CN205033892U - Empty track unmanned aerial vehicle that uses in land - Google Patents
Empty track unmanned aerial vehicle that uses in land Download PDFInfo
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- CN205033892U CN205033892U CN201520827068.7U CN201520827068U CN205033892U CN 205033892 U CN205033892 U CN 205033892U CN 201520827068 U CN201520827068 U CN 201520827068U CN 205033892 U CN205033892 U CN 205033892U
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Abstract
The utility model discloses an empty track unmanned aerial vehicle that uses in land, including the frame, the both sides of frame respectively are equipped with two horns, all are equipped with the screw on each horn, the both sides of frame all be equipped with the track with be used for fixed track and with the detachable track support piece who is connected of frame. The utility model discloses the land of realizing unmanned aerial vehicle is empty dual -purpose, and convenient the dismantlement and the installation is avoided a certain track support piece to damage and is leaded to scrapping of whole unmanned aerial vehicle simultaneously.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, is specifically related to a kind of land sky crawler belt unmanned plane.
Background technology
Unmanned plane comes across the twenties in 20th century the earliest, is at that time to use as the target drone of training.That many country is for describing the term of latest generation robot airplane.From literal, this term can describe from kite, drone, to the cruise missile that V-1 fly bomb comes from development, but in the term of the military, is only limitted to reusable heavier-than-air aircraft.Unmanned plane is of many uses, and cost is low, and efficiency-cost ratio is good; Risk that no one was injured; Viability is strong, and maneuvering performance is good, easy to use, has extremely important effect, more hold out broad prospects at civil area in modern war.
Four-axle aircraft, also known as quadrotor, four-rotor helicopter, is called for short four axles, four rotors.This four-axle aircraft (Quadrotor) is a kind of multi-rotor aerocraft.Four screw propellers of four-axle aircraft are all the simple mechanisms of motor direct-connected, and criss cross layout allows aircraft to obtain the power of main body turning by changing motor speed, thus adjusts self attitude.Concrete ins and outs are told about in " basic exercise principle ".Because the complexity that it is intrinsic, never there is large-scale commercial four-axle aircraft in history.Have benefited from the development of micro electronmechanical control technology in recent years, stable four-axle aircraft obtains to be paid close attention to widely, and application prospect is very considerable.There are Chinese great Jiang Creative Company, French Parrot company, German AscTec company and 3DRobotics company of the U.S. in four-axle aircraft company more well-known in the world.Four-axle aircraft can be in vertical motion, luffing, rolling movement, yawing rotation.
But general unmanned plane cannot accomplish land and air double-used unmanned plane, under some complicated unknown spatial domains and harsher wind conditions, flight has certain risk.Difficulty and certain economic loss is caused to border patrol, nuclear radiation detection, aerial photography, mineral exploration aviation, the condition of a disaster supervision, traffic patrolling, security monitoring etc.
Summary of the invention
The utility model is intended at least to solve one of technical matters existed in prior art.For this reason, the utility model provides a kind of land sky crawler belt unmanned plane, and object is realize unmanned plane land and air double-used, simultaneously for convenience detach and install.
To achieve these goals, the technical scheme that the utility model is taked is:
A kind of land sky uses crawler belt unmanned plane, and comprise frame, the both sides of frame are respectively provided with two horns, and each horn is equipped with screw propeller, the track support that the both sides of described frame are equipped with crawler belt and removably connect for fixing crawler belt and with frame.
The described mode removably connected is clamping.
Described unmanned plane also comprises the spacing ring being located at frame and track support access section.
Described track support is the ox angled construction of inner hollow.
The surrounding of described frame is equipped with infrared exoelectron camera.
Described unmanned plane also comprises the warning device be located in frame.
Described frame is also provided with solar panels.
The material of described track support is ABS resin material.
The beneficial effects of the utility model: the utility model realizes the land and air double-used of unmanned plane, for convenience detach and installation simultaneously, avoid some track supports to damage and cause scrapping of whole unmanned plane, track support is designed to the ox angled construction of hollow, optimize the integral structure of unmanned plane further, reduce crawler belt mounting material, simply, raw MAT'L is saved in a large number, and then alleviate the load capacity of overall unmanned plane, the lift-off of unmanned plane is flown be more prone to, also there is the effect of more stable fixing crawler belt simultaneously.
Accompanying drawing explanation
This specification sheets comprises the following drawings, shown content respectively:
Fig. 1 is the structural representation of the utility model land sky crawler belt unmanned plane;
Fig. 2 is the lateral plan of the utility model land sky crawler belt unmanned plane.
Be labeled as in figure:
1, frame, 2, horn, 3, screw propeller, 4, crawler belt, 5, track support, 6, upper cover plate, 7, lower cover, 8, roller, 9, screw propeller drive motor.
Detailed description of the invention
Contrast accompanying drawing below, by the description to embodiment, be described in further detail detailed description of the invention of the present utility model, object helps those skilled in the art to have more complete, accurate and deep understanding to design of the present utility model, technical scheme, and contribute to its enforcement.
As shown in Figure 1 to Figure 2, a kind of land sky uses crawler belt unmanned plane, comprise frame 1, frame comprises upper cover plate 6 and lower cover 7, the both sides of frame are respectively provided with two horns 2, and each horn 2 is equipped with screw propeller 3, and screw propeller is driven by screw propeller drive motor 9, propeller rotational is made to drive unmanned plane to take off, the track support 5 that the both sides of frame 1 are equipped with crawler belt 4 and removably connect for fixing crawler belt and with frame 1.Preferably, the mode removably connected is clamping.Concrete snap fit can be: four track supports are connected to four end points places of upper cover plate 6, other four track supports are connected to four end points places of lower cover, conveniently clamping, four end points places of upper cover plate 6 and four end points places of lower cover 7 are equipped with the auxiliary section coordinating track support clamping.In order to ensure the firm effect of access section, detouchable spacing ring can also be provided with in access section.Certainly, spacing ring should take the material of lighter weight, such as ABS resin material.In order to realize light weight design, frame 1 can utilize carbon fiber frame, and complete machine frame quality is less, alleviates complete machine weight greatly, ensures certain intensity simultaneously.
Track support 5 is the ox angled construction of inner hollow.The point of each ox angled construction and corresponding upper cover plate and lower cover clamping, the other end can be fixed for the roller 8 driving caterpillar drive, each roller place all can arrange a roller drive motor and drive, but in order to alleviate the overall weight of unmanned plane, the track support 5 being positioned at frame the same side can arrange two roller drive motor in one end of fixed idler whell, roller can comprise two driving wheels be connected with two roller drive motor, two other is flower wheel, driving wheel is driven to rotate by roller drive motor, through the transmission of flower wheel, realize crawler belt and drive unmanned plane land mobile.The material of track support is ABS resin material.Adopt ABS resin material, its impact resistance, resistance to effect of heat, low temperature resistance, chemical proofing and excellent electrical properties, also there is the features such as easy processing, product size is stable, surface gloss property is good.Resin material is enough slim and graceful simultaneously, and rigidity is moderate.This track support can adopt 3D printing technique to make.Flight controller can make use of OpenPilotCC3D flight controller ripe on market.
The surrounding of frame 1 is equipped with infrared exoelectron camera.The design of this structure is convenient to unmanned plane and is gathered image, can detect target environment as required and photograph.Unmanned plane can also comprise the warning device be located in frame.When unmanned plane collects more special picture signal, this picture signal can be delivered in controller and process, be judged by controller, if belong to the state that can report to the police, controller controls warning device and reports to the police, and provides warning to user.
The upper cover plate of frame 1 can also be provided with solar panels.The design of this structure can continue to ensure the position fixing system proper motion in unmanned plane, and convenient when electricity deficiency appears in unmanned plane, user can find in time, prevents the loss of unmanned plane.
Below by reference to the accompanying drawings the utility model is exemplarily described.Obviously, the utility model specific implementation is not subject to the restrictions described above.As long as have employed the improvement of the various unsubstantialities that method of the present utility model is conceived and technical scheme is carried out; Or without improvement, above-mentioned design of the present utility model and technical scheme directly applied to other occasion, all within protection domain of the present utility model.
Claims (8)
1. a land sky uses crawler belt unmanned plane, comprise frame, the both sides of frame are respectively provided with two horns, each horn is equipped with screw propeller, it is characterized in that: the track support that the both sides of described frame are equipped with crawler belt and removably connect for fixing crawler belt and with frame.
2. land sky uses crawler belt unmanned plane according to claim 1, it is characterized in that: described in the mode that removably connects be clamping.
3. land sky uses crawler belt unmanned plane according to claim 2, it is characterized in that: described unmanned plane also comprises the spacing ring being located at frame and track support access section.
4. land sky uses crawler belt unmanned plane according to claim 1, it is characterized in that: described track support is the ox angled construction of inner hollow.
5. land sky uses crawler belt unmanned plane according to claim 1, it is characterized in that: the surrounding of described frame is equipped with infrared exoelectron camera.
6. land sky uses crawler belt unmanned plane according to claim 5, it is characterized in that: described unmanned plane also comprises the warning device be located in frame.
7. land sky uses crawler belt unmanned plane according to claim 1, it is characterized in that: described frame is also provided with solar panels.
8. land sky uses crawler belt unmanned plane according to claim 1, it is characterized in that: the material of described track support is ABS resin material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520827068.7U CN205033892U (en) | 2015-10-21 | 2015-10-21 | Empty track unmanned aerial vehicle that uses in land |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520827068.7U CN205033892U (en) | 2015-10-21 | 2015-10-21 | Empty track unmanned aerial vehicle that uses in land |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205033892U true CN205033892U (en) | 2016-02-17 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520827068.7U Active CN205033892U (en) | 2015-10-21 | 2015-10-21 | Empty track unmanned aerial vehicle that uses in land |
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| CN (1) | CN205033892U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106696619A (en) * | 2017-01-09 | 2017-05-24 | 南京理工大学 | Fortress-type track four-rotor aircraft |
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2015
- 2015-10-21 CN CN201520827068.7U patent/CN205033892U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106696619A (en) * | 2017-01-09 | 2017-05-24 | 南京理工大学 | Fortress-type track four-rotor aircraft |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |