CN203211514U - Fixed-wing aircraft for aerial photographing - Google Patents
Fixed-wing aircraft for aerial photographing Download PDFInfo
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- CN203211514U CN203211514U CN 201220647667 CN201220647667U CN203211514U CN 203211514 U CN203211514 U CN 203211514U CN 201220647667 CN201220647667 CN 201220647667 CN 201220647667 U CN201220647667 U CN 201220647667U CN 203211514 U CN203211514 U CN 203211514U
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Abstract
The utility model discloses a fixed-wing aircraft for aerial photographing and a taking off and landing method of the fixed-wing aircraft. The fixed-wing aircraft comprises a flying wing layout model aeroplane (1), a photographing device and a remote control device, wherein the photographing device and a flight controller (10) are mounted at the middle part of the model aeroplane (1), and the flight controller (10) is electrically connected with a steering gear (7) and an engine (8) of the model aeroplane (1). The fixed-wing aircraft disclosed by the utility model is provided with the flight controller, so that the flight attitude can be automatically adjusted, thereby reducing the influence of flight instability on the quality of photographing.
Description
Technical field
This use is novel to relate to a kind of small-sized unmanned plane and landing method thereof of taking photo by plane.
Background technology
Unmanned plane is taken photo by plane and photographed is as aerial platform with robot airplane, with airborne sensory equipment, as high resolution CCD digital camera, light-duty optical camera, infrared scanner, laser scanner, magnetic determining device etc. obtain information, with computing machine graphicinformation is handled, and be made into image according to certain accuracy requirement.
For taking photo by plane of over the horizon, adopt the fixed-wing aircraft more, existing miniature self-service machine platform is subjected to the interference of air-flow easily because quality is little, has the problem of flight stability deficiency when taking photo by plane, and the vibration of driving engine also influences shooting quality in addition.
The fixed-wing aircraft needs special place usually when landing, be difficult to find suitable landing site in mountain areas such as Guizhou.
Summary of the invention
The novel technical matters that will solve of this use: nobody flight instability that aircraft exists of taking photo by plane at the existing fixed wing, big problem is disturbed in vibrations etc., provide a kind of can stabilized flight and the little fixed-wing unmanned plane of obstacle of vibration, and improved the landing mode.
This use new technique scheme:
A kind of be used to the fixed-wing aircraft of taking photo by plane, the model of an airplane, capture apparatus and the telecommand equipment that comprise the all-wing aircraft layout, it is characterized in that: at the model of an airplane middle part capture apparatus and flight controller are installed, flight controller is electrically connected steering wheel and the driving engine of the model of an airplane.
The model of an airplane is provided with mounting groove, and capture apparatus and flight controller are respectively by unsettled being installed in each self-corresponding mounting groove of plastic cloth.
Model of an airplane right side is provided with the GPS receiver and flight controller is electrically connected.
Model of an airplane right side is provided with pitot and flight controller is electrically connected.
The front end of the model of an airplane is installed camera, and camera is electrically connected with the graphic transmission equipment that is installed in model of an airplane left side.
Vertical wing tip winglet and the wing fence installed on the model of an airplane, the length of wing tip winglet is greater than the chord length of wing wing tip.
This uses novel beneficial effect:
1. be provided with flight controller, can adjust flight attitude automatically, reduce because of the unstable influence to shooting quality of flying.
2. capture apparatus and flight controller and aircraft fuselage are non-being rigidly connected, and can avoid engine vibration to the influence of equipment normal operation so as far as possible.
3. the GPS receiver is set, can makes things convenient for Long-distance Control by the geographic position in the gps system positioning flight.
4. dispose pitot, can detect air velocity in real time, and signal is transmitted auto mat, avoid aircraft stall.
5. dispose camera and the graphic transmission equipment at drive simulating visual angle, aloft driving visual angle is transferred to the control personnel here, can better grasp state of flight.
6. be vertically installed with large-sized wing tip winglet and wing fence on the wing, can improve flight stability.
Description of drawings:
Fig. 1 is this use new structure scheme drawing.
The specific embodiment:
In 2 meters of the model of an airplane 1 preferred dimensions, 3 kilograms of total launching weights are with the high rigidity foamed materials of interior high density fixed-wing telecontrolled aircraft model, be provided with mounting groove at the model of an airplane 1 middle part, capture apparatus 6 and flight controller 10 are respectively by 11 unsettled being installed in each self-corresponding mounting groove of a plastic cloth, and flight controller 10 and steering wheel 7, driving engine 8 are electrically connected.The model of an airplane 1 right side is provided with GPS receiver 13 and pitot 14, all is electrically connected with flight controller 10.The front end of the model of an airplane 1 is installed camera 12, and camera 12 and the graphic transmission equipment 7 that is installed on the model of an airplane 1 are electrically connected, and for preventing and GPS receiver 13 mutual interference mutually, graphic transmission equipment 7 are located at the left side.
The size of the wing tip winglet 2 on the master model aircraft 1 is strengthened, and the length of wing tip winglet 2 is 1.5 ~ 1.8 times of chord length of wing wing tip, and wing fence 4 is installed, and the size of wing fence 4 is also bigger.
Landing method: adopt the artificial hand throwing when taking off or utilize the catapult-launching gear emission, set up rack in predetermined level point during landing, the control model of an airplane 1 hits the net landing.
Claims (6)
1. one kind is used for the fixed-wing aircraft take photo by plane, the model of an airplane (1), capture apparatus and the telecommand equipment that comprise the all-wing aircraft layout, it is characterized in that: at the model of an airplane (1) middle part capture apparatus (6) and flight controller (10) are installed, flight controller (10) is electrically connected steering wheel (7) and the driving engine (8) of the model of an airplane (1).
2. described be used to the fixed-wing aircraft of taking photo by plane according to claim 1, it is characterized in that: the model of an airplane (1) is provided with mounting groove, and capture apparatus (6) and flight controller (10) are respectively by unsettled being installed in each self-corresponding mounting groove of a plastic cloth (11).
3. described be used to the fixed-wing aircraft of taking photo by plane according to claim 1, it is characterized in that: the model of an airplane (1) right side is provided with GPS receiver (13), and flight controller (10) is electrically connected.
4. described be used to the fixed-wing aircraft of taking photo by plane according to claim 1, it is characterized in that: the model of an airplane (1) right side is provided with pitot (14), and flight controller (10) is electrically connected.
5. described be used to the fixed-wing aircraft of taking photo by plane according to claim 1, it is characterized in that: the front end of the model of an airplane (1) is installed camera (12), camera (12) and be installed in graphic transmission equipment (7) electrical connection in the model of an airplane (1) left side.
6. described be used to the fixed-wing aircraft of taking photo by plane according to claim 1, it is characterized in that: go up vertical wing tip winglet (2) and the wing fence (4) installed at the model of an airplane (1), the length of wing tip winglet (2) is greater than the chord length of wing wing tip.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220647667 CN203211514U (en) | 2012-11-30 | 2012-11-30 | Fixed-wing aircraft for aerial photographing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220647667 CN203211514U (en) | 2012-11-30 | 2012-11-30 | Fixed-wing aircraft for aerial photographing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203211514U true CN203211514U (en) | 2013-09-25 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220647667 Expired - Fee Related CN203211514U (en) | 2012-11-30 | 2012-11-30 | Fixed-wing aircraft for aerial photographing |
Country Status (1)
| Country | Link |
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| CN (1) | CN203211514U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102923305A (en) * | 2012-11-30 | 2013-02-13 | 贵州新视界航拍科技有限公司 | Fixed-wing aircraft for aerial photography and method for taking off and landing |
| CN103803093A (en) * | 2014-03-03 | 2014-05-21 | 天津曙光敬业科技有限公司 | Fixed-wing unmanned aerial vehicle aerial shooting device |
| CN109353486A (en) * | 2018-11-12 | 2019-02-19 | 李紫萱 | A kind of balloon soaring plane |
| WO2019118623A1 (en) | 2017-12-12 | 2019-06-20 | American Honda Motor Co., Inc. | Flow fence for an aircraft winglet |
| CN111372850A (en) * | 2017-12-12 | 2020-07-03 | 美国本田有限公司 | Air guide fence for aircraft winglet |
-
2012
- 2012-11-30 CN CN 201220647667 patent/CN203211514U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102923305A (en) * | 2012-11-30 | 2013-02-13 | 贵州新视界航拍科技有限公司 | Fixed-wing aircraft for aerial photography and method for taking off and landing |
| CN103803093A (en) * | 2014-03-03 | 2014-05-21 | 天津曙光敬业科技有限公司 | Fixed-wing unmanned aerial vehicle aerial shooting device |
| CN103803093B (en) * | 2014-03-03 | 2016-03-23 | 天津曙光敬业科技有限公司 | Fixed-wing unmanned plane aerial device |
| WO2019118623A1 (en) | 2017-12-12 | 2019-06-20 | American Honda Motor Co., Inc. | Flow fence for an aircraft winglet |
| CN111372850A (en) * | 2017-12-12 | 2020-07-03 | 美国本田有限公司 | Air guide fence for aircraft winglet |
| EP3724067A4 (en) * | 2017-12-12 | 2021-09-01 | American Honda Motor Co., Inc. | Flow fence for an aircraft winglet |
| US11447238B2 (en) * | 2017-12-12 | 2022-09-20 | American Honda Motor Co., Inc. | Flow fence for an aircraft winglet |
| CN111372850B (en) * | 2017-12-12 | 2024-02-23 | 美国本田有限公司 | Flow fence for aircraft winglets |
| CN109353486A (en) * | 2018-11-12 | 2019-02-19 | 李紫萱 | A kind of balloon soaring plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130925 Termination date: 20151130 |
|
| EXPY | Termination of patent right or utility model |