CN218229427U

CN218229427U - Novel support of unmanned aerial vehicle

Info

Publication number: CN218229427U
Application number: CN202221506756.XU
Authority: CN
Inventors: 郑雄峰; 何剑锋; 雷勇; 任意
Original assignee: Hubei Heju New Material Co ltd
Current assignee: Hubei Polymeric Polymer Material Co ltd
Priority date: 2022-06-15
Filing date: 2022-06-15
Publication date: 2023-01-06
Anticipated expiration: 2032-06-15

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses a novel support of unmanned aerial vehicle, including unmanned aerial vehicle subassembly and support assembly, the unmanned aerial vehicle subassembly includes the fuselage, the top fixedly connected with frame of fuselage, the top edge of frame all is provided with the flabellum, the bottom of fuselage is installed the camera, the outside both sides of fuselage all are provided with the support assembly, the support assembly includes the support, the total of two of support, and the support is installed in the both sides outside of fuselage for bilateral symmetry, the outside of support all is rotated and is connected with the movable sleeve; through having set up the bracket component, when whole unmanned aerial vehicle subassembly top surface falls down, the buffer block at supporting shoe top is direct and the ground contact, and the top surface of having avoided the unmanned aerial vehicle subassembly directly falls and causes its inside component to appear the damage and cause the loss on ground to the buffer block adopts rubber block and spring to constitute, can play the effect of buffering when buffer block and ground contact.

Description

Novel support of unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a novel support of unmanned aerial vehicle.

Background

Unmanned aircraft, abbreviated "drone" and abbreviated "UAV", is an unmanned aircraft that is operated by a radio remote control device and self-contained programmed control means, or autonomously by an onboard computer, either completely or intermittently, and is often more suited to tasks that are too "fool, dirty, or dangerous" than a manned aircraft. Unmanned aerial vehicles can be classified into military and civilian applications. 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; 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 the industrial application and develop the unmanned aerial vehicle technology.

Current unmanned aerial vehicle protects unmanned aerial vehicle's fuselage and flabellum through support and flabellum protective frame, but the support knot is fixed in unmanned aerial vehicle's bottom, when meetting emergency, for example: unmanned aerial vehicle does not have the condition that the weightlessness falls, runs into the barrier and drops etc, and the bottom that unmanned aerial vehicle support can only protect the fuselage does not contact with ground and breaks, and when the fuselage top surface fell to the ground, the support then can not play the effect of protection fuselage, still can cause the damage of unmanned aerial vehicle fuselage and internals like this, causes the loss.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides a novel support of unmanned aerial vehicle possesses and prevents that unmanned aerial vehicle from falling down at emergency and falling the advantage that falls bad, has solved current unmanned aerial vehicle and has protected unmanned aerial vehicle's fuselage and flabellum through support and flabellum protecting frame, but the support knot is fixed in unmanned aerial vehicle's bottom, when meetting emergency, for example: unmanned aerial vehicle does not have the condition that the weightlessness falls, runs into the barrier and drops etc, and the bottom that unmanned aerial vehicle support can only protect the fuselage does not fall into bad with ground contact, and when the fuselage top surface fell to the ground, the support then can not play the effect of protection fuselage, still can cause the damage of unmanned aerial vehicle fuselage and internal element like this, causes the problem of loss.

(II) technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a novel support of unmanned aerial vehicle, includes unmanned aerial vehicle subassembly and bracket component, the unmanned aerial vehicle subassembly includes the fuselage, the top fixedly connected with frame of fuselage, the top edge of frame all is provided with the flabellum, the camera is installed to the bottom of fuselage, the outside both sides of fuselage all are provided with the bracket component, the bracket component includes the support, total two of support, and the support is bilateral symmetry and installs the both sides of fuselage are outside, the outside of support is all rotated and is connected with the movable sleeve, movable sleeve's inside gomphosis has the gag lever post, movable sleeve's top fixedly connected with connecting rod, the top threaded connection of connecting rod has the bracing piece, the supporting shoe is installed at the top of bracing piece, the top fixedly connected with buffer block of supporting shoe, the draw-in groove has been seted up to the outside of bracing piece, the cassette is all installed to the both sides outer wall of frame.

Preferably, the inside of supporting shoe is provided with the dismantlement subassembly, the dismantlement subassembly includes the mounting groove, the mounting groove is seted up in the top middle part of supporting shoe, the inside threaded connection of mounting groove has the screw rod.

Through adopting above-mentioned scheme, through having set up the detaching assembly, use at unmanned aerial vehicle and accomplish the back, be convenient for accomodate whole machine, make it can not occupy too many positions.

Preferably, the whole support is a ladder-shaped rod, an annular groove is formed in the joint of the bottom of the support and the movable sleeve, and a sliding block is arranged at the joint of the movable sleeve and the support.

By adopting the scheme, the annular groove is formed, and the sliding block can facilitate the movement of the whole movable sleeve, vertically fix the movable sleeve and play a role in supporting.

Preferably, the number of the movable sleeves is two, and the two movable sleeves are respectively arranged at the outer parts of the two brackets in a front-back manner.

Through adopting above-mentioned scheme, through installing it respectively in the outside of support, can conveniently support whole unmanned aerial vehicle's top surface when unmanned aerial vehicle accident whereabouts, prevent that unmanned aerial vehicle's top surface from landing and breaking its inside part.

Preferably, the bottom of the support rod is received in the connecting rod through a thread, and the outer wall of the support rod can be clamped in the clamping seat.

Through adopting above-mentioned scheme, through setting the bracing piece to can block in the inside of cassette, the effect that the bracing piece played the support to whole unmanned aerial vehicle of can being convenient for.

Preferably, the buffer blocks are composed of rubber blocks and springs, the number of the buffer blocks is multiple, and the buffer blocks are uniformly distributed on the tops of the supporting blocks.

By adopting the scheme, the rubber block and the spring are combined to form the buffer device, so that the force applied when the rubber block and the spring fall can be buffered conveniently.

Preferably, the clamping groove can be clamped on the outer wall of the bottom of the support, and the clamping seat is integrally shaped like a U.

By adopting the scheme, the U-shaped support rod can be conveniently clamped in the U-shaped support rod to play a role in limiting and fixing.

Preferably, the number of the supporting blocks is two, and the supporting blocks are respectively clamped inside the two clamping seats.

Through adopting above-mentioned scheme, can conveniently prop up whole unmanned aerial vehicle subassembly from fuselage both sides through having set up two, prevent its top surface direct and ground contact.

Preferably, the outer part of the clamping seat is provided with a semicircular clamping groove, and the clamping groove of the clamping seat is made of rubber materials.

Through adopting above-mentioned scheme, can conveniently fix it in the outside of support through having seted up semi-circular draw-in groove, play the effect of being convenient for accomodate.

Preferably, the mounting groove is integrally T-shaped, and the tail end of the mounting groove extends to the inside of the supporting rod.

Through adopting above-mentioned scheme, can conveniently fix the top at the bracing piece with whole supporting shoe through setting it to "T" style of calligraphy to be convenient for dismantle whole supporting shoe down.

(III) advantageous effects

Compared with the prior art, the utility model provides a novel support of unmanned aerial vehicle possesses following beneficial effect:

this novel support of unmanned aerial vehicle, through having set up the bracket component, when whole unmanned aerial vehicle subassembly top surface falls down, the buffer block at supporting shoe top is direct and ground contact, the top surface of having avoided the unmanned aerial vehicle subassembly directly falls and causes its inside component to appear the damage and cause the loss on ground, and the buffer block adopts rubber block and spring to constitute, can play the effect of buffering when buffer block and ground contact, prevent that the inside component of unmanned aerial vehicle subassembly from receiving inertial impact and receiving the damage when descending, whole device protects unmanned aerial vehicle loss reduction when not only emergency, can also be convenient for accomodate the bracket component after whole unmanned aerial vehicle subassembly uses the completion.

Drawings

Fig. 1 is a schematic structural view of the present invention;

fig. 2 is a side view of the present invention;

fig. 3 is a top view of the present invention;

fig. 4 is a schematic diagram of the internal structure of the supporting block in the present invention.

In the figure: 1. an unmanned aerial vehicle component; 11. a body; 12. a frame; 13. a fan blade; 14. a camera; 2. a bracket assembly; 21. a support; 22. an active cannula; 23. a limiting rod; 24. a connecting rod; 25. a support bar; 26. a supporting block; 27. a buffer block; 28. a card slot; 29. a card holder; 3. disassembling the assembly; 31. mounting grooves; 32. a screw.

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.

Example one

A novel support of an unmanned aerial vehicle comprises an unmanned aerial vehicle component 1 and a support component 2, wherein the unmanned aerial vehicle component 1 comprises a body 11, the top of the body 11 is fixedly connected with a frame 12, fan blades 13 are arranged on the top edge of the frame 12, a camera 14 is arranged at the bottom of the body 11, the support component 2 is arranged on two sides of the outer portion of the body 11, the support component 2 comprises a support 21, the whole support 21 is a ladder-shaped rod, a ring groove is formed in the joint of the bottom of the support 21 and a movable sleeve 22, sliding blocks are arranged at the joint of the movable sleeve 22 and the support 21, the number of the support 21 is two, the supports 21 are symmetrically arranged on the outer portions of two sides of the body 11 in a left-right mode, the outer portion of the support 21 is rotatably connected with the movable sleeve 22, the number of the movable sleeve 22 is two, the two movable sleeves 22 are respectively arranged on the outer portions of the two supports 21 in a front-back mode, and the inner portions of the movable sleeves 22 are embedded with a limiting rod 23, the top of the movable sleeve 22 is fixedly connected with a connecting rod 24, the top of the connecting rod 24 is in threaded connection with a supporting rod 25, the bottom of the supporting rod 25 is accommodated in the connecting rod 24 through threads, the outer wall of the supporting rod 25 can be clamped in the clamping seats 29, the top of the supporting rod 25 is provided with two supporting blocks 26, the supporting blocks 26 are respectively clamped in the two clamping seats 29, the top of the supporting block 26 is fixedly connected with a buffer block 27, the buffer block 27 is composed of rubber blocks and springs, the number of the buffer blocks 27 is multiple, the buffer blocks 27 are uniformly distributed on the top of the supporting block 26, the outside of the supporting rod 25 is provided with a clamping groove 28, the clamping groove 28 can be clamped on the outer wall of the bottom of the support 21, the clamping seats 29 are integrally U-shaped, the clamping seats 29 are arranged on the outer walls of two sides of the frame 12, and the outside of the clamping seats 29 is provided with a semi-circular groove, and the groove of the clamping seat 29 is made of rubber.

Referring to fig. 1-4, when the unmanned aerial vehicle assembly 1 encounters an accident, such as weightlessness and falling, or falls when encountering an obstacle, the support frame at the bottom cannot accurately support the unmanned aerial vehicle assembly 1, in order to prevent the unmanned aerial vehicle assembly 11 and the fan blades 13 from being damaged by falling, and a great deal of loss is caused, firstly, the ladder-shaped supports 21 are arranged on two sides of the exterior of the unmanned aerial vehicle assembly 11 to support the whole unmanned aerial vehicle assembly 1, before the unmanned aerial vehicle assembly 1 is controlled to take off, the movable sleeve 22 is rotated first, the movable sleeve 22 is turned over outside the supports 21, the connecting rod 24 at the top of the movable sleeve is vertical, the support rod 25 at the top of the connecting rod 24 is clamped inside the groove of the clamping seat 29, finally, the limiting rod 23 penetrates through the movable sleeve 22 to be fixed inside the supports 21, at this time, the support rod 25 is rotated again, when the threads at the bottom of the support rod 25 reach a stroke, the support block 26 at the top of the support rod 25 is higher than the height of the fan blades 13, when the sudden accident weightlessness falls, when the bottom surface of the unmanned aerial vehicle component 1 falls downwards, the bracket 21 at the bottom of the unmanned aerial vehicle component 1 plays a role in supporting the whole unmanned aerial vehicle component 1, while the top surface of the unmanned aerial vehicle component 1 falls downwards, the buffer block 27 at the top of the supporting block 26 is directly contacted with the ground, thereby avoiding the damage and loss of the elements inside the unmanned aerial vehicle component 1 caused by the direct falling of the top surface of the unmanned aerial vehicle component 1 on the ground, and the buffer block 27 is composed of rubber blocks and springs, which can play a role in buffering when the buffer block 27 is contacted with the ground, preventing the elements inside the unmanned aerial vehicle component 1 from being damaged by the inertia impact when falling, after the whole unmanned aerial vehicle component 1 is used, the limiting rod 23 is drawn out from the inside of the movable sleeve 22, and then the supporting rod 25 is pulled to enable the movable sleeve 22 at the bottom of the supporting rod to rotate outside the bracket 21, make the outside draw-in groove 28 card of bracing piece 25 outside in support 21 bottom, play spacing effect, whole device can not only prevent unmanned aerial vehicle and meet emergency and damage, can also be convenient for accomodate.

Example two

The function of more conveniently storing the whole bracket assembly 2 is added on the basis of the first embodiment.

Supporting shoe 26's inside is provided with removal subassembly 3, and removal subassembly 3 includes mounting groove 31, and mounting groove 31 is whole to be "T" style of calligraphy, and the end of mounting groove 31 extends to the inside of bracing piece 25, and the top middle part at supporting shoe 26 is seted up to mounting groove 31, and the inside threaded connection of mounting groove 31 has screw rod 32.

Referring to fig. 1-4, after whole unmanned aerial vehicle subassembly 1 work is accomplished, in order to be more convenient for accomodate bracket component 2, set up dismantlement subassembly 3, when blocking draw-in groove 28 in the outside of support 21, unscrew screw rod 32 from the inside of mounting groove 31 and take out it again, at this moment directly will lose the supporting shoe 26 of fixed effort directly take off can, be convenient for accomodate of whole device.

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 a novel support of unmanned aerial vehicle which characterized in that: including unmanned aerial vehicle subassembly (1) and bracket component (2), unmanned aerial vehicle subassembly (1) includes fuselage (11), the top fixedly connected with frame (12) of fuselage (11), the top edge of frame (12) all is provided with flabellum (13), camera (14) are installed to the bottom of fuselage (11), the outside both sides of fuselage (11) all are provided with bracket component (2), bracket component (2) include support (21), the total two of support (21), and support (21) are bilateral symmetry and install the both sides of fuselage (11) are outside, the outside of support (21) is all rotated and is connected with movable sleeve (22), the inside gomphosis of movable sleeve (22) has limiting rod (23), the top fixedly connected with connecting rod (24) of movable sleeve (22), the top threaded connection of connecting rod (24) has bracing piece (25), supporting shoe (26) are installed at the top of bracing piece (25), the top fixedly connected with buffer block (27) of supporting shoe (26), card slot (28) have been seted up to the outside of bracing piece (25), the both sides of frame (12) all install cassette (29).

2. The novel unmanned aerial vehicle bracket of claim 1, characterized in that: the supporting shoe (26) is internally provided with a dismounting component (3), the dismounting component (3) comprises a mounting groove (31), the mounting groove (31) is formed in the middle of the top of the supporting shoe (26), and the mounting groove (31) is internally connected with a screw (32) in a threaded manner.

3. The novel unmanned aerial vehicle bracket of claim 1, characterized in that: the support (21) is integrally a ladder-shaped rod, an annular groove is formed in the joint of the bottom of the support (21) and the movable sleeve (22), and a sliding block is arranged at the joint of the movable sleeve (22) and the support (21).

4. The novel unmanned aerial vehicle bracket of claim 1, characterized in that: the number of the movable sleeves (22) is two, and the two movable sleeves (22) are respectively arranged at the outer parts of the two brackets (21) in a front-back mode.

5. The novel support of unmanned aerial vehicle of claim 1, characterized in that: the bottom of the support rod (25) is received into the connecting rod (24) through threads, and the outer wall of the support rod (25) can be clamped inside the clamping seat (29).

6. The novel unmanned aerial vehicle bracket of claim 1, characterized in that: the buffer blocks (27) are composed of rubber blocks and springs, the number of the buffer blocks (27) is multiple, and the buffer blocks (27) are uniformly distributed on the top of the supporting block (26).

7. The novel support of unmanned aerial vehicle of claim 1, characterized in that: the clamping groove (28) can be clamped on the outer wall of the bottom of the support (21), and the clamping seat (29) is integrally shaped like a U.

8. The novel unmanned aerial vehicle bracket of claim 1, characterized in that: the number of the supporting blocks (26) is two, and the supporting blocks (26) are respectively clamped inside the two clamping seats (29).

9. The novel unmanned aerial vehicle bracket of claim 1, characterized in that: the outer part of the clamping seat (29) is provided with a semicircular clamping groove, and the clamping groove of the clamping seat (29) is made of rubber materials.

10. The novel unmanned aerial vehicle bracket of claim 2, characterized in that: the whole mounting groove (31) is T-shaped, and the tail end of the mounting groove (31) extends into the supporting rod (25).