CN214216171U

CN214216171U - Unmanned aerial vehicle frame supporting device for life cycle test of unmanned aerial vehicle

Info

Publication number: CN214216171U
Application number: CN202023183009.0U
Authority: CN
Inventors: 马秋颖
Original assignee: Nanjing Ruizhuohang Aviation Technology Co ltd
Current assignee: Wuxi Yongtuo Zhikong Technology Co ltd
Priority date: 2020-12-25
Filing date: 2020-12-25
Publication date: 2021-09-17
Anticipated expiration: 2030-12-25

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle frame supporting device for unmanned aerial vehicle life cycle test, including supporting the urceolus, the inside of supporting the urceolus is pegged graft and is had the mobile jib, one side of mobile jib is provided with stop gear, the top of mobile jib is bolted to have the bottom plate, the top of bottom plate is bolted to have rolling bearing, the top of rolling bearing is bolted to have the carousel, the both sides that lie in rolling bearing between bottom plate and the carousel are all embedded to have the rolling ball, the top of carousel is bolted to have fixed frame; through having designed convenient to use's carousel, can rotate as required when the test, it is very convenient not only to use, can also improve test effect greatly, reduces and uses the burden, through having designed the arc of being convenient for to fix, can improve the fixed effect to unmanned aerial vehicle greatly, and the fuselage rocks when avoiding testing and causes the damage, has reduced use cost, is worth using widely.

Description

Unmanned aerial vehicle frame supporting device for life cycle test of unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle frame strutting arrangement that is used for unmanned aerial vehicle life cycle test to use.

Background

A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

Need a device to support the unmanned aerial vehicle frame during unmanned aerial vehicle test, unmanned aerial vehicle frame strutting arrangement on the existing market not only can't effectively fix the unmanned aerial vehicle frame when using, the fuselage rocks easily, probably causes unmanned aerial vehicle to take place to damage, and can't carry out the change of angle according to actual test needs during the use, the use burden has been increased, for this reason we have provided an unmanned aerial vehicle frame strutting arrangement that is used for unmanned aerial vehicle life cycle test to solve the problem that the aforesaid exists.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle frame strutting arrangement for unmanned aerial vehicle life cycle test is used, possess the advantage of being convenient for fixed and being convenient for change angle, need a device to support the unmanned aerial vehicle frame when having solved the unmanned aerial vehicle test, unmanned aerial vehicle frame strutting arrangement on the existing market not only can't effectively be fixed to the unmanned aerial vehicle frame when using, the fuselage rocks easily, probably cause unmanned aerial vehicle to take place to damage, and can't carry out the change of angle according to actual test needs when using, the problem of using the burden has been increased.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle frame strutting arrangement for unmanned aerial vehicle life cycle test is with, is including supporting the urceolus, the inside grafting of supporting the urceolus has the mobile jib, one side of mobile jib is provided with stop gear, the top bolt of mobile jib has the bottom plate, the top bolt of bottom plate has rolling bearing, rolling bearing's top bolt has the carousel, the equal embedded rolling ball that has in both sides that just is located rolling bearing between bottom plate and the carousel, the top bolt of carousel has fixed frame, the bottom bolt of fixed frame inner wall has the fixed plate, the equal threaded connection in both sides of fixed plate has the bull stick, the other end of bull stick has the arc through the bearing bolt, the bottom bolt of arc has the slider, the spout has been seted up at the top of fixed plate, and slider and spout looks adaptation.

Preferably, the limiting mechanism comprises a limiting groove, a limiting rod is inserted into the limiting groove, and a reset spring is fixedly sleeved on the outer side of the limiting rod.

Preferably, the bottom of the supporting outer cylinder is bolted with a base, the bottom of the base is bolted with three supports.

Preferably, the outer side of the main rod is fixedly sleeved with a holding cylinder, and the bottom of the holding cylinder is bolted with a baffle.

Preferably, the inner sides of the arc-shaped plates are all bonded with soft pads.

Preferably, the bottoms of all three brackets are bolted with anti-skid balls.

Compared with the prior art, the utility model provides an unmanned aerial vehicle frame strutting arrangement for unmanned aerial vehicle life cycle test is used possesses following beneficial effect:

the turntable convenient to use is designed, so that the turntable can rotate as required during testing, the use is very convenient, the testing effect can be greatly improved, and the use burden is reduced;

through having designed the arc of being convenient for to fix, can improve the fixed effect to unmanned aerial vehicle greatly, the fuselage rocks when avoiding the test and causes the damage, has reduced use cost, is worth using widely.

Drawings

FIG. 1 is a front sectional view of the structure of the present invention;

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

FIG. 3 is an enlarged view of a portion A of FIG. 1 according to the present invention;

fig. 4 is a partially enlarged view of the point B in fig. 1 according to the present invention.

In the figure: 1. supporting the outer cylinder; 2. a main rod; 3. a limiting mechanism; 4. a base plate; 5. a rotating bearing; 6. a turntable; 7. rotating the ball; 8. a fixing frame; 9. a fixing plate; 10. a rotating rod; 11. an arc-shaped plate; 12. a slider; 13. a chute; 14. a limiting groove; 15. a limiting rod; 16. a return spring; 17. a base; 18. a support; 19. a barrel is held; 20. a baffle plate; 21. a soft cushion; 22. an antiskid ball.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Please refer to fig. 1, fig. 2 and fig. 4, an unmanned aerial vehicle frame strutting arrangement for unmanned aerial vehicle life cycle test is used, including supporting urceolus 1, the inside of supporting urceolus 1 is pegged graft there is mobile jib 2, one side of mobile jib 2 is provided with stop gear 3, the top of mobile jib 2 is bolted to have bottom plate 4, the top of bottom plate 4 is bolted to have rolling bearing 5, rolling bearing 5's top is bolted to have carousel 6, it has rolling ball 7 all to inlay in the both sides that just are located rolling bearing 5 between bottom plate 4 and the carousel 6, through having designed convenient to use's carousel 6, can rotate as required when the test, not only it is very convenient to use, can also improve test effect greatly, reduce and use the burden.

Further, stop gear 3 includes spacing groove 14, and the inside grafting of spacing groove 14 has gag lever post 15, and the fixed cover in the outside of gag lever post 15 has connect reset spring 16, through having designed spacing groove 14, gag lever post 15 and reset spring 16, can be convenient for the mobile jib and carry out the regulation of height.

Furthermore, the outer side of the main rod 2 is fixedly sleeved with a holding cylinder 19, the bottom of the holding cylinder 19 is bolted with a baffle 20, and the holding cylinder 19 and the baffle 20 are designed, so that the device can be conveniently held for adjustment.

Please refer to fig. 1, fig. 2 and fig. 3, an unmanned aerial vehicle frame strutting arrangement for unmanned aerial vehicle life cycle test is used, fixed frame 8 has been bolted at the top of carousel 6, fixed plate 9 has been bolted to the bottom of fixed frame 8 inner wall, the equal threaded connection in both sides of fixed plate 9 has bull stick 10, the other end of bull stick 10 has arc 11 through the bearing bolt, the bottom of both sides all is bolted around arc 11 has slider 12, spout 13 has been seted up at the top of fixed plate 9, and

slider

12 and 13 looks adaptations of spout, through having designed the arc 11 of being convenient for to fix, can improve the fixed effect to unmanned aerial vehicle greatly, the fuselage rocks when avoiding the test and causes the damage, use cost is reduced, be worth using widely.

Further, the bottom of the supporting outer cylinder 1 is bolted with a base 17, the bottom of the base 17 is bolted with three supports 18, and the number of the supports 18 is three, so that the stability of the device can be greatly improved.

Further, the inside of arc 11 all bonds and has had cushion 21, through having designed cushion 21, can protect the frame.

Furthermore, the bottoms of the three supports 18 are all bolted with anti-skid balls 22, and the anti-skid balls 22 are designed, so that the friction force can be improved, and the use is safer.

During the use, earlier with device height-adjusting according to the test needs, stimulate the gag lever post 15 to the outside through stop gear 3, can adjust mobile jib 2 in breaking away from the spacing groove 14 until gag lever post 15, adjust the back pine that finishes and open gag lever post 15, can fix once more through reset spring 16's effect, fix the unmanned aerial vehicle frame again, place unmanned aerial vehicle on fixed plate 9 of fixed frame 8, rotate bull stick 10, drive the arc 11 through bull stick 10 and remove to the inboard, until fixed with the unmanned aerial vehicle frame. And improve stability through slider 12 and spout 13, when needing to rotate during the test, can directly rotate through carousel 6, pack up the device and can accomplish the operation after finishing using.

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 frame strutting arrangement for unmanned aerial vehicle life cycle test is used, is including supporting urceolus (1), its characterized in that: the inner part of the support outer barrel (1) is spliced with a main rod (2), one side of the main rod (2) is provided with a limiting mechanism (3), the top of the main rod (2) is bolted with a bottom plate (4), the top of the bottom plate (4) is bolted with a rotating bearing (5), the top of the rotating bearing (5) is bolted with a turntable (6), rotating balls (7) are embedded in two sides between the bottom plate (4) and the turntable (6) and positioned on the rotating bearing (5), the top of the turntable (6) is bolted with a fixed frame (8), the bottom of the inner wall of the fixed frame (8) is bolted with a fixed plate (9), rotating rods (10) are in threaded connection with two sides of the fixed plate (9), the other end of the rotating rods (10) is bolted with an arc-shaped plate (11) through a bearing, and sliding blocks (12) are bolted at the bottoms of the front side and the rear side of the arc-shaped plate (11), the top of the fixed plate (9) is provided with a sliding groove (13), and the sliding block (12) is matched with the sliding groove (13).

2. The drone airframe support device for drone lifecycle testing of claim 1, further comprising: the limiting mechanism (3) comprises a limiting groove (14), a limiting rod (15) is inserted into the limiting groove (14), and a reset spring (16) is fixedly sleeved on the outer side of the limiting rod (15).

3. The drone airframe support device for drone lifecycle testing of claim 1, further comprising: the bottom of the support outer cylinder (1) is bolted with a base (17), the bottom of the base (17) is bolted with three supports (18), and the number of the supports (18) is three.

4. The drone airframe support device for drone lifecycle testing of claim 1, further comprising: the outer side of the main rod (2) is fixedly sleeved with a holding cylinder (19), and the bottom of the holding cylinder (19) is connected with a baffle (20) in a bolted mode.

5. The drone airframe support device for drone lifecycle testing of claim 1, further comprising: soft pads (21) are bonded on the inner sides of the arc-shaped plates (11).

6. The drone airframe support device for drone lifecycle testing of claim 3, wherein: the bottoms of the three brackets (18) are all bolted with anti-skid balls (22).