CN207985194U - A kind of novel unmanned plane of taking photo by plane - Google Patents
A kind of novel unmanned plane of taking photo by plane Download PDFInfo
- Publication number
- CN207985194U CN207985194U CN201820340628.XU CN201820340628U CN207985194U CN 207985194 U CN207985194 U CN 207985194U CN 201820340628 U CN201820340628 U CN 201820340628U CN 207985194 U CN207985194 U CN 207985194U
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- Prior art keywords
- plane
- wing plate
- unmanned plane
- taking photo
- buffer
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Abstract
The utility model discloses a kind of novel unmanned planes of taking photo by plane,Including top intermediate,GPS positioning instrument,Engine,Link,Fuel tank,Buffer,Undercarriage,Lower part intermediate,Empennage,Flow deflector,Control wing plate,Steering engine,Fixed wing plate,Propeller,Supporting rack,Connecting seat,High-precision video camera,Video memory,Non-slip mat,Cushion pad,Air bag,Exhaust outlet,Gas chamber,Protection cap,Million camera lens of simple metal high definition,Recorder,Collet,Linking arm,Glass,Chip,Relay and protecgulum,The right side of fixed wing plate is located at oil tank bottom end and is equipped with steering engine,The side of flow deflector is equipped with buffer,The utility model structure novel,Reasonable design,Cost of manufacture is relatively low,Assembly and disassembly is convenient,Aerial photographing effect is good,Image quality is clearly reliable,With prolonged store function,Geographical location is shown by GPS positioning instrument,Greatly improve security performance,Novel unmanned plane of taking photo by plane is affected by the wind small,Stability is good,Shooting effect is good.
Description
Technical field
The utility model is related to air vehicle technique field, specially a kind of novel unmanned plane of taking photo by plane.
Background technology
UAV, abbreviation unmanned plane are a kind of new concept weapon equipments being in rapidly developing, with machine
Dynamic flexible, rapid reaction, unmanned flight, operation require low advantage, unmanned plane that shadow may be implemented by carrying multiclass sensor
It is the strong supplement of satellite remote sensing and traditional air remote sensing as real-time Transmission, high-risk areas detecting function, currently, unmanned plane
Use scope has widened military affairs, scientific research, civilian three big field, specifically electric power, communication, meteorology, agricultural, sea wherein, newly
Type take photo by plane unmanned plane in above-mentioned multiple fields have extensive use, unmanned plane of taking photo by plane, mainly include unmanned plane and setting exist
Aerial device on unmanned plane, existing unmanned plane, can continuously in the air in flight course due to being influenced by gas shock
Swing vibration, this vibrations and impact force are stronger to the impact endurance test shock of aerial device, it is difficult to ensure aerial device shooting effect, make
At image high definition than low, and aerial device damage is easily caused, the power of unmanned plane is provided by battery, due to unmanned body
Product is small, and limited battery capacity, stream time is restricted, and can not work in the air for a long time, and unmanned plane is as occurred
Failure, quick air crash, dangerous very big, unmanned plane is shot in the air, and by wind-force and itself vibration, stability is poor, influences
Shooting.
Utility model content
The utility model provides a kind of novel unmanned plane of taking photo by plane, and can effectively solve mentioned above in the background art existing
Unmanned plane is by gas shock in the air in flight course due to being influenced, can continuously swing vibration, this vibrations and impact
Power is stronger to the impact endurance test shock of aerial device, it is difficult to ensure aerial device shooting effect, cause image high definition than low, and easily
Aerial device is caused to damage, the power of unmanned plane is provided by battery, since unmanned plane is small, limited battery capacity, continuously
Working time is restricted, and can not work in the air for a long time;And unmanned plane such as breaks down, quick air crash, dangerous very big,
Unmanned plane is shot in the air, and by wind-force and itself vibration, stability is poor, the problems such as influencing to shoot.
To achieve the above object, the utility model provides the following technical solutions:A kind of novel unmanned plane of taking photo by plane, including top
Intermediate 1, GPS positioning instrument, engine, link, fuel tank, buffer, undercarriage, lower part intermediate, empennage, flow deflector, control
Wing plate processed, steering engine, fixed wing plate, propeller, supporting rack, connecting seat, high-precision video camera, video memory, non-slip mat, buffering
Pad, air bag, exhaust outlet, gas chamber, protection cap, million camera lens of simple metal high definition, recorder, collet, linking arm, glass, chip, after
The top of electric appliance and protecgulum, the top intermediate is equipped with GPS positioning instrument, and the left and right sides of top intermediate symmetrically connects
It is connected to link, one end of the link is provided with connecting seat close to inside, and the side of the connecting seat is equipped with high-precision
Video camera is provided with supporting rack on the right side of the top intermediate, and is equipped with engine, and top in the middle part of the intermediate of top
The lower section of intermediate is located at the left and right sides and is symmetrically arranged with propeller, and the side of the propeller is equipped with close to top position
The bottom end of fuel tank, the top intermediate is connected with lower part intermediate, is both provided at left and right sides of the lower part intermediate solid
Determine wing plate, the right side of the fixed wing plate is located at oil tank bottom end and is equipped with steering engine, and the bottom end of the lower part intermediate is close to left and right
Both sides are symmetrically arranged with control wing plate, and flow deflector, the side installation of the flow deflector are provided with below the control wing plate
There are buffer, the bottom end of the buffer to be connected with undercarriage, the inside of the buffer is provided with exhaust close to top position
Mouthful, the lower section of the exhaust outlet, which is located in the middle part of buffer, is provided with air bag, and gas chamber, the gas chamber are provided with below the air bag
Lower section be provided with cushion pad, non-slip mat is provided with below the cushion pad, the outside of the high-precision video camera is provided with
Protection cap, and one end of high-precision video camera is provided with protecgulum, and million camera lens of simple metal high definition is equipped on the inside of the protecgulum,
The lower section of million camera lens of simple metal high definition is equipped with recorder close to side, and the bottom end of the high-precision video camera is provided with
Collet is provided with linking arm below the collet, and the right side of the protecgulum is located at high-precision video camera and is internally provided with glass,
Relay is installed on the glass, and is provided with chip on the right side of glass, video memory is installed on the right side of the chip,
The GPS positioning instrument, video memory input terminal with the output end of engine be electrically connected.
Preferably, the link is of an L-shaped structure, and link is fixedly connected with top intermediate by screw.
Preferably, the bottom end of the lower part intermediate is provided with empennage.
Preferably, wafer array infrared lamp is installed on the right side of the recorder.
Preferably, it is connected by articulate between the collet and linking arm.
Preferably, it is provided with fixed seat on the right side of the linking arm, mounting hole is provided in fixed seat.
Compared with prior art, the beneficial effects of the utility model:The utility model structure novel, reasonable design make
Cost is relatively low, and assembly and disassembly is convenient, and aerial photographing effect is good, and image quality is clearly reliable, has prolonged store function, fixed by GPS
Position instrument shows geographical location, greatly improves security performance, the buffer of installation, avoid during unmanned plane flies in the air due to
When being influenced by gas shock, the continuously swing vibration of generation, to the impact endurance test shock of aerial device, it is difficult to ensure dress of taking photo by plane
The problem of setting shooting effect improves Aerial Images fine definition, and plays a protective role to aerial device, and unmanned plane structure is tight
It gathers, is affected by the wind small, stability is good, and shooting effect is good.
Description of the drawings
Attached drawing is used to provide a further understanding of the present invention, and a part for constitution instruction, with this practicality
Novel embodiment for explaining the utility model, does not constitute limitations of the present invention together.
In the accompanying drawings:
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is the structural schematic diagram of the buffer of the utility model;
Fig. 3 is the structural schematic diagram of the utility model high-precision video camera;
Fig. 4 is the inner mounting structure schematic diagram of the utility model high-precision video camera;
Figure label:1, top intermediate;2, GPS positioning instrument;3, engine;4, link;5, fuel tank;6, buffer;
7, undercarriage;8, lower part intermediate;9, empennage;10, flow deflector;11, wing plate is controlled;12, steering engine;13, fixed wing plate;14, spiral shell
Revolve paddle;15, supporting rack;16, connecting seat;17, high-precision video camera;18, video memory;19, non-slip mat;20, cushion pad;
21, air bag;22, exhaust outlet;23, gas chamber;24, protection cap;25, million camera lens of simple metal high definition;26, recorder;27, collet;
28, linking arm;29, glass;30, chip;31, relay;32, protecgulum.
Specific implementation mode
The preferred embodiment of the utility model is illustrated below in conjunction with attached drawing, it should be understood that described herein excellent
It selects embodiment to be only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment:As shown in Figs 1-4, a kind of technical solution of the utility model offer, a kind of novel unmanned plane of taking photo by plane, including
Top intermediate 1, GPS positioning instrument 2, engine 3, link 4, fuel tank 5, buffer 6, undercarriage 7, lower part intermediate 8, empennage
9, flow deflector 10, control wing plate 11, steering engine 12, fixed wing plate 13, propeller 14, supporting rack 15, connecting seat 16, high-precision image
Machine 17, video memory 18, non-slip mat 19, cushion pad 20, air bag 21, exhaust outlet 22, gas chamber 23, protection cap 24, simple metal are high
Clear million camera lens 25, recorder 26, collet 27, linking arm 28, glass 29, chip 30, relay 31 and protecgulum 32, among top
The top of body 1 is equipped with GPS positioning instrument 2, and the left and right sides of top intermediate 1 is symmetrically connected with link 4, link 4
One end inside is provided with connecting seat 16, the side of connecting seat 16 is equipped with high-precision video camera 17, top intermediate 1
Right side is provided with supporting rack 15, and the middle part of top intermediate 1 is equipped with engine 3, and the lower section of top intermediate 1 is located at a left side
Right both sides are symmetrically arranged with propeller 14, and the side of propeller 14 is equipped with fuel tank 5, top intermediate 1 close to top position
Bottom end be connected with lower part intermediate 8, the left and right sides of lower part intermediate 8 is both provided with fixed wing plate 13, fixed wing plate 13
Right side is located at 5 bottom end of fuel tank and is equipped with steering engine 12, and the bottom end of lower part intermediate 8 is symmetrically arranged with the control wing close to the left and right sides
The lower section of plate 11, control wing plate 11 is provided with flow deflector 10, and the side of flow deflector 10 is equipped with buffer 6, the bottom end of buffer 6
It is connected with undercarriage 7, the inside of buffer 6 is provided with exhaust outlet 22 close to top position, and the lower section of exhaust outlet 22 is located at buffering
6 middle part of device is provided with air bag 21, and the lower section of air bag 21 is provided with gas chamber 23, and the lower section of gas chamber 23 is provided with cushion pad 20, buffering
The lower section of pad 20 is provided with non-slip mat 19, and the outside of high-precision video camera 17 is provided with protection cap 24, and high-precision video camera 17
One end be provided with protecgulum 32, the inside of protecgulum 32 is equipped with million camera lens 25 of simple metal high definition, million camera lens of simple metal high definition
25 lower section is equipped with recorder 26 close to side, and the bottom end of high-precision video camera 17 is provided with collet 27, the lower section of collet 27
It is provided with linking arm 28, the right side of protecgulum 32 is located at high-precision video camera 17 and is internally provided with glass 29, is equipped on glass 29
Relay 31, and the right side of glass 29 is provided with chip 30, the right side of chip 30 is equipped with video memory 18, GPS positioning instrument
2, the input terminal of video memory 18 is electrically connected with the output end of engine 3.
In order to enable connection is firm, stablizes the integration of enhancing structure, in the present embodiment, it is preferred that link 4 is L-shaped
Structure, and link 4 is fixedly connected with top intermediate 1 by screw.
In order to enhance the stability of novel unmanned plane during flying of taking photo by plane, in the present embodiment, it is preferred that the bottom of lower part intermediate 8
End is provided with empennage 9.
In order to improve aerial photographing effect, the clarity of picture is improved, in the present embodiment, it is preferred that pacify on the right side of recorder 26
Equipped with wafer array infrared lamp.
It takes photo by plane angle for the ease of control, enhances the picture sense of reality, in the present embodiment, it is preferred that collet 27 and linking arm
It is connected by articulate between 28.
It is firm in order to make to connect between linking arm 28 and link 4, in the present embodiment, it is preferred that the right side of linking arm 28
It is provided with fixed seat, mounting hole is provided in fixed seat.
The operation principle and process for using of the utility model:It is novel to take photo by plane unmanned plane in actual use, first,
The top of top intermediate 1 is equipped with GPS positioning instrument 2, shows geographical location by GPS positioning instrument, greatly improves security performance,
One end of link 4 is provided with connecting seat 16 close to inside, in order to enable connection is firm, stablizes the integration of enhancing structure, makes
It obtains link 4 and is designed to L-type structure, and link 4 is fixedly connected with top intermediate 1 by screw, the right side of top intermediate 1
Side is provided with supporting rack 15, plays a supporting role, the stability of airflight when improving navigation, the middle part peace of top intermediate 1
Equipped with engine 3, convenient for providing power resources to equipment of entirely taking photo by plane, secondly, the bottom end of lower part intermediate 8 is provided with empennage 9,
The lower section of top intermediate 1 is located at the left and right sides and is symmetrically arranged with propeller 14, in order to enhance novel unmanned plane during flying of taking photo by plane
Stability, the side of propeller 14 is equipped with fuel tank 5 close to top position, convenient for refueling to novel unmanned plane of taking photo by plane, provides
The left and right sides of energy, lower part intermediate 8 is both provided with fixed wing plate 13, and the right side of fixed wing plate 13 is located at 5 bottom end of fuel tank peace
Equipped with steering engine 12, the lower section of control wing plate 11 is provided with flow deflector 10, and the bottom end of buffer 6 is connected with undercarriage 7, and installation is delayed
Device 6 is rushed, when avoiding during unmanned plane flies in the air due to being influenced by gas shock, shake is continuously waved in generation
It is dynamic, to the impact endurance test shock of aerial device, it is difficult to which close over is leaned in the inside of the problem of ensureing aerial device shooting effect, buffer 6
Position is provided with exhaust outlet 22, and the lower section of air bag 21 is provided with gas chamber 23, and the lower section of cushion pad 20 is provided with non-slip mat 19, high-precision
The outside of degree video camera 17 is provided with protection cap 24, convenient for carrying out safeguard protection, one end of high-precision video camera 17 to video camera
It is provided with protecgulum 32, the lower section of million camera lens 25 of simple metal high definition is equipped with recorder 26 close to side, finally, in order to improve boat
Effect is clapped, improves the clarity of picture, the right side of recorder 26 is equipped with wafer array infrared lamp, and the lower section of collet 27 is provided with
Linking arm 28, firm in order to make to connect between linking arm 28 and link 4, the right side of linking arm 28 is provided with fixed seat, fixed
It is provided with mounting hole on seat, relay 31 is installed, the right side of chip 30 is equipped with video memory 18, novel knot on glass 29
Structure is novel, and reasonable design, cost of manufacture is relatively low, and assembly and disassembly is convenient, and aerial photographing effect is good, and image quality is clearly reliable, has for a long time
Store function, improve Aerial Images fine definition, play a protective role to aerial device, unmanned plane is compact-sized, wind-engaging
Power influence is small, and stability is good, and shooting effect is good.
Finally it should be noted that:The foregoing is merely the preferred embodiments of the utility model, are not limited to this reality
With novel, although the utility model is described in detail with reference to the foregoing embodiments, those skilled in the art is come
Say, still can with technical scheme described in the above embodiments is modified, or to which part technical characteristic into
Row equivalent replacement.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on, should all
It is included within the scope of protection of this utility model.
Claims (6)
1. a kind of novel unmanned plane of taking photo by plane, including top intermediate (1), GPS positioning instrument (2), engine (3), link (4),
Fuel tank (5), buffer (6), undercarriage (7), lower part intermediate (8), empennage (9), flow deflector (10), control wing plate (11), rudder
Machine (12), fixed wing plate (13), propeller (14), supporting rack (15), connecting seat (16), high-precision video camera (17), video are deposited
Reservoir (18), non-slip mat (19), cushion pad (20), air bag (21), exhaust outlet (22), gas chamber (23), protection cap (24), simple metal
Million camera lens of high definition (25), recorder (26), collet (27), linking arm (28), glass (29), chip (30), relay (31)
With protecgulum (32), it is characterised in that:The top of the top intermediate (1) is equipped with GPS positioning instrument (2), and top intermediate
(1) the left and right sides is symmetrically connected with link (4), and one end of the link (4) is provided with connecting seat close to inside
(16), the side of the connecting seat (16) is equipped with high-precision video camera (17), is provided on the right side of the top intermediate (1)
Supporting rack (15), and engine (3) is installed in the middle part of top intermediate (1), and the lower section of top intermediate (1) is located at left and right
Both sides are symmetrically arranged with propeller (14), and the side of the propeller (14) is equipped with fuel tank (5) close to top position, described
The bottom end of top intermediate (1) is connected with lower part intermediate (8), is both provided at left and right sides of the lower part intermediate (8) solid
Determine wing plate (13), the right side of the fixed wing plate (13) is located at fuel tank (5) bottom end and is equipped with steering engine (12), the lower part intermediate
(8) bottom end is symmetrically arranged with control wing plate (11) close to the left and right sides, is provided with and leads below the control wing plate (11)
The side of flow (10), the flow deflector (10) is equipped with buffer (6), and the bottom end of the buffer (6) is connected with undercarriage
(7), the inside of the buffer (6) is provided with exhaust outlet (22) close to top position, and the lower section of the exhaust outlet (22) is located at
Air bag (21) is provided in the middle part of buffer (6), is provided with gas chamber (23) below the air bag (21), under the gas chamber (23)
Side is provided with cushion pad (20), and non-slip mat (19), the high-precision video camera (17) are provided with below the cushion pad (20)
Outside be provided with protection cap (24), and one end of high-precision video camera (17) is provided with protecgulum (32), the protecgulum (32)
Inside is equipped with million camera lens of simple metal high definition (25), and the lower section of million camera lens of simple metal high definition (25) is installed close to side
There are recorder (26), the bottom end of the high-precision video camera (17) to be provided with collet (27), the lower section setting of the collet (27)
There are linking arm (28), the right side of the protecgulum (32) to be located at high-precision video camera (17) and be internally provided with glass (29), the glass
Relay (31) is installed on glass (29), and is provided with chip (30) on the right side of glass (29), the right side peace of the chip (30)
Equipped with video memory (18), the GPS positioning instrument (2), steering engine (12), video memory (18) input terminal and engine
(3) output end is electrically connected.
2. the novel unmanned plane of taking photo by plane of one kind according to claim 1, it is characterised in that:The L-shaped knot of the link (4)
Structure, and link (4) is fixedly connected with top intermediate (1) by screw.
3. the novel unmanned plane of taking photo by plane of one kind according to claim 1, it is characterised in that:The bottom of the lower part intermediate (8)
End is provided with empennage (9).
4. the novel unmanned plane of taking photo by plane of one kind according to claim 1, it is characterised in that:Pacify on the right side of the recorder (26)
Equipped with wafer array infrared lamp.
5. the novel unmanned plane of taking photo by plane of one kind according to claim 1, it is characterised in that:The collet (27) and linking arm
(28) it is connected by articulate between.
6. the novel unmanned plane of taking photo by plane of one kind according to claim 1, it is characterised in that:It is set on the right side of the linking arm (28)
It is equipped with fixed seat, mounting hole is provided in fixed seat.
Priority Applications (1)
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CN201820340628.XU CN207985194U (en) | 2018-03-13 | 2018-03-13 | A kind of novel unmanned plane of taking photo by plane |
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CN201820340628.XU CN207985194U (en) | 2018-03-13 | 2018-03-13 | A kind of novel unmanned plane of taking photo by plane |
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CN201820340628.XU Expired - Fee Related CN207985194U (en) | 2018-03-13 | 2018-03-13 | A kind of novel unmanned plane of taking photo by plane |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109334973A (en) * | 2018-11-14 | 2019-02-15 | 惟创新(武汉)科技有限公司 | A kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing |
-
2018
- 2018-03-13 CN CN201820340628.XU patent/CN207985194U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109334973A (en) * | 2018-11-14 | 2019-02-15 | 惟创新(武汉)科技有限公司 | A kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing |
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CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181019 Termination date: 20190313 |