CN219172656U

CN219172656U - Effectual unmanned aerial vehicle of shock attenuation

Info

Publication number: CN219172656U
Application number: CN202222445303.7U
Authority: CN
Inventors: 寿思翔
Original assignee: Wuhan Huachenmao Technology Co ltd
Current assignee: Wuhan Huachenmao Technology Co ltd
Priority date: 2022-09-15
Filing date: 2022-09-15
Publication date: 2023-06-13
Anticipated expiration: 2032-09-15

Abstract

The utility model provides an unmanned aerial vehicle with a good damping effect, which comprises an unmanned aerial vehicle, wherein a threaded pipe is welded on the lower surface of the unmanned aerial vehicle, a damping mechanism is arranged at one end of the threaded pipe, a lifting handle is fixedly arranged on the surface of the unmanned aerial vehicle, a sheath is sleeved on the outer ring of the lifting handle, and a clamping mechanism is arranged at one end of the unmanned aerial vehicle. This effectual unmanned aerial vehicle of shock attenuation, through threaded rod, fixed sleeve, movable rod, first spring and the setting of base, when using, pass through the threaded rod with fixed sleeve and install the one end at the screwed pipe, then at the in-process that unmanned aerial vehicle descends, the base can contact ground earlier, and the movable rod can stretch out and draw back at fixed sleeve's one end under the effect of first spring, and first spring can absorb most impact force to play the absorbing effect.

Description

Effectual unmanned aerial vehicle of shock attenuation

Technical Field

The utility model relates to the related technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a good shock absorption effect.

Background

Unmanned aerial vehicle is abbreviated as unmanned aerial vehicle, is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, and unmanned aerial vehicle uses more and more extensively at current each trade now, and unmanned aerial vehicle is in the in-process that the flight was fallen, easily because operator's mistake leads to unmanned aerial vehicle to be impaired at the too fast unmanned aerial vehicle that leads to of in-process speed that falls, so, especially needs an unmanned aerial vehicle that shock attenuation effect is good.

But current effectual unmanned aerial vehicle of shock attenuation, at the in-process of using, most unmanned aerial vehicle is at the in-process of descending, because the operator error easily, leads to unmanned aerial vehicle at the in-process speed of descending too fast for unmanned aerial vehicle bears great impact force, makes unmanned aerial vehicle impaired easily.

Disclosure of Invention

The utility model aims to provide an unmanned aerial vehicle with good damping effect, so as to solve the problems that the unmanned aerial vehicle with good damping effect in the prior art is provided, but most unmanned aerial vehicles are easy to damage due to the fact that the unmanned aerial vehicle is too fast in the falling process due to operator errors in the falling process in the use process of the unmanned aerial vehicle, and the unmanned aerial vehicle bears larger impact force.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an effectual unmanned aerial vehicle of shock attenuation, includes unmanned aerial vehicle, unmanned aerial vehicle's below surface welding has the screwed pipe, the one end of screwed pipe is provided with damper, unmanned aerial vehicle's fixed surface installs the handle, the outer lane cover of handle is equipped with the sheath, unmanned aerial vehicle's one end is provided with fixture.

Preferably, the damping mechanism comprises a threaded rod, a fixed sleeve, a movable rod, a first spring and a base, wherein one end of the threaded pipe is connected with the threaded rod, the fixed sleeve is welded at one end of the threaded rod, one end of the fixed sleeve penetrates through the movable rod, the first spring is sleeved at one end of the movable rod, and the base is welded at one end of the movable rod.

Preferably, the movable rod and the fixed sleeve form a telescopic structure, and the fixed sleeve is in threaded connection with the threaded pipe through a threaded rod.

Preferably, the handle is fixedly connected with the unmanned aerial vehicle, and the sheath is tightly attached to the handle.

Preferably, the fixture includes fixed bolster, fixed orifices, fixing bolt, fixed plate, screw hole, second spring and stripper plate, the below both sides fixed mounting of unmanned aerial vehicle has the fixed bolster, the fixed orifices has been seted up on the surface of fixed bolster, the one end of fixed orifices runs through there is fixing bolt, the one end of fixed bolster is provided with the fixed plate, the screw hole has been seted up to the surface both sides of fixed plate, the welding of the below of fixed plate has the second spring, the one end welding of second spring has the stripper plate.

Preferably, the fixing holes are distributed on the surface of the fixing support at equal intervals, and one end of the fixing bolt penetrates through the fixing holes and is in threaded connection with the threaded holes.

Preferably, one side of the fixing plate is attached to the fixing support, and the second springs are symmetrically arranged on the central axis of the fixing plate.

Compared with the prior art, the utility model has the beneficial effects that: this effectual unmanned aerial vehicle of shock attenuation, through threaded rod, fixed sleeve, movable rod, first spring and the setting of base, when using, pass through the threaded rod with fixed sleeve and install the one end at the screwed pipe, then at the in-process that unmanned aerial vehicle descends, the base can contact ground earlier, and the movable rod can stretch out and draw back at fixed sleeve's one end under the effect of first spring, and first spring can absorb most impact force to play the absorbing effect.

Drawings

FIG. 1 is a schematic diagram of a side view of the present utility model;

FIG. 2 is a schematic view of a shock absorbing mechanism according to the present utility model;

FIG. 3 is a schematic view showing the mutual cooperation structure of the fixing plate and the extrusion plate;

fig. 4 is an enlarged schematic view of the structure of fig. 1 a according to the present utility model.

In the figure: 1. unmanned plane; 2. a threaded tube; 3. a damping mechanism; 301. a threaded rod; 302. fixing the sleeve; 303. a movable rod; 304. a first spring; 305. a base; 4. a handle; 5. a sheath; 6. a clamping mechanism; 601. a fixed bracket; 602. a fixing hole; 603. a fixing bolt; 604. a fixing plate; 605. a threaded hole; 606. a second spring; 607. and extruding the plate.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-4, the present utility model provides a technical solution: the utility model provides a effectual unmanned aerial vehicle of shock attenuation, includes unmanned aerial vehicle 1, and unmanned aerial vehicle 1's below surface welding has screwed pipe 2, and screwed pipe 2's one end is provided with damper 3, and unmanned aerial vehicle 1's fixed surface installs handle 4, and handle 4's outer lane cover is equipped with sheath 5, and unmanned aerial vehicle 1's one end is provided with fixture 6.

Further, the damping mechanism 3 includes threaded rod 301, fixed sleeve 302, movable rod 303, first spring 304 and base 305, the one end of screwed pipe 2 is connected with threaded rod 301, the one end welding of threaded rod 301 has fixed sleeve 302, the one end of fixed sleeve 302 has run through movable rod 303, the one end cover of movable rod 303 is equipped with first spring 304, the one end welding of movable rod 303 has base 305, when using, through threaded rod 301, fixed sleeve 302, movable rod 303, first spring 304 and base 305's setting, install the fixed sleeve 302 at the one end of screwed pipe 2 through threaded rod 301, then at unmanned aerial vehicle 1 in-process that descends, base 305 can contact the ground earlier, and movable rod 303 can stretch out and draw back at the one end of fixed sleeve 302 under the effect of first spring 304, and first spring 304 can absorb most impact force, thereby play the absorbing effect.

Further, the movable rod 303 and the fixed sleeve 302 form a telescopic structure, the fixed sleeve 302 is in threaded connection with the threaded pipe 2 through the threaded rod 301, and the fixed sleeve 302 can be conveniently installed and detached through the arrangement of the threaded pipe 2.

Further, handle 4 and unmanned aerial vehicle 1 fixed connection, sheath 5 closely laminate with handle 4, through handle 4 and sheath 5's setting, can be convenient for carry unmanned aerial vehicle 1.

Further, fixture 6 includes fixed bolster 601, fixed orifices 602, fixing bolt 603, fixed plate 604, screw hole 605, second spring 606 and stripper plate 607, fixed bolster 601 has been installed to the below both sides of unmanned aerial vehicle 1, fixed orifices 602 have been seted up on the surface of fixed bolster 601, fixing bolt 603 has been run through to one end of fixed orifices 602, one end of fixed bolster 601 is provided with fixed plate 604, screw hole 605 has been seted up to the surface both sides of fixed plate 604, the second spring 606 has been welded to the below of fixed plate 604, the one end welding of second spring 606 has stripper plate 607, through fixed bolster 601, fixed orifices 602, fixing bolt 603, fixed plate 604, screw hole 605, second spring 606 and stripper plate 607 set up, when using, install fixed bolster 601 in the below of unmanned aerial vehicle 1, can make unmanned aerial vehicle 1 have the function of carrying through fixed bolster 601, then install fixed plate 604 in one side of fixed bolster 601 through screw hole 605 and fixing bolt, and the mounted position of fixed plate 604 can be adjusted through fixed orifice 602, make the stripper plate 607 can carry out the article of centre gripping under the effect of second spring 606 to the fixed bolster.

Further, the fixing holes 602 are distributed on the surface of the fixing bracket 601 at equal intervals, one end of the fixing bolt 603 penetrates through the fixing holes 602 and the threaded holes 605 to be in threaded connection, and the fixing holes 602 are arranged in multiple groups so as to be convenient for adjusting the height of the fixing plate 604.

Further, one side of the fixing plate 604 is attached to the fixing bracket 601, the second springs 606 are symmetrically arranged on the central axis of the fixing plate 604, and the pressing plate 607 can be better clamped by the arrangement of the second springs 606.

Working principle: firstly, the fixing sleeve 302 is installed at one end of the threaded pipe 2 through the threaded rod 301, then in the falling process of the unmanned aerial vehicle 1, the base 305 can firstly contact the ground, the movable rod 303 stretches out and draws back at one end of the fixing sleeve 302 under the action of the first spring 304, and the first spring 304 can absorb most impact force, so that the shock absorption effect is achieved, secondly, the fixing support 601 is installed below the unmanned aerial vehicle 1, the unmanned aerial vehicle 1 can have a carrying function through the fixing support 601, then the fixing plate 604 is installed at one side of the fixing support 601 through the threaded holes 605 and the fixing bolts 603, the installation position of the fixing plate 604 can be adjusted through the fixing holes 602, the extruding plate 607 can clamp objects on the fixing support 601 under the action of the second spring 606, and finally the unmanned aerial vehicle 1 can be carried through the handle 4, so that the unmanned aerial vehicle with good shock absorption effect is achieved.

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

Claims

1. Effectual unmanned aerial vehicle of shock attenuation, including unmanned aerial vehicle (1), its characterized in that: the utility model discloses a unmanned aerial vehicle, including unmanned aerial vehicle (1), screw thread pipe (2) of below surface welding, the one end of screw thread pipe (2) is provided with damper (3), the fixed surface of unmanned aerial vehicle (1) installs handle (4), the outer lane cover of handle (4) is equipped with sheath (5), the one end of unmanned aerial vehicle (1) is provided with fixture (6).

2. The unmanned aerial vehicle with good shock attenuation effect according to claim 1, wherein the shock attenuation mechanism (3) comprises a threaded rod (301), a fixed sleeve (302), a movable rod (303), a first spring (304) and a base (305), one end of the threaded pipe (2) is connected with the threaded rod (301), one end of the threaded rod (301) is welded with the fixed sleeve (302), one end of the fixed sleeve (302) penetrates through the movable rod (303), one end of the movable rod (303) is sleeved with the first spring (304), and one end of the movable rod (303) is welded with the base (305).

3. The unmanned aerial vehicle with good shock absorption effect according to claim 2, wherein the movable rod (303) and the fixed sleeve (302) form a telescopic structure, and the fixed sleeve (302) is in threaded connection with the threaded tube (2) through the threaded rod (301).

4. The unmanned aerial vehicle with good damping effect according to claim 1, wherein the lifting handle (4) is fixedly connected with the unmanned aerial vehicle (1), and the sheath (5) is tightly attached to the lifting handle (4).

5. The unmanned aerial vehicle with good shock absorption effect according to claim 1, wherein the clamping mechanism (6) comprises a fixing support (601), a fixing hole (602), fixing bolts (603), a fixing plate (604), threaded holes (605), second springs (606) and a squeezing plate (607), the fixing support (601) is fixedly arranged on two sides of the lower portion of the unmanned aerial vehicle (1), the fixing hole (602) is formed in the surface of the fixing support (601), the fixing bolts (603) penetrate through one end of the fixing hole (602), the fixing plate (604) is arranged at one end of the fixing support (601), the threaded holes (605) are formed in two sides of the surface of the fixing plate (604), the second springs (606) are welded below the fixing plate (604), and the squeezing plate (607) is welded at one end of the second springs (606).

6. The unmanned aerial vehicle with good damping effect according to claim 5, wherein the fixing holes (602) are distributed on the surface of the fixing support (601) at equal intervals, and one end of the fixing bolt (603) penetrates through the fixing holes (602) and is in threaded connection with the threaded holes (605).

7. The unmanned aerial vehicle with good damping effect according to claim 5, wherein one side of the fixing plate (604) is attached to the fixing bracket (601), and the second springs (606) are symmetrically arranged on the central axis of the fixing plate (604).