CN116039979A - Unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device and use method - Google Patents
Unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device and use method Download PDFInfo
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- CN116039979A CN116039979A CN202310185910.0A CN202310185910A CN116039979A CN 116039979 A CN116039979 A CN 116039979A CN 202310185910 A CN202310185910 A CN 202310185910A CN 116039979 A CN116039979 A CN 116039979A
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- 238000000034 method Methods 0.000 title claims abstract description 14
- 230000007246 mechanism Effects 0.000 claims description 72
- 230000000087 stabilizing effect Effects 0.000 claims description 11
- 230000006835 compression Effects 0.000 claims description 9
- 238000007906 compression Methods 0.000 claims description 9
- 238000010586 diagram Methods 0.000 description 4
- 239000003381 stabilizer Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/30—Assessment of water resources
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Abstract
The invention relates to data acquisition, in particular to an unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device and a using method thereof, wherein the method comprises the following steps: step one: the lifting force is generated through rotation of a plurality of impellers, and the driving device moves to a designated collecting position; step two: driving the rotating seat and the swinging arm I to move, driving the acquisition device to move, and adjusting the position of the acquisition device; step three: the acquisition device completes data acquisition; different data acquisition equipment can be carried according to different use demands, and the position of the data acquisition device is adjusted according to different use demands.
Description
Technical Field
The invention relates to data acquisition, in particular to an unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device and a using method thereof.
Background
In data acquisition, data video or audio data of gathering also includes some temperatures etc. still need gather some samples sometimes, and some data acquisition's place is unfavorable for manual work, consequently need accomplish data acquisition with the help of auxiliary assembly such as unmanned aerial vehicle, along with data acquisition requirement's improvement, corresponding requirement to unmanned aerial vehicle is also higher and higher, need unmanned aerial vehicle to carry multiple data acquisition equipment to can be according to different user demand, adjustment data acquisition's position.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device and a using method thereof, which can carry different data acquisition equipment according to different using requirements and adjust the position of the data acquisition device according to different using requirements.
The aim of the invention is achieved by the following technical scheme:
the utility model provides an aviation geophysical prospecting data acquisition device based on unmanned aerial vehicle, includes support ring I, rotates on the support ring I and is connected with two swivel rings I, fixedly connected with on the support ring I drives swivel ring I and carries out pivoted power unit I, and power unit I prefers servo motor;
the rotating ring I is rotationally connected with a rotating seat, the rotating ring I is fixedly connected with a power mechanism II which drives the rotating seat to rotate, the power mechanism II is preferably a servo motor, the rotating seat is rotationally connected with a swinging arm I, the rotating seat is fixedly connected with a power mechanism III which drives the swinging arm I to swing, the power mechanism III is preferably a servo motor, the swinging arm I is hinged with a swinging seat, the swinging arm I is fixedly connected with a power mechanism IV which drives the swinging seat to swing, the power mechanism IV is preferably a servo motor, the swinging seat is rotationally connected with a rotating seat, the swinging seat is fixedly connected with a power mechanism V which drives the rotating seat to rotate, the power mechanism V is preferably a servo motor, and the rotating seat is fixedly connected with a collecting device;
the acquisition device is a camera device, an audio acquisition device or a sensor;
the acquisition device is a mechanical clamping hand;
the support ring I is internally provided with a telescopic support, a screw rod is rotationally connected to the telescopic support, threads at two ends of the screw rod are opposite in rotation direction, a power mechanism VI for driving the screw rod to rotate is fixedly connected to the telescopic support, the power mechanism VI is preferably a servo motor, two ends of the screw rod are respectively provided with a telescopic cylinder through threads, the outer ends of the two telescopic cylinders are respectively fixedly connected with a ball body, the telescopic support is slidably connected with a plurality of expansion seats, a plurality of connecting rods are hinged between the expansion seats and the two telescopic cylinders, the expansion seats are slidably connected to the support ring I, and a compression spring I is fixedly connected between the expansion seats and the support ring I;
the support ring I is fixedly connected with a support ring II, the support ring II is rotationally connected with a stabilizing ring, the support ring II is fixedly connected with a power mechanism VII for driving the stabilizing ring to rotate, and the power mechanism VII is preferably a servo motor;
the two telescopic cylinders are respectively and rotatably connected with a rotary ring II, each rotary ring II is fixedly connected with a plurality of telescopic mechanisms, each telescopic cylinder is fixedly connected with a power mechanism VIII for driving the rotary ring II to rotate, and the power mechanism VIII is preferably a servo motor;
the two spheres are respectively provided with an arc cavity in clearance fit, the two arc cavities are respectively connected with an arc shell in a rotating way, and a compression spring II is fixedly connected between the telescopic end of the telescopic mechanism and the arc shells;
two swing arms II are hinged to the two arc cavities, a rotating support is fixedly connected to each swing arm II, an impeller is rotatably connected to each rotating support, a power mechanism IX for driving the swing arms II to swing is fixedly connected to the arc cavities, and the power mechanism IX is preferably a servo motor.
The application method of the unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device comprises the following steps of:
step one: the lifting force is generated through rotation of a plurality of impellers, and the driving device moves to a designated collecting position;
step two: driving the rotating seat and the swinging arm I to move, driving the acquisition device to move, and adjusting the position of the acquisition device;
step three: the acquisition device completes data acquisition.
Drawings
The invention will be described in further detail with reference to the accompanying drawings and detailed description.
FIG. 1 is a schematic diagram of a method of using an unmanned aerial vehicle-based geophysical prospecting data acquisition device according to the present invention;
fig. 2 is a schematic structural diagram of an unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device according to the present invention;
fig. 3 is a schematic diagram of the internal structure of the unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device;
FIG. 4 is a schematic view of the structure of the support ring of the present invention;
FIG. 5 is a schematic view of the telescopic bracket of the present invention;
FIG. 6 is a schematic view of the stabilizing ring structure of the present invention;
FIG. 7 is a schematic diagram of the wobble plate structure of the present invention;
FIG. 8 is a schematic view of the arc housing structure of the present invention;
FIG. 9 is a schematic view of the telescopic cylinder of the present invention;
fig. 10 is a schematic sectional view of the arc housing of the present invention.
In the figure:
a support ring I11; a rotating ring I12;
a rotating seat 21; swing arm I22; a swing seat 23; a rotating seat 24; a collection device 25;
a telescopic bracket 31; a screw 32; a telescopic cylinder 33; a sphere 34; a link 35; an expansion seat 36;
a support ring II 41; a stabilizer ring 42;
a rotating ring II 51; a telescopic mechanism 52;
a circular arc cavity 61; a circular arc housing 62;
Description of the embodiments
The invention is described in further detail below with reference to the accompanying drawings.
As shown in fig. 1 to 10, the structure and function of an unmanned aerial vehicle-based aerospace data acquisition device will be described in detail;
the utility model provides an aviation geophysical prospecting data acquisition device based on unmanned aerial vehicle, includes support ring I11, rotates on support ring I11 and is connected with two swivel rings I12, fixedly connected with on support ring I11 drives swivel ring I12 and carries out pivoted power unit I, and power unit I prefers servo motor;
the rotating ring I12 is rotationally connected with a rotating seat 21, the rotating ring I12 is fixedly connected with a power mechanism II for driving the rotating seat 21 to rotate, the power mechanism II is preferably a servo motor, the rotating seat 21 is rotationally connected with a swinging arm I22, the rotating seat 21 is fixedly connected with a power mechanism III for driving the swinging arm I22 to swing, the power mechanism III is preferably a servo motor, the swinging arm I22 is hinged with a swinging seat 23, the swinging arm I22 is fixedly connected with a power mechanism IV for driving the swinging seat 23 to swing, the power mechanism IV is preferably a servo motor, the swinging seat 23 is rotationally connected with a rotating seat 24, the swinging seat 23 is fixedly connected with a power mechanism V for driving the rotating seat 24 to rotate, the power mechanism V is preferably a servo motor, and the rotating seat 24 is fixedly connected with a collecting device 25;
when the device is used, after moving to a designated position, the power mechanism I is started, the output shaft of the power mechanism I starts to rotate, the output shaft of the power mechanism I drives the rotary ring I12 to rotate, the rotary ring I12 drives the rotary seat 21 to rotate, the rotary seat 21 drives the swing arm I22 to move, the swing arm I22 drives the swing seat 23 to move, the swing seat 23 drives the rotary seat 24 to move, the rotary seat 24 drives the acquisition device 25 to move, and then the acquisition device 25 moves to different positions;
starting a power mechanism II, wherein an output shaft of the power mechanism II starts to rotate, the output shaft of the power mechanism II drives a rotating seat 21 to rotate, the rotating seat 21 drives a swinging arm I22 to move, the swinging arm I22 drives a swinging seat 23 to move, the swinging seat 23 drives a rotating seat 24 to move, and the rotating seat 24 drives a collecting device 25 to move, so that the collecting device 25 moves to different positions;
starting a power mechanism III, wherein an output shaft of the power mechanism III starts to rotate, the output shaft of the power mechanism III drives a swing arm I22 to move, the swing arm I22 drives a swing seat 23 to move, the swing seat 23 drives a rotating seat 24 to move, and the rotating seat 24 drives a collecting device 25 to move, so that the collecting device 25 moves to different positions;
starting a power mechanism IV, wherein an output shaft of the power mechanism IV starts to rotate, the output shaft of the power mechanism IV drives a swinging seat 23 to swing, the swinging seat 23 drives a rotating seat 24 to move, and the rotating seat 24 drives a collecting device 25 to move, so that the collecting device 25 moves to different positions;
starting the power mechanism V, wherein an output shaft of the power mechanism V starts to rotate, and the output shaft of the power mechanism V drives the rotating seat 24 to rotate, and the rotating seat 24 drives the acquisition device 25 to move, so that the acquisition device 25 moves to different positions;
further, the acquisition device 25 may be a camera device, an audio acquisition device or a sensor, where the camera device may acquire video data, the audio acquisition may acquire audio data, and the sensor may acquire information such as temperature;
further, the collecting device 25 may be a mechanical hand, which may be a mechanical hand in the prior art, for clamping and collecting a sample of an object;
further, when the collecting device 25 is a mechanical gripper, in order to ensure the hidden carrying of the sample, the power mechanism I, the power mechanism II, the power mechanism III, the power mechanism IV and the power mechanism V can be started to drive the collecting device 25 to move, so that the collecting device 25 moves into the supporting ring I11, and further the side edge of the supporting ring I11 is buckled through the two circular arc shells 62, and further the sealed carrying and the transportation of the sample are completed;
the telescopic support 31 is arranged in the support ring I11, the screw rod 32 is rotationally connected to the telescopic support 31, threads at two ends of the screw rod 32 are opposite in rotation direction, the power mechanism VI for driving the screw rod 32 to rotate is fixedly connected to the telescopic support 31, the power mechanism VI is preferably a servo motor, two ends of the screw rod 32 are respectively connected with the telescopic cylinders 33 through threads, the outer ends of the two telescopic cylinders 33 are respectively fixedly connected with a ball 34, a plurality of expansion seats 36 are slidably connected to the telescopic support 31, a plurality of connecting rods 35 are hinged between the expansion seats 36 and the two telescopic cylinders 33, the expansion seats 36 are slidably connected to the support ring I11, and a compression spring I is fixedly connected between the expansion seats 36 and the support ring I11;
the support ring I11 is fixedly connected with a support ring II 41, the support ring II 41 is rotationally connected with a stabilizing ring 42, the support ring II 41 is fixedly connected with a power mechanism VII for driving the stabilizing ring 42 to rotate, and the power mechanism VII is preferably a servo motor;
the two telescopic cylinders 33 are respectively and rotatably connected with a rotary ring II 51, each rotary ring II 51 is fixedly connected with a plurality of telescopic mechanisms 52, the telescopic cylinders 33 are fixedly connected with a power mechanism VIII for driving the rotary rings II 51 to rotate, and the power mechanism VIII is preferably a servo motor;
the two spheres 34 are respectively provided with an arc cavity 61 in clearance fit, the two arc cavities 61 are respectively connected with an arc shell 62 in a rotating way, and a compression spring II is fixedly connected between the telescopic end of the telescopic mechanism 52 and the arc shells 62;
two swing arms II 71 are hinged to the two circular arc cavities 61, a rotating bracket 72 is fixedly connected to each swing arm II 71, an impeller 73 is rotatably connected to each rotating bracket 72, a power mechanism IX for driving the swing arms II 71 to swing is fixedly connected to the circular arc cavities 61, and the power mechanism IX is preferably a servo motor;
as shown in fig. 3, when the device is required to fly on the sky, four impellers 73 are started, and the four impellers 73 rotate to generate a certain lifting force so as to drive the device to fly in the sky;
further, the power mechanism IX can be started, the output shaft of the power mechanism IX starts to rotate, the output shaft of the power mechanism IX drives the swing arm II 71 to move, the swing arm II 71 drives the rotating bracket 72 to move, and the rotating bracket 72 drives the impeller 73 to move, so that the position of the impeller 73 is adjusted, and different use requirements are met;
further, as shown in fig. 3, the four impellers 73 may be driven by the swing arm ii 71 to move, so that the swing arm ii 71 is accommodated inside the stabilizing ring 42, and the stabilizing ring 42 protects the outside of the impellers 73, i.e. when the impellers collide, the impellers 73 collide with the outside of the stabilizing ring 42 first, so as to protect the impellers 73 to a certain extent;
further, when the device is required to generate certain inclined flight, namely steering or inclined flight is required, the telescopic mechanism 52 is started, the telescopic mechanism 52 can be a hydraulic cylinder or an electric push rod, the telescopic end of the telescopic mechanism 52 drives the compression spring II to move, the compression spring II is pulled, the compression spring II pulls the arc shell 62, the arc shell 62 drives the arc cavity 61 to move, so that the arc cavity 61 generates certain deflection, the arc cavity 61 drives the corresponding swing arm II 71 to move, and the inclined direction of the impeller 73 is adjusted, so that the flight in different directions is completed;
further, since the device is required to be stable in the process of data acquisition, namely, the device is required to be in a relatively static state, the data acquisition stability is ensured, the power mechanism VII can be started, the output shaft of the power mechanism VII starts to rotate, the output shaft of the power mechanism VII drives the stabilizing ring 42 to rotate, the stabilizing ring 42 rotates to generate centrifugal force, transverse centrifugal force is generated, and the device is stabilized at a certain position by utilizing rotational inertia;
further, a motor for driving the arc shell 62 to rotate is fixedly connected to the arc cavity 61, the motor is started, an output shaft of the motor drives the arc shell 62 to rotate, centrifugal force is generated by rotation of the arc shell 62, vertical centrifugal force is generated, and the device is stabilized at a certain position by utilizing rotational inertia;
further, in order to ensure the stability of the device in the flying process, wind resistance is reduced, and meanwhile, damage to the acquisition device 25 is reduced, or damage to a sample clamped on the acquisition device 25 is reduced;
the device comprises an arc shell 62 which can be buckled with each other, a power mechanism VI is started, an output shaft of the power mechanism VI starts to rotate, the output shaft of the power mechanism VI drives a screw rod 32 to rotate, the screw rod 32 drives two telescopic cylinders 33 to be close to each other through threads when rotating, the two telescopic cylinders 33 respectively drive two spheres 34 to be close to each other, the two spheres 34 drive two arc cavities 61 to be close to each other, the two arc cavities 61 drive the two arc shells 62 to be close to each other, the two arc shells 62 are closed on a supporting ring I11, and then in the flying process of the device, the acquisition device 25 is accommodated in the arc shells 62 under the drive of a rotating seat 21 and a swinging arm I22, the two arc shells 62 and the supporting ring I11 form a complete sphere, and the purposes of protecting and hiding the acquisition device 25 are also generated to a certain extent when the flying wind resistance is reduced;
when the device moves to a designated position, the power mechanism VI is started, so that the two arc shells 62 are separated, the acquisition device 25 is exposed under the drive of the rotating seat 21 and the swinging arm I22, and data acquisition is completed.
The application method of the unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device comprises the following steps of:
step one: the plurality of impellers 73 rotate to generate lifting force, and the driving device moves to a designated collecting position;
step two: the rotating seat 21 and the swing arm I22 are driven to move, the acquisition device 25 is driven to move, and the position of the acquisition device 25 is adjusted;
step three: the acquisition device 25 completes the acquisition of data.
Claims (10)
1. Unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device, including supporting ring I (11), its characterized in that: the device is characterized in that two rotating rings I (12) are rotatably connected to the supporting ring I (11), a rotating seat (21) is rotatably connected to the rotating ring I (12), a swinging arm I (22) is rotatably connected to the rotating seat (21), a swinging seat (23) is hinged to the swinging arm I (22), a rotating seat (24) is rotatably connected to the swinging seat (23), and a collecting device (25) is fixedly connected to the rotating seat (24).
2. The unmanned aerial vehicle-based aerospace data acquisition device according to claim 1, wherein: the acquisition device (25) is an image pickup device, an audio acquisition device or a sensor.
3. The unmanned aerial vehicle-based aerospace data acquisition device according to claim 1, wherein: the acquisition device (25) is a mechanical clamping hand.
4. The unmanned aerial vehicle-based aerospace data acquisition device according to claim 1, wherein: a telescopic support (31) is arranged in the support ring I (11), a screw rod (32) is connected to the telescopic support (31) in a rotating mode, threads at two ends of the screw rod (32) are opposite in rotation direction, telescopic cylinders (33) are connected to two ends of the screw rod (32) through threads, and spheres (34) are fixedly connected to the outer ends of the two telescopic cylinders (33).
5. The unmanned aerial vehicle-based aerospace data acquisition device according to claim 4, wherein: a plurality of expansion seats (36) are connected to the telescopic support (31) in a sliding mode, a plurality of connecting rods (35) are hinged between the expansion seats (36) and the two telescopic cylinders (33), the expansion seats (36) are connected to the support ring I (11) in a sliding mode, and a compression spring I is fixedly connected between the expansion seats (36) and the support ring I (11).
6. The unmanned aerial vehicle-based aerospace data acquisition device according to claim 5, wherein: the support ring I (11) is fixedly connected with a support ring II (41), and the support ring II (41) is rotatably connected with a stabilizing ring (42).
7. The unmanned aerial vehicle-based aerospace data acquisition device according to claim 6, wherein: the two telescopic cylinders (33) are respectively and rotatably connected with a rotary ring II (51), and each rotary ring II (51) is fixedly connected with a plurality of telescopic mechanisms (52).
8. The unmanned aerial vehicle-based aerospace data acquisition device according to claim 7, wherein: the two spheres (34) are provided with arc cavities (61) in clearance fit, the arc cavities (61) are rotationally connected with arc shells (62), and compression springs II are fixedly connected between the telescopic ends of the telescopic mechanisms (52) and the arc shells (62).
9. The unmanned aerial vehicle-based aerospace data acquisition device according to claim 8, wherein: two swing arms II (71) are hinged on the two arc cavities (61), a rotating support (72) is fixedly connected to each swing arm II (71), and an impeller (73) is rotatably connected to each rotating support (72).
10. A method of using an unmanned aerial vehicle-based geophysical prospecting data acquisition apparatus as claimed in claim 9, wherein: the method comprises the following steps:
step one: generating lifting force through rotation of a plurality of impellers (73), and moving the driving device to a designated collecting position;
step two: the rotary seat (21) and the swing arm I (22) are driven to move, the acquisition device (25) is driven to move, and the position of the acquisition device (25) is adjusted;
step three: the acquisition device (25) completes the acquisition of data.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310185910.0A CN116039979A (en) | 2023-03-01 | 2023-03-01 | Unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device and use method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202310185910.0A CN116039979A (en) | 2023-03-01 | 2023-03-01 | Unmanned aerial vehicle-based aviation geophysical prospecting data acquisition device and use method |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117340887A (en) * | 2023-11-16 | 2024-01-05 | 泰州学院 | Computer remote operation robot |
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2023
- 2023-03-01 CN CN202310185910.0A patent/CN116039979A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117340887A (en) * | 2023-11-16 | 2024-01-05 | 泰州学院 | Computer remote operation robot |
| CN117340887B (en) * | 2023-11-16 | 2024-05-17 | 泰州学院 | Computer remote operation robot |
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