CN218806711U

CN218806711U - Formula horn is inserted soon to unmanned aerial vehicle

Info

Publication number: CN218806711U
Application number: CN202222418469.XU
Authority: CN
Inventors: 付晓亮
Original assignee: Shenzhen Beinuosi Technology Co ltd
Current assignee: Shenzhen Beinuosi Technology Co ltd
Priority date: 2022-09-13
Filing date: 2022-09-13
Publication date: 2023-04-07
Anticipated expiration: 2032-09-13

Abstract

The utility model discloses an unmanned aerial vehicle is with inserting formula horn soon, including unmanned aerial vehicle combined mechanism, stop gear, elasticity block mechanism and side protection machanism, unmanned aerial vehicle combined mechanism's the left and right sides is provided with stop gear, and stop gear's inside is provided with elasticity block mechanism, the end of elasticity block mechanism is provided with side protection machanism, elasticity block mechanism includes linking arm, mounting groove, baffle, spring unit and stopper, and the pointed end of linking arm is provided with the mounting groove, the inside middle-end of mounting groove is provided with the baffle. This unmanned aerial vehicle is with inserting horn soon, spring unit's setting can be with linking arm embedding to the fixed block in, the spring unit on the linking arm point end and the mutual elastic clamping of spacing groove on the fixed block afterwards, because spring unit block and the spacing inslot on the linking arm for screw hole on linking arm and the fixed block utilizes external fastening screw to carry out the rotation to it each other, and is fixed.

Description

Formula horn is inserted soon to unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle is with inserting formula horn soon.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. And unmanned aerial vehicle's rotor generally sets up on the horn, and unmanned aerial vehicle generally has a plurality of horns, receives weather and environmental impact, and the horn often can break down in the use, needs timely maintenance or change.

As in application No.: CN202120491041.0, the utility model discloses an unmanned aerial vehicle fast-insertion type horn, which comprises a body, two first fixed blocks are symmetrically fixed at two ends of the body, a first limit groove is respectively arranged in the two first fixed blocks, the horn is arranged on one side of the first fixed block, a limit block is fixed at one end of the horn, a plurality of clamping grooves are equidistantly arranged in the bottom end of the limit block, and the limit block is embedded into the first limit groove; through the first fixed block, the extrusion piece, the sliding block, the fixture block, the stopper, the spring, first sliding tray, the second sliding tray, the third sliding tray, the draw-in groove, first spacing groove of design, make things convenient for quick installation and the dismantlement of horn, this kind of structure of inserting soon has saved the time, has improved work efficiency, keeps off lid, fourth sliding tray, connecting block, plastic pellet, second spacing groove through the design, can avoid the extrusion piece to be pressed easily.

An unmanned aerial vehicle horn similar to the above application still has following not enough at present:

unmanned aerial vehicle horn on the market in use structure is complicated, and the horn dismouting is comparatively inconvenient, wastes time and energy, and whole volume is great, is difficult for carrying, for this, we propose an unmanned aerial vehicle with inserting formula horn soon.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle is with inserting formula horn soon to solve the unmanned aerial vehicle horn in use structure that proposes in the above-mentioned background art complicated, the horn dismouting is comparatively inconvenient, wastes time and energy, and whole volume is great, the difficult problem of carrying.

In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle is with formula horn of inserting soon, includes unmanned aerial vehicle combined mechanism, stop gear, elasticity block mechanism and side protection machanism, unmanned aerial vehicle combined mechanism's the left and right sides is provided with stop gear, and stop gear's inside is provided with elasticity block mechanism, elasticity block mechanism's end is provided with side protection machanism, elasticity block mechanism includes linking arm, mounting groove, baffle, spring assembly and stopper, and the pointed end of linking arm is provided with the mounting groove, the inside middle-end of mounting groove is provided with the baffle, and the upper and lower both sides of baffle are provided with spring assembly, spring assembly's pointed end is provided with the stopper.

Furthermore, the connecting arm forms an elastic structure with the limiting mechanism through the spring assembly, and the spring assembly is tightly attached to the connecting arm.

Further, stop gear includes fixed block, inside groove, spacing groove and screw hole, and the middle part of fixed block is provided with the inside groove, the upper and lower both sides of fixed block are provided with the spacing groove, and the avris of spacing groove is provided with the screw hole.

Furthermore, the fixing block wraps the elastic clamping mechanism, and the threaded hole is communicated with the elastic clamping mechanism.

Further, side protection mechanism includes rotating assembly, protection casing and fastener, and rotating assembly's bottom is provided with the protection casing, the bottom of protection casing is provided with the fastener.

Furthermore, the protection casing is in the shape of hollow 'L', and the protection casing passes through the fastener and constitutes the helicitic texture with rotating assembly.

Further, unmanned aerial vehicle combined mechanism includes organism, frame and rubber pad, and the bottom of organism is provided with the frame, the bottom of frame is provided with the rubber pad.

Compared with the prior art, the beneficial effects of the utility model are that: this formula horn is inserted soon to unmanned aerial vehicle, spring unit's setting can be with linking arm embedding to the fixed block in, the spring unit on the linking arm point end afterwards and the mutual elastic clamping in spacing groove on the fixed block, because spring unit block and spacing inslot on the linking arm for screw hole on linking arm and the fixed block is to it each other, utilizes external fastening screw to carry out the rotation fixed.

The linking arm passes through spring unit and stop gear constitutes elastic construction, can imbed the linking arm to the fixed block in through spring unit's setting, and the spring unit on the linking arm is pointed at afterwards and the mutual elastic block of spacing groove on the fixed block, and the linking arm can effectively be fixed to the fastening screw of collocation, and the stopper can play the effect that resets through the spring unit in the mounting groove, makes things convenient for the connection of linking arm, and overall structure is simple, and it is comparatively convenient to peg graft, portable.

The fixed block is wrapping up elasticity block mechanism, when the linking arm is embedded into to the fixed block inside, because spring unit block and spacing inslot on the linking arm for screw hole on linking arm and the fixed block is to it each other, utilizes external fastening screw to carry out the rotation fixed, and the combination effect between reinforcing linking arm and the fixed block improves stability between them, avoids taking place the danger that drops because of external factor when using, improves the security.

Drawings

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

FIG. 2 is a schematic view of a partial enlarged structure at A in FIG. 1 according to the present invention;

fig. 3 is a schematic view of the three-dimensional structure of the limiting mechanism of the present invention.

In the figure: 1. an unmanned aerial vehicle combination mechanism; 101. a body; 102. a frame; 103. a rubber pad; 2. a limiting mechanism; 201. a fixed block; 202. an inner tank; 203. a limiting groove; 204. a threaded hole; 3. an elastic clamping mechanism; 301. a connecting arm; 302. mounting grooves; 303. a partition plate; 304. a spring assembly; 305. a limiting block; 4. a side protection mechanism; 401. a rotating assembly; 402. a protective cover; 403. a fastener.

Detailed Description

As shown in fig. 1, a quick-insertion type horn for an unmanned aerial vehicle includes: unmanned aerial vehicle combined mechanism 1, the left and right sides of unmanned aerial vehicle combined mechanism 1 is provided with stop gear 2, and stop gear 2's inside is provided with elasticity block mechanism 3, the end of elasticity block mechanism 3 is provided with side protection mechanism 4, unmanned aerial vehicle combined mechanism 1 includes organism 101, frame 102 and rubber pad 103, and the bottom of organism 101 is provided with frame 102, the bottom of frame 102 is provided with rubber pad 103, side protection mechanism 4 includes rotating assembly 401, protection casing 402 and fastener 403, and rotating assembly 401's bottom is provided with protection casing 402, the bottom of protection casing 402 is provided with fastener 403, protection casing 402 is cavity ' L ' form, and protection casing 402 passes through fastener 403 and rotating assembly 401 constitution helicitic texture, protection casing 402 encloses the cover through fastener 403 and installs in the below of rotating assembly 401, when taking or holding unmanned aerial vehicle, can protect the hand not hindered by the screw, also can avoid the injury to the screw, still can make unmanned aerial vehicle's flight resistant and impact, increase the protection.

As shown in fig. 2, a formula horn is inserted soon to unmanned aerial vehicle, the end of elasticity block mechanism 3 is provided with side protection mechanism 4, elasticity block mechanism 3 includes linking arm 301, mounting groove 302, baffle 303, spring unit 304 and stopper 305, and the most advanced of linking arm 301 is provided with mounting groove 302, the inside middle-end of mounting groove 302 is provided with baffle 303, and the upper and lower both sides of baffle 303 are provided with spring unit 304, spring unit 304's most advanced is provided with stopper 305, linking arm 301 passes through spring unit 304 and constitutes elastic construction with stop mechanism 2, and closely laminate between spring unit 304 and the linking arm 301, can imbed linking arm 301 to fixed block 201 in through spring unit 304's setting, spring unit 304 on the most advanced of linking arm 301 and the mutual elastic clamping of the spacing groove 203 on the fixed block 201 afterwards, collocation fastening screw can effectively fix linking arm 301, and stopper 305 can play the effect of reseing through the spring unit 304 in mounting groove 302, make things convenient for the connection of linking arm 301, overall structure is simple, it is comparatively convenient to peg graft, and convenient to carry.

As shown in fig. 3, a fast-insertion type horn for an unmanned aerial vehicle, the limiting mechanism 2 includes a fixing block 201, an inner groove 202, a limiting groove 203 and a threaded hole 204, the inner groove 202 is disposed in the middle of the fixing block 201, the limiting groove 203 is disposed on the upper and lower sides of the fixing block 201, the threaded hole 204 is disposed on the side of the limiting groove 203, the elastic clamping mechanism 3 is wrapped on the fixing block 201, and the threaded hole 204 and the elastic clamping mechanism 3 are communicated with each other, when the connecting arm 301 is embedded into the fixing block 201, because the spring assembly 304 on the connecting arm 301 is clamped in the limiting groove 203, the connecting arm 301 and the threaded hole 204 on the fixing block 201 are mutually aligned, and are rotationally fixed by using external fastening screws, so that the combination effect between the connecting arm 301 and the fixing block 201 is enhanced, the stability of the connecting arm and the fixing block is improved, the danger of falling off due to external factors during use is avoided, and the safety is improved.

In conclusion, this unmanned aerial vehicle is with inserting formula horn soon, at first when installing the horn to unmanned aerial vehicle, setting through spring assembly 304 can be with linking arm 301 embedding to fixed block 201 in, the mutual elastic clamping of spacing groove 203 on the most advanced spring assembly 304 of linking arm 301 and the fixed block 201 afterwards, and stopper 305 can play the reset effect through the spring assembly 304 in mounting groove 302, make things convenient for the high-speed joint of linking arm 301, because in spring assembly 304 block and the spacing groove 203 on the linking arm 301, make linking arm 301 and the screw hole 204 on the fixed block 201 to it each other, utilize external fastening screw to carry out the rotation and fix, strengthen the combination effect between linking arm 301 and the fixed block 201, protection casing 402 is installed in the below of rotating assembly 401 through fastener 403 and is enclosed the cover at last, when taking or holding unmanned aerial vehicle, can protect hand not hindered by the screw, also can avoid the injury to the screw, can also make unmanned aerial vehicle's the collision resistant and impact-resistant.

Claims

1. The utility model provides an unmanned aerial vehicle is with inserting horn soon, includes unmanned aerial vehicle combined mechanism (1), stop gear (2), elasticity block mechanism (3) and side protection machanism (4), its characterized in that: the left and right sides of unmanned aerial vehicle combined mechanism (1) is provided with stop gear (2), and the inside of stop gear (2) is provided with elasticity block mechanism (3), the end of elasticity block mechanism (3) is provided with side protection mechanism (4), elasticity block mechanism (3) are including linking arm (301), mounting groove (302), baffle (303), spring unit (304) and stopper (305), and the pointed end of linking arm (301) is provided with mounting groove (302), the inside middle-end of mounting groove (302) is provided with baffle (303), and the upper and lower both sides of baffle (303) are provided with spring unit (304), the pointed end of spring unit (304) is provided with stopper (305).

2. The quick-insertion type horn for the unmanned aerial vehicle according to claim 1, characterized in that: the connecting arm (301) and the limiting mechanism (2) form an elastic structure through the spring assembly (304), and the spring assembly (304) is tightly attached to the connecting arm (301).

3. The quick-insertion type horn for the unmanned aerial vehicle according to claim 1, characterized in that: the limiting mechanism (2) comprises a fixing block (201), an inner groove (202), a limiting groove (203) and a threaded hole (204), the inner groove (202) is arranged in the middle of the fixing block (201), the limiting groove (203) is arranged on the upper side and the lower side of the fixing block (201), and the threaded hole (204) is arranged on the side of the limiting groove (203).

4. The quick-insertion type horn for the unmanned aerial vehicle according to claim 3, characterized in that: the fixed block (201) is wrapped by the elastic clamping mechanism (3), and the threaded hole (204) is communicated with the elastic clamping mechanism (3).

5. The quick-insertion type horn for the unmanned aerial vehicle according to claim 1, characterized in that: the side protection mechanism (4) comprises a rotating assembly (401), a protection cover (402) and a fastener (403), the protection cover (402) is arranged at the bottom of the rotating assembly (401), and the fastener (403) is arranged at the bottom of the protection cover (402).

6. The quick-insertion type horn for the unmanned aerial vehicle according to claim 5, wherein: the protective cover (402) is hollow and L-shaped, and the protective cover (402) and the rotating component (401) form a thread structure through a fastener (403).

7. The quick-insertion type horn for the unmanned aerial vehicle of claim 1, characterized in that: unmanned aerial vehicle combined mechanism (1) includes organism (101), frame (102) and rubber pad (103), and the bottom of organism (101) is provided with frame (102), the bottom of frame (102) is provided with rubber pad (103).