CN215972114U - Unmanned aerial vehicle capable of being parked for long time - Google Patents
Unmanned aerial vehicle capable of being parked for long time Download PDFInfo
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- CN215972114U CN215972114U CN202121344074.9U CN202121344074U CN215972114U CN 215972114 U CN215972114 U CN 215972114U CN 202121344074 U CN202121344074 U CN 202121344074U CN 215972114 U CN215972114 U CN 215972114U
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- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle capable of being parked for a long time, which comprises an unmanned aerial vehicle body and a station mechanism arranged at the bottom of the unmanned aerial vehicle body; the station mechanism comprises two symmetrically arranged undercarriages, and each undercarriage is connected with the unmanned aerial vehicle body through a plurality of support frames; the unmanned aerial vehicle body comprises a body and wings arranged on two sides of the body respectively, wherein each wing is provided with a rotor wing, the body comprises a shell, a camera, a controller, a lithium battery and a solar cell panel, the camera is arranged on the bottom surface of the shell, and the controller and the lithium battery are arranged in the shell; the cruising ability of the unmanned aerial vehicle is improved through a double power supply mode of a lithium battery and a solar panel, and the camera and the rotor wing are preferentially powered by the solar panel; the station height of the unmanned aerial vehicle can be adjusted to meet the optimal height of photography and video shooting and meteorological observation; the streamline design of fuselage can reduce the influence of crosswind to unmanned aerial vehicle to reduce the risk that unmanned aerial vehicle turned on one's side.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle capable of being parked for a long time.
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 completely or intermittently, by an onboard computer.
The multi-rotor electric unmanned aerial vehicle has the great defect that the endurance time is short, and the service functions of the unmanned aerial vehicle are limited to a great extent by the duration time, for example, the functions of long-time photography and shooting, meteorological observation, reconnaissance and the like are difficult to realize.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an unmanned aerial vehicle capable of being located for a long time aiming at the defects in the prior art.
The technical scheme for solving the problems comprises the following steps: an unmanned aerial vehicle capable of being parked for a long time comprises an unmanned aerial vehicle body and a station mechanism arranged at the bottom of the unmanned aerial vehicle body;
the station mechanism comprises two symmetrically arranged undercarriages, and each undercarriage is connected with the unmanned aerial vehicle body through a plurality of support frames;
the unmanned aerial vehicle body includes the fuselage and sets up the wing in the fuselage both sides respectively, is equipped with the rotor on every wing, the fuselage includes the shell, camera, controller, lithium cell, solar cell panel, the camera sets up in the shell bottom surface, controller, lithium cell setting are in the shell, solar cell panel sets up at the shell top surface, lithium cell, solar cell panel connection director, camera, rotor connection director.
Furthermore, each support frame is provided with a support sole, and the support soles are arranged on the support frames in a vertically adjustable manner through the adjusting mechanisms.
Furthermore, the adjusting mechanism comprises a rail, a slider, a push head, a screw rod and a through screw rod motor, the rail is arranged along the support frame and is fixedly connected to the support frame, the through screw rod motor is arranged at the lower end of the rail and is fixed to the support frame, the through screw rod motor is screwed on the screw rod, the push head is arranged at the upper end of the screw rod and is fixedly connected with the slider, the slider is slidably connected to the rail, and the support sole is connected to the bottom end of the screw rod.
Furthermore, a baffle is arranged at the top end of the track.
Furthermore, a level gauge is further arranged in the machine body, and the through type screw rod motor is connected with the controller.
Furthermore, the shell adopts a streamline structure, and the curved surface angle of the bottom surface is larger than that of the top surface.
The utility model has the following beneficial effects:
the utility model provides an unmanned aerial vehicle capable of being parked for a long time, the endurance of the unmanned aerial vehicle is improved through a double power supply mode of a lithium battery and a solar cell panel, and a camera and a rotor wing are preferentially powered by the solar cell panel; the station height of the unmanned aerial vehicle can be adjusted to meet the optimal height of photography and video shooting and meteorological observation; the streamline design of fuselage can reduce the influence of crosswind to unmanned aerial vehicle to reduce the risk that unmanned aerial vehicle turned on one's side.
Drawings
FIG. 1 is a front view of the support sole of the present invention fully stowed;
FIG. 2 is a top view of the support sole of the present invention fully extended;
FIG. 3 is a schematic view of the adjustment mechanism;
FIG. 4 is an electrical control diagram of the present invention;
in the figure: 1-undercarriage, 2-support frame, 3-support sole, 4-track, 5-slide block, 6-push head, 7-screw rod, 8-through screw rod motor, 9-baffle, 10-fuselage, 11-wing, 12-rotor wing, 13-shell, 14-camera, 15-controller, 16-lithium battery, 17-solar panel and 18-level.
Detailed Description
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
As shown in fig. 1 to 4, an unmanned aerial vehicle capable of long-term residence comprises an unmanned aerial vehicle body and a residence mechanism arranged at the bottom of the unmanned aerial vehicle body;
the station mechanism comprises two symmetrically-arranged undercarriage bodies, each undercarriage body is connected with the unmanned aerial vehicle body through two support frames, a support sole is arranged on each support frame, the support soles are arranged on the support frames in an up-and-down adjustable mode through an adjusting mechanism, the adjusting mechanism comprises a rail, a slider, a push head, a lead screw and a through lead screw motor, the rail is arranged along the support frames and is fixedly connected onto the support frames, the through lead screw motor is arranged at the lower end of the rail and is fixed onto the support frames, the through lead screw motor is connected onto the lead screw in a rotating mode, the push head is arranged at the upper end of the lead screw and is fixedly connected with the slider, the slider is connected onto the rail in a sliding mode, a baffle is arranged at the top end of the rail, and the support soles are connected to the bottom end of the lead screw.
The unmanned aerial vehicle body includes the fuselage and sets up the wing in the fuselage both sides respectively, is equipped with the rotor on every wing, the fuselage includes the shell, camera, controller, lithium cell, solar cell panel, the shell adopts streamlined structure and the curved surface angle of bottom surface is greater than the curved surface angle of top surface, so during the air flow, because the flow does not change, but the above-mentioned air will be less than the bottom surface along top surface speed, according to hydrodynamics, the air current velocity of flow is fast down, so the pressure that forms is less than the fuselage top, so produce decurrent thrust, reduced the danger of turning on one's side of crosswind to unmanned aerial vehicle. The camera is arranged on the bottom surface of the shell, the controller and the lithium battery are arranged in the shell, the solar panel is arranged on the top surface of the shell, the lithium battery and the solar panel are connected with the controller, the camera and the rotor wing preferentially use the solar panel to supply power, and the lithium battery is adopted to supply power when the sun does not exist.
Four through lead screw motor connection director, still be equipped with the spirit level in the fuselage, spirit level connection director, the protrusion of through lead screw motor corotation and reversal control lead screw, according to the protrusion of four support soles of topography control, guarantee that the unmanned aerial vehicle body keeps the level, after the organism keeps the level, the rotor stops the rotation completely. When the side wind is big, when inclination reaches the limit value, unmanned aerial vehicle starts the rotor and takes off, can prevent to turn on one's side, also can select the foot point of falling or return voyage again.
The above description is only a preferred embodiment of the present invention, and not intended to limit the present invention in other forms, and any person skilled in the art may apply the above modifications or changes to the equivalent embodiments with equivalent changes, without departing from the technical spirit of the present invention, and any simple modification, equivalent change and change made to the above embodiments according to the technical spirit of the present invention still belong to the protection scope of the technical spirit of the present invention.
Claims (6)
1. An unmanned aerial vehicle that can long time stay, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body and a station mechanism arranged at the bottom of the unmanned aerial vehicle body;
the station mechanism comprises two symmetrically arranged undercarriages, and each undercarriage is connected with the unmanned aerial vehicle body through a plurality of support frames;
the unmanned aerial vehicle body includes the fuselage and sets up the wing in the fuselage both sides respectively, is equipped with the rotor on every wing, the fuselage includes the shell, camera, controller, lithium cell, solar cell panel, the camera sets up in the shell bottom surface, controller, lithium cell setting are in the shell, solar cell panel sets up at the shell top surface, lithium cell, solar cell panel connection director, camera, rotor connection director.
2. The drone capable of long-term residence according to claim 1, wherein: each support frame is provided with a support sole, and the support soles can be vertically adjusted on the support frames through the adjusting mechanisms.
3. The drone capable of long-term residence according to claim 2, wherein: the adjusting mechanism comprises a rail, a sliding block, a push head, a screw rod and a through screw rod motor, the rail is arranged along the support frame and is fixedly connected to the support frame, the through screw rod motor is arranged at the lower end of the rail and is fixed to the support frame, the through screw rod motor is screwed on the screw rod, the push head is arranged at the upper end of the screw rod and is fixedly connected with the sliding block, the sliding block is connected to the rail in a sliding mode, and the supporting foot palm is connected to the bottom end of the screw rod.
4. The drone capable of long-term residence according to claim 3, wherein: and a baffle is arranged at the top end of the track.
5. The drone capable of long-term residence according to claim 3, wherein: the machine body is also internally provided with a level gauge, and the through type screw rod motor is connected with the controller.
6. The drone capable of long-term residence according to any one of claims 1 to 5, characterized in that: every the undercarriage is respectively through two support frames and this body coupling of unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121344074.9U CN215972114U (en) | 2021-06-17 | 2021-06-17 | Unmanned aerial vehicle capable of being parked for long time |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121344074.9U CN215972114U (en) | 2021-06-17 | 2021-06-17 | Unmanned aerial vehicle capable of being parked for long time |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215972114U true CN215972114U (en) | 2022-03-08 |
Family
ID=80578109
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121344074.9U Active CN215972114U (en) | 2021-06-17 | 2021-06-17 | Unmanned aerial vehicle capable of being parked for long time |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215972114U (en) |
-
2021
- 2021-06-17 CN CN202121344074.9U patent/CN215972114U/en active Active
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