CN218907648U

CN218907648U - Landform aviation unmanned aerial vehicle that shoots

Info

Publication number: CN218907648U
Application number: CN202222595737.5U
Authority: CN
Inventors: 刘申虎
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-09-29
Filing date: 2022-09-29
Publication date: 2023-04-25
Anticipated expiration: 2032-09-29

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a landform aerial photographing unmanned aerial vehicle. The technical proposal comprises: fuselage, rail guard and solar panel subassembly, the inside both sides of fuselage are installed the solar panel subassembly that extends, and solar panel subassembly includes electric putter, and electric putter end is through three solar cell panels of connecting plate fixed mounting, and the spout has all been seted up to three solar cell panel insides, and the slider has all slidable mounting in the spout, and three solar cell panel is through fixed connection's slider and spout cooperation sliding connection. According to the utility model, the three groups of solar panels are driven to move through the connecting plate by the electrifying operation of the electric push rod, and can be fully unfolded when the solar panels are mutually matched and unfolded to the top end through the sliding blocks and the sliding grooves in the solar panels, so that the function of supplying power to the solar panels is realized, the problem that the unmanned aerial vehicle can not continue aerial photography due to the fact that the battery power is exhausted after long-time flying is avoided, and the cruising performance of the unmanned aerial vehicle is improved.

Description

Landform aviation unmanned aerial vehicle that shoots

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a landform aerial photographing unmanned aerial vehicle.

Background

Unmanned aerial vehicle is called unmanned aerial vehicle entirely, and english abbreviation is UAV, is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, or by on-vehicle computer totally or intermittently independently, unmanned aerial vehicle takes photo by plane and refers to taking the earth's topography and obtain the top view from the sky with unmanned aerial vehicle, and the camera of taking photo by plane can be controlled by the photographer, also can shoot or remote control automatically.

By way of retrieval, patent publication No. CN108275279a discloses a drone comprising: the device comprises an engine, a transfer case, a plurality of speed regulators, a positive propeller and a negative propeller; the transfer case comprises a first driving gear, and the first driving gear is sleeved on an output shaft of the engine; the speed regulator includes the speed governing input shaft, the speed governing input shaft with first drive gear drive is connected, the speed regulator with positive oar and anti-oar transmission are connected, CN108275279A among the prior art in the in-process of use, if carelessly receive birds striking paddle, lead to unmanned aerial vehicle serious damage even crash easily, there is the potential safety hazard of crash, influence unmanned aerial vehicle flight's security and life, in view of this we propose an topography aviation unmanned aerial vehicle of shooing to solve current problem.

Disclosure of Invention

The utility model aims to provide a landform aerial photographing unmanned aerial vehicle, which aims to solve the problems in the background technology.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle is shot in landform aviation, includes fuselage, rail guard and solar panel subassembly, the rail guard is installed to the bottom screw thread in the fuselage outside, the rail guard includes down the disc, down the disc top is installed the bumper bar through the bolt equidistance, the disc is installed through the bolt to the bumper bar top, the solar panel subassembly that extends is installed to the inside both sides of fuselage, solar panel subassembly includes electric putter, electric putter end is through three solar cell panel of connecting plate fixed mounting, the spout has all been seted up to three solar cell panel inside, the inside slider that all slidable mounting of spout has, three solar cell panel pass through fixed connection's slider and spout cooperation sliding connection.

Can be connected lower disc and last disc through the bumper bar in the rail guard, form top, bottom and side safety protection, thereby carry out the protection at no dead angle to the fuselage, the anticollision function of fuselage has been increased, make its paddle can not take place direct impact with birds and trees at the in-process of flight, the security of fuselage at the striking in-process has been improved, the problem that the paddle when carelessly receiving birds striking, lead to the serious damage of fuselage even crash has been solved, the potential safety hazard of paddle receiving the striking and crash has been reduced, the safety in flight has been ensured in the setting of rail guard, the life of fuselage has been prolonged, drive three solar cell panel through the connecting plate through electric putter circular telegram operation, and solar cell panel can expand completely when expanding to the top through inside slider and spout each other, thereby the function of solar cell panel power supply has been realized, unmanned aerial vehicle long-time flight to battery electric quantity exhaustion and the problem that can't continue taking photo, unmanned aerial vehicle continuation performance has been improved, and the convenience of outdoor shooting has also been promoted at the same time.

Preferably, the front surface of the machine body is fixedly provided with a shaft bracket, one side of the shaft bracket is fixedly provided with a protection shaft seat, the inside of the protection shaft seat is fixedly provided with the output end of the servo motor, the inside of the shaft bracket is rotatably provided with a camera through a shaft lever, and the other side of the shaft lever is fixedly connected with the output end of the servo motor. The protection shaft seat can be fixed through the shaft bracket, the protection shaft seat can protect the servo motor inside the protection shaft seat from being damaged, the servo motor can drive the camera to rotate when being electrified, adjustment of different angles is carried out, adjustment of shooting angles of the camera is realized, and multi-angle shooting of the camera is realized.

Preferably, the lock catch is embedded and installed at the top of the machine body, and the storage battery box is installed on the back of the machine body through the lock catch. The storage battery box can be fixedly locked through the lock catch, the storage battery box is prevented from loosening, and the storage battery in the storage battery box can supply power for the video camera, the servo motor, the motor and the electric push rod.

Preferably, landing gears are fixedly arranged on two sides of the bottom end of the machine body, and a damping sponge sleeve is sleeved on the periphery of the bottom end of the landing gear. Can play shock-absorbing function when unmanned aerial vehicle descends through the undercarriage, shock attenuation sponge cover has more improved shock attenuation effect, avoids unmanned aerial vehicle to produce violent striking with ground when descending and causes the damage.

Preferably, the center of the top of the lower disc is fixedly provided with a screw, and the insides of the upper disc and the lower disc are fixedly provided with cross guard frames. The bottom at the fuselage can be installed down to the disc through the screw, and the rail guard of being convenient for is dismantled and assembled, makes things convenient for the fuselage to accomodate, and the cross protection frame has increased the fastness of last disc and lower disc simultaneously, has improved last disc and lower disc protection effect.

Preferably, two groups of propeller rods are respectively and fixedly arranged on two sides of the machine body, a motor is fixedly arranged at the top of the tail end of each propeller rod, and a propeller is fixedly arranged at the output end of each motor. The motor is electrified to run to drive the propeller to rotate at a high speed, and the high-speed rotating propeller can control the take-off of the airframe, so that the flying capacity of the airframe is realized.

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

1. can be connected lower disc and last disc through the bumper bar in the rail guard, form top, bottom and side safety protection, thereby carry out the protection at no dead angle to the fuselage, the anticollision function of fuselage has been increased, make its fuselage can not take place direct impact with birds at the in-process paddle of flight, the safety of fuselage in the striking in-process has been guaranteed, when having solved the paddle and inadvertently receiving birds striking, the problem that leads to the serious damage of fuselage and crash even, the potential safety hazard of paddle receiving striking and crash has been reduced, the safety of fuselage at the flight has been ensured in the setting of rail guard, the life of fuselage has been prolonged.

2. The three groups of solar panels are driven to move through the connecting plate by the electric push rod to move through the electric push rod, and the three groups of solar panels can be completely unfolded when the solar panels are mutually matched and unfolded to the top through the sliding blocks and the sliding grooves in the solar panels, so that the function of supplying power to the solar panels is realized, the problem that the unmanned aerial vehicle flies to the battery for a long time until the battery is exhausted and the battery needs to be replaced for aerial photography is avoided, the endurance performance of the unmanned aerial vehicle is improved, and meanwhile, the convenience of outdoor shooting of the unmanned aerial vehicle is improved.

Drawings

FIG. 1 is a schematic top view of the present utility model;

FIG. 2 is a schematic view of an expanded solar panel structure according to the present utility model;

FIG. 3 is a schematic side view of the present utility model;

FIG. 4 is a schematic view of a partial structure of a solar panel assembly according to the present utility model;

FIG. 5 is a schematic view of a partial structure of a guard rail according to the present utility model;

fig. 6 is a schematic view of a partial structure of a camera according to the present utility model.

In the figure: 1. a body; 101. locking; 102. a battery case; 2. landing gear; 201. damping sponge sleeve; 3. a guard rail; 301. an anti-collision rod; 302. an upper disc; 303. a lower disc; 304. a screw; 4. a propeller shaft; 401. a propeller; 402. a motor; 5. a solar panel assembly; 501. a solar cell panel; 502. a slide block; 503. a chute; 504. an electric push rod; 505. a connecting plate; 6. a camera; 601. a shaft bracket; 602. a protection shaft seat; 603. a servo motor.

Detailed Description

The technical scheme of the utility model is further described below with reference to the attached drawings and specific embodiments.

Example 1

As shown in fig. 1, fig. 2, fig. 3, fig. 4, fig. 5 and fig. 6, the utility model provides a landform aerial photographing unmanned aerial vehicle, which comprises a body 1, a protective guard 3 and a solar panel assembly 5, wherein the protective guard 3 is arranged at the bottom end threads on the outer side of the body 1, the protective guard 3 comprises a lower disc 303, an anti-collision rod 301 is arranged at the top of the lower disc 303 at equal intervals through bolts, an upper disc 302 is arranged at the top of the anti-collision rod 301 through bolts, extended solar panel assemblies 5 are arranged at two sides of the inner side of the body 1, the solar panel assembly 5 comprises an electric push rod 504, three groups of solar panels 501 are fixedly arranged at the tail ends of the electric push rod 504 through connecting plates 505, sliding grooves 503 are formed in the three groups of solar panels 501, sliding blocks 502 are slidably arranged in the sliding grooves 503, two groups of propeller rods 4 are fixedly arranged at two sides of the body 1 respectively, a motor 402 is fixedly arranged at the top of the tail ends of the propeller rods 4, a propeller 401 is fixedly arranged at the output end of the motor 402, a shaft seat 601 is fixedly arranged at one side of the body 1, three groups of solar panels 501 are fixedly arranged at the motor 602, a motor 602 is fixedly arranged at the other side of the shaft seat 601, and is fixedly connected with the other side of the motor 602, which is fixedly arranged at the other side of the motor 602, and is fixedly connected with the output shaft seat 603.

The working principle of the landform aviation photographing unmanned aerial vehicle based on the embodiment 1 is as follows: the motor 402 is electrified to run to drive the propeller 401 to rotate at a high speed, the propeller 401 rotating at a high speed can control the take-off of the machine body 1, the anti-collision rod 301 in the protective guard 3 can connect the lower disc 303 with the upper disc 302 to form top, bottom and side safety protection, so that the machine body 1 is protected without dead angle, the anti-collision function of the propeller 401 is increased, the propeller 401 cannot directly collide with birds in the flying process, the safety of the machine body 1 in flying is ensured by the arrangement of the protective guard 3, the service life of the machine body 1 is prolonged, the servo motor 603 is electrified to drive the camera 6 to rotate, different angles of adjustment are carried out, the shooting angle of the camera 6 is adjusted, the camera 6 is shot at multiple angles, the electric push rod 504 is electrified to drive the three groups of solar panels 501 to move through the connecting plate 505, and the solar panels 501 can be fully unfolded when being mutually matched with the sliding blocks 502 and the sliding grooves 503 in the inside to be forwards unfolded to the top, and the function of supplying power to the solar panels is realized.

Example two

As shown in fig. 1, fig. 2, fig. 3, and fig. 5, the present utility model provides a geomorphic aerial photographing unmanned aerial vehicle, and compared with the first embodiment, the present embodiment further includes: the lock catch 101 is embedded and installed at the top of the machine body 1, the storage battery box 102 is installed on the back of the machine body 1 through the lock catch 101, the landing gear 2 is fixedly installed on two sides of the bottom end of the machine body 1, the shock-absorbing sponge sleeve 201 is sleeved on the periphery of the bottom end of the landing gear 2, the screw 304 is fixedly installed at the center of the top of the lower disc 303, and the cross protection frames are fixedly installed in the upper disc 302 and the lower disc 303.

In this embodiment, as shown in fig. 1, 2 and 3, the storage battery box 102 can be locked by the lock catch 101, and the storage battery in the storage battery box 102 can supply power to the video camera 6, the servo motor 603, the motor 402 and the electric push rod 504; as shown in fig. 1, 2 and 3, the landing gear 2 can play a role in damping when the unmanned aerial vehicle lands, so that the damping sponge sleeve 201 further improves the damping effect and avoids damage caused by violent impact between the unmanned aerial vehicle and the ground when the unmanned aerial vehicle lands; as shown in fig. 5, the lower disc 303 can be mounted at the bottom of the machine body 1 through the screw member 304, so that the protective fence 3 is convenient to mount and dismount, and the machine body 1 is convenient to store, and meanwhile, the cross guard increases the firmness of the upper disc 302 and the lower disc 303, and improves the protection effect of the upper disc 302 and the lower disc 303.

The above-described embodiments are merely a few preferred embodiments of the present utility model, and many alternative modifications and combinations of the above-described embodiments will be apparent to those skilled in the art based on the technical solutions of the present utility model and the related teachings of the above-described embodiments.

Claims

1. The utility model provides an unmanned aerial vehicle is shot in landform aviation, includes fuselage (1), rail guard (3) and solar panel subassembly (5), its characterized in that: the utility model discloses a solar cell panel, including fuselage (1), bottom screw thread in fuselage (1) outside is installed rail guard (3), rail guard (3) include disc (303) down, down disc (303) top is through bolt equidistance install crash bar (301), crash bar (301) top is through bolt installation disc (302), solar panel subassembly (5) that extend are installed to the inside both sides of fuselage (1), solar panel subassembly (5) include electric putter (504), three solar cell panel (501) of electric putter (504) end through connecting plate (505) fixed mounting, spout (503) have all been seted up in three solar cell panel (501) are inside, slider (502) are all installed to inside slidable mounting of spout (503), three solar cell panel (501) are through fixed connection's slider (502) and spout (503) cooperation sliding connection.

2. The geomorphic aerial photographing unmanned aerial vehicle according to claim 1, wherein: the camera is characterized in that a shaft bracket (601) is fixedly arranged on the front surface of the machine body (1), a protection shaft seat (602) is fixedly arranged on one side of the shaft bracket (601), the output end of a servo motor (603) is fixedly arranged in the protection shaft seat (602), a camera (6) is rotatably arranged in the shaft bracket (601) through a shaft rod, and the other side of the shaft rod is fixedly connected with the output end of the servo motor (603).

3. The geomorphic aerial photographing unmanned aerial vehicle according to claim 1, wherein: the lock catch (101) is embedded and installed at the top of the machine body (1), and the storage battery box (102) is fixedly installed on the back of the machine body (1) through the lock catch (101).

4. The geomorphic aerial photographing unmanned aerial vehicle according to claim 1, wherein: landing gear (2) is fixedly arranged on two sides of the bottom end of the machine body (1), and a damping sponge sleeve (201) is sleeved on the periphery of the bottom end of the landing gear (2).

5. The geomorphic aerial photographing unmanned aerial vehicle according to claim 1, wherein: screw thread pieces (304) are fixedly arranged in the center of the top of the lower disc (303), and cross guard frames are fixedly arranged in the upper disc (302) and the lower disc (303).

6. The geomorphic aerial photographing unmanned aerial vehicle according to claim 1, wherein: two groups of propeller rods (4) are respectively and fixedly arranged on two sides of the machine body (1), a motor (402) is fixedly arranged at the top of the tail end of each propeller rod (4), and a propeller (401) is fixedly arranged at the output end of each motor (402).