Rotary tool for unmanned aerial vehicle

Abstract

The invention discloses a rotating tool for an unmanned aerial vehicle, and the rotating tool comprises a rack which is provided with a front supporting seat and a rear supporting seat; the supporting roller is rotationally mounted on the supporting seat; each group of clamping rings comprises two clamping rings, the two clamping rings are arranged on the supporting rollers of the two supporting seats respectively, each clamping ring is provided with a lower clamping semi-ring and an upper clamping semi-ring which are detachably connected, and the lower clamping semi-rings and the upper clamping semi-rings are matched with each other to be used for clamping the unmanned aerial vehicle; the clamping tool is used for clamping the clamping ring; the indicating assembly is installed on the rack, matched with the tail end face of the unmanned aerial vehicle and used for positioning the axial position of the unmanned aerial vehicle. According to the rotating tool, axial positioning of the unmanned aerial vehicle can be facilitated by arranging the indicating assembly, so that it is guaranteed that the corresponding position of the unmanned aerial vehicle can be accurately matched with the clamping ring, and the mounting efficiency is effectively improved.

Description

Technical Field

[0001] The present invention relates to the field of unmanned aerial vehicle tooling equipment, and in particular to a rotary tooling for unmanned aerial vehicles. Background Art

[0002] In the process of preparing to perform corresponding tasks, the UAV needs to frequently install or debug various parts of the fuselage. Usually, the UAV is clamped by a rotating fixture. When the UAV cooperates with the rotating fixture, there is a rough clamping area. When the aircraft is hoisted to the rotating fixture, manual positioning or debugging is required to ensure that the fixture of the rotating fixture can clamp the aircraft. This method is difficult to position, requires multiple debugging, and is time-consuming. Summary of the invention

[0003] In view of the above problems, the present invention proposes a rotating tooling for a UAV.

[0004] The technical solution adopted by the present invention is as follows:

[0005] A rotary tooling for a drone, comprising:

[0006] The frame has two support seats spaced apart in front and back, one of the two support seats being a front support seat and the other being a rear support seat;

[0007] A supporting roller is rotatably mounted on the supporting seat, and the outer side wall of the supporting roller has an annular groove;

[0008] At least one group of clamping rings, each group of clamping rings includes two clamping rings, the two clamping rings are respectively arranged on the support rollers of the two support seats, the clamping rings can rotate around their own axes, the clamping rings have a lower clamping half ring and an upper clamping half ring that are detachably connected, the clamping rings are embedded in the annular grooves of the plurality of support rollers, and the lower clamping half ring and the upper clamping half ring cooperate with each other to clamp the drone;

[0009] A clamping tool, mounted on the support seat, is used to clamp the clamping ring so that the clamping ring is fixed relative to the support seat, thereby fixing the UAV relative to the frame;

[0010] The indicating assembly is mounted on the frame and cooperates with the tail end face of the UAV to locate the axial position of the UAV.

[0011] The rotary tooling of the present application can facilitate the axial positioning of the UAV by setting an indicating component, thereby ensuring that the corresponding position of the UAV can accurately cooperate with the clamping ring, effectively improving the installation efficiency.

[0012] In actual use, one operation method is to use the lifting tool to place the drone above the two support seats, and quickly locate the axial position of the drone by cooperating with the indicator component and the tail of the drone. After the positioning is completed, the drone is released, and the lower clamping half rings of the two support seats support the drone (at this time, the clamping tool clamps the lower clamping half ring), and then the upper clamping half ring is installed. The lower clamping half ring and the upper clamping half ring cooperate with each other to clamp the drone. After completion, the drone can be flipped over (release the clamping component before flipping), and after flipping to the specified angle, the clamping tool clamps the clamping ring again.

[0013] In actual use, the drone can be flipped by manually rotating the wings.

[0014] The clamping tool serves to fix the body and prevent the drone from flipping over.

[0015] In one embodiment of the present invention, the indication component includes:

[0016] The base has a limit block, and the rear support seat is located between the front support seat and the limit block;

[0017] A calibration vertical plate, the lower end of which is rotatably mounted on the base, the lower part of the calibration vertical plate facing the rear support seat is used to abut against the limit block, and when the calibration vertical plate abuts against the limit block, the calibration vertical plate is in a vertical state, and the upper part of the calibration vertical plate facing the rear support seat is used to cooperate with the tail end face of the drone to perform axial positioning of the drone;

[0018] An indication circuit is arranged on the base, the indication circuit has a reminder element and a trigger switch, and the calibration vertical plate is located between the limit block and the trigger switch;

[0019] A resetting elastic member, cooperating with the calibration vertical plate, is used to have a rotation tendency to return to a vertical state when the calibration vertical plate is not subjected to external pressure;

[0020] The bending portion is fixed on the side of the calibration vertical plate facing away from the rear support seat, and the lower end of the bending portion is aligned with the trigger switch; when the calibration vertical plate is pressed and rotated toward the side away from the limit block, the bending portion cooperates with the trigger switch to trigger the trigger switch and make the reminder element work.

[0021] Working principle of the indicator component: when the tail end face of the UAV is in vertical contact with one side of the calibration vertical plate, the axial position of the UAV is accurate. During actual operation, the rotating tooling makes the tail end face of the UAV contact with one side of the calibration vertical plate. When the tail position is backward, it will drive the calibration vertical plate to rotate to the side away from the limit block, so that the bending part will trigger the reminder element to remind the operator to move the UAV forward. Through this feedback, quick adjustments can be made to achieve the axial positioning of the UAV.

[0022] It should be noted that, during accurate positioning, the tail end face of the drone is in contact with one side of the calibration vertical plate, and the reminder element is not triggered.

[0023] In actual use, the resetting elastic member can be a torsion spring (arranged on the rotation axis of the calibration vertical plate and the base) or a tension spring, in which case one end of the tension spring is connected to the base and the other end is connected to the calibration vertical plate.

[0024] In actual use, the calibration vertical plate is preferably an elastic plate (which can be deformed when under pressure and can be reset when not under pressure). This arrangement can protect the aircraft and prevent damage to the aircraft structure due to collision with the aircraft.

[0025] In one embodiment of the present invention, the lower end of the bending portion has an elastic pin, and the elastic pin cooperates with the trigger switch.

[0026] The elastic pin can retract when pressed, so as to ensure that the trigger switch can be reliably triggered when the calibration vertical plate rotates.

[0027] In one embodiment of the present invention, the bending portion has a horizontal section and a vertical section, and the elastic pin is disposed at the lower end of the vertical section.

[0028] In one embodiment of the present invention, the reminder element includes at least one of an indicator light and an alarm.

[0029] In one embodiment of the present invention, the clamping tool is a vise or an electric clamp.

[0030] In one embodiment of the present invention, one of the lower clamping half ring and the upper clamping half ring has a slot and a positioning hole connected to the slot, and the other has a plug column for inserting into the slot, the plug column has a through hole, and the clamping ring also includes a positioning pin. When the lower clamping half ring and the upper clamping half ring are plugged into each other, the positioning pin passes through the positioning hole and the through hole to fix the lower clamping half ring and the upper clamping half ring.

[0031] In actual use, preferably, the positioning pin is a quick-release pin, which can achieve rapid disassembly and facilitate rapid removal of the drone from the rotating fixture after debugging is completed.

[0032] In one embodiment of the present invention, the rotary tooling has multiple sets of clamping rings, and different sets of clamping rings cooperate with different drones;

[0033] The front support seat is slidably arranged on the frame, and the front support seat can adjust the front and rear positions;

[0034] The indicating component is slidably arranged on the frame, and the indicating component can adjust the front and rear positions.

[0035] This arrangement enables the rotary fixture to adapt to a variety of different drones (different drones have different support point positions and clamping ring sizes).

[0036] In one embodiment of the present invention, the frame has a first slide rail, the front support seat is slidably disposed on the first slide rail, and the first slide rail has a first scale mark and a first threaded hole;

[0037] The rotating tool also includes a first locking bolt, which is threadedly matched with the first threaded hole. The first locking bolt is used to support the front support seat after the front support seat is adjusted into place, so that the front support seat and the first slide rail are relatively fixed.

[0038] After loosening the first locking bolt, the front support seat can be adjusted forward and backward. The front support seat can be adjusted to a corresponding position through the first scale mark, and then the first locking bolt can be locked.

[0039] In one embodiment of the present invention, it further includes a mounting seat and a second locking bolt, wherein the base is slidably disposed on the mounting seat;

[0040] The base is provided with a second scale mark, and the base is provided with a rack;

[0041] An adjusting gear and an operating handle fixed to the adjusting gear are rotatably mounted on the mounting seat, and the adjusting gear is meshed with the rack;

[0042] The side wall of the mounting seat has a second threaded hole; the second locking bolt is threadedly matched with the second threaded hole, and the second locking bolt is used to support the base after the base is adjusted into place, so that the base and the mounting seat are relatively fixed.

[0043] After loosening the second locking bolt, the position of the base can be adjusted forward and backward by rotating the operating handle, the base can be adjusted to a corresponding position by the second scale mark, and then the second locking bolt can be locked.

[0044] The beneficial effect of the present invention is that the rotary tooling of the present application can facilitate the axial positioning of the UAV by setting the indicating component, thereby ensuring that the corresponding position of the UAV can accurately cooperate with the clamping ring, effectively improving the installation efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0045] Figure 1 is a schematic diagram of a rotary tooling;

[0046] Figure 2 It is a schematic diagram after the lower clamping half ring and the upper clamping half ring are separated;

[0047] Figure 3 This is a schematic diagram of the drone installed on the rotating tooling;

[0048] Figure 4 yes Figure 3 The enlarged view of point A in the middle;

[0049] Figure 5 It is a schematic diagram of the tail of the drone causing the calibration vertical plate to rotate;

[0050] Figure 6 yes Figure 5 The enlarged view of point B in the middle;

[0051] Figure 7 is a schematic diagram of the base and adjustment gear.

[0052] The reference numerals in the figures are:

[0053] 100. UAV; 101. tail; 1. frame; 2a. front support seat; 2b. rear support seat; 21. support roller; 211. annular groove; 22. first slide rail; 221. first scale mark; 222. first threaded hole; 223. first locking bolt; 3. clamping ring; 31. lower clamping half ring; 311. slot; 312. positioning hole; 32. upper clamping half ring; 321. plug post; 322. through hole; 33. fixed Position pin; 4. Clamping tool; 5. Indicator assembly; 51. Base; 511. Limit block; 512. Second scale mark; 513. Rack; 52. Calibration vertical plate; 531. Reminder element; 532. Trigger switch; 54. Bending portion; 541. Horizontal section; 542. Vertical section; 543. Elastic pin; 55. Mounting seat; 551. Adjusting gear; 552. Operating handle; 553. Second threaded hole; 56. Second locking bolt. DETAILED DESCRIPTION

[0054] In order to make the purpose, technical scheme and advantages of the embodiments of the present application clearer, the technical scheme in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, rather than all of the embodiments. The components of the embodiments of the present application described and shown in the drawings here can be arranged and designed in various different configurations.

[0055] In the description of this application, it should be noted that the terms "inside", "outside", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, or the orientation or positional relationship in which the product of the application is usually placed when in use, which is only for the convenience of describing this application and simplifying the description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on this application. In addition, the terms "first", "second", etc. are only used to distinguish the description, and cannot be understood as indicating or implying relative importance.

[0056] In the description of this application, it should also be noted that, unless otherwise clearly specified and limited, the terms "disposed" and "connected" 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 direct connection, or an indirect connection through an intermediate medium, or it can be the internal communication of two elements. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0057] The present invention is described in detail below in conjunction with the accompanying drawings.

[0058] like Figures 1 to 7 As shown, a rotary tooling for a drone, comprising:

[0059] The frame 1 has two support seats spaced apart from each other, one of which is a front support seat 2a and the other is a rear support seat 2b;

[0060] The supporting roller 21 is rotatably mounted on the supporting seat, and the outer side wall of the supporting roller 21 has an annular groove 211;

[0061] At least one group of clamping rings 3, each group of clamping rings 3 includes two clamping rings 3, the two clamping rings 3 are respectively arranged on the supporting rollers 21 of the two supporting seats, the clamping rings 3 can rotate around their own axes, the clamping rings 3 have a lower clamping half ring 31 and an upper clamping half ring 32 that are detachably connected, the clamping rings 3 are embedded in the annular grooves 211 of the plurality of supporting rollers 21, and the lower clamping half ring 31 and the upper clamping half ring 32 cooperate with each other to clamp the drone 100;

[0062] The clamping tool 4 is installed on the support seat and is used to clamp the clamping ring 3 to fix the clamping ring relative to the support seat, thereby fixing the UAV 100 relative to the frame 1;

[0063] The indicating assembly 5 is mounted on the frame 1 and cooperates with the end surface of the tail 101 of the UAV 100 to locate the axial position of the UAV 100 .

[0064] The rotary tooling of the present application can facilitate the axial positioning of the drone 100 by providing the indicating component 5, thereby ensuring that the corresponding position of the drone 100 can accurately cooperate with the clamping ring 3, effectively improving the installation efficiency.

[0065] In actual use, one operation method is to use a lifting tool to place the drone 100 above the two support seats, and quickly locate the axial position of the drone 100 by cooperating with the indicator component 5 and the tail 101 of the drone 100. After the positioning is completed, the drone 100 is released, and the lower clamping half ring 31 of the two support seats supports the drone 100 (at this time, the clamping tool 4 clamps the lower clamping half ring 31), and then the upper clamping half ring 32 is installed. The lower clamping half ring 31 and the upper clamping half ring 32 cooperate with each other to clamp the drone 100. After completion, the drone 100 can be flipped over (release the clamping component before flipping), and after flipping to the specified angle, the clamping frame tool clamps the clamping ring 3 again.

[0066] In actual use, the UAV 100 can be flipped by manually rotating the wings.

[0067] The clamping tool 4 serves to fix the body and prevent the drone 100 from flipping over.

[0068] like Figure 1 , 4 As shown in 5, in this embodiment, the indicating component 5 includes:

[0069] The base 51 has a limit block 511, and the rear support seat 2b is located between the front support seat 2a and the limit block 511;

[0070] The calibration vertical plate 52 has a lower end that is rotatably mounted on the base 51. The lower portion of the calibration vertical plate 52 facing the rear support seat 2b is used to abut against the limit block 511. When the calibration vertical plate 52 abuts against the limit block 511, the calibration vertical plate 52 is in a vertical state. The upper portion of the calibration vertical plate 52 facing the rear support seat 2b is used to cooperate with the end face of the tail 101 of the drone 100 to perform axial positioning of the drone 100.

[0071] The indicating circuit is arranged on the base 51, and the indicating circuit has a reminder element 531 and a trigger switch 532, and the calibration vertical plate 52 is located between the limit block 511 and the trigger switch 532;

[0072] The resetting elastic member (omitted and not shown in the figure) cooperates with the calibration vertical plate 52 and is used to have a rotation tendency to return to a vertical state when the calibration vertical plate 52 is not subjected to external pressure;

[0073] The bending portion 54 is fixed to the side of the calibration vertical plate 52 facing away from the rear support seat 2b, and the lower end of the bending portion 54 is aligned with the trigger switch 532; when the calibration vertical plate 52 is pressed to rotate toward the side away from the limit block 511, the bending portion 54 cooperates with the trigger switch 532 to trigger the trigger switch 532, so that the reminder element 531 works.

[0074] Working principle of the indicating component 5: when the end face of the tail 101 of the UAV 100 is in vertical contact with one side of the calibration vertical plate 52, the axial position of the UAV 100 is accurate. During actual operation, the rotating tooling makes the end face of the tail 101 of the UAV 100 contact with one side of the calibration vertical plate 52. When the tail 101 is positioned backward, it will drive the calibration vertical plate 52 to rotate toward the side away from the limit block 511, so that the bending portion 54 will trigger the reminder element 531 to remind the operator to move the UAV 100 forward. Through this feedback, quick adjustments can be made to achieve the axial positioning of the UAV 100.

[0075] It should be noted that, when accurately positioned, the end surface of the tail portion 101 of the drone 100 is in contact with one surface of the calibration vertical plate 52 , and the reminder element 531 is not triggered to work.

[0076] In actual use, the reset elastic member can be a torsion spring (arranged on the rotation axis of the calibration vertical plate 52 and the base 51), or a tension spring, in which case one end of the tension spring is connected to the base 51 and the other end is connected to the calibration vertical plate 52.

[0077] In actual use, the calibration vertical plate 52 is preferably an elastic plate (which can be deformed when under pressure and can be reset when not under pressure). This arrangement can protect the aircraft and prevent damage to the aircraft structure due to collision with the aircraft.

[0078] like Figure 4 and 6 As shown, in this embodiment, the lower end of the bending portion 54 has an elastic pin 543 , and the elastic pin 543 cooperates with the trigger switch 532 .

[0079] The elastic pin 543 can retract when pressed, ensuring that the trigger switch 532 can be reliably triggered when the calibration vertical plate 52 rotates.

[0080] like Figure 4 As shown, in this embodiment, the bending portion 54 has a horizontal section 541 and a vertical section 542 , and the elastic pin 543 is disposed at the lower end of the vertical section 542 .

[0081] In this embodiment, the reminder element 531 includes at least one of an indicator light and an alarm.

[0082] In this embodiment, the clamping tool 4 is a vise or an electric clamp.

[0083] like Figure 1 and 2As shown, in this embodiment, one of the lower clamping half ring 31 and the upper clamping half ring 32 has a slot 311 and a positioning hole 312 connected to the slot 311, and the other has a plug column 321 for inserting into the slot 311, and the plug column has a through hole 322. The clamping ring 3 also includes a positioning pin 33. When the lower clamping half ring 31 and the upper clamping half ring 32 are plugged into each other, the positioning pin 33 passes through the positioning hole 312 and the through hole 322 to fix the lower clamping half ring 31 and the upper clamping half ring 32.

[0084] In actual use, preferably, the positioning pin 33 is a quick-release pin, which can achieve rapid disassembly and facilitate rapid removal of the drone 100 from the rotating fixture after debugging is completed.

[0085] like Figure 1 As shown, in this embodiment, the rotary tooling has multiple sets of clamping rings 3, and different sets of clamping rings 3 cooperate with different drones 100;

[0086] The front support seat 2a is slidably arranged on the frame 1, and the front support seat 2a can adjust the front and rear positions;

[0087] The indicating assembly 5 is slidably arranged on the frame 1 , and the indicating assembly 5 can adjust the front and rear positions.

[0088] This configuration enables the rotary fixture to adapt to a variety of different drones 100 (different drones 100 have different support point positions and different sizes of the clamping rings 3).

[0089] like Figure 1 As shown, in this embodiment, the frame 1 has a first slide rail 22, the front support seat 2a is slidably disposed on the first slide rail 22, and the first slide rail 22 has a first scale mark 221 and a first threaded hole 222;

[0090] The rotating fixture also includes a first locking bolt 223, which is threadedly matched with the first threaded hole 222. The first locking bolt 223 is used to support the front support seat 2a after the front support seat 2a is adjusted into place, so that the front support seat 2a and the first slide rail 22 are relatively fixed.

[0091] After loosening the first locking bolt 223 , the front support seat 2a can be adjusted forward and backward. The front support seat 2a can be adjusted to a corresponding position through the first scale mark 221 , and then the first locking bolt 223 can be locked.

[0092] like Figure 1 , 4 As shown in FIG. 7 , in this embodiment, a mounting seat 55 and a second locking bolt 56 are further included, and the base 51 is slidably disposed on the mounting seat 55 ;

[0093] The base 51 has a second scale mark 512 and a rack 513;

[0094] An adjusting gear 551 and an operating handle 552 fixed to the adjusting gear 551 are rotatably mounted on the mounting seat 55, and the adjusting gear 551 is meshed with the rack 513;

[0095] The side wall of the mounting seat 55 has a second threaded hole 553 ; the second locking bolt 56 is threadedly engaged with the second threaded hole 553 , and the second locking bolt 56 is used to support the base 51 after the base 51 is adjusted into place, so that the base 51 and the mounting seat 55 are relatively fixed.

[0096] After loosening the second locking bolt 56 , the position of the base 51 can be adjusted forward and backward by rotating the operating handle 552 , and the base 51 can be adjusted to a corresponding position by the second scale mark 512 , and then the second locking bolt 56 can be locked.

[0097] The above description is only a preferred embodiment of the present invention, and does not limit the patent protection scope of the present invention. Any equivalent structural transformation made by using the contents of the present invention and the drawings, directly or indirectly used in other related technical fields, is also included in the protection scope of the present invention.

Claims

1. A rotary tooling for a drone, characterized in that: include: The frame has two support seats spaced apart in front and back, one of the two support seats being a front support seat and the other being a rear support seat; A supporting roller is rotatably mounted on the supporting seat, and the outer side wall of the supporting roller has an annular groove; At least one group of clamping rings, each group of clamping rings includes two clamping rings, the two clamping rings are respectively arranged on the support rollers of the two support seats, the clamping rings can rotate around their own axes, the clamping rings have a lower clamping half ring and an upper clamping half ring that are detachably connected, the clamping rings are embedded in the annular grooves of the plurality of support rollers, and the lower clamping half ring and the upper clamping half ring cooperate with each other to clamp the drone; A clamping tool, mounted on the support seat, is used to clamp the clamping ring so that the clamping ring is fixed relative to the support seat, thereby fixing the UAV relative to the frame; The indicating assembly is mounted on the frame and cooperates with the tail end face of the UAV to locate the axial position of the UAV.

2. The rotary tooling for a drone as claimed in claim 1, characterized in that: The indication component comprises: The base has a limit block, and the rear support seat is located between the front support seat and the limit block; A calibration vertical plate, the lower end of which is rotatably mounted on the base, the lower part of the calibration vertical plate facing the rear support seat is used to abut against the limit block, and when the calibration vertical plate abuts against the limit block, the calibration vertical plate is in a vertical state, and the upper part of the calibration vertical plate facing the rear support seat is used to cooperate with the tail end face of the drone to perform axial positioning of the drone; An indication circuit is arranged on the base, the indication circuit has a reminder element and a trigger switch, and the calibration vertical plate is located between the limit block and the trigger switch; A resetting elastic member, cooperating with the calibration vertical plate, is used to have a rotation tendency to return to a vertical state when the calibration vertical plate is not subjected to external pressure; The bending portion is fixed on the side of the calibration vertical plate facing away from the rear support seat, and the lower end of the bending portion is aligned with the trigger switch; when the calibration vertical plate is pressed and rotated toward the side away from the limit block, the bending portion cooperates with the trigger switch to trigger the trigger switch and make the reminder element work.

3. The rotary tooling for a drone as claimed in claim 2, characterized in that: The lower end of the bending portion is provided with an elastic pin, and the elastic pin cooperates with the trigger switch.

4. The rotary tooling for a drone as claimed in claim 3, characterized in that: The bending portion has a horizontal section and a vertical section, and the elastic pin is arranged at the lower end of the vertical section.

5. The rotary tooling for a drone as claimed in claim 2, characterized in that: The reminder element includes at least one of an indicator light and an alarm.

6. The rotary tooling for a drone as claimed in claim 1, characterized in that: The clamping tool is a vise or an electric clamp.

7. The rotary tooling for a drone as claimed in claim 1, characterized in that: Among the lower clamping half ring and the upper clamping half ring, one has a slot and a positioning hole connected to the slot, and the other has a plug column for inserting into the slot. The plug column has a through hole, and the clamping ring also includes a positioning pin. When the lower clamping half ring and the upper clamping half ring are plugged into each other, the positioning pin passes through the positioning hole and the through hole to fix the lower clamping half ring and the upper clamping half ring.

8. The rotary tooling for a drone as claimed in claim 1, characterized in that: The rotary tooling has multiple sets of clamping rings, and different sets of clamping rings are matched with different drones; The front support seat is slidably arranged on the frame, and the front support seat can adjust the front and rear positions; The indicating component is slidably arranged on the frame, and the indicating component can adjust the front and rear positions.

9. The rotary tooling for a drone as claimed in claim 8, characterized in that: The frame is provided with a first slide rail, the front support seat is slidably arranged on the first slide rail, and the first slide rail is provided with a first scale mark and a first threaded hole; The rotating tool also includes a first locking bolt, which is threadedly matched with the first threaded hole. The first locking bolt is used to support the front support seat after the front support seat is adjusted into place, so that the front support seat and the first slide rail are relatively fixed.

10. The rotary tooling for a drone as claimed in claim 8, characterized in that: It also includes a mounting seat and a second locking bolt, the base being slidably disposed on the mounting seat; The base is provided with a second scale mark, and the base is provided with a rack; An adjusting gear and an operating handle fixed to the adjusting gear are rotatably mounted on the mounting seat, and the adjusting gear is meshed with the rack; The side wall of the mounting seat has a second threaded hole; the second locking bolt is threadedly matched with the second threaded hole, and the second locking bolt is used to support the base after the base is adjusted into place, so that the base and the mounting seat are relatively fixed.

Images