CN218086016U

CN218086016U - Anticollision unmanned aerial vehicle

Info

Publication number: CN218086016U
Application number: CN202222013716.8U
Authority: CN
Inventors: 李雪丹; 刘佳宜; 陈钊; 王秀贤; 刘蒙蒙; 吕美琳; 郭强
Original assignee: Shaanxi Zaowu Liangshi Technology Co ltd
Current assignee: Shaanxi Zaowu Liangshi Technology Co ltd
Priority date: 2022-08-02
Filing date: 2022-08-02
Publication date: 2022-12-20
Anticipated expiration: 2032-08-02

Abstract

The utility model discloses an anticollision unmanned aerial vehicle relates to the unmanned aerial vehicle field, and the screw outside on the organism is equipped with protector, and the camera both sides of organism below all articulate the first end of bracing piece, and the second end of bracing piece is connected with the movable pulley, and the first end of bracing piece articulates the first end that has damping spring. The utility model provides an anticollision unmanned aerial vehicle connects through protection network and second connecting rod, and the lead screw runs through the second end and the fixed block of second connecting rod and is connected with the head rod for unmanned aerial vehicle buffer stop can dismantle, reduces occupation space, is connected with damping spring on the bracing piece, and damping spring can play the effect of protection organism when unmanned aerial vehicle falls to the ground, and damping spring can fold in the bracing piece, and the bracing piece can fold on the head rod, can not occupy great space when unmanned aerial vehicle accomodates, the utility model is simple in operation, the practicality is strong, convenient to use.

Description

Anticollision unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned aerial vehicle field, concretely relates to anticollision unmanned aerial vehicle.

Background

Unmanned aerial vehicle wide application is taken photo by plane, agriculture, express delivery transportation, fields such as disaster rescue, if unmanned aerial vehicle breaks down the phenomenon that unmanned aerial vehicle falls, the last part of unmanned aerial vehicle receives strong striking and can damage, if do not have the dropproof protection can bring serious economic loss, therefore most unmanned aerial vehicle all install buffer stop, but present unmanned aerial vehicle buffer stop only has the protection to unmanned aerial vehicle's screw, because inertia can cause the damage to the organism when unmanned aerial vehicle falls to the ground, and unmanned aerial vehicle's buffer stop is fixed, can not dismantle, be unfavorable for unmanned aerial vehicle to accomodate.

In view of this, the present invention is especially provided.

Disclosure of Invention

The utility model provides an above-mentioned problem, provide an anticollision unmanned aerial vehicle, solved when unmanned aerial vehicle falls to the ground because inertia can cause the problem of damage to the organism.

The utility model adopts the technical proposal that: an anti-collision unmanned aerial vehicle is characterized by comprising a supporting rod and a machine body;

a protective device is arranged on the outer side of the propeller on the machine body, and the protective device is detachably connected with the machine body; the camera both sides of organism below all articulate the first end of bracing piece, the second end of bracing piece is connected with the movable pulley, the first end of bracing piece articulates there is damping spring's first end, damping spring's second end and organism can be dismantled the connection.

Furthermore, damping spring's second end is equipped with first through-hole, the lateral wall of organism is equipped with first screw, be equipped with first screw rod in the first screw, and first screw rod runs through first through-hole and first screw spiro union.

Furthermore, both ends of the machine body are provided with fixing blocks, a first connecting rod is arranged on the machine body on one side of each fixing block, and the first connecting rods are connected with the machine body in a sliding mode.

Furthermore, a first sliding groove is formed below the machine body on one side of the fixing block, second sliding grooves are formed in the two sides of the first sliding groove, and the first connecting rod slides in the first sliding groove and the second sliding groove.

Furthermore, a second screw hole is formed in the fixing block, a lead screw is arranged in the second screw hole, a second through hole is formed in the first connecting rod, the lead screw is rotatably connected with the second through hole, and the lead screw penetrates through the second through hole and is in threaded connection with the second screw hole.

Further, the lead screw is rotatably connected with the second through hole.

Furthermore, a first groove is formed in the supporting rod, and the damping spring is detachably clamped in the first groove.

Furthermore, the first end of the supporting rod is hinged with the machine body through a first rotating shaft, and the first end of the damping spring is hinged with the supporting rod through a second rotating shaft.

Furthermore, the protection device comprises a protection net, a T-shaped connecting rod and a second connecting rod; all be equipped with the third spout on the organism of screw both sides, two all be equipped with T type connecting rod in the third spout, and the horizontal pole of T type connecting rod slides in the third spout, be equipped with the protection network on the montant of T type connecting rod, the montant lateral wall of T type connecting rod is connected with the first end of second connecting rod, the second end and the lead screw of second connecting rod can dismantle the connection.

Furthermore, a third screw hole is formed in the second end of the second connecting rod, and the lead screw is in threaded connection with the third screw hole.

The utility model has the advantages that:

the utility model provides an anticollision unmanned aerial vehicle connects through protection network and second connecting rod, and the lead screw runs through the second end and the fixed block of second connecting rod and is connected with the head rod for unmanned aerial vehicle buffer stop can dismantle, reduces occupation space, is connected with damping spring on the bracing piece, and damping spring can play the effect of protection organism when unmanned aerial vehicle falls to the ground, and damping spring can fold in the bracing piece, and the bracing piece can fold on the head rod, can not occupy great space when unmanned aerial vehicle accomodates, the utility model is simple in operation, the practicality is strong, convenient to use.

In addition to the above-described objects, features and advantages, the present invention has other objects, features and advantages. The present invention will be described in further detail with reference to the drawings.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this application, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification.

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic view of the screw assembly of the present invention;

FIG. 3 is a schematic view of the installation of the protection device of the present invention;

fig. 4 is a schematic structural view of the first chute and the second chute of the present invention;

FIG. 5 is a schematic view of the first screw installation of the present invention;

fig. 6 is a plan view of the protection net of the present invention;

fig. 7 is a schematic view of the folding of the support rod of the present invention;

fig. 8 is a schematic view of a first groove structure of the present invention.

Reference numerals are as follows:

1 is a support rod; 101 is a sliding wheel; 102 is a first groove; 2 is a machine body; 201 is a second chute; 202 is a first chute; 203 is a first screw hole; 204 is a first screw; 205 is a third chute; 3 is a damping spring; 301 is a first through hole; 4 is a first connecting rod; 401 is a second screw hole; 5 is a second rotating shaft; 6 is a protective device; 601 is a protective net; 602 is a T-shaped connecting rod; 603 is a second connecting rod; 604 is a third screw hole; 7 is a fixed block; 701 is a second through hole; 702 is a lead screw; and 8, a first rotating shaft.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.

In the description of the present invention, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

Referring to fig. 1 to 8, an anti-collision unmanned aerial vehicle comprises a support rod 1 and a machine body 2; the protective device 6 is arranged on the outer side of the propeller on the machine body 2, the protective device 6 can protect the propeller on the machine body 2, the protective device 6 and the machine body 2 are detachably connected, and the protective device 6 can be detached from the machine body 2 when not in use; the two sides of the camera below the machine body 2 are both hinged with a first end of a supporting rod 1, the first end of the supporting rod 1 is hinged with the machine body 2 through a first rotating shaft 8, and the first end of the supporting rod 1 can rotate around the machine body 2; the second end of the supporting rod 1 is connected with a sliding wheel 101, and the sliding wheel 101 can drive the whole device to slide on the ground; the first end of the supporting rod 1 is hinged with the first end of a damping spring 3, the first end of the damping spring 3 is hinged with the supporting rod 1 through a second rotating shaft 5, and the first end of the damping spring 3 can rotate around the supporting rod 1; the second end of damping spring 3 and organism 2 can be dismantled and be connected, first through-hole 301 has been seted up to damping spring 3's second end, first screw 203 is installed to the lateral wall of organism 2, install first screw 204 in the first screw 203, and first screw 204 runs through first through-hole 301 and first screw 203 spiro union, when using, pass first screw 204 first through-hole 301 and screw up with first screw 203 spiro union, damping spring 3's second end and organism 2 fixed connection this moment, when needs are folding, take out first screw 204 from first through-hole 301 and first screw 203, dismantle between damping spring 3's the second end and the organism 2 and open, as figure 5.

Two ends of the machine body 2 are respectively provided with a fixed block 7, a first connecting rod 4 is arranged on the machine body 2 at one side of each fixed block 7, the first connecting rods 4 are connected with the machine body 2 in a sliding manner, and the first connecting rods 4 can slide left and right on the machine body 2; first chute 202 has been seted up to the organism 2 below of fixed block 7 one side, second spout 201 has all been seted up to the both sides of first spout 202, first connecting rod 4 slides in first spout 202 and second spout 201, the first end of first connecting rod 4 is T type structure, the horizontal pole of T type structure slides from side to side in first spout 202 and second spout 201, second screw 701 has been seted up on fixed block 7, install lead screw 702 in the second screw 701, lead screw 702 and the spiro union of second screw 701 have been seted up on first connecting rod 4, lead screw 702 and second through-hole 401 rotate the connection, lead screw 702 only rotates in second through-hole 401 and does not slide, lead screw 702 runs through second through-hole 401 and second screw 701 spiro union, rotate lead screw 702, can drive first connecting rod 4 and move left or right, lead screw 702 moves left or right in second screw 701 simultaneously, as figure 2.

The supporting rod 1 is provided with a first groove 102, the damping spring 3 is detachably clamped in the first groove 102, when the supporting rod needs to be folded, the damping spring 3 can be clamped in the first groove 102, and when the supporting rod does not need to be folded, the damping spring 3 can be taken out of the first groove 102; the protection device 6 comprises a protective net 601, a T-shaped connecting rod 602 and a second connecting rod 603; the machine body 2 on both sides of the propeller is provided with third sliding grooves 206, T-shaped connecting rods 602 are arranged in the two third sliding grooves 206, the cross rods of the T-shaped connecting rods 602 slide in the third sliding grooves 206, and the cross rods of the T-shaped connecting rods 602 can slide up and down in the third sliding grooves 206; the protective net 601 is mounted on a vertical rod of the T-shaped connecting rod, the movement of a cross rod of the T-shaped connecting rod 602 drives the protective net 601 to move together, the side wall of the vertical rod of the T-shaped connecting rod 602 is connected with a first end of a second connecting rod 603, a second end of the second connecting rod 603 is detachably connected with a lead screw 702, when the unmanned aerial vehicle is used, the second end of the second connecting rod 603 is fixedly connected with the lead screw 702, and when the unmanned aerial vehicle needs to be folded, the second end of the second connecting rod 603 and the lead screw 702 can be detached; a third screw hole 604 is formed in the second end of the second connecting rod 603, the lead screw 702 is in threaded connection with the third screw hole 604, when the unmanned aerial vehicle needs to be used, the lead screw 702 penetrates through the third screw hole 604, the second through hole 401 and the second screw hole 701, and the lead screw 702 and the second end of the second connecting rod 603 are in a threaded connection state; when the unmanned aerial vehicle needs to be folded, the screw rod 702 is screwed to move the screw rod 702 to the right, when the screw rod 702 comes out of the third screw hole 604, the second ends of the screw rod 702 and the second connecting rod 603 are detached, then the screw rod 702 is adjusted, the screw rod 702 drives the first connecting rod 4 to move, and the support rod 1 is adjusted to be placed on the first connecting rod 4 by rotating the screw rod 702 forwards and reversely, as shown in fig. 3.

The utility model discloses a working process:

when the unmanned aerial vehicle is used, the screw 702 is adjusted, the support rod 1 is taken down from the first connecting rod 4, the damping spring 3 is taken out from the first groove 102, the first screw 204 penetrates through the first through hole 301 and is screwed with the first screw hole 203, at the moment, the support rod 1, the machine body 2 and the damping spring 3 are in a fixed state, the screw 702 is screwed reversely, the screw 702 moves rightwards, the cross rod of the T-shaped connecting rod 602 is placed into the third sliding groove 206, the T-shaped connecting rod 602 slides downwards, the T-shaped connecting rod 602 drives the protective net 601 and the second connecting rod 603 to move downwards, when the T-shaped connecting rod 602 slides to the bottom of the third sliding groove 206, the screw 702 is screwed forwards, the screw 702 is screwed with the third screw hole 604 until the screw 702 penetrates through the third screw hole 604, at the moment, the second connecting rod 603, the protective net 601 and the T-shaped connecting rod 602 are in a fixed state, the unmanned aerial vehicle can be used, when the unmanned aerial vehicle is used, the screw 702 is screwed backwards, the screw 702 is moved out from the third screw hole 604, at the second connecting rod 603 and the second connecting rod 603, the protective net 603 and the support rod 603 and the T-shaped connecting rod 602 and the damping spring 3 are taken out, and the first connecting rod 3 and the first connecting rod 702 are taken out, and the first groove 102, and the damping spring 3, and the first groove 102 are taken out, and the damping spring 3, and the first groove 102, and the second groove 102 are taken out, and the damping spring 3 are taken out.

The above description is only for the preferred embodiment of the present invention, and is not intended to limit the present invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included within the protection scope of the present invention.

Claims

1. An anti-collision unmanned aerial vehicle is characterized by comprising a support rod (1) and a vehicle body (2); a protective device (6) is arranged on the outer side of the propeller on the machine body (2), and the protective device (6) is detachably connected with the machine body (2); the camera both sides of organism (2) below all articulate the first end that has bracing piece (1), the second end of bracing piece (1) is connected with movable pulley (101), the first end of bracing piece (1) articulates the first end that has damping spring (3), the second end and organism (2) of damping spring (3) are the connection of dismantling.

2. An unmanned aerial vehicle for collision avoidance according to claim 1, wherein the second end of the damping spring (3) is provided with a first through hole (301), the side wall of the machine body (2) is provided with a first screw hole (203), a first screw rod (204) is arranged in the first screw hole (203), and the first screw rod (204) penetrates through the first through hole (301) and is in threaded connection with the first screw hole (203).

3. An anti-collision unmanned aerial vehicle according to claim 1, wherein fixing blocks (7) are arranged at two ends of the machine body (2), a first connecting rod (4) is arranged on the machine body (2) on one side of each fixing block (7), and the first connecting rods (4) are slidably connected with the machine body (2).

4. An anti-collision unmanned aerial vehicle according to claim 3, wherein a first sliding groove (202) is arranged below the body (2) on one side of the fixing block (7), second sliding grooves (201) are arranged on two sides of the first sliding groove (202), and the first connecting rod (4) slides in the first sliding groove (202) and the second sliding grooves (201).

5. The unmanned aerial vehicle of claim 3, wherein a second screw hole (701) is formed in the fixing block (7), a lead screw (702) is arranged in the second screw hole (701), a second through hole (401) is formed in the first connecting rod (4), the lead screw (702) is rotatably connected with the second through hole (401), and the lead screw (702) penetrates through the second through hole (401) and is in threaded connection with the second screw hole (701).

6. The unmanned aerial vehicle of claim 1, wherein the support rod (1) is provided with a first groove (102), and the damping spring (3) is detachably clamped in the first groove (102).

7. An anticollision unmanned aerial vehicle according to claim 1, the first end of the support rod (1) and the body (2) are hinged through a first rotating shaft (8), and the first end of the damping spring (3) and the support rod (1) are hinged through a second rotating shaft (5).

8. An unmanned aerial vehicle for collision avoidance according to claim 5, said guard (6) comprising a protective mesh (601), a T-shaped connecting rod (602), a second connecting rod (603); all be equipped with third spout (205), two on organism (2) of screw both sides all be equipped with T type connecting rod (602) in third spout (205), and the horizontal pole of T type connecting rod (602) slides in third spout (205), be equipped with protection network (601) on the montant of T type connecting rod, the montant lateral wall of T type connecting rod (602) is connected with the first end of second connecting rod (603), the second end and lead screw (702) of second connecting rod (603) can be dismantled and connect.

9. An unmanned aerial vehicle according to claim 8, wherein the second end of the second connecting rod (603) is provided with a third screw hole (604), and the screw rod (702) and the third screw hole (604) are screwed.