide plate, and a through hole is provided on the inner side of the groove to pass through the guide plate.

[0016] The groove design allows the regulator to be easily installed within it, ensuring its stability.

[0017] As a preferred embodiment of this utility model, the regulator includes a pressure plate that is fitted into a groove, and two sets of upper and lower pressure plates are fixedly connected to the right side wall of the pressure plate. The thickness of the pressure plates is half of the groove, and the pressure plates are made of beryllium copper.

[0018] The pressure plate is designed to pass through the perforation during regulator installation, and can be deformed by bending the pressure plate and pressed onto the other side wall of the guide plate to ensure the clamping effect.

[0019] As a preferred embodiment of this utility model, a support plate is fixedly installed on the left side wall of the pressure plate, and a sleeve is fixedly installed on the top of the support plate.

[0020] The support plate is designed to allow for adjustment of the guide plate's rotation angle by pulling the support column with the servo mount, thus achieving the corresponding adjustment effect.

[0021] As a preferred embodiment of this utility model, a rectangular card holder is fixedly connected to the top of the output shaft of the rotating shaft, a rectangular groove adapted to the specifications of the card holder is opened at the bottom of the guide plate, and screw holes are also opened at the top of the guide plate and the card holder.

[0022] The design of the mounting bracket allows the guide plate to be directly snapped onto it in the initial state, ensuring a vertical installation between the guide plate and the wing plate without the need for manual adjustment.

[0023] This utility model provides a mounting structure for a servo motor mount in a drone. It has the following advantages:

[0024] The mounting structure for the servo mount of this UAV, through the sleeve on the servo mount and guide plate, facilitates the clamping of the servo mount into the slot and groove in the sleeve by pressing the pressure column and the locking block on its bottom side, eliminating the need for threaded assembly. This greatly reduces the complexity of operation while ensuring the stability of its rotational assembly. At the same time, the setting of the adjuster also facilitates its insertion into the guide plate, and the adjuster can be clamped onto the guide plate by direct levering, further simplifying the installation operation and solving the problem of cumbersome and inefficient screw-type assembly operation in existing devices. Attached Figure Description

[0025] Figure 1 This is a schematic diagram of the structure of this utility model;

[0026] Figure 2 This is a schematic diagram of the structure of the wing plate of this utility model;

[0027] Figure 3 This is a schematic diagram of the structure of the regulator of this utility model;

[0028] Figure 4 This is a schematic diagram of the servo mount of this utility model;

[0029] Figure 5 This is a structural schematic diagram of the support column of this utility model.

[0030] In the diagram: 1. Wing plate; 11. Engine slot; 12. Mounting hole; 2. Guide plate; 21. Perforation; 22. Disc slot; 3. Servo mount; 31. Motor mount; 32. Mounting clip; 33. Shaft; 34. Clip seat; 4. Adjuster; 41. Pressure plate; 42. Pressure plate; 43. Support plate; 5. Guide plate; 51. Screw hole; 6. Support post; 61. Pressure post; 62. Clip block; 7. Sleeve; 71. Post groove; 72. Clip groove. Detailed Implementation

[0031] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0032] Please see Figure 1-5 This utility model provides a technical solution: an installation structure for a servo mount for a drone, including a wing plate 1 and a guide plate 2 rotatably mounted on its tail side; a slot 11 for placing a servo mount 3 is provided on the side wall of the wing plate 1, the main body of the servo mount 3 is a motor mount 31, the output shaft of the motor mount 31 is a rotating shaft 33, the top of the rotating shaft 33 is fitted with a guide plate 5, and four sets of sleeves 7 are fixedly installed on the guide plate 5; an adjuster 4 is assembled in the guide plate 2, and sleeves 7 are also fixedly installed on the adjuster 4, and a support column 6 is rotatably mounted between the guide plate 5 and the sleeves 7 on the adjuster 4; the support column 6 is U-shaped, and two sets of pressure columns 61 are fixedly connected to the bottom end of the support column 6, and two sets of locking blocks 62 are fixedly connected to the bottom end of the two sets of pressure columns 61; and the sleeves 7 are provided with column grooves 71 and locking grooves 72 that are compatible with the specifications of the pressure columns 61 and locking blocks 62.

[0033] The mounting structure of the servo mount for the UAV, through the setting of the sleeve 7 on the servo mount 3 and the guide plate 5, makes it easy to clamp the servo mount onto the slot 72 and column groove 71 in the sleeve 7 by pressing the pressure column 61 and the locking block 62 on its bottom side, without the need for threaded assembly. This greatly reduces the complexity of operation while ensuring the stability of its rotational assembly. At the same time, the setting of the adjuster 4 also makes it easy to insert into the guide plate 2, and the adjuster 4 can be clamped onto the guide plate 2 by directly turning it, further simplifying the installation operation and solving the problem of cumbersome and inefficient operation of the screw assembly of the existing device.

[0034] Example 2:

[0035] A through groove 71 is provided between the top and center of the sleeve 7, and a slot 72 is provided on the inner side of the sleeve 7 at the bottom of the groove 71. The groove 71 and the slot 72 are provided to facilitate the pressing of the bottom of the column 6, the pressure column 61 and the locking block 62, into the sleeve 7, so as to ensure the rotation effect and the assembly effect at the same time, and ensure stability.

[0036] Four sets of symmetrically distributed mounting holes 12 are provided on the side wall of the wing plate 1. The motor base 31 in the servo mount 3 is fixedly installed with mounting clips 32 located outside the mounting holes 12, and the mounting clips 32 and the mounting holes 12 are assembled together by bolts. The mounting holes 12 and the mounting clips 32 facilitate the fixed installation of the servo mount 3 on the wing plate 1, ensuring its installation stability.

[0037] A groove 22 is provided on the side wall of the guide plate 2, and a through hole 21 is provided on the inner side of the groove 22 to pass through the guide plate 2; wherein, the groove 22 is provided to facilitate the mounting of the adjuster 4 in it, ensuring its stability.

[0038] The regulator 4 includes a pressure plate 41 that is fitted into the groove 22. Two sets of pressure plates 42 are fixedly connected to the right side wall of the pressure plate 41. The thickness of the pressure plate 42 is half that of the groove 22, and the pressure plate 42 is made of beryllium copper. The pressure plate 42 is designed to pass through the through hole 21 when the regulator 4 is installed, and can be deformed by bending the pressure plate 42 and pressed onto the other side wall of the guide plate 2 to ensure the fitting effect.

[0039] A support plate 43 is fixedly installed on the left side wall of the pressure plate 41, and a sleeve 7 is fixedly installed on the top of the support plate 43; wherein, the support plate 43 is set so that the rotation angle of the guide plate 2 can be adjusted by pulling the support column 6 through the servo base 3, so as to achieve the corresponding adjustment effect.

[0040] A rectangular mounting base 34 is fixedly connected to the top of the output shaft of the rotating shaft 33. The bottom of the guide plate 5 is provided with a rectangular groove that matches the specifications of the mounting base 34. The top of the guide plate 5 and the mounting base 34 are also provided with screw holes 51. The mounting base 34 is designed to allow the guide plate 5 to be directly mounted on it in the initial state, ensuring the vertical installation effect between the guide plate 5 and the wing plate 1 without the need for manual adjustment.

[0041] The working principle and usage process of this utility model are as follows: When the device is required to work, the servo mount 3 is fixedly installed on the wing plate 1 by tightening bolts. At the same time, the adjuster 4 is inserted into the guide plate 2, and the pressure plate 42 is deformed and pressed against the side wall of the guide plate 2 by turning it. Finally, the pressure column 61 and the locking block 62 at the bottom of the receiving column 6 are pressed into the column groove 71 and the locking groove 72 in the sleeve 7, ensuring both the locking effect and the rotation effect. The operation is simple and the installation effect is good, which solves the problem that the existing device is difficult to install the wing plate 1 efficiently according to the requirements.

[0042] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. It will be apparent to those skilled in the art that this utility model is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or basic characteristics of this utility model. Therefore, the embodiments should be considered exemplary and non-limiting in all respects. The scope of this utility model is defined by the appended claims rather than the foregoing description, and thus all variations falling within the meaning and scope of equivalents of the claims are intended to be included within this utility model. No reference numerals in the claims should be construed as limiting the scope of the claims.

[0043] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider 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 mounting structure for a servo mount for an unmanned aerial vehicle (UAV), comprising a wing plate (1) and a guide plate (2) rotatably mounted thereon on its tail side. The side wall of the wing plate (1) is provided with a slot (11) for placing the servo mount (3). The main body of the servo mount (3) is a motor mount (31). The output shaft of the motor mount (31) is a rotating shaft (33). A guide plate (5) is clamped at the top of the rotating shaft (33). Four sets of sleeves (7) are fixedly installed on the guide plate (5). An adjuster (4) is assembled in the guide plate (2), and a sleeve (7) is also fixedly installed on the adjuster (4). A support column (6) is rotatably fitted between the guide plate (5) and the sleeve (7) on the adjuster (4). The receiving column (6) is U-shaped. Two sets of pressure columns (61) are fixedly connected to the bottom end of the receiving column (6). The bottom ends of the two sets of pressure columns (61) are fixedly connected to the locking blocks (62). The sleeve (7) is provided with column grooves (71) and locking grooves (72) that are compatible with the specifications of the pressure columns (61) and locking blocks (62).

2. The mounting structure for a servo mount of a UAV according to claim 1, characterized in that: A through groove (71) is provided between the top and the center of the sleeve (7), and a slot (72) is provided on the inner side of the sleeve (7) at the bottom of the groove (71).

3. The mounting structure for a servo mount of a UAV according to claim 1, characterized in that: The wing plate (1) has four sets of symmetrically distributed mounting holes (12) on its side wall. The motor mount (31) in the servo mount (3) is fixedly installed with a mounting clip (32) located outside the mounting holes (12), and the mounting clip (32) and the mounting holes (12) are assembled together by bolts.

4. The mounting structure for a servo mount of a UAV according to claim 1, characterized in that: The guide plate (2) has a groove (22) on its side wall, and a through hole (21) is provided on the inner side of the groove (22) to pass through the guide plate (2).

5. The mounting structure for a servo mount of a UAV according to claim 4, characterized in that: The regulator (4) includes a pressure plate (41) fitted in a groove (22). Two sets of pressure plates (42) are fixedly connected to the right side wall of the pressure plate (41). The thickness of the pressure plate (42) is half that of the groove (22), and the pressure plate (42) is made of beryllium copper.

6. The mounting structure for a servo mount of a UAV according to claim 5, characterized in that: A support plate (43) is fixedly installed on the left side wall of the pressure plate (41), and a sleeve (7) is fixedly installed on the top of the support plate (43).

7. The mounting structure for a servo mount of a UAV according to claim 1, characterized in that: The top of the output shaft of the rotating shaft (33) is fixedly connected to a rectangular card holder (34). The bottom of the guide plate (5) is provided with a rectangular groove that matches the specifications of the card holder (34). The top of the guide plate (5) and the card holder (34) are also provided with screw holes (51).

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