CN217836018U

CN217836018U - Folding supporting mechanism of unmanned aerial vehicle

Info

Publication number: CN217836018U
Application number: CN202222237803.1U
Authority: CN
Inventors: 黄翔
Original assignee: Nanjing Xinqi Ruidong Information Technology Co ltd
Current assignee: Nanjing Xinqi Ruidong Information Technology Co ltd
Priority date: 2022-08-25
Filing date: 2022-08-25
Publication date: 2022-11-18
Anticipated expiration: 2032-08-25

Abstract

The utility model discloses a folding supporting mechanism of unmanned aerial vehicle, including unmanned aerial vehicle, unmanned aerial vehicle bottom movable mounting has the connecting block, connecting block top fixed mounting has the iron plate, the supporting shoe is installed to the inside gomphosis of connecting block, the groove has been seted up to the connecting block bottom, accomodate the inside gomphosis of inslot and install the supporting shoe, the bumper shock absorber is installed to supporting shoe top symmetry, the equal nested reset spring of installing of bumper shock absorber outer wall, the mounting groove has been seted up to unmanned aerial vehicle bottom symmetry, the iron plate is installed to the inside gomphosis of mounting groove, and the supporting shoe receives the effect of power back rebound, drives the bumper shock absorber rebound of top installation simultaneously at the in-process of removing, upwards extrudees reset spring like this can reduce the direct effect of power on unmanned aerial vehicle, has reduced the damage to unmanned aerial vehicle effectively, has promoted unmanned aerial vehicle's life.

Description

Folding supporting mechanism of unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned aerial vehicle supporting mechanism technical field specifically is a folding supporting mechanism of unmanned aerial vehicle.

Background

The pilotless plane is called unmanned plane for short, and is a pilotless plane controlled by radio remote control equipment and a self-contained program control device.

The supporting mechanism is needed to be used to play a supporting role for an unmanned aerial vehicle when the existing unmanned aerial vehicle is landed in the using process, the traditional unmanned aerial vehicle supporting mechanism is a supporting mode adopting a rod, the supporting mode has certain defects, so that the anti-vibration of the supporting structure can cause damage to the parts inside the unmanned aerial vehicle when the unmanned aerial vehicle is landed, and meanwhile, the supporting device is large in size, inconvenient to carry and fold.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides a folding supporting mechanism of unmanned aerial vehicle, the anti-shake of supporting mechanism can cause the damage to the inside part of unmanned aerial vehicle when having solved current unmanned aerial vehicle descending, and the great inconvenient problem of carrying and folding of strutting arrangement volume simultaneously.

(II) technical scheme

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides a folding supporting mechanism of unmanned aerial vehicle, includes unmanned aerial vehicle, unmanned aerial vehicle bottom movable mounting has the connecting block, connecting block top fixed mounting has the iron plate, the supporting shoe is installed to the inside gomphosis of connecting block, the groove has been seted up to the connecting block bottom, it installs the supporting shoe to accomodate the inside gomphosis of inslot, the bumper shock absorber is installed to supporting shoe top symmetry, the equal nested reset spring of installing of bumper shock absorber outer wall, the mounting groove has been seted up to unmanned aerial vehicle bottom symmetry, the iron plate is installed to the inside gomphosis of mounting groove.

Preferably, the magnet is symmetrically arranged inside the mounting groove, the mounting bins are symmetrically arranged inside the supporting blocks, and the second through holes are symmetrically arranged at one end of the accommodating groove.

Preferably, the second through hole penetrating connection block extends to the inside of the installation bin, and the inside of the installation bin is provided with a return spring.

Preferably, first through-hole has been seted up at connecting block both ends, first through-hole extends to accomodate the inslot portion, the inside equal movable mounting of first through-hole has the kelly, the equal fixed mounting limiting plate of kelly one end.

Preferably, limiting holes are formed in the two ends of the supporting block, limiting rods are symmetrically arranged on the outer wall of the shock absorber, one end of the reset spring is attached to the outer wall of the limiting rods, and one end of the reset spring is arranged on the inner wall of the installation bin.

(III) advantageous effects

The utility model provides a folding supporting mechanism of unmanned aerial vehicle. The method has the following beneficial effects:

1. this folding supporting mechanism of unmanned aerial vehicle, through the bumper shock absorber, supporting mechanism's anti-shake can cause the damage to the inside part of unmanned aerial vehicle when reset spring and supporting shoe set up and solved traditional unmanned aerial vehicle landing effectively, because the reason of gravity descends downwards when unmanned aerial vehicle lands, can produce an ascending power in the twinkling of an eye of falling to the ground, the supporting shoe receives the effect back rebound of power, simultaneously drive the bumper shock absorber rebound of top installation at the in-process that removes, upwards extrude the in-process that can reduce the power direct action like this on unmanned aerial vehicle with reset spring like this, the damage to unmanned aerial vehicle has been reduced effectively, unmanned aerial vehicle's life has been promoted.

2. This folding supporting mechanism of unmanned aerial vehicle, through reset spring, accomodate the great inconvenient problem of carrying and folding of traditional unmanned aerial vehicle strutting arrangement volume of having solved effectively in setting up of groove and second through-hole, can make the supporting shoe can imbed completely and accomodate inslot portion to accomodating inslot portion extrusion under the condition of not using, then press inside with kelly one end, make kelly one end gomphosis to spacing downthehole portion, just so make the supporting shoe accomodate the inslot portion completely, the volume of supporting mechanism has been reduced effectively like this, conveniently carry and fold.

Drawings

Fig. 1 is a schematic overall structure diagram of the present invention;

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

FIG. 3 is a schematic view of the internal structure of the connecting block of the present invention;

fig. 4 is a schematic view of the structure of the support block of the present invention.

In the figure, 1, an unmanned aerial vehicle; 2. connecting blocks; 3. a support block; 4. mounting grooves; 5. a magnet; 6. an iron block; 7. a limiting hole; 8. a clamping rod; 9. a limiting plate; 10. a first through hole; 11. a receiving groove; 12. a shock absorber; 13. a second through hole; 14. installing a bin; 15. a return spring; 16. a limiting rod.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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. 1-4, an embodiment of the present invention provides a technical solution: the utility model provides a folding supporting mechanism of unmanned aerial vehicle, includes unmanned

aerial vehicle

1, 1 bottom movable mounting of unmanned aerial vehicle has connecting

block

2, 2 top fixed mounting of connecting block have iron plate 6, supporting shoe 3 is installed to 2 inside gomphosis of connecting block, 2 bottoms of connecting block have been seted up and have been accomodate groove 11, accomodate 11 inside gomphosis of groove and install supporting shoe 3, bumper shock absorber 12 is installed to 3 top symmetries of supporting shoe, reset spring 15 is all nested to install to bumper shock absorber 12 outer wall, mounting groove 4 has been seted up to 1 bottom symmetry of unmanned aerial vehicle, iron plate 6 is installed to 4 inside gomphosis of mounting groove, accomodates setting up of groove 11 and has made things convenient for the installation of supporting shoe 3, and the damage that power caused to unmanned aerial vehicle can be reduced to the setting of bumper shock absorber 12 and reset spring 15 simultaneously.

Magnet 5 is all installed to inside symmetry of mounting groove 4, installation storehouse 14 has been seted up to 3 inside symmetries of supporting shoe, accomodate 11 one end symmetries of groove and seted up second through-hole 13, magnet 5 sets up and can play an absorbent effect to iron plate 6 for connecting block 2 can the gomphosis install inside mounting groove 4.

Inside second through-hole 13 through connection piece 2 extends to

installation storehouse

14, 14 inside all install reset spring 15 of installing the storehouse, the installation of installation storehouse 14 has made things convenient for reset spring 15's installation, and reset spring 15's setting can play a absorbing effect effectively simultaneously.

First through-hole 10 has been seted up at 2 both ends of connecting block, inside first through-hole 10 extended to accomodate groove 11, the inside equal movable mounting of first through-hole 10 has kelly 8, the equal fixed mounting limiting plate 9 of kelly 8 one end, setting up of first through-hole 10 has made things convenient for the installation of kelly 8, and limiting plate 9's setting can play a spacing effect to kelly 8 simultaneously.

Spacing hole 7 has all been seted up at 3 both ends of supporting shoe, gag lever post 16 is installed to the equal symmetry of 12 outer walls of bumper shock absorbers, the laminating of 15 one ends of reset spring is at gag lever post 16 outer walls, the 14 inner walls in installation bin are installed to 15 one ends of reset spring, and the setting of bumper shock absorber 12 can reduce the damage that the impact force led to the fact unmanned aerial vehicle effectively, and setting up of gag lever post 16 can play a limiting displacement to reset spring 15 simultaneously.

The working principle is as follows: because the reason of gravity descends downwards when unmanned aerial vehicle descends, can produce an ascending power in the twinkling of an eye that falls to the ground, supporting shoe 3 receives effect back rebound, simultaneously drive the 12 rebound of bumper shock absorber of top installation at the in-process that removes, like this with reset spring 15 upwards extrusion can reduce power direct action like this on unmanned aerial vehicle moving, the damage to unmanned aerial vehicle has been reduced effectively, can make supporting shoe 3 can imbed inside the groove 11 to accomodating groove 11 completely with supporting shoe 3 under the condition of not using, then press inside with 8 one end of kelly inside, make 8 one end gomphosis of kelly to spacing hole 7 inside, just so make supporting shoe 3 accomodate inside the groove completely, supporting mechanism's volume has been reduced like this effectively, conveniently carry and fold.

The utility model discloses a 1, unmanned aerial vehicle; 2. connecting blocks; 3. a support block; 4. mounting grooves; 5. a magnet; 6. an iron block; 7. a limiting hole; 8. a clamping rod; 9. a limiting plate; 10. a first through hole; 11. a receiving groove; 12. a shock absorber; 13. a second through hole; 14. installing a bin; 15. a return spring; 16. the stop lever and the parts are all universal standard parts or parts known by the technicians in the field, and the structure and the principle of the stop lever are known by the technicians in technical manuals or by conventional experimental methods.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims

1. The utility model provides a folding supporting mechanism of unmanned aerial vehicle which characterized in that: including unmanned aerial vehicle (1), unmanned aerial vehicle (1) bottom movable mounting has connecting block (2), connecting block (2) top fixed mounting has iron plate (6), supporting shoe (3) are installed to connecting block (2) inside gomphosis, connecting block (2) bottom has been seted up and has been accomodate groove (11), accomodate groove (11) inside gomphosis and install supporting shoe (3), bumper shock absorber (12) are installed to supporting shoe (3) top symmetry, reset spring (15) are all nested to install to bumper shock absorber (12) outer wall, mounting groove (4) have been seted up to unmanned aerial vehicle (1) bottom symmetry, iron plate (6) are installed to mounting groove (4) inside gomphosis.

2. The foldable support mechanism of unmanned aerial vehicle of claim 1, wherein: magnet (5) are all installed to the inside symmetry of mounting groove (4), installation storehouse (14) have been seted up to supporting shoe (3) inside symmetry, second through-hole (13) have been seted up to holding groove (11) one end symmetry.

3. The foldable support mechanism of unmanned aerial vehicle of claim 2, wherein: inside second through-hole (13) through connection piece (2) inside extends to installation storehouse (14), return spring (15) are all installed to installation storehouse (14) inside.

4. The foldable support mechanism of unmanned aerial vehicle of claim 1, wherein: first through-hole (10) have been seted up at connecting block (2) both ends, inside first through-hole (10) extended to accomodate groove (11), the inside equal movable mounting of first through-hole (10) has kelly (8), the equal fixed mounting limiting plate (9) of kelly (8) one end.

5. The foldable support mechanism of unmanned aerial vehicle of claim 1, wherein: spacing hole (7) have all been seted up at supporting shoe (3) both ends, gag lever post (16) are installed to the equal symmetry of bumper shock absorber (12) outer wall, reset spring (15) one end laminating is in gag lever post (16) outer wall, reset spring (15) one end is installed at installation storehouse (14) inner wall.