CN206900658U - A kind of improved fixed-wing aerial survey unmanned plane - Google Patents
A kind of improved fixed-wing aerial survey unmanned plane Download PDFInfo
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- CN206900658U CN206900658U CN201720642975.3U CN201720642975U CN206900658U CN 206900658 U CN206900658 U CN 206900658U CN 201720642975 U CN201720642975 U CN 201720642975U CN 206900658 U CN206900658 U CN 206900658U
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Abstract
The utility model discloses a kind of improved fixed-wing aerial survey unmanned plane, belong to aerial survey of unmanned aerial vehicle technical field.A kind of improved fixed-wing aerial survey unmanned plane, including fuselage, the inner upper of the fuselage is fixedly connected with aerial camera, navigator is fixedly connected with below the aerial camera, the underside of the navigator is connected with signal receiver, enging cabin is fixedly connected with below the signal receiver, fuel tank is fixedly connected with below the enging cabin, central controller is fixedly connected with below the fuel tank, propeller is fixedly connected with the upside of the wing, aileron is fixedly connected with the downside of the wing, the afterbody of the fuselage is fixedly connected with tailplane, elevator is fixedly connected with the downside of the tailplane, the middle underside of the fuselage is connected with undercarriage；It has the characteristics that mobility is high, aerial survey effect is good, convenient and efficient, greatly reduces cost.
Description
Technical field
Aerial survey of unmanned aerial vehicle technical field is the utility model is related to, more specifically to a kind of improved fixed-wing aerial survey
Unmanned plane.
Background technology
Aerial survey of unmanned aerial vehicle is the strong supplement of traditional aerophotogrammetry means, has maneuverability, efficiently quick, fine
Accurately, the features such as operating cost is low, applied widely, with short production cycle, in zonule and flight area in hardship high-resolution shadow
As being had a clear superiority in terms of quick obtaining, with the development of unmanned plane and digital camera technology, the number based on unmanned aerial vehicle platform
Word aerial photographing technology has shown that its unique advantage, and unmanned plane is combined so that " unmanned plane numeral low latitude with aerophotogrammetry
Remote sensing " turns into a brand-new developing direction in air remote sensing field, and unmanned plane can be widely applied to national Important Project and build
If, calamity emergency and processing, territory supervision, development of resources, new rural village and town development etc., especially base surveying,
Land resources survey monitoring, land utilization dynamic monitors, digital city is built and emergency disaster relief surveying and mapping data obtains etc. tool
There are bright prospects.
Existing fixed-wing aerial survey UAV Maneuver is not strong, can not meet the requirement of a wide range of aerial survey, and falls
Machine accident, critical component can not be protected if blast occurs for fuel tank.
Utility model content
1. technical problems to be solved
It is not strong for existing fixed-wing aerial survey UAV Maneuver, the requirement and generation of a wide range of aerial survey can not be met
The present situation that critical component can not be protected if blast occurs for fuel tank during accident, the purpose of this utility model are to provide one
The improved fixed-wing aerial survey unmanned plane of kind, realizes that high maneuverability meets the requirement of a wide range of aerial survey, while have certain guarantor to fuel tank
Shield then protects critical component.
2. technical scheme
To solve the above problems, the utility model adopts the following technical scheme that:
A kind of improved fixed-wing aerial survey unmanned plane, including fuselage, the inner upper of the fuselage, which is fixedly connected with, takes photo by plane
Camera, navigator is fixedly connected with below the aerial camera, for controlling the direction of unmanned plane during flying, the navigator
Underside is connected with signal receiver, and enging cabin is fixedly connected with below the signal receiver, for for unmanned plane
Big power is provided, fuel tank is fixedly connected with below the enging cabin, central controller, institute are fixedly connected with below the fuel tank
State and parachute compartment is fixedly connected with below central controller, unmanned plane and critical component, institute are protected during for landing or occur accident
State and power supply be fixedly connected with below parachute compartment, the aerial camera, navigator, signal receiver, enging cabin, fuel tank,
Parachute compartment, power supply, central controller are all connected to the inside of fuselage, and the middle both sides of the fuselage are fixed by wing link to be connected
Wing is connected to, described wing link one end is fixedly connected with fuselage, and the other end is fixedly connected with wing, the upside of the wing
Propeller is fixedly connected with, the propeller is connected with enging cabin, is fixedly connected with aileron on the downside of the wing, institute
The afterbody for stating fuselage is fixedly connected with tailplane, and for changing the flying height of unmanned plane, the downside of the tailplane is consolidated
Surely elevator is connected with, the middle underside of the fuselage is connected with undercarriage, and the aerial camera, navigator, signal connect
Device and power supply is received to be electrically connected with by the traverse net in cabin and central controller.
Preferably, the aerial camera is configured with infrared thermography, for preventing accident and being detected at night.
Preferably, the outside surrounding of the fuel tank is provided with preventing collision protection cover, oil during for preventing air crash accident
Case explodes.
Preferably, damping device is provided with the undercarriage, damping when landing for unmanned plane.
3. beneficial effect
Compared with prior art, the beneficial effects of the utility model are：
（1）Enging cabin is fixedly connected with below signal receiver, for providing big power for unmanned plane, central controller
Lower section is fixedly connected with parachute compartment, protects unmanned plane and critical component, the afterbody of fuselage to consolidate during for landing or occur accident
Surely tailplane is connected with, for changing the flying height of unmanned plane, it has, and mobility is high, aerial survey effect is good, convenient and efficient
The features such as.
（2）Aerial camera is configured with infrared thermography, for preventing accident and being detected at night, considerably reduces peace
Full accident and realize round-the-clock detection.
（3）The outside surrounding of tobacco tar case is provided with preventing collision protection cover, fuel tank explosion during for preventing air crash accident,
Protect critical component.
（4）Damping device is provided with undercarriage, damping when landing for unmanned plane, reduce unmanned plane critical component by
The probability of damage.
Brief description of the drawings
Fig. 1 is top view of the present utility model；
Fig. 2 is landing gear structure schematic diagram of the present utility model；
Fig. 3 is the utility model circuit block diagram.
Label declaration in figure：
1st, aerial camera；2nd, navigator；3rd, signal receiver；4th, propeller；5th, wing；6th, aileron；7th, fuel tank；8th, land
Umbrella cabin；9th, tailplane；10th, elevator；11st, power supply；12nd, central controller；13rd, wing link；14th, enging cabin；15th, machine
Body；16th, undercarriage.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment；The technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe；Obviously；Described embodiment is only the utility model part of the embodiment；Rather than whole
Embodiment.Based on the embodiment in the utility model；Those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained；Belong to the scope of the utility model protection.
Fig. 1-3, a kind of improved fixed-wing aerial survey unmanned plane, including fuselage 15, the inner upper of fuselage 15 is referred to consolidate
Surely aerial camera 1 is connected with, the lower section of aerial camera 1 is fixedly connected with navigator 2, for controlling the direction of unmanned plane during flying,
The underside of navigator 2 is connected with signal receiver 3, and the lower section of signal receiver 3 is fixedly connected with enging cabin 14, is used for
Big power is provided for unmanned plane, the lower section of enging cabin 14 is fixedly connected with fuel tank 7, and the lower section of fuel tank 7 is fixedly connected with middle control
Device 12, the lower section of central controller 12 are fixedly connected with parachute compartment 8, and unmanned plane and crucial portion are protected during for landing or occur accident
Part, the lower section of parachute compartment 8 are fixedly connected with power supply 11, aerial camera 1, navigator 2, signal receiver 3, enging cabin 14,
Fuel tank 7, parachute compartment 8, power supply 11, central controller 12 are all connected to the inside of fuselage 15, and the middle both sides of fuselage 15 pass through wing
Link 13 is fixedly connected with wing 5, and the one end of wing link 13 is fixedly connected with fuselage 15, and the other end is fixedly connected with wing
5, the upside of wing 5 is fixedly connected with propeller 4, and propeller 4 is connected with enging cabin 14, and the downside of wing 5, which is fixed, to be connected
Aileron 6 is connected to, the afterbody of fuselage 15 is fixedly connected with tailplane 9, for changing the flying height of unmanned plane, tailplane 9
Downside be fixedly connected with elevator 10, the middle underside of fuselage 15 is connected with undercarriage 16, aerial camera 1, navigator
2nd, signal receiver 3 and power supply 11 are electrically connected with by the traverse net in cabin and central controller 12.
Aerial camera 1 is configured with infrared thermography, for preventing accident and being detected at night.
The outside surrounding of fuel tank 7 is provided with preventing collision protection cover, fuel tank explosion during for preventing air crash accident.
Damping device is provided with undercarriage 16, damping when landing for unmanned plane.
Operation principle：The first step；The service condition of each part of unmanned plane is checked comprehensively, confirms errorless rear standby for takeoff work
Make, second step；The outside surrounding for opening fuel tank 7 is provided with preventing collision protection cover, and fuel tank 7 is filled it up with into oil, then will be filled with electricity
Power supply 11 is fixed on the specified location of fuselage 15, and signal receiver 3 is connected with ground control terminal, is then ready for taking off, will
Ready unmanned plane is placed on ejector, and the engine start in enging cabin 14 is made propeller by transmission device
4 rotate, then air ejector for starting transmitting unmanned plane, the 3rd step；After unmanned plane lift-off, ground control terminal communicates instructions to signal and connect
Device 3 is received, signal receiver 3 will instruct the heading for passing to navigator 2 and controlling unmanned plane, if the height of aircraft need to be changed,
Ground control terminal communicates instructions to signal receiver 3 and signal is passed into central controller 12, and central controller 12 is controlled by elevator 10
Tailplane 9 processed carrys out change of flight height, and after reaching designated area, ground control terminal communicates instructions to signal receiver 3 and will
Signal passes to aerial camera 1 and starts to detect, and after task terminates, reduces the flying height of unmanned plane, central controller 12 makes parachute
Cabin works, and releases a parachute, and unmanned plane landing is simultaneously closed off the power of unmanned plane, to unmanned plane disassembly ＆ recycling after landing.
It is described above；The only preferable embodiment of the utility model；But the scope of protection of the utility model is not
It is confined to this；Any one skilled in the art is in the technical scope that the utility model discloses；According to this practicality
New technical scheme and its improvement design is subject to equivalent substitution or change；It should all cover in the scope of protection of the utility model
It is interior.
Claims (4)
1. a kind of improved fixed-wing aerial survey unmanned plane, including fuselage（15）, it is characterised in that：The fuselage（15）Top consolidate
Surely it is connected with aerial camera（1）, the aerial camera（1）Lower section be provided with navigator（2）, the navigator（2）Lower section set
There is signal receiver（3）, the signal receiver（3）Lower section be provided with enging cabin（14）, the enging cabin（14）Under
Side is provided with fuel tank（7）, the fuel tank（7）Lower section be provided with central controller（12）, the central controller（12）Lower section be provided with parachute
Cabin（8）, the parachute compartment（8）Lower section be provided with power supply（11）, the aerial camera（1）, navigator（2）, signal receiver
（3）, enging cabin（14）, fuel tank（7）, parachute compartment（8）, power supply（11）, central controller（12）It is all connected to fuselage（15）It is interior
Portion, the fuselage（15）Middle both sides pass through wing link（13）It is fixedly connected with wing（5）, the wing link
（13）One end is fixedly connected with fuselage（15）, the other end is fixedly connected with wing（5）, the wing（5）Upside be fixedly connected
There is propeller（4）, the propeller（4）With enging cabin（14）Drive connection, the wing（5）Downside be fixedly connected with pair
The wing（6）, the fuselage（15）Afterbody be fixedly connected with tailplane（9）, the tailplane（9）Downside be fixedly connected with
Elevator（10）, the fuselage（15）Middle underside be connected with undercarriage（16）, the aerial camera（1）, navigator
（2）, signal receiver（3）And power supply（11）Pass through the traverse net and central controller in cabin（12）It is electrically connected with.
A kind of 2. improved fixed-wing aerial survey unmanned plane according to claim 1, it is characterised in that：The aerial camera
（1）It is configured with infrared thermoviewer.
A kind of 3. improved fixed-wing aerial survey unmanned plane according to claim 1, it is characterised in that：The fuel tank（7）'s
Outside surrounding is provided with preventing collision protection cover.
A kind of 4. improved fixed-wing aerial survey unmanned plane according to claim 1, it is characterised in that：The undercarriage（16）
On be provided with damping device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720642975.3U CN206900658U (en) | 2017-06-05 | 2017-06-05 | A kind of improved fixed-wing aerial survey unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720642975.3U CN206900658U (en) | 2017-06-05 | 2017-06-05 | A kind of improved fixed-wing aerial survey unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206900658U true CN206900658U (en) | 2018-01-19 |
Family
ID=61286855
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720642975.3U Expired - Fee Related CN206900658U (en) | 2017-06-05 | 2017-06-05 | A kind of improved fixed-wing aerial survey unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206900658U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113264183A (en) * | 2021-05-17 | 2021-08-17 | 中建八局第四建设有限公司 | Civil unmanned aerial vehicle-based engineering investigation method |
| WO2021232753A1 (en) * | 2020-05-22 | 2021-11-25 | 深圳市大疆创新科技有限公司 | Aircraft and aircraft control system |
-
2017
- 2017-06-05 CN CN201720642975.3U patent/CN206900658U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021232753A1 (en) * | 2020-05-22 | 2021-11-25 | 深圳市大疆创新科技有限公司 | Aircraft and aircraft control system |
| CN113264183A (en) * | 2021-05-17 | 2021-08-17 | 中建八局第四建设有限公司 | Civil unmanned aerial vehicle-based engineering investigation method |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180119 Termination date: 20180605 |
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| CF01 | Termination of patent right due to non-payment of annual fee |