CN111361725A - Carry on small-size laser radar's oil-electricity and mix unmanned aerial vehicle - Google Patents
Carry on small-size laser radar's oil-electricity and mix unmanned aerial vehicle Download PDFInfo
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- CN111361725A CN111361725A CN202010234021.5A CN202010234021A CN111361725A CN 111361725 A CN111361725 A CN 111361725A CN 202010234021 A CN202010234021 A CN 202010234021A CN 111361725 A CN111361725 A CN 111361725A
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- 230000007246 mechanism Effects 0.000 claims abstract description 11
- 230000003139 buffering effect Effects 0.000 claims description 7
- 230000002146 bilateral effect Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 14
- 230000008569 process Effects 0.000 abstract description 11
- 230000009471 action Effects 0.000 abstract description 7
- 230000005611 electricity Effects 0.000 abstract description 3
- 230000006978 adaptation Effects 0.000 abstract description 2
- 230000008859 change Effects 0.000 abstract description 2
- 230000003287 optical effect Effects 0.000 description 4
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000002592 echocardiography Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 230000010365 information processing Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- 238000012544 monitoring process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
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- B64D27/026—
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Optical Radar Systems And Details Thereof (AREA)
Abstract
The invention discloses a gasoline-electric hybrid unmanned aerial vehicle carrying a small laser radar, which comprises an unmanned aerial vehicle body and a driving mechanism, wherein support frames are fixedly connected to two sides of the bottom of the unmanned aerial vehicle body, the top of the unmanned aerial vehicle body is movably connected with the small laser radar body, a mounting bar is fixedly connected to the bottom of the small laser radar body, and one side of the mounting bar extends to the outside of the small laser radar body. This carry on small-size laser radar's mixed unmanned aerial vehicle of oil electricity sets up the mounting bar through the bottom at small-size laser radar body, utilizes mounting bar and spout looks adaptation, and through the spacing slip of spacing groove and stopper, can play preliminary spacing fixed action to small-size laser radar body, the cooperation threaded rod with change the cover, can realize not needing to dismantle with the help of the instrument to the fastening process of small-size laser radar body, the process of operation is simple, convenient to use.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an oil-electricity hybrid unmanned aerial vehicle carrying a small laser radar.
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. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
Small-size lidar needs manual installation on unmanned aerial vehicle before carrying out the operation task, and current hybrid unmanned aerial vehicle of oil electricity is when the small-size lidar of installation, mostly fastens through a plurality of bolts, need dismantle with the help of the instrument during dismantlement, and the process of operation is loaded down with trivial details to unmanned aerial vehicle's wing is fixed, can not accomodate after falling to the ground, and is inconvenient to place. The common electric unmanned aerial vehicle mostly adopts a lithium battery as a power source, and the short endurance time of the common electric unmanned aerial vehicle also becomes an industry pain point. Therefore, the hybrid oil-electricity unmanned aerial vehicle carrying the small laser radar is provided.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides an oil-electricity hybrid unmanned aerial vehicle carrying a small laser radar, and solves the problems that the existing oil-electricity hybrid unmanned aerial vehicle is inconvenient to install and disassemble when the small laser radar is installed, the wings of the unmanned aerial vehicle are fixed, and the unmanned aerial vehicle cannot be accommodated after falling to the ground; meanwhile, the problem that the common electric unmanned aerial vehicle mostly adopts a lithium battery and has short endurance time is solved.
In order to achieve the purpose, the invention is realized by the following technical scheme: a gasoline-electric hybrid unmanned aerial vehicle carrying a small laser radar comprises an unmanned aerial vehicle body and a driving mechanism, wherein two sides of the bottom of the unmanned aerial vehicle body are fixedly connected with supporting frames, the top of the unmanned aerial vehicle body is movably connected with the small laser radar body, the bottom of the small laser radar body is fixedly connected with a mounting bar, one side of the mounting bar extends to the outside of the small laser radar body, the top of the unmanned aerial vehicle body is provided with a sliding groove, two sides of the inner wall of the sliding groove are provided with limiting grooves, two sides of the mounting bar are fixedly connected with limiting blocks, the outer surfaces of the two limiting blocks are in sliding connection with the inner surface of the limiting grooves, the back of the unmanned aerial vehicle body is in threaded connection with a threaded rod, one end of the threaded rod penetrates through the unmanned aerial vehicle body and extends to the inside of the, the other end of the threaded rod is fixedly connected with a rotating sleeve.
Preferably, the driving mechanism comprises a driving motor and a driving blade, and the surface of the output of the driving motor is fixedly connected with the inner surface of the driving blade.
Preferably, the equal fixedly connected with sliding sleeve in below of unmanned aerial vehicle body both sides, two the equal sliding connection of internal surface of sliding sleeve has the slide bar.
Preferably, the top ends of the two sliding rods are fixedly connected with fixing seats, and one side of each fixing seat is fixedly connected with one side of a driving motor.
Preferably, the equal fixedly connected with hydraulic stem in both sides of unmanned aerial vehicle body, two the one end that the hydraulic stem was kept away from each other all with one side fixed connection of fixing base.
Preferably, the bottom fixedly connected with camera device of unmanned aerial vehicle body, and the fixed surface of unmanned aerial vehicle body is connected with the buffering strip, the bilateral symmetry sets up around the unmanned aerial vehicle body of buffering strip.
Advantageous effects
The invention provides an oil-electricity hybrid unmanned aerial vehicle carrying a small laser radar. Compared with the prior art, the method has the following beneficial effects:
(1) the oil-electricity hybrid unmanned aerial vehicle carrying the small laser radar comprises an unmanned aerial vehicle body, wherein the top of the unmanned aerial vehicle body is movably connected with the small laser radar body, the bottom of the small laser radar body is fixedly connected with a mounting bar, one side of the mounting bar extends to the outside of the small laser radar body, the top of the unmanned aerial vehicle body is provided with a sliding groove, two sides of the inner wall of the sliding groove are respectively provided with a limiting block, the outer surfaces of the two limiting blocks are respectively connected with the inner surface of the limiting groove in a sliding manner, the back surface of the unmanned aerial vehicle body is in threaded connection with a threaded rod, one end of the threaded rod penetrates through the unmanned aerial vehicle body and extends into the sliding groove, one end of the threaded rod is in threaded connection with the back surface of the mounting bar, the other end of the threaded rod is fixedly connected with a rotating, through the spacing slip of spacing groove and stopper, can play preliminary spacing fixed action to small-size laser radar body, cooperation threaded rod and commentaries on classics cover can realize not needing to dismantle with the help of the instrument the fastening process to small-size laser radar body, and the process of operation is simple, convenient to use.
(2) This carry on hybrid unmanned aerial vehicle of small-size laser radar, through including driving motor and driving vane at actuating mechanism, the surface of driving motor output and driving vane's internal surface fixed connection, the equal fixedly connected with sliding sleeve in below of unmanned aerial vehicle body both sides, the equal sliding connection of internal surface of two sliding sleeves has the slide bar, the equal fixedly connected with fixing base in top of two slide bars, one side of fixing base and one side fixed connection of driving motor, the equal fixedly connected with hydraulic stem in both sides of unmanned aerial vehicle body, the one end that two hydraulic stems kept away from each other all with one side fixed connection of fixing base, fix actuating mechanism through setting up the fixing base, the cooperation sliding sleeve, slide bar and hydraulic stem, can realize the flexible of unmanned aerial vehicle wing, can accomodate after falling to the ground, conveniently place.
(3) This carry on hybrid unmanned aerial vehicle of small-size laser radar, bottom fixedly connected with camera device through at the unmanned aerial vehicle body, and the fixed surface of unmanned aerial vehicle body is connected with the buffering strip, the bilateral symmetry sets up around the buffering strip at the unmanned aerial vehicle body, through setting up camera device, can conveniently take notes the movement track of unmanned aerial vehicle body, set up the buffering strip around the unmanned aerial vehicle body, can play fine guard action to the unmanned aerial vehicle body, general electric drive carries on laser radar's unmanned aerial vehicle, the duration only has 20 minutes, adopt hybrid power driven unmanned aerial vehicle, it can reach 90 minutes to carry on laser radar duration, very big promotion carries on small-size laser radar's unmanned aerial vehicle duration, unmanned aerial vehicle's work efficiency has been improved, it is more convenient to use.
Drawings
FIG. 1 is a front view of the outer structure of the present invention;
FIG. 2 is a front view of a portion of the present invention;
FIG. 3 is a top view of a portion of the structure of the present invention;
fig. 4 is a partial enlarged view of the invention at a in fig. 3.
In the figure: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, a driving mechanism 2, a driving motor 21, a driving blade 22, a supporting frame 3, a small laser radar body 4, a mounting bar 5, a sliding groove 6, a limiting groove 7, a limiting block 8, a threaded rod 9, a rotating sleeve 10, a camera device 11, a buffer bar 12, a sliding sleeve 13, a sliding rod 14, a fixed seat 15 and a hydraulic rod 16.
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. 1-4, the present invention provides a technical solution: a gasoline-electricity hybrid unmanned aerial vehicle carrying a small laser radar comprises an unmanned aerial vehicle body 1 and a driving mechanism 2, wherein the unmanned aerial vehicle body 1 is driven by gasoline-electricity hybrid power, a camera device 11 is fixedly connected to the bottom of the unmanned aerial vehicle body 1, the motion track of the unmanned aerial vehicle body 1 can be conveniently recorded by arranging the camera device 11, a buffer strip 12 is fixedly connected to the surface of the unmanned aerial vehicle body 1, the buffer strips 12 are arranged at the front and the back of the unmanned aerial vehicle body 1 and can play a good protection role on the unmanned aerial vehicle body 1, the buffer strips 12 are symmetrically arranged at the front and the back of the unmanned aerial vehicle body 1, hydraulic rods 16 are fixedly connected to both sides of the unmanned aerial vehicle body 1, the hydraulic rods 16 are electrically connected with an external power supply, the ends of the two hydraulic rods 16, which are far away from each other, are fixedly connected with one side of a, the inner surfaces of the two sliding sleeves 13 are both connected with sliding rods 14 in a sliding manner, the top ends of the two sliding rods 14 are both fixedly connected with a fixed seat 15, one side of the fixed seat 15 is fixedly connected with one side of a driving motor 21, a driving mechanism 2 comprises a driving motor 21 and a driving blade 22, the driving motor 21 is electrically connected with an external power supply, the surface output by the driving motor 21 is fixedly connected with the inner surface of the driving blade 22, two sides of the bottom of an unmanned aerial vehicle body 1 are both fixedly connected with supporting frames 3, the top of the unmanned aerial vehicle body 1 is movably connected with a small laser radar body 4, the laser radar is a radar system for detecting the position, the speed and other characteristic quantities of a target by emitting laser beams, the working principle is to emit detection signals (laser beams) to the target, then the received signals (target echoes) reflected from the target, relevant information of the target, such as target distance, azimuth, altitude, speed, attitude, even shape and other parameters, can be obtained, so that the target such as an airplane, a missile and the like can be detected, tracked and identified; the novel unmanned aerial vehicle comprises a laser transmitter, an optical receiver, a rotary table, an information processing system and the like, wherein the laser changes electric pulses into optical pulses to be transmitted out, the optical receiver restores the optical pulses reflected from a target into electric pulses to be transmitted to a display, the bottom of a small laser radar body 4 is fixedly connected with a mounting bar 5, one side of the mounting bar 5 extends to the outside of the small laser radar body 4, the top of the unmanned aerial vehicle body 1 is provided with a chute 6, two sides of the inner wall of the chute 6 are both provided with limiting grooves 7, two sides of the mounting bar 5 are both fixedly connected with limiting blocks 8, the outer surfaces of the two limiting blocks 8 are both in sliding connection with the inner surfaces of the limiting grooves 7, the back of the unmanned aerial vehicle body 1 is in threaded connection with a threaded rod 9, one end of the threaded rod 9 penetrates through the unmanned aerial vehicle body 1 and extends to the, the other end fixedly connected with of threaded rod 9 changes cover 10, bottom through at small-size laser radar body 4 sets up mounting bar 5, utilize mounting bar 5 and 6 looks adaptations of spout, spacing slip through spacing groove 7 and stopper 8, can play preliminary spacing fixed action to small-size laser radar body 4, cooperation threaded rod 9 with change cover 10, can realize the fastening process to small-size laser radar body 4, need not dismantle with the help of the instrument, the process of operation is simple, high durability and convenient use, the content of not doing detailed description in this specification simultaneously all belongs to the well-known prior art of technical staff in the field.
When the small laser radar fixing device works, firstly, the small laser radar body 4 is placed at the top of the unmanned aerial vehicle body 1, so that the mounting bar 5 at the bottom of the small laser radar body 4 is matched with the sliding groove 6, then the limiting blocks 8 at two sides of the mounting bar 5 slide along the inner surface of the limiting groove 7, when the limiting blocks 8 abut against the innermost side of the limiting groove 7, a preliminary limiting fixing effect can be achieved on the small laser radar body 4, at the moment, the rotating sleeve 10 is rotated to drive the threaded rod 9 to rotate, the threaded rod 9 is clamped into the mounting bar 5, the fastening process of the small laser radar body 4 can be realized, the small laser radar fixing device does not need to be disassembled by means of tools, the operation process is simple, the use is convenient, at the moment, the driving motor 21 is started, the driving blade 22 is rotated to provide power, when the small laser radar fixing device is used, reverse operation for hydraulic stem 16 to the inboard accomodate actuating mechanism 2 can, above be exactly the whole theory of operation of the hybrid unmanned aerial vehicle of the oil electricity that carries on small-size laser radar.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
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 invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a carry on small-size laser radar's hybrid unmanned aerial vehicle, includes unmanned aerial vehicle body (1) and actuating mechanism (2), the equal fixedly connected with support frame (3) in both sides of unmanned aerial vehicle body (1) bottom, its characterized in that: the top of the unmanned aerial vehicle body (1) is movably connected with a small laser radar body (4), the bottom of the small laser radar body (4) is fixedly connected with a mounting bar (5), one side of the mounting bar (5) extends to the outside of the small laser radar body (4), the top of the unmanned aerial vehicle body (1) is provided with a sliding groove (6), two sides of the inner wall of the sliding groove (6) are respectively provided with a limiting groove (7), two sides of the mounting bar (5) are respectively fixedly connected with a limiting block (8), the outer surfaces of the two limiting blocks (8) are respectively in sliding connection with the inner surface of the limiting groove (7), the back of the unmanned aerial vehicle body (1) is in threaded connection with a threaded rod (9), one end of the threaded rod (9) penetrates through the unmanned aerial vehicle body (1) and extends to the inside of the sliding groove (6), one end of the threaded rod (9) is in threaded connection with, the other end of the threaded rod (9) is fixedly connected with a rotating sleeve (10).
2. The hybrid unmanned aerial vehicle carrying a small laser radar as claimed in claim 1, wherein: the driving mechanism (2) comprises a driving motor (21) and a driving blade (22), and the surface output by the driving motor (21) is fixedly connected with the inner surface of the driving blade (22).
3. The hybrid unmanned aerial vehicle carrying a small laser radar as claimed in claim 1, wherein: the equal fixedly connected with sliding sleeve (13) in below of unmanned aerial vehicle body (1) both sides, two the equal sliding connection of internal surface of sliding sleeve (13) has slide bar (14).
4. The hybrid unmanned aerial vehicle carrying a small laser radar as claimed in claim 3, wherein: the top of two slide bar (14) all fixedly connected with fixing base (15), one side of fixing base (15) and one side fixed connection of driving motor (21).
5. The hybrid unmanned aerial vehicle carrying a small laser radar as claimed in claim 1, wherein: the equal fixedly connected with hydraulic stem (16) in both sides of unmanned aerial vehicle body (1), two the one end that hydraulic stem (16) kept away from each other all with one side fixed connection of fixing base (15).
6. The hybrid unmanned aerial vehicle carrying a small laser radar as claimed in claim 1, wherein: the bottom fixedly connected with camera device (11) of unmanned aerial vehicle body (1), and the fixed surface of unmanned aerial vehicle body (1) is connected with buffering strip (12), buffering strip (12) bilateral symmetry sets up around unmanned aerial vehicle body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010234021.5A CN111361725A (en) | 2020-03-28 | 2020-03-28 | Carry on small-size laser radar's oil-electricity and mix unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010234021.5A CN111361725A (en) | 2020-03-28 | 2020-03-28 | Carry on small-size laser radar's oil-electricity and mix unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN111361725A true CN111361725A (en) | 2020-07-03 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202010234021.5A Pending CN111361725A (en) | 2020-03-28 | 2020-03-28 | Carry on small-size laser radar's oil-electricity and mix unmanned aerial vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111824441A (en) * | 2020-07-24 | 2020-10-27 | 河南交通职业技术学院 | Unmanned aerial vehicle radar detection device for roads and bridges |
| CN112173113A (en) * | 2020-11-12 | 2021-01-05 | 重庆凯创荣智能科技有限公司 | Damping device of high-altitude rescue unmanned aerial vehicle and using method |
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| CN107826244A (en) * | 2017-11-15 | 2018-03-23 | 安徽工程大学 | A kind of six shaft rotating devices of aircraft |
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| CN111824441A (en) * | 2020-07-24 | 2020-10-27 | 河南交通职业技术学院 | Unmanned aerial vehicle radar detection device for roads and bridges |
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| CN112173113A (en) * | 2020-11-12 | 2021-01-05 | 重庆凯创荣智能科技有限公司 | Damping device of high-altitude rescue unmanned aerial vehicle and using method |
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