CN109732515B

CN109732515B - Horizontal installation debugging device of unmanned aerial vehicle driving system

Info

Publication number: CN109732515B
Application number: CN201910071643.8A
Authority: CN
Inventors: 吴清槐; 韩叙
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-01-25
Filing date: 2019-01-25
Publication date: 2020-08-28
Anticipated expiration: 2039-01-25
Also published as: CN109732515A

Abstract

The invention discloses a horizontal mounting and debugging device of an unmanned aerial vehicle power system, which comprises an assembly table, an assembly rail, a second rail and a telescopic foot support, wherein a bearing bracket is arranged above the assembly table, a bearing rod is arranged on the bearing bracket, the inner side of the first adjusting ring is connected with a second adjusting ring, the first rail is arranged above the second adjusting ring, a first connecting groove is formed in the first rail, the telescopic foot support is positioned below the assembly table, a mounting seat is connected to the telescopic foot support, and the telescopic foot support is mutually connected with the assembly table through the mounting seat. This horizontal installation debugging device of unmanned aerial vehicle driving system, the convenience carries out the horizontal stabilization centre gripping to the power motor that needs the assembly to the convenience assembles the motor, avoids the motor to appear the condition of slope and angle migration in the assembling process, has improved the stability of motor assembly and has improved the stability of unmanned aerial vehicle flight.

Description

Horizontal installation debugging device of unmanned aerial vehicle driving system

Technical Field

The invention relates to the technical field of unmanned aerial vehicles, in particular to a horizontal installation and debugging device for an unmanned aerial vehicle power system.

Background

Unmanned aerial vehicle is a small-size flying machine, it is multi-purpose to carry out the aerial photograph or supplementary agricultural medicine sprays, current unmanned aerial vehicle spare part is mostly carried out manual combination assembly by the workman, inefficiency, the assembly accuracy is not high simultaneously, lead to unmanned aerial vehicle to appear unstable condition in flight in-process easily, especially unmanned aerial vehicle power motor's assembly is especially important, the angle deviation appears in the motor assembly leads to unmanned aerial vehicle can't stabilize in flight in-process and hover or change flight direction, influence normal flight operation, the crash condition can appear if serious, thereby unmanned aerial vehicle's product quality has been reduced, influence unmanned aerial vehicle's normal use.

Disclosure of Invention

The invention aims to provide a horizontal installation and debugging device of an unmanned aerial vehicle power system, which aims to solve the problems that the angle deviation of the motor assembly of the unmanned aerial vehicle in the background technology easily causes that the unmanned aerial vehicle can not stably hover or change the flying direction in the flying process, so that the normal flying operation is influenced, and the crash condition can be caused seriously, so that the product quality of the unmanned aerial vehicle is reduced, and the normal use of the unmanned aerial vehicle is influenced.

In order to achieve the purpose, the invention provides the following technical scheme: a horizontal installation and debugging device of an unmanned aerial vehicle power system comprises an assembly table, an assembly track, a second track and a telescopic foot support, wherein a bearing bracket is installed above the assembly table, a bearing rod is installed on the bearing bracket, a level gauge is installed below the assembly table, a first adjusting ring is arranged above the assembly table, a second adjusting ring is connected to the inner side of the first adjusting ring, a handle rod is fixed on the second adjusting ring, a first track is installed above the second adjusting ring, a first connecting groove is formed in the first track, a first connecting block is arranged on the inner side of the first connecting groove and is connected with the first track through the first connecting groove, the assembly track is located above the first track, a vertical shaft is installed below the assembly track, the assembly track is connected with the first connecting block through the vertical shaft, a second connecting groove is formed in the assembly track, and the assembly clamp is installed to the orbital top of assembly, the below of assembly clamp is provided with the second connecting block, and the assembly clamp passes through second connecting block and second spread groove and assembly track interconnect to be provided with the fastening bolt on the assembly clamp, the second track is located first orbital outside, and installs the montant on the second track, the adjustment tank has been seted up on the montant, and the inboard of adjustment tank installs the regulation pole, install the regulating block on the regulation pole, and it has the connecting hole to reserve on the regulating block, the regulating block passes through the connecting hole and adjusts pole interconnect, and is fixed with clamping device on the regulating block, flexible foot supports the below that is located the assembly bench, and is connected with the mount pad on the flexible foot supports to flexible foot supports through mount pad and assembly bench interconnect.

Preferably, the support bracket is of an annular structure, the support rods are obliquely arranged relative to the support bracket, and the support rods are distributed on the inner side of the support bracket at equal angles.

Preferably, the bearing rod comprises a loop bar, a support rod, a reset spring and a foot pad, the inner side of the loop bar is provided with the support rod and the reset spring respectively, the reset spring is installed on the support rod, the support rod is connected with the loop bar through the reset spring, and the foot pad is installed on the support rod.

Preferably, the bracing piece passes through reset spring and loop bar constitution extending structure, and bracing piece and callus on the sole constitution revolution mechanic to the callus on the sole is the rubber material.

Preferably, the inner side of the first adjusting ring is provided with threads, the first adjusting ring is nested on the outer side of the second adjusting ring, and the second adjusting ring is fixedly connected with the first track.

Preferably, the first track and the second track are both of an annular structure, and the first track and the second track respectively form a sliding structure with the first connecting block and the vertical rod.

Preferably, the number of the assembling tracks is 6, the assembling tracks and the first connecting block form a rotating structure through vertical shafts, and the connecting structure between the assembling tracks and the assembling clamps is the same as the connecting structure between the second tracks and the vertical shafts.

Preferably, the adjusting rod is in threaded connection with the adjusting block, the adjusting block and the vertical rod form a sliding structure, and the adjusting rod and the vertical rod form a rotating structure.

Compared with the prior art, the invention has the beneficial effects that: the unmanned aerial vehicle power system is horizontally provided with a debugging device,

1. the power motor to be assembled can be horizontally and stably clamped conveniently, so that the motor can be assembled conveniently, the conditions of inclination and angle deviation of the motor in the assembling process are avoided, the assembling stability of the motor is improved, and the flying stability of the unmanned aerial vehicle is improved;

2. the assembly rail can slide on the first rail, so that an assembler can adjust the assembly rail conveniently according to the requirements of a four-wing unmanned aerial vehicle or a six-wing unmanned aerial vehicle, stable assembly of two types of unmanned aerial vehicles is facilitated, and the adaptability of different types of unmanned aerial vehicles is improved;

3. the glass cover is filled with moisture, and convenience of customers observes according to water flat line and judges whether sleeve internal fixation motor is located horizontal position, and then convenience of customers passes through the angle of the motor in sleeve and the support adjustment sleeve, is favorable to the motor to be in horizontal position and assembles, avoids appearing the condition of angular deflection.

Drawings

FIG. 1 is a schematic view of an overall front cross-sectional structure of the present invention;

FIG. 2 is a schematic view of the mounting rail mounting structure of the present invention;

FIG. 3 is a schematic view of a support bar according to the present invention;

FIG. 4 is a schematic view of the support bar mounting structure of the present invention;

FIG. 5 is a schematic view of the adjusting block mounting structure of the present invention;

FIG. 6 is a schematic view of a first tuning ring configuration of the present invention;

fig. 7 is an enlarged schematic view of the invention at a in fig. 1.

In the figure: 1. an assembly table; 2. a support bracket; 3. a support rod; 301. a loop bar; 302. a support bar; 303. a return spring; 304. a foot pad; 4. a level gauge; 5. a first adjusting ring; 6. a second adjusting ring; 7. a handle bar; 8. a first track; 9. a first connecting groove; 10. a first connection block; 11. a vertical axis; 12. assembling a track; 13. a second connecting groove; 14. assembling the clamp; 15. a second connecting block; 16. fastening bolts; 17. a second track; 18. a vertical rod; 19. an adjustment groove; 20. adjusting a rod; 21. an adjusting block; 22. connecting holes; 23. a clamping device; 24. the telescopic leg support; 25. and (7) mounting a seat.

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.

Referring to fig. 1-7, the present invention provides a technical solution: a horizontal installation and debugging device of an unmanned aerial vehicle power system comprises an assembly table 1, an assembly rail 12, a second rail 17 and a telescopic foot support 24, wherein a bearing bracket 2 is installed above the assembly table 1, a bearing rod 3 is installed on the bearing bracket 2, the bearing bracket 2 is of an annular structure, the bearing rod 3 is obliquely arranged relative to the bearing bracket 2, the bearing rod 3 is distributed at equal angles on the inner side of the bearing bracket 2, and is convenient for carrying out adaptive laminating support on an unmanned aerial vehicle main body, the bearing rod 3 comprises a sleeve rod 301, a support rod 302, a reset spring 303 and a foot pad 304, the inner side of the sleeve rod 301 is respectively provided with the support rod 302 and the reset spring 303, the support rod 302 is provided with the reset spring 303, the support rod 302 forms a telescopic structure with the sleeve rod 301 through the reset spring 303, the support rod 302 and the foot pad 304 form a rotary structure, and the foot pad 304 is made of rubber, the support rod 302 is convenient for driving the foot, the bottom shape of the unmanned aerial vehicle can be adapted conveniently, the supporting rod 302 is connected with the loop bar 301 through the reset spring 303, the foot pad 304 is mounted on the supporting rod 302, the flexible movement of the supporting rod 3 is facilitated, the level 4 is mounted below the assembly table 1, the first adjusting ring 5 is arranged above the assembly table 1, threads are arranged on the inner side of the first adjusting ring 5, the first adjusting ring 5 is nested on the outer side of the second adjusting ring 6, the second adjusting ring 6 is fixedly connected with the first rail 8, and the height of the second adjusting ring 6 on the first adjusting ring 5 can be adjusted spirally;

the inner side of the first adjusting ring 5 is connected with a second adjusting ring 6, a handle bar 7 is fixed on the second adjusting ring 6, a first track 8 is installed above the second adjusting ring 6, a first connecting groove 9 is formed in the first track 8, the first track 8 and a second track 17 are both of an annular structure, the first track 8 and the second track 17 respectively form a sliding structure with a first connecting block 10 and a vertical bar 18, so that sliding displacement adjustment can be conveniently carried out on the corresponding assembling track 12 and the vertical bar 18, the inner side of the first connecting groove 9 is provided with the first connecting block 10, the first connecting block 10 is connected with the first track 8 through the first connecting groove 9, the assembling track 12 is positioned above the first track 8, a vertical shaft 11 is installed below the assembling track 12, the assembling track 12 is connected with the first connecting block 10 through the vertical shaft 11, the number of the assembling tracks 12 is 6, the assembly rail 12 and the first connecting block 10 form a rotating structure through the vertical shaft 11, the connecting structure between the assembly rail 12 and the assembly clamp 14 is the same as the connecting structure between the second rail 17 and the vertical shaft 18, angle adjustment and displacement adjustment of an unmanned aerial vehicle arm fixed on the assembly clamp 14 are facilitated, the second connecting groove 13 is formed in the assembly rail 12, and the assembly clamp 14 is installed above the assembly rail 12;

a second connecting block 15 is arranged below the assembling clamp 14, the assembling clamp 14 is connected with the assembling track 12 through the second connecting block 15 and a second connecting groove 13, a fastening bolt 16 is arranged on the assembling clamp 14, the second track 17 is positioned on the outer side of the first track 8, a vertical rod 18 is arranged on the second track 17, an adjusting groove 19 is arranged on the vertical rod 18, an adjusting rod 20 is arranged on the inner side of the adjusting groove 19, the adjusting rod 20 is in threaded connection with an adjusting block 21, the adjusting block 21 and the vertical rod 18 form a sliding structure, the adjusting rod 20 and the vertical rod 18 form a rotating structure, the adjusting rod 20 is convenient for driving the adjusting block 21 to slide and adjust the vertical position on the vertical rod 18, the adjusting rod 20 is provided with an adjusting block 21, a connecting hole 22 is reserved on the adjusting block 21, the adjusting block 21 is connected with the adjusting rod 20 through the connecting hole 22, and a clamping device 23 is fixed on the adjusting block 21, the telescopic foot supports 24 are located below the assembly table 1, mounting seats 25 are connected to the telescopic foot supports 24, and the telescopic foot supports 24 are connected with the assembly table 1 through the mounting seats 25.

The working principle is as follows: according to the structure shown in fig. 1, the position of the assembly table 1 is adjusted through the telescopic foot supports 24 firstly until the level gauge 4 on the assembly table 1 is in a horizontal position, at the moment, the unmanned aerial vehicle main body is placed on the supporting rod 3 on the inner side of the supporting bracket 2, the supporting rod 302 on the supporting rod 3 is extruded by the unmanned aerial vehicle main body, the extruded supporting rod 302 is subjected to self-adaptive telescopic adjustment on the inner side of the loop bar 301 through the reset spring 303, so that the supporting rod 302 drives the foot pad 304 to attach and support the unmanned aerial vehicle main body, the stability of supporting the unmanned aerial vehicle main body is improved, and the unmanned aerial vehicle main body can be adapted to unmanned;

according to the drawings of fig. 1-7, after the main body of the unmanned aerial vehicle is supported and placed, the arm of the unmanned aerial vehicle is placed on the assembly clamp 14, the fastening bolt 16 on the assembly clamp 14 is used for stably clamping the arm of the unmanned aerial vehicle, so that the arm of the unmanned aerial vehicle is clamped and fixed, then the motor base of the unmanned aerial vehicle is installed on the clamping device 23, and the clamping device 23 at the moment drives the motor base of the unmanned aerial vehicle to maintain a horizontal position, so that the motor of the unmanned aerial vehicle is convenient to install;

as shown in fig. 1-7, after the placement of the drone motor base and drone motor in a horizontal position is completed, the adjusting rod 20 is manually rotated, at this time, the adjusting rod 20 drives the adjusting block 21 to slide and displace in the adjusting groove 19 on the vertical rod 18 through the connecting hole 22 until the adjusting block 21 drives the motor of the unmanned aerial vehicle to adjust to a proper height through the clamping device 23, then the vertical rod 18 is adjusted in a sliding way through the second track 17 until the vertical rod 18 drives the motor of the unmanned aerial vehicle to slide and shift to a position corresponding to the arm of the unmanned aerial vehicle through the clamping device 23, then the height of the motor of the unmanned aerial vehicle is continuously adjusted through the adjusting rod 20 until the motor of the unmanned aerial vehicle is conveniently assembled on the arm of the unmanned aerial vehicle, after the unmanned aerial vehicle motor is assembled on the arm of the unmanned aerial vehicle, unscrewing the clamping device 23, and then evacuating the clamping device 23 from the unmanned aerial vehicle motor and the base;

according to fig. 1-7, after the motor of the unmanned aerial vehicle is assembled, the assembly clamp 14 is manually pushed to slide on the assembly track 12 through the second connecting block 15 until the assembly clamp 14 slides to be close to the main body of the unmanned aerial vehicle on the support bracket 2 with the arm of the unmanned aerial vehicle, and at the same time, the vertical shaft 11 can perform angular rotation adjustment on the assembly clamp 14 and the arm of the unmanned aerial vehicle, and the assembly clamp 14 can perform position adjustment on the first track 8 through the first connecting block 10 and the first connecting groove 9, and the user can also perform rotation adjustment on the height of the second adjusting ring 6 on the inner side of the first adjusting ring 5 by driving the second adjusting ring 6 through the lever 7, so as to conveniently drive the arm of the unmanned aerial vehicle in the assembly clamp 14 to adjust the height until the corresponding mounting positions of the arm of the unmanned aerial vehicle and the main body of the unmanned aerial vehicle are performed, thereby facilitating the accurate installation, the condition of assembly error is avoided, and the horizontal installation and debugging device of the unmanned aerial vehicle power system is convenient for users to use.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle driving system horizontal installation debugging device, includes assembly bench (1), assembly track (12), second track (17) and flexible foot support (24), its characterized in that: a bearing bracket (2) is installed above the assembly table (1), a bearing rod (3) is installed on the bearing bracket (2), a level gauge (4) is installed below the assembly table (1), a first adjusting ring (5) is arranged above the assembly table (1), a second adjusting ring (6) is connected to the inner side of the first adjusting ring (5), a handle rod (7) is fixed on the second adjusting ring (6), a first rail (8) is installed above the second adjusting ring (6), a first connecting groove (9) is formed in the first rail (8), a first connecting block (10) is arranged on the inner side of the first connecting groove (9), the first connecting block (10) is connected with the first rail (8) through the first connecting groove (9), the assembly rail (12) is located above the first rail (8), and a vertical shaft (11) is installed below the assembly rail (12), and the assembly track (12) is connected with the first connecting block (10) through a vertical shaft (11), a second connecting groove (13) is arranged on the assembly track (12), an assembly clamp (14) is installed above the assembly track (12), a second connecting block (15) is arranged below the assembly clamp (14), the assembly clamp (14) is connected with the assembly track (12) through the second connecting block (15) and the second connecting groove (13), a fastening bolt (16) is arranged on the assembly clamp (14), the second track (17) is positioned at the outer side of the first track (8), a vertical rod (18) is installed on the second track (17), an adjusting groove (19) is formed in the vertical rod (18), an adjusting rod (20) is installed on the inner side of the adjusting groove (19), an adjusting block (21) is installed on the adjusting rod (20), and a connecting hole (22) is reserved on the adjusting block (21), adjusting block (21) are through connecting hole (22) and regulation pole (20) interconnect, and are fixed with clamping device (23) on adjusting block (21), flexible foot supports (24) and is located the below of mount table (1), and is connected with mount pad (25) on flexible foot supports (24) to flexible foot supports (24) are through mount pad (25) and mount table (1) interconnect.

2. The horizontal installation and debugging device of the unmanned aerial vehicle power system of claim 1, characterized in that: the supporting bracket (2) is of an annular structure, the supporting rods (3) are obliquely arranged relative to the supporting bracket (2), and the supporting rods (3) are distributed on the inner side of the supporting bracket (2) at equal angles.

3. The horizontal installation and debugging device of the unmanned aerial vehicle power system of claim 1, characterized in that: the bearing rod (3) comprises a sleeve rod (301), a supporting rod (302), a reset spring (303) and a foot pad (304), the inner side of the sleeve rod (301) is provided with the supporting rod (302) and the reset spring (303) respectively, the reset spring (303) is installed on the supporting rod (302), the supporting rod (302) is connected with the sleeve rod (301) through the reset spring (303), and the foot pad (304) is installed on the supporting rod (302).

4. The horizontal installation and debugging device of the unmanned aerial vehicle power system of claim 3, characterized in that: the support rod (302) and the sleeve rod (301) form a telescopic structure through a return spring (303), the support rod (302) and the foot pad (304) form a rotating structure, and the foot pad (304) is made of rubber.

5. The horizontal installation and debugging device of the unmanned aerial vehicle power system of claim 1, characterized in that: the inner side of the first adjusting ring (5) is provided with threads, the first adjusting ring (5) is nested on the outer side of the second adjusting ring (6), and the second adjusting ring (6) is fixedly connected with the first track (8).

6. The horizontal installation and debugging device of the unmanned aerial vehicle power system of claim 1, characterized in that: the first track (8) and the second track (17) are both of an annular structure, and the first track (8) and the second track (17) respectively form a sliding structure with the first connecting block (10) and the vertical rod (18).

7. The horizontal installation and debugging device of the unmanned aerial vehicle power system of claim 1, characterized in that: the number of the assembly tracks (12) is 6, the assembly tracks (12) form a rotating structure with the first connecting block (10) through the vertical shafts (11), and the connecting structure between the assembly tracks (12) and the assembly clamps (14) is the same as that between the second tracks (17) and the vertical rods (18).

8. The horizontal installation and debugging device of the unmanned aerial vehicle power system of claim 1, characterized in that: the adjusting rod (20) is in threaded connection with the adjusting block (21), the adjusting block (21) and the vertical rod (18) form a sliding structure, and the adjusting rod (20) and the vertical rod (18) form a rotating structure.