CN107323652A - A kind of empty dual-purpose unmanned plane of water - Google Patents
A kind of empty dual-purpose unmanned plane of water Download PDFInfo
- Publication number
- CN107323652A CN107323652A CN201710577416.3A CN201710577416A CN107323652A CN 107323652 A CN107323652 A CN 107323652A CN 201710577416 A CN201710577416 A CN 201710577416A CN 107323652 A CN107323652 A CN 107323652A
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- China
- Prior art keywords
- unmanned plane
- main body
- fixed
- wing
- motor
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Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- 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
- 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
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Toys (AREA)
- Accessories Of Cameras (AREA)
Abstract
The invention provides a kind of empty dual-purpose unmanned plane of water, it includes unmanned plane main body, the both sides of unmanned plane main body set wing respectively, the bottom surface of wing is fixed with micro-blade pump, the bottom surface at inboard end is hinged with unmanned plane main body, the side one end at inboard end, which is fixed with connecting rod I, the other end and is fixed with bearing, bearing, is provided with guide and limit axle, and support is provided with the track coordinated with guide and limit axle in unmanned plane main body；Also it is fixed with unmanned plane main body on bracket assembly, bracket assembly and motor is installed, motor band movable eccentric wheel is rotated, and eccentric wheel drives push rod to move forward and backward by connecting rod II, is that wing-folding or expansion provide power；The afterbody of the unmanned plane main body is fixed with the tail plate of V-shaped arrangement, the opposite end of the V-arrangement inner chamber of tail plate is symmetrically installed with electric rotating machine, two electric rotating machines can drive empennage hood around the center rotating of motor shaft, auxiliary power is provided for the flight of unmanned plane, the unmanned plane can in the air and underwater operation.
Description
Technical field
The present invention relates to a kind of unmanned plane, especially a kind of empty dual-purpose unmanned plane of water.
Background technology
With the development of science and technology, UAV (abbreviation unmanned plane) application is more and more extensive, and it can be applied to
Take photo by plane, agricultural plant protection, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric power are patrolled
The fields such as inspection, movies-making.But, these operations are simply carried out in the air, it is impossible to carry out operation under water, so as to limit it
Working space, here it is the weak point present in prior art.
The content of the invention
The technical problem to be solved in the present invention, aiming at the deficiency present in prior art, and provides a kind of water sky two
With unmanned plane, the unmanned plane both can operation in the air, can also operation under water, its working space is wide.
This programme is achieved by the following technical measures：The empty dual-purpose unmanned plane of the water includes unmanned plane main body and long-range
Control module, the both sides of the unmanned plane main body are respectively arranged with wing assembly, and the wing assembly includes wing, the bottom of wing
Face is fixed with micro-blade pump, and the outboard end of wing, which is fixed with flank hood, the flank hood, to be provided with by flank motor
The flank propeller of driving, bottom surface and the unmanned plane main body at inboard end are hinged, and the side one end at inboard end is fixed with
Connecting rod I, the other end, which are fixed with bearing, bearing, is provided with guide and limit axle, and support is provided with unmanned plane main body limits with being oriented to
The track that position axle coordinates；Also it is fixed with bracket assembly, bracket assembly in the unmanned plane main body and motor is installed, motor
Output shaft on eccentric wheel is installed, eccentric wheel is hinged by connecting rod II with push rod, and push rod and mounting bracket assembly are connected, two connecting rods
I opposite end is hinged with mounting bracket assembly respectively；The afterbody of the unmanned plane main body is fixed with the tail plate of V-shaped arrangement, tail
The opposite end of the V-arrangement inner chamber of wing plate is symmetrically installed with electric rotating machine, and the output end of two electric rotating machines passes through bearing and empennage respectively
Hood is connected, and empennage motor and the empennage propeller being driven by it are provided with the empennage hood；The unmanned plane main body
Head, which is provided with camera, unmanned plane main body, is additionally provided with main controller module, power module, signal transmitting and receiving module and data
Memory module, power module passes through electromagnetic relay and motor, empennage motor, two micro-blade pumps, two flank motors respectively
With the electrical connection of two electric rotating machines, power module, each electromagnetic relay, signal transmitting and receiving module, camera and data memory module are equal
Electrically connected with main controller module, remote control module is electrically connected with signal transmitting and receiving module.
Above-mentioned connecting rod I and track are the arcuate structure being adapted with wing-folding track, to facilitate wing-folding to pack up or
Expansion.
Vertical support bar has been respectively fixedly connected in the two ends of above-mentioned track, and two vertical support bars are fixedly mounted on unmanned plane main body
On, to be adapted with the height of wing, facilitate wing along track activity.
The anglec of rotation of above-mentioned empennage hood can fly to be rotated along bearing centre 360 according to aerial or underwater operation
Action edge is needed to adjust the angle of empennage hood, and auxiliary power is provided using the flight for realizing empennage propeller as unmanned plane.
Above-mentioned main controller module is MCU chip or dsp chip.
Above-mentioned mounting bracket assembly includes upper mounting plate and lower installation board, and one end is fixed between upper mounting plate and lower installation board
Fixed column, the other end are fixed with hinge, and the push rod is connected with fixed column, and two connecting rod I opposite end is hinged with hinge respectively, is adopted
After this structure, push rod drives upper mounting plate, lower installation board and hinge movable by fixed column, so as to realize two connecting rods
I and then realizes that the folding of wing is packed up or deployed around the rotation of hinge.
Above-mentioned bracket assembly includes support frame, and the upper end of support frame, which is fixed with installing plate, installing plate, is fixed with motor cabinet,
Motor is horizontally arranged on motor cabinet, and the stable support for realizing motor by this structure is installed,.
Above-mentioned flank hood and empennage hood are the rotary structure of both ends open, can both reduce the traveling of unmanned plane
Resistance, can ensure the normal operation of propeller again.
Above-mentioned camera is connected by camera fix bar and unmanned plane main body, can so camera is arranged at nobody
At the housing of owner's body, so as to increase the coverage of camera.
The beneficial effect of this programme：
1st, the unmanned plane both can operation in the air, can also operation under water, in the air during operation, two wings expansion,
In underwater work, two wing-foldings are packed up；
2nd, motor band movable eccentric wheel rotate, eccentric wheel by connecting rod II drive push rod move forward and backward, be wing-folding or
Expansion provides power；
3rd, the pin joint of the bottom surface at inboard end and unmanned plane main body is as the fulcrum of wing-folding, and push rod is by installing
Frame assembly drives two connecting rod I to be rotated around hinge, so that wing is realized using its pin joint with unmanned plane main body as fulcrum, machine
When the wing is rotated, guide and limit axle coordinates with track, realizes that the rotation to wing is oriented to；
4th, two electric rotating machines can drive empennage hood around the center rotating of motor shaft, so as to adjust the axis of empennage propeller
Direction, to adapt to different resistance situations during aerial or underwater operation, auxiliary power is provided for the flight of unmanned plane；
5th, during operation in the air, two wings deploy, two micro-blade air pump inoperatives, now empennage propeller and two flank spiral shells
Rotation oar provides power for the flight of unmanned plane；
6th, under water operation when, two wing-foldings are retracted to the position parallel with unmanned plane direct of travel, to reduce nobody
The running resistance of machine, now two flank propellers do not work, empennage propeller and two micro-blade pumps carry for the flight of unmanned plane
For power.
Brief description of the drawings
Fig. 1 is the structural representation of the specific embodiment of the invention.
Fig. 2 is the broken section structural representation of the specific embodiment of the invention.
Fig. 3 is Fig. 2 side structure schematic view.
Fig. 4 is Fig. 2 dimensional structure diagram.
Fig. 5 is the control principle drawing of the specific embodiment of the invention.
In figure, 1- flank hoods, 2- flank motors, 3- flank propellers, 4- wings, 5- tracks, 6- unmanned plane main bodys, 7-
Tail plate, 8- empennage hoods, 9- empennage motors, 10- bearings, 11- electric rotating machines, 12- empennage propellers, 13- bracket assemblys,
14- connecting rods II, 15- push rod, 16- main controller modules, 17- mounting bracket assemblies, 18- camera fix bars, 19- cameras, 20-
Connecting rod I, 21- hinge, 22- upper mounting plates, 23- lower installation boards, 24- fixed columns, 25- guide and limit axles, 26- bearings, 27- is vertical
Support bar, 28- motor cabinets, 29- installing plates, 30- motor, 31- eccentric wheels, 32- support frames, 33- micro-blade pumps.
Embodiment
For the technical characterstic for illustrating this programme can be understood, below by embodiment, and its accompanying drawing is combined, to we
Case is illustrated.
A kind of empty dual-purpose unmanned plane of water, as illustrated, it includes unmanned plane main body 6 and remote control module, it is described nobody
The both sides of owner's body 6 are respectively arranged with wing assembly, and the wing assembly includes wing 4, and the bottom surface of wing 4 is fixed with manophyll
Piece pump 33, the outboard end of wing 4 is fixed with flank hood 1, and flank hood 1 is the rotary structure of both ends open, the flank
The flank propeller 3 driven by flank motor 2 is provided with hood 1, bottom surface and the unmanned plane main body 6 of the medial extremity of wing 4 are hinged,
The fulcrum that the pin joint rotates as wing 4, side one end of the medial extremity of wing 4 is fixed with connecting rod I20, the other end and is fixed with axle
Hold the rail for being provided with 26, bearing 26 and being supported in guide and limit axle 25, unmanned plane main body 6 and being provided with and coordinate with guide and limit axle 25
Vertical support bar 27 has been respectively fixedly connected in road 5, specifically, the two ends of track 5, and two vertical support bars 27 are fixedly mounted on unmanned plane
In main body 6, to be adapted with the height of wing 4, facilitate wing 4 movable along track 5, connecting rod I20 and track 5 are and the folding of wing 4
The adaptable arcuate structure in folded track, packs up or deploys to facilitate wing 4 to fold.
Also it is fixed with the unmanned plane main body 6 on bracket assembly 13, bracket assembly 13 and motor 30, motor is installed
Eccentric wheel 31 is installed, eccentric wheel 31 is hinged by connecting rod II14 with push rod 15 on 30 output shaft, push rod 15 and mounting bracket are total
It is connected into 17, two connecting rod I20 opposite end is hinged with mounting bracket assembly 17 respectively.Specifically, bracket assembly 13 includes support
Frame 32, the upper end of support frame 32, which is fixed with installing plate 29, installing plate 29, is fixed with motor cabinet 28, and motor 30 is horizontally arranged at
On motor cabinet 28.Mounting bracket assembly 17 includes upper mounting plate 22 and lower installation board 23, between upper mounting plate 22 and lower installation board 23
One end is fixed with fixed column 24, the other end and is fixed with hinge 21, and the push rod 15 is connected with fixed column 24, two connecting rod I20 phase
Opposite end is hinged with hinge 21 respectively.
The afterbody of the unmanned plane main body 6 is fixed with the tail plate 7 of V-shaped arrangement, the V-arrangement inner chamber of tail plate 7 it is relative
End is symmetrically installed with electric rotating machine 11, and the output end of two electric rotating machines 11 is connected by bearing 10 with empennage hood 8 respectively, empennage
Hood 8 is to be provided with empennage motor 9 and the empennage spiral shell being driven by it in the rotary structure of both ends open, the empennage hood 8
Oar 12 is revolved, the anglec of rotation of empennage hood 8, can be according to aerial or underwater operation flight to be rotated along the center 360 of bearing 10
Power needs to adjust the angle of empennage hood 8, to realize that empennage propeller 12 provides auxiliary power for the flight of unmanned plane.
The head (relative one end i.e. with being provided with the afterbody of tail plate 7) of the unmanned plane main body 6 is provided with camera
19, specifically, camera 19 is connected by camera fix bar 18 and unmanned plane main body 6.It is additionally provided with unmanned plane main body 6
Main controller module 16, power module, signal transmitting and receiving module and data memory module, preferably main controller module 16 are MCU core
Piece or dsp chip, power module pass through electromagnetic relay and motor 30, empennage motor 9, two micro-blade pumps 33, two respectively
The electric rotating machine 11 of flank motor 2 and two is electrically connected, power module, each electromagnetic relay, signal transmitting and receiving module, the sum of camera 19
Electrically connected according to memory module with main controller module 16, remote control module is electrically connected with signal transmitting and receiving module, operating personnel
Can be by the flight of remote control module remote control unmanned plane.
In the air during operation, two wings 4 deploy, and main controller module 16 controls two micro-blade pumps 33 not work, and together
When control both sides wing motor 2 and empennage motor 9 work so that realize the flank propeller 3 of empennage propeller 12 and two be unmanned plane
Flight provide power.When wing 4 deploys, motor 30 is rotated with movable eccentric wheel 31, and eccentric wheel 31 is driven by connecting rod II14
(i.e. empennage end) is mobile backward for push rod 15, and power, bottom surface and the unmanned plane main body 6 of the medial extremity of wing 4 are provided for the expansion of wing 4
The fulcrum that pin joint rotates as wing 4, push rod 15 drives two connecting rod I20 to be rotated around hinge 21 by mounting bracket assembly 17, from
And wing 4 is realized using its pin joint with unmanned plane main body 6 as fulcrum, and when wing 4 is rotated, guide and limit axle 25 and track
5 coordinate, and realize that the rotation to wing 4 is oriented to.
Under water during operation, two wings 4 fold and are retracted to the position parallel with unmanned plane direct of travel, to reduce unmanned plane
Running resistance, now two flank propellers 3 do not work, the control empennage motor 9 and two micro-blade pumps of main controller module 16
33 work, so as to realize that the micro-blade pump 33 of empennage propeller 12 and two provides power for the flight of unmanned plane.Wing 4, which is folded, to be received
When rising, motor 30 is rotated with movable eccentric wheel 31, and eccentric wheel 31 drives push rod 15 to move forward by connecting rod II14, is wing 4
Expansion provides power, the fulcrum that the bottom surface of the medial extremity of wing 4 rotates with the pin joint of unmanned plane main body 6 as wing 4, push rod 15
Two connecting rod I20 are driven to be rotated around hinge 21 by mounting bracket assembly 17, so as to realize wing 4 with its hinge with unmanned plane main body 6
Contact is fulcrum, and when wing 4 is rotated, guide and limit axle 25 coordinates with track 5, realizes that the rotation to wing 4 is oriented to.
Technical characteristic (such as water-proof part) in the present invention without description can realize by or using prior art, herein
Repeat no more, certainly, described above is not limitation of the present invention, and the present invention is also not limited to above-mentioned embodiment, this
The variations, modifications, additions or substitutions that the those of ordinary skill in field is made in the essential scope of the present invention, should also belong to this
The protection domain of invention.
Claims (9)
1. a kind of empty dual-purpose unmanned plane of water, it includes unmanned plane main body and remote control module, the both sides of the unmanned plane main body
Wing assembly is respectively arranged with, it is characterized in that：The wing assembly includes wing, and the bottom surface of wing is fixed with micro-blade pump,
The outboard end of wing is fixed with flank hood, the flank hood and is provided with by the motor-driven flank propeller of flank, machine
The bottom surface of wing medial extremity is hinged with unmanned plane main body, and the side one end at inboard end is fixed with connecting rod I, the other end and is fixed with axle
Hold, support in guide and limit axle, unmanned plane main body is installed in bearing the track coordinated with guide and limit axle is installed；The nothing
Also it is fixed with man-machine main body on bracket assembly, bracket assembly and motor is installed, bias is installed on the output shaft of motor
Wheel, eccentric wheel is hinged by connecting rod II with push rod, and push rod is connected with mounting bracket assembly, two connecting rod I opposite end respectively with installation
Frame assembly is hinged；The afterbody of the unmanned plane main body is fixed with the tail plate of V-shaped arrangement, the V-arrangement inner chamber of tail plate it is relative
End is symmetrically installed with electric rotating machine, and the output end of two electric rotating machines is connected by bearing with empennage hood respectively, the empennage machine
Empennage motor and the empennage propeller being driven by it are installed in cover；The head of the unmanned plane main body is provided with camera, nothing
Main controller module, power module, signal transmitting and receiving module and data memory module, power module point are additionally provided with man-machine main body
Do not electrically connected by electromagnetic relay with motor, empennage motor, two micro-blade pumps, two flank motors and two electric rotating machines,
Power module, each electromagnetic relay, signal transmitting and receiving module, camera and data memory module are electrically connected with main controller module
Connect, remote control module is electrically connected with signal transmitting and receiving module.
2. the empty dual-purpose unmanned plane of water according to claim 1, it is characterized in that：The connecting rod I and track are and wing-folding
The adaptable arcuate structure in track.
3. the empty dual-purpose unmanned plane of water according to claim 2, it is characterized in that：The two ends of the track have been respectively fixedly connected vertically
Support bar, two vertical support bars are fixedly mounted in unmanned plane main body.
4. the empty dual-purpose unmanned plane of water according to claim 3, it is characterized in that：The anglec of rotation of the empennage hood is along axle
Center 360 is held to rotate.
5. the empty dual-purpose unmanned plane of water according to claim 4, it is characterized in that：The main controller module be MCU chip or
Dsp chip.
6. the empty dual-purpose unmanned plane of water according to claim 5, it is characterized in that：The mounting bracket assembly include upper mounting plate and
Lower installation board, one end is fixed with fixed column, the other end and is fixed with hinge between upper mounting plate and lower installation board, and the push rod is with consolidating
Fixed column is connected, and two connecting rod I opposite end is hinged with hinge respectively.
7. the empty dual-purpose unmanned plane of water according to claim 6, it is characterized in that：The bracket assembly includes support frame, support
The upper end of frame, which is fixed with installing plate, installing plate, is fixed with motor cabinet, and motor is horizontally arranged on motor cabinet.
8. the empty dual-purpose unmanned plane of water according to claim 7, it is characterized in that：The flank hood and empennage hood are two
The rotary structure of end opening.
9. the empty dual-purpose unmanned plane of water according to claim 8, it is characterized in that：The camera by camera fix bar with
Unmanned plane main body is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710577416.3A CN107323652A (en) | 2017-07-14 | 2017-07-14 | A kind of empty dual-purpose unmanned plane of water |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710577416.3A CN107323652A (en) | 2017-07-14 | 2017-07-14 | A kind of empty dual-purpose unmanned plane of water |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107323652A true CN107323652A (en) | 2017-11-07 |
Family
ID=60227236
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710577416.3A Withdrawn CN107323652A (en) | 2017-07-14 | 2017-07-14 | A kind of empty dual-purpose unmanned plane of water |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107323652A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108284932A (en) * | 2018-01-05 | 2018-07-17 | 惠安耐亚节能科技有限公司 | A kind of underwater anticollision unmanned plane for shooting |
| CN109760836A (en) * | 2019-03-12 | 2019-05-17 | 姜佩奇 | A kind of amphibious submersible of air-sea |
| CN110171562A (en) * | 2019-05-24 | 2019-08-27 | 孙思为 | A kind of unmanned plane rotor control structure |
| CN110979666A (en) * | 2019-12-27 | 2020-04-10 | 浙江大学 | Water-air robot |
| CN111532426A (en) * | 2020-04-22 | 2020-08-14 | 中国空气动力研究与发展中心 | Aircraft with V-shaped empennage and multiple rotors in vertical take-off and landing layout |
| CN113306696A (en) * | 2021-07-07 | 2021-08-27 | 陕西航天时代导航设备有限公司 | Folding wing unfolding mechanism |
| CN113665306A (en) * | 2021-10-25 | 2021-11-19 | 中国空气动力研究与发展中心空天技术研究所 | Cross-medium aircraft water-air dual-purpose empennage |
| CN114802705A (en) * | 2022-04-18 | 2022-07-29 | 上海电气集团股份有限公司 | Wing folding structure for unmanned aerial vehicle |
-
2017
- 2017-07-14 CN CN201710577416.3A patent/CN107323652A/en not_active Withdrawn
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108284932A (en) * | 2018-01-05 | 2018-07-17 | 惠安耐亚节能科技有限公司 | A kind of underwater anticollision unmanned plane for shooting |
| CN108284932B (en) * | 2018-01-05 | 2019-11-22 | 东阳市善水环境工程有限公司 | A kind of underwater anticollision unmanned plane for shooting |
| CN109760836A (en) * | 2019-03-12 | 2019-05-17 | 姜佩奇 | A kind of amphibious submersible of air-sea |
| CN110171562A (en) * | 2019-05-24 | 2019-08-27 | 孙思为 | A kind of unmanned plane rotor control structure |
| CN110979666A (en) * | 2019-12-27 | 2020-04-10 | 浙江大学 | Water-air robot |
| CN110979666B (en) * | 2019-12-27 | 2021-09-21 | 浙江大学 | Water-air robot |
| CN111532426A (en) * | 2020-04-22 | 2020-08-14 | 中国空气动力研究与发展中心 | Aircraft with V-shaped empennage and multiple rotors in vertical take-off and landing layout |
| CN113306696A (en) * | 2021-07-07 | 2021-08-27 | 陕西航天时代导航设备有限公司 | Folding wing unfolding mechanism |
| CN113665306A (en) * | 2021-10-25 | 2021-11-19 | 中国空气动力研究与发展中心空天技术研究所 | Cross-medium aircraft water-air dual-purpose empennage |
| CN113665306B (en) * | 2021-10-25 | 2022-01-04 | 中国空气动力研究与发展中心空天技术研究所 | Cross-medium aircraft water-air dual-purpose empennage |
| CN114802705A (en) * | 2022-04-18 | 2022-07-29 | 上海电气集团股份有限公司 | Wing folding structure for unmanned aerial vehicle |
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Application publication date: 20171107 |