CN216805794U

CN216805794U - Unmanned aerial vehicle with stable flight

Info

Publication number: CN216805794U
Application number: CN202123177399.5U
Authority: CN
Inventors: 马婧雯
Original assignee: Shandong Rundong Aerospace Technology Co ltd
Current assignee: Shandong Rundong Aerospace Technology Co ltd
Priority date: 2021-12-16
Filing date: 2021-12-16
Publication date: 2022-06-24
Anticipated expiration: 2031-12-16

Abstract

The utility model discloses an unmanned aerial vehicle with stable flight, which comprises a body, wherein wings are fixedly arranged on two sides of the body, a propeller is rotatably arranged at one end of the tops of the wings, supporting frames are fixedly arranged on two sides of the bottom of the body, an anti-toppling supporting leg is connected and arranged on one side of each supporting frame, a limiting rod is fixedly arranged on the inner side of each supporting frame, and a spring is sleeved at one end of each limiting rod; prevent empting the stabilizer blade through installing at this unmanned aerial vehicle's the bracing frame, prevent empting the stability that the organism can be guaranteed to the stabilizer blade through installing, and prevent empting the stabilizer blade and pass through spacing installation, can play certain cushioning effect through preventing empting the stabilizer blade and spring, and when unmanned aerial vehicle flies usually, preheat the structure through the surface mounting at this camera, when this unmanned aerial vehicle flies, if the surperficial fog that produces of camera, the accessible preheats the structure and produces the heat, through preheating the structure with the fog evaporation on camera surface, produce certain influence when avoiding the camera to use.

Description

Unmanned aerial vehicle with stable flight

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle with stable flight.

Background

An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either fully or intermittently, by an onboard computer. Unmanned aircraft are often more suited to tasks that are too "fool, messy, or dangerous" than manned aircraft. Unmanned aerial vehicles can be classified into military and civilian applications. For military use, unmanned aerial vehicles are divided into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industrial application are really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries also actively expand the industrial application and develop the unmanned aerial vehicle technology.

The stable unmanned aerial vehicle of current flight, when unmanned aerial vehicle is using usually, when the unmanned aerial vehicle of flight when descending, if ground unevenness, perhaps the organism stops the slope after, leads to this unmanned aerial vehicle to empty easily, influences the stability of placing, parks the easy unstable problem of in-process at unmanned aerial vehicle, we propose a stable unmanned aerial vehicle of flight for this reason.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide an unmanned aerial vehicle with stable flight, and aims to solve the problems that when the unmanned aerial vehicle is used and the flying unmanned aerial vehicle lands, if the ground is uneven or the body of the unmanned aerial vehicle inclines after stopping, the unmanned aerial vehicle is prone to toppling, placement stability is affected, and the unmanned aerial vehicle is prone to instability in the process of stopping.

In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an unmanned aerial vehicle that flight is stable, includes the organism, the both sides fixed mounting of organism has the wing, just the top one end of wing is rotated and is installed the screw, the bottom both sides fixed mounting of organism has the support frame, one side of support frame is connected and has been installed and is prevented empting the stabilizer blade, the inboard fixed gag lever post of having installed of support frame, the pot head of gag lever post is established and is installed the spring, the other end of preventing empting the stabilizer blade is provided with the stop collar of integral type, the one end of preventing empting the stabilizer blade is established spacingly on the gag lever post through the stop collar cover.

Preferably, the bottom of the machine body is fixedly provided with a camera, the front surface of the camera is provided with a preheating ring, the inner side of the preheating ring is provided with a mica sheet, and the inner side of the mica sheet is embedded with an electric heating wire.

Preferably, two heating wires are wound on the inner side of the preheating ring.

Preferably, the supporting frame and the other end of the anti-toppling support leg are both provided with rubber pads.

Preferably, the installation inclination angle between the anti-toppling support leg and the support frame is thirty degrees, and the support frame is parallel to the bottom of the anti-toppling support leg.

Preferably, the bottom of the machine body is provided with four support frames, and the four support frames are provided with anti-toppling support legs.

Compared with the prior art, the utility model has the beneficial effects that:

(1) when the unmanned aerial vehicle is used, when the flying unmanned aerial vehicle lands, if the ground is uneven or the unmanned aerial vehicle body inclines after stopping, the unmanned aerial vehicle body is easy to topple over to influence the placing stability;

(2) when unmanned aerial vehicle flies usually, because unmanned aerial vehicle can fly at certain height, if air temperature is low in the air, can lead to producing the fog on the lens of camera, the shooting effect when influence flight, preheat the structure through the surface mounting at this camera, when this unmanned aerial vehicle flies, if the surface of camera produces the fog, the accessible preheats the structure and produces the heat, through preheating the structure with the fog evaporation on camera surface, produce certain influence when avoiding the camera to use.

Drawings

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

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

FIG. 3 is a schematic view of the structure of the camera of the present invention;

in the figure: 1. a body; 2. a propeller; 3. an airfoil; 4. a camera; 5. a support frame; 6. the anti-toppling support leg; 7. a spring; 8. a limiting sleeve; 9. a limiting rod; 10. preheating a ring; 11. mica sheets; 12. an electric heating wire.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1, fig. 2 and fig. 3, the present invention provides a technical solution: an unmanned aerial vehicle with stable flight comprises a machine body 1, wings 3 are fixedly arranged on two sides of the machine body 1, and one end of the top of the wing 3 is rotatably provided with a propeller 2, two sides of the bottom of the machine body 1 are fixedly provided with a support frame 5, one side of the support frame 5 is connected with an anti-toppling support leg 6, the inner side of the support frame 5 is fixedly provided with a limit rod 9, one end of the limit rod 9 is sleeved with a spring 7, the other end of the anti-toppling support leg 6 is provided with an integrated limit sleeve 8, one end of the anti-toppling support leg 6 is sleeved and limited on the limit rod 9 through the limit sleeve 8, by installing the anti-toppling support leg 6 on the support frame 5 of the unmanned aerial vehicle, the stability of the machine body 1 can be ensured through the installed anti-toppling support leg 6, can play certain cushioning effect through preventing empting stabilizer blade 6 and spring 7, guarantee the stability when this unmanned aerial vehicle parks, prevent to empty.

For better use, in this embodiment, preferably, the bottom of the machine body 1 is fixedly provided with the camera 4, the front surface of the camera 4 is provided with the preheating ring 10, the inner side of the preheating ring 10 is provided with the mica sheet 11, the inner side of the mica sheet 11 is embedded with the heating wire 12, mist can be prevented from being generated on the front surface of the camera 4 through the heating wire 12, for better evaporation of the mist, in this embodiment, preferably, the inner side of the preheating ring 10 is wound with two heating wires 12, so as to improve evaporation efficiency of the mist, for better placement, in this embodiment, preferably, the supporting frame 5 and the other end of the anti-toppling supporting leg 6 are both provided with rubber pads, so as to ensure that the machine body 1 is stably supported on the ground, for better support, in this embodiment, preferably, the installation inclination angle between the anti-toppling supporting leg 6 and the supporting frame 5 is thirty degrees, and the supporting frame 5 is parallel to the bottom of the anti-toppling supporting leg 6, for more stable placement, in the present embodiment, preferably, four supporting frames 5 are installed at the bottom of the machine body 1, and anti-toppling supporting legs 6 are installed on all the four supporting frames 5, so that the machine body can be prevented from toppling in multiple angles.

The working principle and the using process of the utility model are as follows: when the unmanned aerial vehicle is in use, when the flying unmanned aerial vehicle lands, if the ground is uneven, or the body 1 tilts after stopping, the body 1 is easy to topple and the placing stability is affected, by installing the anti-toppling support leg 6 on the support frame 5 of the unmanned aerial vehicle, if the body 1 tilts after stopping, the body 1 can be supported by the anti-toppling support leg 6, the other end of the anti-toppling support leg 6 during supporting can be extruded on the limit rod 9 through the limit sleeve 8 for limiting movement, meanwhile, the spring 7 is extruded, the spring 7 deforms under stress to generate buffer action force, the stability of the body 1 can be ensured by the installed anti-toppling support leg 6, and the anti-toppling support leg 6 plays a certain buffer action through limiting installation, the stability when the unmanned aerial vehicle is parked is ensured, and generally, when the unmanned aerial vehicle flies, because no person can fly at a certain height, if the air temperature is low in the air, fog can be generated on the lens of the camera 4, the shooting effect when influence flight, through the surface mounting at camera 4 preheats ring 10, preheats the inboard of ring 10 and install heating wire 12 around establishing, when this unmanned aerial vehicle flight, if preheat the surface production fog of ring 10, heating wire 12 can turn into heat energy production heat with the electric energy, evaporates through preheating the fog on structure with camera 4 surface, avoids camera 4 to receive the influence of fog when using.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments 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. The utility model provides an unmanned aerial vehicle that flight is stable, includes organism (1), the both sides fixed mounting of organism (1) has wing (3), just screw (2), its characterized in that are installed in the rotation of top one end of wing (3): the utility model discloses a prevent machine body, including organism (1), bottom both sides fixed mounting have support frame (5), one side of support frame (5) is connected and has been installed and prevent empting stabilizer blade (6), the inboard fixed gag lever post (9) of having installed of support frame (5), the pot head of gag lever post (9) is established and is installed spring (7), the other end that prevents empting stabilizer blade (6) is provided with stop collar (8) of integral type, the one end of preventing empting stabilizer blade (6) is established the limit on gag lever post (9) through stop collar (8) cover.

2. A drone of claim 1, which is stable in flight and characterized in that: the utility model discloses a preheating machine, including organism (1), the bottom fixed mounting of organism (1) has camera (4), preheating ring (10) have been installed to the front surface of camera (4), mica sheet (11) have been installed to the inboard of preheating ring (10), the inboard of mica sheet (11) is inlayed and is installed heating wire (12).

3. A drone of claim 2, which is stable in flight and characterized in that: two heating wires (12) are wound on the inner side of the preheating ring (10).

4. A drone of claim 1, which is stable in flight and characterized in that: rubber pads are arranged at the other ends of the supporting frame (5) and the anti-toppling support leg (6).

5. A drone of claim 1, which is stable in flight and characterized in that: the installation inclination angle between the anti-toppling supporting leg (6) and the supporting frame (5) is thirty degrees, and the supporting frame (5) is parallel to the bottom of the anti-toppling supporting leg (6).

6. A drone of claim 1, which is stable in flight and characterized in that: the bottom of the machine body (1) is provided with four support frames (5), and the four support frames (5) are provided with anti-toppling support legs (6).