CN107933901A - A kind of multifunction aircraft - Google Patents
A kind of multifunction aircraft Download PDFInfo
- Publication number
- CN107933901A CN107933901A CN201711186196.8A CN201711186196A CN107933901A CN 107933901 A CN107933901 A CN 107933901A CN 201711186196 A CN201711186196 A CN 201711186196A CN 107933901 A CN107933901 A CN 107933901A
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- Prior art keywords
- plate
- welded
- rack
- horn
- shaft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000005259 measurement Methods 0.000 claims abstract description 16
- 238000009434 installation Methods 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- 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
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The invention discloses a kind of multifunction aircraft, including rack, the surrounding of the rack is welded with horn, and four horns are symmetrical arranged two-by-two, the bottom of the rack is welded with four landing chassis, and four landing chassis are symmetrical arranged two-by-two, placing groove is offered at the top of the rack, and electric power supply control system is installed in placing groove, the bottom of the landing chassis is provided with pulley, and the both sides of horn are installed with infrared distance measurement equipment, the top side that two horns on same level axis are located remotely from each other is rotatablely equipped with propeller, the bottom of the horn is installed with supply line's group, and it is installed with LED light at the top of a horn in four horns.Practicality of the present invention is high, by infrared distance measurement equipment and GPS, easy to aircraft road, aircraft is effectively protected, and prevent the loss of aircraft, and by spring and shaft, easy to which the angle of camera device is adjusted.
Description
Technical field
The present invention relates to vehicle technology field, more particularly to a kind of multifunction aircraft.
Background technology
Nowadays aircraft applications is more and more extensive, there is very wide application prospect in military and civilian field, and
Aircraft is mostly driven using motor, and small with noise, the advantages that being quick on the draw, and Flight Vehicle Structure is simple, is easily manipulated,
It can realize and target is monitored from the air, meet demand of taking photo by plane of photographer etc., through retrieval, mandate publication No. is
A kind of multifunction aircraft disclosed in CN206520756U, including upper shell and lower housing shell, the upper shell top are equipped with more
A flying rotor for being used to fly, lower housing shell bottom are equipped with multiple underwater propellers for underwater propulsion, the upper shell with
The both sides place of being combined of lower housing shell is respectively equipped with a passage, and the lower housing shell is equipped with the rotation that can fly from the side that two wing passages stretch out
Swing device, the passway both sides of upper shell and lower housing shell the junction passage are equipped with a pair of guide rails, it is described per a pair of guide rails on
Equipped with a slide plate, slide plate is equipped with the side underwater propeller being vertically arranged, and is equipped with sealing baffle at the top of the passway, side is underwater
Tablet is equipped with the top of propeller, sealing device is equipped between the tablet and sealing baffle, it can not only realize aerial fly
Row, the navigation of the water surface, moreover it is possible to complete the action moved under water under water, realize flights of dwelling truly more, its is easy to operate, can be with
Used as a platform or carrier, but it amphibious can only fly, comprehensive function is less, and camera devices most at present
It is not easy to carry out angular adjustment, it is impossible to carry out comprehensive shooting, therefore we have proposed a kind of multifunction aircraft to be used for
Solve the above problems.
The content of the invention
Based on technical problem existing for background technology, the present invention proposes a kind of multifunction aircraft.
A kind of multifunction aircraft proposed by the present invention, including rack, the surrounding of the rack are welded with horn, and four
A horn is symmetrical arranged two-by-two, and the bottom of the rack is welded with four landing chassis, and four landing chassis are symmetrical arranged two-by-two, institute
State and placing groove is offered at the top of rack, and electric power supply control system is installed in placing groove, the bottom of the landing chassis is provided with
Pulley, and the both sides of horn are installed with infrared distance measurement equipment, two on same level axis horn is mutually remote
From top side be rotatablely equipped with propeller, the bottom of the horn is installed with supply line's group, and four horns
In a horn at the top of be installed with LED light, line joint, and four horns are installed with the top of the rack
In a horn at the top of be installed with GPS.
Preferably, the bottom of the rack is welded with two symmetrically arranged vertical plates, and the bottom weldering of two vertical plates
Same bottom plate is connected to, mounting groove is offered at the top of the bottom plate, and push-rod electric machine is installed in mounting groove, the push rod electricity
Connecting plate is welded with the output shaft of machine, and pushing plate is welded with the top of connecting plate, is rotatablely equipped with the top of the bottom plate
Rotor plate, and the side that two rotor plates are located remotely from each other is welded with multiple springs, multiple bullets on same rotor plate
The same end of spring is welded on same vertical plate, and the pushing plate is in contact with two rotor plates, and two rotor plates
Top contact have same movable plate, two vertical plate sides close to each other offer shifting chute, the movable plate
Both sides are extended respectively in two shifting chutes, and the top both sides of movable plate are welded with placement plate, two placement plates it is same
Side is equipped with shaft, and two vertical plate sides close to each other offer rotation slot, and the both ends of the shaft extend respectively to
In corresponding rotation slot, and the bottom of shaft is welded with fixed plate, and the side of the fixed plate is installed with camera device.
Preferably, the propeller includes two screw rods, and two screw rods are symmetrical arranged.
Preferably, infrared distance measurement equipment, LED light, GPS and the camera device pass through supply line's group and power supply control
System is electrically connected.
Preferably, the landing chassis is arcuate structure.
Preferably, sliding block is installed, the inner wall of rotation slot is equipped with endless glide, and sliding block and ring on the outside of the shaft
Shape slide is slidably connected.
Preferably, the quantity of the spring on same rotor plate is two to four, and two to four springs are equidistant
It is welded in the side of corresponding vertical plate.
Preferably, the bottom of the push-rod electric machine is welded with installing plate, and push-rod electric machine is screwed on by installing plate
In the bottom interior wall of mounting groove.
Preferably, the placement plate is provided with first gear close to the side of shaft, and shaft is pacified close to the side of placement plate
Equipped with second gear, and first gear is meshed with second gear.
Preferably, the side inner wall that the both sides of the movable plate are located remotely from each other with two shifting chutes respectively is slidably connected.
Compared with prior art, the beneficial effects of the invention are as follows：
(1) rack, horn, camera device, landing chassis, electric power supply control system, pulley, infrared distance measurement equipment and spiral are passed through
Paddle is engaged, easy to aircraft road, be effectively protected aircraft；
(2) it is engaged by supply line's group, LED light, line joint and GPS, accurately aircraft is positioned, is prevented
The only loss of aircraft；
(3) by vertical plate, bottom plate, mounting groove, push-rod electric machine, connecting plate, pushing plate, rotor plate, spring, movable plate,
Shifting chute, placement plate, shaft, rotation slot and fixed plate are engaged, and start push-rod electric machine, and the output shaft of push-rod electric machine drives connection
Plate is moved, and connecting plate drives pushing plate to be moved, and pushing plate drives rotor plate to be rotated, rotor plate extruding spring,
Rotor plate drives movable plate to be moved at the same time, and movable plate drives shaft to be rotated by placement plate, easy to camera device
Angle be adjusted.
Practicality of the present invention is high, by infrared distance measurement equipment and GPS, easy to aircraft road, be effectively protected winged
Row device, and prevent the loss of aircraft, and by spring and shaft, easy to which the angle of camera device is adjusted.
Brief description of the drawings
Fig. 1 is a kind of structure diagram of multifunction aircraft proposed by the present invention；
Fig. 2 is a kind of main structure diagram of multifunction aircraft proposed by the present invention；
Fig. 3 is a kind of overlooking the structure diagram of multifunction aircraft proposed by the present invention；
Fig. 4 is a kind of side structure schematic view of multifunction aircraft proposed by the present invention；
Fig. 5 is the partial structurtes signal of the camera device in a kind of fixed plate of multifunction aircraft proposed by the present invention
Figure.
In figure：1 rack, 2 horns, 3 camera devices, 4 landing chassis, 5 electric power supply control systems, 6 pulleys, 7 infrared distance measurement equipment,
8 propellers, 9 supply line's groups, 10LED lamps, 11 line joints, 12GPS, 13 vertical plates, 14 bottom plates, 15 mounting grooves, 16 push rods
Motor, 17 connecting plates, 18 pushing plates, 19 rotor plates, 20 springs, 21 movable plates, 22 shifting chutes, 23 placement plates, 24 shafts, 25 turns
Dynamic groove, 26 fixed plates.
Embodiment
The present invention is made with reference to specific embodiment further to explain.
Embodiment
With reference to Fig. 1-5, a kind of multifunction aircraft, including rack 1 are proposed in the present embodiment, the surrounding of rack 1 is welded
Horn 2 is connected to, and four horns 2 are symmetrical arranged two-by-two, the bottom of rack 1 is welded with four landing chassis 4, and four landing chassis 4
It is symmetrical arranged two-by-two, the top of rack 1 offers placing groove, and electric power supply control system 5 is provided with placing groove, landing chassis 4
Bottom is provided with pulley 6, and the both sides of horn 2 are installed with infrared distance measurement equipment 7, and two on same level axis
The top side that a horn 2 is located remotely from each other is rotatablely equipped with propeller 8, and the bottom of horn 2 is installed with supply line's group
9, and the top of a horn 2 in four horns 2 is installed with LED light 10, the top of rack 1 is installed with circuit and connects
First 11, and the top of a horn 2 in four horns 2 is installed with GPS 12, passes through rack 1, horn 2, camera device
3rd, landing chassis 4, electric power supply control system 5, pulley 6, infrared distance measurement equipment 7 and propeller 8 are engaged, easy to aircraft road,
It is effectively protected aircraft；It is engaged by supply line's group 9, LED light 10, line joint 11 and GPS 12, it is accurately right
Aircraft is positioned, and prevents the loss of aircraft；Pass through vertical plate 13, bottom plate 14, mounting groove 15, push-rod electric machine 16, connection
Plate 17, pushing plate 18, rotor plate 19, spring 20, movable plate 21, shifting chute 22, placement plate 23, shaft 24, rotation slot 25 and solid
Fixed board 26 is engaged, and starts push-rod electric machine 16, and the output shaft of push-rod electric machine 16 drives connecting plate 17 to be moved, 17 band of connecting plate
Dynamic pushing plate 18 is moved, and pushing plate 18 drives rotor plate 19 to be rotated, and rotor plate 19 extrudes spring 20, while rotor plate
19 drive movable plates 21 are moved, and movable plate 21 drives shaft 24 to be rotated by placement plate 23, easy to camera device 3
Angle be adjusted, practicality of the present invention is high, by infrared distance measurement equipment 7 and GPS 12, easy to aircraft road, effectively
Protect aircraft, and the loss of aircraft is prevented, and by spring 20 and shaft 24, easy to the angle to camera device 3
Degree is adjusted.
In the present embodiment, the bottom of rack 1 is welded with two symmetrically arranged vertical plates 13, and the bottom of two vertical plates 13
Portion is welded with same bottom plate 14, and the top of bottom plate 14 offers mounting groove 15, and push-rod electric machine 16 is provided with mounting groove 15,
Connecting plate 17 is welded with the output shaft of push-rod electric machine 16, and the top of connecting plate 17 is welded with pushing plate 18, the top of bottom plate 14
Portion is rotatablely equipped with rotor plate 19, and the side that two rotor plates 19 are located remotely from each other is welded with multiple springs 20, positioned at same
The same end of multiple springs 20 on a rotor plate 19 is welded on same vertical plate 13, pushing plate 18 and two rotor plates
19 are in contact, and the top contact of two rotor plates 19 has a same movable plate 21, two vertical plates 13 it is close to each other one
Side offers shifting chute 22, and the both sides of movable plate 21 are extended respectively in two shifting chutes 22, and the top two of movable plate 21
Side is welded with placement plate 23, and the same sides of two placement plates 23 is equipped with shaft 24, and two vertical plates 13 it is close to each other one
Side offers rotation slot 25, and the both ends of shaft 24 are extended respectively in corresponding rotation slot 25, and the bottom weldering of shaft 24
Fixed plate 26 is connected to, the side of fixed plate 26 is installed with camera device 3, and propeller 8 includes two screw rods, and two spiral shells
Swing arm is symmetrical arranged, and infrared distance measurement equipment 7, LED light 10, GPS 12 and camera device 3 are automatically controlled by supply line's group 9 and confession
System 5 processed is electrically connected, and landing chassis 4 is arcuate structure, and the outside of shaft 24 is provided with sliding block, and the inner wall of rotation slot 25 is equipped with
Endless glide, and sliding block is slidably connected with endless glide, the quantity of the spring 20 on same rotor plate 19 is two to four
It is a, and two to four springs 20 are equidistantly welded in the side of corresponding vertical plate 13, the bottom of push-rod electric machine 16 is welded with
Installing plate, and push-rod electric machine 16 is screwed on by installing plate in the bottom interior wall of mounting groove 15, placement plate 23 is close to shaft
24 side is provided with first gear, and shaft 24 is provided with second gear close to the side of placement plate 23, and first gear and the
Two gears are meshed, and the side inner wall that the both sides of movable plate 21 are located remotely from each other with two shifting chutes 22 respectively is slidably connected, and passes through
Rack 1, horn 2, camera device 3, landing chassis 4, electric power supply control system 5, pulley 6, infrared distance measurement equipment 7 and propeller 8 match
Close, easy to aircraft road, be effectively protected aircraft；Pass through supply line's group 9, LED light 10,11 and of line joint
GPS 12 is engaged, and accurately aircraft is positioned, and prevents the loss of aircraft；Pass through vertical plate 13, bottom plate 14, installation
Groove 15, push-rod electric machine 16, connecting plate 17, pushing plate 18, rotor plate 19, spring 20, movable plate 21, shifting chute 22, placement plate 23,
Shaft 24, rotation slot 25 and fixed plate 26 are engaged, and start push-rod electric machine 16, and the output shaft of push-rod electric machine 16 drives connecting plate 17
Moved, connecting plate 17 drives pushing plate 18 to be moved, and pushing plate 18 drives rotor plate 19 to be rotated, and rotor plate 19 squeezes
Pressing spring 20, while rotor plate 19 drives movable plate 21 to be moved, movable plate 21 drives shaft 24 to carry out by placement plate 23
Rotate, easy to which the angle of camera device 3 is adjusted, practicality of the present invention is high, by infrared distance measurement equipment 7 and GPS 12,
Easy to aircraft road, be effectively protected aircraft, and prevent the loss of aircraft, and pass through spring 20 and shaft
24, easy to which the angle of camera device 3 is adjusted.
In the present embodiment, in use, due to the presence of infrared distance measurement equipment 7, LED light 10 and GPS 12, easy to aircraft
Road, be effectively protected aircraft, and prevent the loss of aircraft, start push-rod electric machine 16, the output of push-rod electric machine 16
Axis drives connecting plate 17 to be moved, and connecting plate 17 drives pushing plate 18 to be moved, and pushing plate 18 drives rotor plate 19 to carry out
Rotate, rotor plate 19 extrudes spring 20, while rotor plate 19 drives movable plate 21 to be moved so that movable plate 21 is in shifting chute
Slided on 22 inner wall, movable plate 21 drives placement plate 23 to be moved, the first gear in placement plate 23 and shaft 24
On second gear be meshed so that shaft 24 is rotated, shaft 24 drive fixed plate 26 rotated, fixed plate 26 drives
Camera device 3 is rotated, easy to which the angle of camera device 3 is adjusted.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art the invention discloses technical scope in, technique according to the invention scheme and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (9)
1. a kind of multifunction aircraft, including rack (1), it is characterised in that the surrounding of the rack (1) is welded with horn
(2), and four horns (2) are symmetrical arranged two-by-two, and the bottom of the rack (1) is welded with four landing chassis (4), and four landings
Frame (4) is symmetrical arranged two-by-two, offers placing groove at the top of the rack (1), and electric power supply control system is provided with placing groove
(5), the bottom of the landing chassis (4) is provided with pulley (6), and the both sides of horn (2) are installed with infrared distance measurement equipment
(7), the top side that two horns (2) on same level axis are located remotely from each other is rotatablely equipped with propeller (8), institute
The bottom for stating horn (2) is installed with supply line's group (9), and the top of a horn (2) in four horns (2) is fixed
LED light (10) is installed, line joint (11), and one in four horns (2) are installed with the top of the rack (1)
GPS (12) is installed with the top of horn (2), the bottom of the rack (1) is welded with two symmetrically arranged vertical plates
(13), and the bottoms of two vertical plates (13) is welded with same bottom plate (14), and installation is offered at the top of the bottom plate (14)
Groove (15), and push-rod electric machine (16) is installed in mounting groove (15), it is welded with connection on the output shaft of the push-rod electric machine (16)
Plate (17), and pushing plate (18) is welded with the top of connecting plate (17), it is rotatablely equipped with rotor plate at the top of the bottom plate (14)
(19), and the side that is located remotely from each other of two rotor plates (19) is welded with multiple springs (20), positioned at same rotor plate (19)
On the same ends of multiple springs (20) be welded on same vertical plate (13), the pushing plate (18) and two rotor plates
(19) it is in contact, and the top contact of two rotor plates (19) has same movable plate (21), two vertical plates (13) are mutual
Close side offers shifting chute (22), and the both sides of the movable plate (21) are extended respectively in two shifting chutes (22),
And the top both sides of movable plate (21) are welded with placement plate (23), the same side of two placement plates (23) is equipped with shaft (24),
And two vertical plate (13) sides close to each other offer rotation slot (25), the both ends of the shaft (24) extend respectively to
In corresponding rotation slot (25), and the bottom of shaft (24) is welded with fixed plate (26), and the side of the fixed plate (26) is consolidated
Dingan County is equipped with camera device (3).
2. a kind of multifunction aircraft according to claim 1, it is characterised in that the propeller (8) includes two spiral shells
Swing arm, and two screw rods are symmetrical arranged.
3. a kind of multifunction aircraft according to claim 1, it is characterised in that the infrared distance measurement equipment (7), LED
Lamp (10), GPS (12) and camera device (3) are electrically connected by supply line's group (9) and electric power supply control system (5).
4. a kind of multifunction aircraft according to claim 1, it is characterised in that the landing chassis (4) is arcuate structure.
5. a kind of multifunction aircraft according to claim 2, it is characterised in that be provided with the outside of the shaft (24)
Sliding block, the inner wall of rotation slot (25) is equipped with endless glide, and sliding block is slidably connected with endless glide.
6. a kind of multifunction aircraft according to claim 2, it is characterised in that on same rotor plate (19)
The quantity of spring (20) is two to four, and two to four springs (20) are equidistantly welded in the one of corresponding vertical plate (13)
Side.
A kind of 7. multifunction aircraft according to claim 2, it is characterised in that the bottom weldering of the push-rod electric machine (16)
Installing plate is connected to, and push-rod electric machine (16) is screwed on by installing plate in the bottom interior wall of mounting groove (15).
8. a kind of multifunction aircraft according to claim 2, it is characterised in that the placement plate (23) is close to shaft
(24) side is provided with first gear, and shaft (24) is provided with second gear, and the first tooth close to the side of placement plate (23)
Wheel is meshed with second gear.
A kind of 9. multifunction aircraft according to claim 2, it is characterised in that the both sides difference of the movable plate (21)
The side inner wall being located remotely from each other with two shifting chutes (22) is slidably connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711186196.8A CN107933901A (en) | 2017-11-24 | 2017-11-24 | A kind of multifunction aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711186196.8A CN107933901A (en) | 2017-11-24 | 2017-11-24 | A kind of multifunction aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107933901A true CN107933901A (en) | 2018-04-20 |
Family
ID=61930192
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711186196.8A Pending CN107933901A (en) | 2017-11-24 | 2017-11-24 | A kind of multifunction aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107933901A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205837224U (en) * | 2016-07-15 | 2016-12-28 | 张宇川 | A kind of scalable is taken photo by plane unmanned plane |
| CN106647790A (en) * | 2016-12-27 | 2017-05-10 | 重庆大学 | Four-rotor unmanned aerial vehicle aircraft system oriented to complex environment and flying method |
| CN107315423A (en) * | 2017-08-23 | 2017-11-03 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of new patrol unmanned machine inspection device and method for inspecting |
| US10060746B2 (en) * | 2014-03-24 | 2018-08-28 | SZ DJI Technology Co., Ltd | Methods and systems for determining a state of an unmanned aerial vehicle |
| EP3408175A1 (en) * | 2016-01-25 | 2018-12-05 | Above Surveying Ltd. | Utilising uavs for detecting defects in solar panel arrays |
-
2017
- 2017-11-24 CN CN201711186196.8A patent/CN107933901A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10060746B2 (en) * | 2014-03-24 | 2018-08-28 | SZ DJI Technology Co., Ltd | Methods and systems for determining a state of an unmanned aerial vehicle |
| EP3408175A1 (en) * | 2016-01-25 | 2018-12-05 | Above Surveying Ltd. | Utilising uavs for detecting defects in solar panel arrays |
| CN205837224U (en) * | 2016-07-15 | 2016-12-28 | 张宇川 | A kind of scalable is taken photo by plane unmanned plane |
| CN106647790A (en) * | 2016-12-27 | 2017-05-10 | 重庆大学 | Four-rotor unmanned aerial vehicle aircraft system oriented to complex environment and flying method |
| CN107315423A (en) * | 2017-08-23 | 2017-11-03 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of new patrol unmanned machine inspection device and method for inspecting |
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Effective date of abandoning: 20211126 |