CN206652246U - Fixed wing aircraft model plane are investigated over the ground - Google Patents
Fixed wing aircraft model plane are investigated over the ground Download PDFInfo
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- CN206652246U CN206652246U CN201720414983.2U CN201720414983U CN206652246U CN 206652246 U CN206652246 U CN 206652246U CN 201720414983 U CN201720414983 U CN 201720414983U CN 206652246 U CN206652246 U CN 206652246U
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- fuselage
- bottom plate
- model plane
- plate
- fixed wing
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Abstract
Fixed wing aircraft model plane are investigated over the ground the utility model discloses a kind of, including fuselage, fuselage includes bottom plate, side plate and cover plate, cover plate is arranged on above bottom plate, the quantity of side plate is two pieces, two blocks of side plates are symmetricly set on the left and right sides of bottom plate, waist is provided with wing, wing is connected with side plate, the afterbody of fuselage is provided with tailplane and vertical tail, tailplane is connected with bottom plate, vertical tail is connected with cover plate, the head of fuselage is provided with engine, propeller is installed on the output shaft of engine, the bottom of bottom plate is provided with the high-definition camera for captured in real-time picture, visual signal transmitter for the picture transmission captured by high-definition camera to be gone out is installed in fuselage, high-definition camera is connected with visual signal transmitter.The utility model realizes the requirement of real-time Transmission image under high-performance cruise using graphic transmission equipment, and people can not change the deficiency in investigation direction in real time according to the picture that model plane photograph during perfect conventional investigation.
Description
Technical field
A kind of aircraft model is the utility model is related to, fixed wing aircraft model plane are investigated over the ground more particularly, to a kind of.
Background technology
In actual life, due to various regions territorial environment feature difference, so when people reach a certain zone of ignorance, always
It can worry for oneself to destination along road situation or the target found.In conventional investigation, due to region ring
The complexity in border, weather conditions it is changeable, zone of ignorance is not known about, model plane signal transmission hysteresis, cause people can not basis
The picture that model plane photograph changes investigation direction in real time.
Utility model content
The purpose of this utility model is to overcome above-mentioned deficiency of the prior art, there is provided a kind of fixed-wing of investigation over the ground flies
Machine model plane, it realizes the requirement of real-time Transmission image under high-performance cruise using graphic transmission equipment, perfect conventional to investigate
People can not change the deficiency in investigation direction in real time according to the picture that model plane photograph in journey.
To achieve the above object, the technical solution adopted in the utility model is：It is a kind of to investigate fixed wing aircraft model plane over the ground,
It is characterized in that：Including fuselage, the fuselage includes bottom plate, side plate and cover plate, and the cover plate is arranged on the top of bottom plate, described
The quantity of side plate is two pieces, and two blocks of side plates are symmetricly set on the left and right sides of bottom plate, and bottom and the bottom plate of the side plate connect
Connect, the top of the side plate is connected with cover plate, wing is provided with the middle part of the fuselage, the wing is connected with side plate, described
The afterbody of fuselage is provided with tailplane and vertical tail, and the tailplane is connected with bottom plate, the vertical tail and cover plate
Connection, the head of the fuselage is provided with engine, propeller, the bottom of the bottom plate is provided with the output shaft of the engine
Portion is provided with the high-definition camera for captured in real-time picture, is provided with the fuselage for by captured by high-definition camera
The visual signal transmitter that picture transmission is gone out, the high-definition camera are connected with visual signal transmitter.
The above-mentioned fixed wing aircraft model plane of investigation over the ground, it is characterised in that：The bottom of the bottom plate is also equipped with infrared heat
As instrument, the thermal infrared imager is located at the rear of high-definition camera.
The above-mentioned fixed wing aircraft model plane of investigation over the ground, it is characterised in that：It is provided with the cover plate for survey aircraft
The laser range finder of flying height.
The above-mentioned fixed wing aircraft model plane of investigation over the ground, it is characterised in that：The head of the fuselage is also equipped with infrared keep away
Hinder sensor.
The above-mentioned fixed wing aircraft model plane of investigation over the ground, it is characterised in that：The span of the fixed wing aircraft model plane is
1000mm, the length of the fuselage is 810mm.
The above-mentioned fixed wing aircraft model plane of investigation over the ground, it is characterised in that：The high-definition camera is the height of 8,000,000 pixels
Clear camera.
The above-mentioned fixed wing aircraft model plane of investigation over the ground, it is characterised in that：The wing is detachably connected with side plate, described
Tailplane is detachably connected with bottom plate, and the vertical tail is detachably connected with cover plate.
The utility model has advantages below compared with prior art：
1st, in order to solve the territorial environment for complexity, changeable climate condition, aircraft model transmission signal is not known about
Zone of ignorance, caused people can not change the target area in investigation direction in real time according to the picture that aircraft model photographs, this
Utility model carries out realtime graphic shooting by installing high-definition camera in the bottom of bottom plate, is met with this to target area
Investigation demand.
2nd, the utility model can be widely suitable for the various complex environments such as more mountains, hilliness area and (rain, blows
Deng) under investigation, suitable for military affairs investigation, personnel search and rescue, road prospecting etc., for user provide conveniently.
3rd, the utility model size is relatively small, be able to can also be utilized infrared at night using thermal infrared imager expansion investigation
The autonomous avoiding obstacles of avoidance sensor, it is ensured that the safety of aircraft is maked a return voyage.
4th, the utility model making is simple, cost is low；Take off apart from short, mode of taking off is various；It is dismantled and assembled, easy to carry,
It is simple to operate；Shooting picture is clear, is applicable wide-long shot, can return in real time.
Below by drawings and examples, the utility model is described in further detail.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Description of reference numerals:
1-engine；2-bottom plate；3-side plate；
4-cover plate；5-tailplane；6-vertical tail；
7-wing；8-propeller；9-high-definition camera；
10-visual signal transmitter；11-thermal infrared imager；12-laser range finder；
13-IR evading obstacle sensors.
Embodiment
As shown in figure 1, the utility model includes fuselage, the fuselage includes bottom plate 2, side plate 3 and cover plate 4, the cover plate 4
The top of bottom plate 2 is arranged on, the quantity of the side plate 3 is two pieces, and two blocks of side plates 3 are symmetricly set on the left and right two of bottom plate 2
Side, the bottom of the side plate 3 are connected with bottom plate 2, and the top of the side plate 3 is connected with cover plate 4, is provided with the middle part of the fuselage
Wing 7, the wing 7 are connected with side plate 3, and the afterbody of the fuselage is provided with tailplane 5 and vertical tail 6, the level
Empennage 5 is connected with bottom plate 2, and the vertical tail 6 is connected with cover plate 4, and the head of the fuselage is provided with engine 1, the hair
Propeller 8 is installed, the bottom of the bottom plate 2 is provided with the high-definition camera for captured in real-time picture on the output shaft of motivation 1
First 9, the visual signal transmitter 10 for the picture transmission captured by high-definition camera 9 to be gone out is installed in the fuselage,
The high-definition camera 9 is connected with visual signal transmitter 10.
The high-definition camera 9 that the utility model is installed by the bottom of bottom plate 2 can return the image collected in real time, and high definition is taken the photograph
First 9 coverage of picture is wide, can return the image collected in real time；High-definition camera 9 is connected on visual signal transmitter 10, can
The image transmitting collected to picture sensor.Picture sensor can be connected with display, pass through display
The picture of passback can be shown；(such as rain, blow, the more woodss in mountain region, hills gully) all can be just under various complex situations
Often work, to big Small object, far and near object all can high-definition shooting, realize the function by manipulate target run region, therefore can
Use suitable for the various complex environments such as more mountains, hilliness area, to meet investigation demand of the people to target area, fly simultaneously
Scanning frequency degree is fast, flight stability.Fixed wing aircraft model plane use monomotor, have climbing speed it is fast, can short distance take off
Or hand throwing type takes off.
As shown in figure 1, the bottom of the bottom plate 2 is also equipped with thermal infrared imager 11, the thermal infrared imager 11 is positioned at height
The rear of clear camera 9, thermal infrared imager 11 accurately can find target in the case of night dark, can be very good
Complete night investigation tasks.
As shown in figure 1, the laser range finder 12 for survey aircraft flying height is installed on the cover plate 4.
As shown in figure 1, the head of the fuselage is also equipped with IR evading obstacle sensors 13, so can autonomous regulation fly
The flight attitude of machine model plane, avoiding obstacles, the safety coefficient of flight is improved, helps operator preferably to control nobody to fly
Machine.
In the present embodiment, the span of the fixed wing aircraft model plane is 1000mm, and the length of the fuselage is 810mm.
In the present embodiment, the high-definition camera 9 is the high-definition camera of 8,000,000 pixels, captured by this high-definition camera
Picture it is clear, and long transmission distance, collocation aircraft can complete remote investigation.
In the present embodiment, the wing 7 is detachably connected with side plate 3, and the tailplane 5 is detachably connected with bottom plate 2,
The vertical tail 6 is detachably connected with cover plate 4, is easily installed dismounting, convenient to carry.
Operation principle of the present utility model is：First, taken off according to environmental condition, arrive in the region overhead to be investigated by plane,
The captured in real-time image of high-definition camera 9, the image information of collection is transferred to picture signal using visual signal transmitter 10 and connect
Device is received, is then analyzed according to target information, so as to have a better understanding to zone of ignorance.Then, manipulator is according to reality
Border situation can be incorporated.
It is described above, only it is preferred embodiment of the present utility model, not the utility model is imposed any restrictions, every
Any simple modification, change and the equivalent structure transformation made according to the utility model technical spirit to above example, still
Belong in the protection domain of technical solutions of the utility model.
Claims (7)
1. a kind of investigate fixed wing aircraft model plane over the ground, it is characterised in that：Including fuselage, the fuselage includes bottom plate (2), side plate
(3) and cover plate (4), the cover plate (4) are arranged on the top of bottom plate (2), and the quantity of the side plate (3) is two pieces, described in two pieces
Side plate (3) is symmetricly set on the left and right sides of bottom plate (2), and the bottom of the side plate (3) is connected with bottom plate (2), the side plate (3)
Top be connected with cover plate (4), wing (7) is installed, the wing (7) is connected with side plate (3), described in the middle part of the fuselage
The afterbody of fuselage is provided with tailplane (5) and vertical tail (6), and the tailplane (5) is connected with bottom plate (2), described to hang down
Fin (6) is connected with cover plate (4), and the head of the fuselage is provided with engine (1), on the output shaft of the engine (1)
Propeller (8) is installed, the bottom of the bottom plate (2) is provided with the high-definition camera (9) for captured in real-time picture, the machine
Visual signal transmitter (10) for the picture transmission captured by high-definition camera (9) to be gone out, the height are installed in body
Clear camera (9) is connected with visual signal transmitter (10).
2. according to the fixed wing aircraft model plane of investigation over the ground described in claim 1, it is characterised in that：The bottom of the bottom plate (2)
Thermal infrared imager (11) is also equipped with, the thermal infrared imager (11) is located at the rear of high-definition camera (9).
3. according to the fixed wing aircraft model plane of investigation over the ground described in claim 1 or 2, it is characterised in that：Pacify on the cover plate (4)
Equipped with the laser range finder (12) for survey aircraft flying height.
4. according to the fixed wing aircraft model plane of investigation over the ground described in claim 1 or 2, it is characterised in that：The head of the fuselage
It is also equipped with IR evading obstacle sensors (13).
5. according to the fixed wing aircraft model plane of investigation over the ground described in claim 1 or 2, it is characterised in that：The fixed wing aircraft
The span of model plane is 1000mm, and the length of the fuselage is 810mm.
6. according to the fixed wing aircraft model plane of investigation over the ground described in claim 1 or 2, it is characterised in that：The high-definition camera
(9) it is the high-definition camera of 8,000,000 pixels.
7. according to the fixed wing aircraft model plane of investigation over the ground described in claim 1 or 2, it is characterised in that：The wing (7) and side
Plate (3) is detachably connected, and the tailplane (5) is detachably connected with bottom plate (2), and the vertical tail (6) can with cover plate (4)
Dismantling connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720414983.2U CN206652246U (en) | 2017-04-19 | 2017-04-19 | Fixed wing aircraft model plane are investigated over the ground |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720414983.2U CN206652246U (en) | 2017-04-19 | 2017-04-19 | Fixed wing aircraft model plane are investigated over the ground |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206652246U true CN206652246U (en) | 2017-11-21 |
Family
ID=60317904
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720414983.2U Expired - Fee Related CN206652246U (en) | 2017-04-19 | 2017-04-19 | Fixed wing aircraft model plane are investigated over the ground |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206652246U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108609201A (en) * | 2018-06-06 | 2018-10-02 | 中电科芜湖通用航空产业技术研究院有限公司 | Verification machine is compared in light-duty single-shot hybrid power aeroplane contracting |
| CN111846227A (en) * | 2020-07-30 | 2020-10-30 | 西安航空学院 | Adopt bionical separation to flow miniature unmanned aerial vehicle of wing section |
-
2017
- 2017-04-19 CN CN201720414983.2U patent/CN206652246U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108609201A (en) * | 2018-06-06 | 2018-10-02 | 中电科芜湖通用航空产业技术研究院有限公司 | Verification machine is compared in light-duty single-shot hybrid power aeroplane contracting |
| CN111846227A (en) * | 2020-07-30 | 2020-10-30 | 西安航空学院 | Adopt bionical separation to flow miniature unmanned aerial vehicle of wing section |
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Legal Events
| 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: 20171121 Termination date: 20180419 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |