CN209757507U - Fixing frame for unmanned aerial vehicle - Google Patents

Abstract

The utility model discloses a fixing frame for unmanned aerial vehicle, including the unmanned aerial vehicle body, the below fixed welding of unmanned aerial vehicle body has two sets of supporting legs, and the below both sides fixed welding of two sets of supporting legs has the sleeve pipe, the inside swing joint of sleeve pipe has the rotatory pipe, the both sides fixed connection of rotatory pipe has the bracing piece, the below an organic whole of bracing piece is provided with the hem, the cover has the support horizontal pole on the hem, the supporting leg is located the below fixed welding of sleeve pipe and has first spring fixing base, the middle part fixed welding of bracing piece has the second spring fixing base, open the inboard of first spring fixing base and second spring fixing base has the caulking groove, it has the spring to peg graft between the caulking groove on the first spring fixing base and the caulking groove on the second spring fixing base, the through-hole interpolation has the bolt, this fixing frame for unmanned aerial vehicle, and light in structure has good, the shock absorption effect is good, and the shock absorption device is worthy of great popularization.

Description

Fixing frame for unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a mount for unmanned aerial vehicle.

background

Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane aircraft, and the like. Compared with a manned airplane, the unmanned aerial vehicle has the characteristics of small volume, low manufacturing cost and convenience in use, and the fixing frame of the existing unmanned aerial vehicle base is a rigid support, does not have the buffering function and is easy to damage due to vibration when landing, so that the invention provides the fixing frame for the unmanned aerial vehicle to solve the problems.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a mount for unmanned aerial vehicle to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: a fixing frame for an unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein two groups of supporting legs are fixedly welded below the unmanned aerial vehicle body, sleeves are fixedly welded on two sides below the two groups of supporting legs, a rotating pipe is movably connected inside the sleeves and can rotate in the sleeves, supporting rods are fixedly connected on two sides of the rotating pipe and can be conveniently used for supporting the unmanned aerial vehicle body through the arranged supporting rods, a folded edge is integrally arranged below the supporting rods, a supporting cross rod is sleeved on the folded edge and can be used for fixing a rubber sleeve, the supporting legs are fixedly welded below the sleeves and are provided with first spring fixing seats, second spring fixing seats are fixedly welded in the middle of the supporting rods, caulking grooves are formed in the inner sides of the first spring fixing seats and the inner grooves in the second spring fixing seats, springs are inserted between the caulking grooves in the first spring fixing seats and the caulking grooves in the second spring fixing seats, the first spring fixing seat and the second spring fixing seat are provided with through holes, the through holes are internally inserted with bolts, the first spring fixing seat and the second spring fixing seat are arranged to conveniently fix the springs, and the supporting rods are conveniently supported by the arranged springs to have good buffering effect.

Preferably, the rubber sleeve is sleeved on the outer side of the supporting cross rod and has a protection effect.

Preferably, the height of the supporting cross rod at the lower end of the supporting rod is lower than that of the lower end of the supporting leg.

Preferably, the support rod is a magnesium-aluminum alloy steel pipe, the diameter of the support rod is one-cm, and the arranged magnesium-aluminum alloy support rod has the characteristics of light weight and slight height.

Preferably, the two ends of the spring are respectively abutted to the caulking grooves on the first spring fixing seat and the second spring fixing seat, the bolt penetrates through the gap between the springs, and the springs have a good buffering effect.

Compared with the prior art, the beneficial effects of the utility model are as follows: this mount for unmanned aerial vehicle, during the use, both sides at two sets of supporting legs are provided with the sleeve pipe, at the intraductal rotation of cover and be provided with the swivel pipe, the both sides of swivel pipe are connected with the bracing piece, be provided with certain angle between bracing piece and the supporting leg, certain cushion effect has conveniently in unmanned aerial vehicle descending, through the spring that sets up, the spring has certain elasticity, when falling the ground, can play the effect to the bracing piece buffering, this mount for unmanned aerial vehicle, the structure is light, has good cushioning effect, the shock attenuation is effectual, be worth wideling popularize.

Drawings

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

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

fig. 3 is a schematic view of the fixing base structure of the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. supporting legs; 3. a sleeve; 4. rotating the tube; 5. a support bar; 6. a rubber sleeve; 7. a first spring holder; 8. a spring; 9. a second spring fixing seat; 10. caulking grooves; 11. a through hole; 12. a bolt; 13. folding edges; 14. a support rail.

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.

Referring to fig. 1-3, a fixing frame for an unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, two sets of supporting legs 2 are fixedly welded below the unmanned aerial vehicle body 1, sleeves 3 are fixedly welded on two sides below the two sets of supporting legs 2, a rotating pipe 4 is movably connected inside the sleeve 3, the rotating pipe 4 can rotate in the sleeve 3, supporting rods 5 are fixedly connected on two sides of the rotating pipe 4, the supporting rods 5 are arranged to conveniently support the unmanned aerial vehicle body 1, a folded edge 13 is integrally arranged below the supporting rods 5, a supporting cross rod 14 is sleeved on the folded edge 13, the supporting cross rod 14 is arranged to fix a rubber sleeve 6, a first spring fixing seat 7 is fixedly welded below the sleeve 3 on the supporting legs 2, a second spring fixing seat 9 is fixedly welded in the middle of the supporting rods 5, and caulking grooves 10 are formed in the inner sides of the first spring fixing seat 7 and the second spring fixing seat 9, the spring 8 is inserted between the embedded groove 10 on the first spring fixing seat 7 and the embedded groove 10 on the second spring fixing seat 9, the through holes 11 are formed in the first spring fixing seat 7 and the second spring fixing seat 9, the inserting pins 12 are inserted in the through holes 11, the spring 8 can be conveniently fixed through the arranged first spring fixing seat 7 and the second spring fixing seat 9, the supporting rod 5 can be conveniently supported through the arranged spring 8, and the supporting rod 5 has a good buffering effect.

Specifically, the rubber sleeve 6 is sleeved outside the supporting cross bar 14, and the rubber sleeve 6 has a protection effect.

Specifically, the height of the cross rod 14 at the lower end of the support rod 5 is lower than that of the lower end of the support leg 2.

Specifically, the support rod 5 is a magnesium-aluminum alloy steel pipe, the diameter of the support rod 5 is 0.8-1.5cm, and the magnesium-aluminum alloy support rod 5 is light in weight and slightly high in degree.

Specifically, the two ends of the spring 8 respectively abut against the caulking groove 10 on the first spring fixing seat 7 and the caulking groove 10 on the second spring fixing seat 9, the bolt 12 penetrates through the gap between the springs 8, and the springs 8 have a good buffering effect.

The working principle is as follows: this mount for unmanned aerial vehicle, during the use, both sides at two sets of supporting legs 2 are provided with sleeve pipe 3, it is provided with rotatory pipe 4 to be provided with at the intraductal rotation of sleeve pipe 3, the both sides of rotatory pipe 4 are connected with bracing piece 5, be provided with certain angle between bracing piece 5 and the supporting leg 2, certain buffer power has conveniently when unmanned aerial vehicle descends, spring 8 through setting up, spring 8 has certain elasticity, when falling the ground, can play the effect to bracing piece 5 buffering, this mount for unmanned aerial vehicle, moreover, the steam generator is light in structure, good cushioning effect has, the shock attenuation is effectual, be worth wideling popularize.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.

Claims (5)

1. The utility model provides a mount for unmanned aerial vehicle, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle is characterized in that two groups of supporting legs (2) are fixedly welded below the unmanned aerial vehicle body (1), sleeves (3) are fixedly welded on two sides below the two groups of supporting legs (2), a rotating pipe (4) is movably connected inside the sleeves (3), supporting rods (5) are fixedly connected on two sides of the rotating pipe (4), a folding edge (13) is integrally arranged below the supporting rods (5), a supporting cross rod (14) is sleeved on the folding edge (13), a first spring fixing seat (7) is fixedly welded below the sleeves (3) on the supporting legs (2), a second spring fixing seat (9) is fixedly welded in the middle of the supporting rods (5), caulking grooves (10) are formed in the inner sides of the first spring fixing seat (7) and the second spring fixing seat (9), and springs (8) are inserted between the caulking grooves (10) on the first spring fixing seat (7) and the caulking grooves (10) on the second spring fixing seat (9), the first spring fixing seat (7) and the second spring fixing seat (9) are provided with through holes (11), and inserting pins (12) are inserted into the through holes (11).

2. The mount for the unmanned aerial vehicle according to claim 1, wherein: the outer side of the supporting cross bar (14) is sleeved with a rubber sleeve (6).

3. The mount for the unmanned aerial vehicle according to claim 1, wherein: the height of the supporting cross rod (14) at the lower end of the supporting rod (5) is lower than that of the lower end of the supporting leg (2).

4. The mount for the unmanned aerial vehicle according to claim 1, wherein: the support rod (5) is a magnesium-aluminum alloy steel pipe, and the diameter of the support rod (5) is 0.8-1.5 cm.

5. The mount for the unmanned aerial vehicle according to claim 1, wherein: the two ends of the spring (8) are respectively abutted into the caulking groove (10) on the first spring fixing seat (7) and the caulking groove (10) on the second spring fixing seat (9), and the bolt (12) penetrates through a gap between the tube springs (8).