CN215972164U - Ship cabin close-range detection unmanned aerial vehicle - Google Patents
Ship cabin close-range detection unmanned aerial vehicle Download PDFInfo
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- CN215972164U CN215972164U CN202122657805.1U CN202122657805U CN215972164U CN 215972164 U CN215972164 U CN 215972164U CN 202122657805 U CN202122657805 U CN 202122657805U CN 215972164 U CN215972164 U CN 215972164U
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Abstract
The utility model discloses an unmanned aerial vehicle for ship cabin close-up detection, which has the technical scheme that: the aircraft comprises an aircraft body, wherein a flight controller is embedded in the top surface of the aircraft body, two wings are respectively and fixedly installed on the left side and the right side of the aircraft body, a motor box is fixedly installed on the outer circular wall surface of one end of each wing, a driving motor is fixedly installed in the motor box, and a rotor wing is fixedly sleeved on the outer circular wall surface of a rotating shaft of the driving motor; the signal sensor is embedded in the top surface of the aircraft body, and the driving motor and the signal sensor are electrically connected with the flight controller; through setting up high definition digtal camera, when needs closely shoot, the first step motor of accessible remote control drives high definition digtal camera and rotates, realizes the effect of the shooting angle of control high definition digtal camera, can effectually avoid needing staff control unmanned aerial vehicle to adjust the shooting angle, easily touch near barrier scheduling problem.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle for ship cabin close-up inspection.
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.
For example, chinese patent publication No. CN214252053U proposes a photo-luminescence-based unmanned aerial vehicle detection device, in which an infrared camera senses light transmitted through a narrow-band filter, images defects inside a photovoltaic module, and transmits the formed image to a display device.
However, the above-mentioned photo-luminescence-based drone detection devices also have some drawbacks, such as: when closely monitoring, the detection angle of infrared camera can't be adjusted, needs staff control unmanned aerial vehicle to come to adjust the shooting position of infrared camera, not only the complicated work of being not convenient for of operation, still touches near barrier easily and leads to the machine to damage, for solving above-mentioned problem, we provide a boats and ships cabin near sight detection unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
In view of the problems mentioned in the background art, the utility model aims to provide a ship cabin close-up detection unmanned aerial vehicle to solve the problems mentioned in the background art.
The technical purpose of the utility model is realized by the following technical scheme:
a ship cabin close-up detection unmanned aerial vehicle comprises: the aircraft comprises an engine body, wherein a flight controller is embedded in the top surface of the engine body, two wings are respectively and fixedly installed on the left side and the right side of the engine body, a motor box is fixedly installed on the outer circular wall surface of one end of each wing, a driving motor is fixedly installed in the motor box, and a rotor wing is fixedly sleeved on the outer circular wall surface of a rotating shaft of the driving motor; the signal sensor is embedded in the top surface of the aircraft body, and the driving motor and the signal sensor are electrically connected with the flight controller; and the monitoring and adjusting assembly is arranged on one side of the machine body and used for adjusting and detecting angles.
Through adopting above-mentioned technical scheme, through setting up signal sensor for connect external wireless device, be convenient for control unmanned aerial vehicle flight and remove, through setting up monitoring adjustment assembly, can effectually avoid needing staff control unmanned aerial vehicle to come to adjust the shooting position of shooter, not only the complicated work of being not convenient for of operation, still touch near barrier easily and lead to the machine to damage the scheduling problem.
Preferably, the monitoring and adjusting assembly comprises: the aircraft comprises an engine body, an adjusting groove, a first stepping motor, a second stepping motor and a flight controller, wherein the adjusting groove is formed in one side of the engine body, a rotating groove is formed in one side of the adjusting groove, the first stepping motor is fixedly installed in the rotating groove, and the first stepping motor is electrically connected with the flight controller; high definition digtal camera, high definition digtal camera sets up the inside of adjustment tank, high definition digtal camera with flight controller electric connection together, the round hole of high definition digtal camera one side with first step motor axis of rotation is fixed cup joints together.
Through adopting above-mentioned technical scheme, through setting up high definition digtal camera, when needs closely shoot, the first step motor of accessible remote control drives high definition digtal camera and rotates, realizes the effect of the shooting angle of control high definition digtal camera, can effectually avoid needing staff control unmanned aerial vehicle to adjust the shooting angle, easily touch near barrier scheduling problem.
Preferably, the monitoring and adjusting assembly further comprises: the two supporting blocks are fixedly installed on the bottom surface of the machine body, the inner circle wall surface of the supporting block on the right side is fixedly sleeved with a second stepping motor, and the inner circle wall surface of the supporting block on the left side is fixedly sleeved with a bearing seat; laser radar, laser radar sets up the bottom surface of organism, laser radar's excircle wall fixed mounting has two spliced poles, one of them the spliced pole with the interior round wall of bearing frame is fixed to be cup jointed together, another the spliced pole with second step motor axis of rotation fixed connection is in the same place, second step motor and laser radar all with flight controller electric connection is in the same place.
Through adopting above-mentioned technical scheme, through setting up laser radar, accessible remote control second step motor drives laser radar and rotates when using to in monitor more comprehensive external data information.
Preferably, a strong light is fixedly mounted on the top surface of the aircraft body, and the strong light is electrically connected with the flight controller.
Through adopting above-mentioned technical scheme, through setting up the strong light lamp, make high definition digtal camera can shoot more clear picture.
Preferably, a buzzer is embedded in the right side of the aircraft body, and the buzzer is electrically connected with the flight controller.
Through adopting above-mentioned technical scheme, through setting up bee calling organ, make this unmanned aerial vehicle can realize long-range voice broadcast, increase the practicality.
Preferably, the four corners of the bottom surface of the machine body are fixedly provided with foot rests, and the bottom surfaces of the foot rests are fixedly provided with rubber blocks.
Through adopting above-mentioned technical scheme, through setting up the foot rest, this unmanned aerial vehicle of being convenient for descends, through setting up the block rubber, vibrations when can effectually reducing unmanned aerial vehicle to descend.
In summary, the utility model mainly has the following beneficial effects:
through setting up signal sensor, be used for connecting external wireless device, be convenient for control unmanned aerial vehicle flight removes, through setting up monitoring adjustment assembly, can effectually avoid needing staff control unmanned aerial vehicle to come to adjust the shooting position of shooter, not only the complicated work of being not convenient for of operation, still touch near barrier easily and lead to the machine to damage the scheduling problem, through setting up high definition digtal camera, when needs closely shoot, accessible remote control first step motor drives high definition digtal camera and rotates, realize the effect of the shooting angle of control high definition digtal camera, can effectually avoid needing staff control unmanned aerial vehicle to adjust the shooting angle, easily touch near barrier scheduling problem.
Through setting up laser radar, accessible remote control second step motor drives laser radar and rotates when using to in monitoring more comprehensive external data information, through setting up the strong light, make high definition digtal camera can shoot more clear picture, through setting up bee calling organ, make this unmanned aerial vehicle can realize long-range voice broadcast, increase the practicality, through setting up the foot rest, be convenient for this unmanned aerial vehicle descends, through setting up the block rubber, vibrations when can effectually reduce unmanned aerial vehicle to descend.
Drawings
FIG. 1 is a schematic perspective view of the present invention;
FIG. 2 is a schematic view of a portion of the enlarged structure of A in FIG. 1;
FIG. 3 is a schematic view of the support block structure of the present invention.
Reference numerals: 1. a body; 2. a flight controller; 3. an airfoil; 4. a motor case; 5. a drive motor; 6. a rotor; 7. a signal sensor; 8. an adjustment groove; 9. a rotating groove; 10. a first stepper motor; 11. A high-definition camera; 12. a support block; 13. a second stepping motor; 14. a bearing seat; 15. a laser radar; 16. connecting columns; 17. a highlight lamp; 18. a buzzer; 19. a foot rest; 20. a rubber block.
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 and 2, a ship cabin close-up detection unmanned aerial vehicle comprises: organism 1, organism 1's top surface is embedded to have flight controller 2, organism 1's the left and right sides is fixed mounting two wings 3 respectively, the excircle wall fixed mounting of 3 one ends of wing has motor case 4, the inside fixed mounting driving motor 5 of motor case 4, the excircle wall of driving motor 5 axis of rotation is fixed to have cup jointed rotor 6, organism 1's top surface is embedded to have signal sensor 7, driving motor 5 all is in the same place with flight controller 2 electric connection with signal sensor 7, through setting up signal sensor 7, be used for connecting external wireless device, be convenient for control unmanned aerial vehicle flight and remove, one side of organism 1 is provided with the monitoring adjusting part, be used for the regulation and detection angle, the monitoring adjusting part includes: the adjusting groove 8 is formed in one side of the machine body 1, the rotating groove 9 is formed in one side of the adjusting groove 8, the first stepping motor 10 is fixedly installed in the rotating groove 9, the first stepping motor 10 is electrically connected with the flight controller 2, through the arrangement of the monitoring and adjusting assembly, the problem that a worker needs to control an unmanned aerial vehicle to adjust the shooting position of the shooting device can be effectively avoided, operation is complex and inconvenient, and the problem that nearby obstacles are easily touched to cause machine damage and the like is solved, the high-definition camera 11 is arranged in the adjusting groove 8, the high-definition camera 11 is electrically connected with the flight controller 2, a round hole in one side of the high-definition camera 11 is fixedly sleeved with a rotating shaft of the first stepping motor 10, through the arrangement of the high-definition camera 11, when close-distance shooting is needed, the first stepping motor 10 can be remotely controlled to drive the camera 11 to rotate, the effect of the shooting angle of realization control high definition digtal camera 11 can effectually be avoided needing staff control unmanned aerial vehicle to adjust the shooting angle, easily touches near barrier scheduling problem.
Referring to fig. 1 and 3, the monitoring and adjusting assembly further includes: two supporting shoes 12, the equal fixed mounting in bottom surface of organism 1 of two supporting shoes 12, the interior circle wall that is located right side supporting shoe 12 is fixed to be cup jointed second step motor 13, the interior circle wall that is located left side supporting shoe 12 is fixed to be cup jointed bearing frame 14, the bottom surface of organism 1 is provided with laser radar 15, laser radar 15's excircle wall fixed mounting has two spliced poles 16, one of them spliced pole 16 is fixed to be cup jointed together with the interior circle wall of bearing frame 14, another spliced pole 16 is in the same place with 13 axis of rotation fixed connection of second step motor, second step motor 13 and laser radar 15 all are in the same place with flight controller 2 electric connection, through setting up laser radar 15, accessible remote control second step motor 13 drives laser radar 15 and rotates when using, so that monitor more comprehensive external data information.
Referring to fig. 1, top surface fixed mounting of organism 1 has strong light 17, strong light 17 is in the same place with flight controller 2 electric connection, through setting up strong light 17, make high definition digtal camera 11 can shoot more clear picture, organism 1's right side is embedded to have bee calling organ 18, bee calling organ 18 is in the same place with flight controller 2 electric connection, through setting up bee calling organ 18, make this unmanned aerial vehicle can realize long-range voice broadcast, increase the practicality, the equal fixed mounting in four corners position of organism 1 bottom surface has foot rest 19, foot rest 19's bottom surface fixed mounting has rubber block 20, through setting up foot rest 19, be convenient for this unmanned aerial vehicle to descend, through setting up rubber block 20, can effectually reduce the vibrations when unmanned aerial vehicle descends.
The working principle is as follows: referring to fig. 1, 2 and 3, when the unmanned aerial vehicle is used, the wireless device is connected with the unmanned aerial vehicle through the signal sensor 7 to realize control, the high-definition camera 11 is arranged, when the unmanned aerial vehicle needs to be shot in a close range, the high-definition camera 11 can be driven to rotate through the remote control first stepping motor 10, the effect of controlling the shooting angle of the high-definition camera 11 is realized, the problems that a worker needs to control the unmanned aerial vehicle to adjust the shooting angle, nearby obstacles are easy to touch and the like can be effectively solved, the laser radar 15 is arranged, the laser radar 15 can be driven to rotate through the remote control second stepping motor 13 when the unmanned aerial vehicle is used, more comprehensive external data information can be monitored, a clearer picture can be shot by the high-intensity light 17, the unmanned aerial vehicle can realize remote voice broadcast by arranging the buzzer 18, increase the practicality, through setting up foot rest 19, this unmanned aerial vehicle of being convenient for descends, through setting up rubber block 20, vibrations when can effectually reducing unmanned aerial vehicle descending.
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 (6)
1. The utility model provides a boats and ships cabin is close to viewing and is detected unmanned aerial vehicle which characterized in that includes:
the aircraft comprises an aircraft body (1), wherein a flight controller (2) is embedded in the top surface of the aircraft body (1), two wings (3) are fixedly installed on the left side and the right side of the aircraft body (1) respectively, a motor box (4) is fixedly installed on the outer circular wall surface of one end of each wing (3), a driving motor (5) is fixedly installed in the motor box (4), and a rotor wing (6) is fixedly sleeved on the outer circular wall surface of a rotating shaft of the driving motor (5);
the signal sensor (7) is embedded in the top surface of the airplane body (1), and the driving motor (5) and the signal sensor (7) are electrically connected with the flight controller (2);
the monitoring and adjusting assembly is arranged on one side of the machine body (1) and used for adjusting and detecting angles.
2. The ship cabin close-up detection unmanned aerial vehicle of claim 1, wherein the monitoring and adjusting assembly comprises:
the airplane comprises an airplane body (1), an adjusting groove (8), a rotating groove (9), a first stepping motor (10) and a flight controller (2), wherein the adjusting groove (8) is formed in one side of the airplane body (1), the rotating groove (9) is formed in one side of the adjusting groove (8), the first stepping motor (10) is fixedly installed inside the rotating groove (9), and the first stepping motor (10) is electrically connected with the flight controller (2);
high definition digtal camera (11), high definition digtal camera (11) set up the inside of adjustment tank (8), high definition digtal camera (11) with flight controller (2) electric connection together, the round hole of high definition digtal camera (11) one side with first step motor (10) axis of rotation is fixed the cover and is linked together.
3. The vessel hold near observation detection unmanned aerial vehicle of claim 1, wherein the monitoring adjustment assembly further comprises:
the two supporting blocks (12) are fixedly installed on the bottom surface of the machine body (1), the inner circle wall surface of the supporting block (12) on the right side is fixedly sleeved with a second stepping motor (13), and the inner circle wall surface of the supporting block (12) on the left side is fixedly sleeved with a bearing seat (14);
laser radar (15), laser radar (15) set up the bottom surface of organism (1), the excircle wall fixed mounting of laser radar (15) has two spliced poles (16), one of them spliced pole (16) with the interior circle wall of bearing frame (14) is fixed cup joints together, another spliced pole (16) with second step motor (13) axis of rotation fixed connection is in the same place, second step motor (13) and laser radar (15) all with flight controller (2) electric connection is in the same place.
4. The ship cabin close-up detection unmanned aerial vehicle of claim 1, characterized in that a floodlight (17) is fixedly installed on the top surface of the machine body (1), and the floodlight (17) and the flight controller (2) are electrically connected together.
5. The ship cabin close-up detection unmanned aerial vehicle of claim 1, characterized in that a buzzer (18) is embedded in the right side of the machine body (1), and the buzzer (18) is electrically connected with the flight controller (2).
6. The ship cabin close-up detection unmanned aerial vehicle of claim 1, characterized in that foot rests (19) are fixedly installed at four corners of the bottom surface of the machine body (1), and rubber blocks (20) are fixedly installed on the bottom surfaces of the foot rests (19).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122657805.1U CN215972164U (en) | 2021-11-02 | 2021-11-02 | Ship cabin close-range detection unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122657805.1U CN215972164U (en) | 2021-11-02 | 2021-11-02 | Ship cabin close-range detection unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215972164U true CN215972164U (en) | 2022-03-08 |
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ID=80511609
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122657805.1U Active CN215972164U (en) | 2021-11-02 | 2021-11-02 | Ship cabin close-range detection unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215972164U (en) |
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2021
- 2021-11-02 CN CN202122657805.1U patent/CN215972164U/en active Active
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