CN103803093A - Fixed-wing unmanned aerial vehicle aerial shooting device - Google Patents
Fixed-wing unmanned aerial vehicle aerial shooting device Download PDFInfo
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- CN103803093A CN103803093A CN201410074355.5A CN201410074355A CN103803093A CN 103803093 A CN103803093 A CN 103803093A CN 201410074355 A CN201410074355 A CN 201410074355A CN 103803093 A CN103803093 A CN 103803093A
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Abstract
The invention relates to a fixed-wing unmanned aerial vehicle aerial shooting device which comprises an imaging device, a fixing frame, a sliding rail and a transmission system. The sliding rail is arranged at the front end of a vehicle head of a fixed-wing unmanned aerial vehicle and extends to the bottom of the vehicle head along the top of the vehicle head, the imaging device is fixed to the fixing frame, the fixing frame is installed on the sliding rail, and the transmission system is connected with the fixing frame. The fixing frame slides on the sliding rail through the transmission system. According to the fixed-wing unmanned aerial vehicle aerial shooting device, the sliding rail is arranged at the front end of the vehicle head, the imaging device can slide to the top or the bottom of the vehicle head along the sliding rail, and damage to the imaging device when the unmanned aerial vehicle takes off and lands is reduced; the fixed-wing unmanned aerial vehicle aerial shooting device is simple in structure and low in manufacturing cost.
Description
Technical field
The invention belongs to the unmanned plane technical field of taking photo by plane, be specifically related to a kind of fixed-wing unmanned plane aerial device.
Background technology
There is voyage advantage far away, fireballing for the fixed-wing unmanned plane of taking photo by plane, its general wheeled sliding race formula that adopts of taking off, in prior art, aerial device is generally installed on unmanned plane body below, because of the hypersensitivity of aerial device, when Fixed Wing AirVehicle takes off, be easy to aerial device to cause damage.
In patent of invention 201120560788.3, disclose and a kind of aerial device has been installed on the rotary head on head.But the landing modes of fixed-wing unmanned plane is generally parachuting and hits two kinds, net, easy damage aircraft when parachuting landing, adopt landed to the less net mode that hits of aircraft damage more at present, but tail up while hitting net landing, aerial device is arranged on head position, is easy to damage.And the cost of The Cloud Terrace is very expensive, structure is also comparatively complicated.
Summary of the invention
In the time rising and falling, reduce the technical matters to aerial device infringement for solving fixed-wing unmanned plane, the present invention proposes a kind of fixed-wing unmanned plane aerial device of slide rail type.
Technical scheme of the present invention is: a kind of fixed-wing unmanned plane aerial device, comprises imaging device, fixed mount, slide rail and driving system; Described slide rail is arranged at the head front end of fixed-wing unmanned plane, extends to head bottom along head top, and imaging device is fixed on fixed mount, and fixed mount is installed on slide rail, and driving system is connected with fixed mount.Fixed mount slides on slide rail by driving system.
Described driving system comprises the steering wheel a and steering wheel b, coil a and coil b, assembly pulley and the hawser group that are arranged on described fixed-wing unmanned plane head top; Assembly pulley comprises pulley a, pulley b and pulley c, and hawser group comprises hawser a and hawser b.The output shaft of described steering wheel a is connected with the main shaft of coil a, when steering wheel a work, and band moving winding a rotation.The output shaft of steering wheel b is connected with the main shaft of coil b, when steering wheel b work, and band moving winding b rotation.Hawser a one end is upper around coil a, and the other end is walked around pulley a and is connected with fixed mount rear end, and go up around coil b hawser b one end, and the other end walks around pulley b, walk around pulley c along slide rail is connected with fixed mount front end.
Described pulley a and pulley b are fixed on head top by vertical shaft a, and vertical shaft a is between slide rail and steering wheel a and steering wheel b, and pulley a and pulley b are socketed on vertical shaft a from top to bottom.
Described pulley c is fixed on head bottom by vertical shaft b, and pulley c is socketed on vertical shaft b.
When fixed-wing unmanned plane takes off or lands, by driving system, imaging device is transported to head top along slide rail; When fixed-wing unmanned plane aloft hovers, driving system is delivered to head bottom by imaging device along slide rail, starts shooting work.
Beneficial effect of the present invention is: head front end is arranged slide rail by the present invention, makes imaging device to slide into head top or bottom along slide rail, the infringement to imaging device while having reduced unmanned plane landing; And the present invention is simple in structure, cost of manufacture is lower.
Accompanying drawing explanation
Fig. 1 is one of structural representation of the present invention;
Fig. 2 is two of structural representation of the present invention;
Fig. 3 is three of structural representation of the present invention.
Wherein, 1, steering wheel a; 2, coil a; 3, hawser a; 4, pulley a; 5, vertical shaft a; 6, fixed mount; 7, imaging device; 8, slide rail; 9, hawser b; 10, vertical shaft b; 11, pulley c; 12, head; 13, pulley b; 14, steering wheel b; 15, coil b.
The specific embodiment
Illustrate the present invention below in conjunction with accompanying drawing.
As shown in Figure 1-Figure 3, fixed-wing unmanned plane aerial device of the present invention, comprises imaging device 7, fixed mount 6, slide rail 8 and driving system.Slide rail 8 be arranged at fixed-wing unmanned plane head 12 front ends, extend to head 12 bottoms along head 12 tops, imaging device 7 is fixed on fixed mount 6, fixed mount 6 is installed on slide rail 8, driving system is connected with fixed mount 6.
Driving system comprises the steering wheel a1 and steering wheel b14, coil a2 and coil b15, assembly pulley and the hawser group that are arranged on fixed-wing unmanned plane head 12 tops.Assembly pulley comprises pulley a4, pulley b13 and pulley c11, and hawser group comprises hawser a3 and hawser b9.The output shaft of steering wheel a1 is connected with the main shaft of coil a2, the output shaft of steering wheel b14 is connected with the main shaft of coil b15, hawser a3 one end is on coil a2, the other end is walked around pulley a4 and is connected with fixed mount 6 rear ends, hawser b9 one end is upper around coil b15, and the other end walks around pulley b13, walk around pulley c11 along slide rail 8 is connected with fixed mount 6 front ends.
Pulley a4 and pulley b13 are fixed on head 12 tops by vertical shaft a5, and vertical shaft a5 is between slide rail 8 and steering wheel a1 and steering wheel b14, and pulley a4 and pulley b13 are socketed on vertical shaft a5 from top to bottom.
Pulley c11 is fixed on head 12 bottoms by vertical shaft b10, and pulley c11 is socketed on vertical shaft b10.
When fixed-wing unmanned plane takes off or lands, by driving system, imaging device 7 is transported to head 12 tops along slide rail 8; When fixed-wing unmanned plane aloft hovers, driving system is delivered to head 12 bottoms by imaging device 7 along slide rail 8, starts shooting work.Specific works process is as follows:
When fixed-wing unmanned plane takes off or lands, steering wheel a1 work, steering wheel b14 does not lock.Steering wheel a1, by band moving winding a2, makes hawser a3 slowly be wrapped in coil a2 upper, and hawser a3 changes the direction of power by pulley a4, and affects fixed mount 6 to slide to head 12 tops along slide rail 8.Hawser b9 and fixed mount 6 front ends are connected, and it is respectively by after pulley c11 and pulley b13 changed course, slowly from coil b15 around getting off.Fixed mount 6 slides to behind head 12 tops, by steering wheel a1 and steering wheel b14 locking, imaging device is fixed on to head top.
When fixed-wing unmanned plane aloft hovers, steering wheel b14 work, steering wheel a1 does not lock.Steering wheel b14, by band moving winding b15, makes hawser b9 slowly be wrapped in coil b15 upper, and hawser b9 changes the direction of power by pulley b13 and pulley c11, and affects fixed mount 6 to slide to head 12 bottoms along slide rail 8 from head 12 tops.Hawser a3 and fixed mount 6 rear ends are connected, and it is by after pulley a4 changed course, slowly from coil a2 around getting off.Fixed mount 6 slides to behind head 12 bottoms, and by steering wheel a1 and steering wheel b14 locking, the imaging device 7 being fixed on fixed mount 6 starts shooting work.
Fixed-wing unmanned plane, in the time taking photo by plane, according to the needs of the angle of taking photo by plane, can be controlled the position of steering wheel a1 and steering wheel b14 adjustment imaging device 7 simultaneously, determines suitable shooting angle.
Claims (4)
1. a fixed-wing unmanned plane aerial device, described fixed-wing unmanned plane comprises head (12), it is characterized in that: described aerial device comprises imaging device (7), fixed mount (6), slide rail (8) and driving system; Described slide rail (8) is arranged at head (12) front end, extends to head (12) bottom along head (12) top, described imaging device (7) is fixed on fixed mount (6), it is upper that fixed mount (6) is installed on slide rail (8), and driving system is connected with fixed mount (6).
2. fixed-wing unmanned plane aerial device according to claim 1, is characterized in that, described driving system comprises the steering wheel a(1 that is arranged on head (12) top) and steering wheel b(14), coil a(2) and coil b(15), assembly pulley and hawser group; Described assembly pulley comprises pulley a(4), pulley b(13) and pulley c(11), hawser group comprises hawser a(3) and hawser b(9); Steering wheel a(1) output shaft and coil a(2) main shaft be connected, steering wheel b(14) output shaft and coil b(15) main shaft be connected, hawser a(3) one end is around coil a(2) on, the other end is walked around pulley a(4) be connected with fixed mount (6) rear end, hawser b(9) one end is around coil b(15) upper, the other end is walked around pulley b(13), walk around pulley c(11 along slide rail (8)) be connected with fixed mount (6) front end.
3. fixed-wing unmanned plane aerial device according to claim 2, it is characterized in that, described pulley a(4) and pulley b(13) by vertical shaft a(5) be fixed on head (12) top, vertical shaft a(5) be positioned at slide rail (8) and steering wheel a(1) and steering wheel b(14) between, pulley a(4) and pulley b(13) be socketed on vertical shaft a(5 from top to bottom) on.
4. fixed-wing unmanned plane aerial device according to claim 2, is characterized in that, described pulley c(11) by vertical shaft b(10) be fixed on head (12) bottom, pulley c(11) be socketed on vertical shaft b(10) on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410074355.5A CN103803093B (en) | 2014-03-03 | 2014-03-03 | Fixed-wing unmanned plane aerial device |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201410074355.5A CN103803093B (en) | 2014-03-03 | 2014-03-03 | Fixed-wing unmanned plane aerial device |
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| CN103803093A true CN103803093A (en) | 2014-05-21 |
| CN103803093B CN103803093B (en) | 2016-03-23 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697312A (en) * | 2016-12-01 | 2017-05-24 | 安徽天鹰兄弟无人机科技创新有限公司 | Mounting structure of photographic mechanism of unmanned aerial vehicle |
| 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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| CN201626554U (en) * | 2009-12-07 | 2010-11-10 | 深圳市大疆创新科技有限公司 | Three-freedom-degree inertia stabilization aerial photography cradle head |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697312A (en) * | 2016-12-01 | 2017-05-24 | 安徽天鹰兄弟无人机科技创新有限公司 | Mounting structure of photographic mechanism of unmanned aerial vehicle |
| 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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| Publication number | Publication date |
|---|---|
| CN103803093B (en) | 2016-03-23 |
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Application publication date: 20140521 Assignee: TIANJIN SHUGUANG TIANCHENG TECHNOLOGY Co.,Ltd. Assignor: TIANJIN AURORA UAV TECHNOLOGY Co.,Ltd. Contract record no.: 2017990000086 Denomination of invention: Fixed-wing unmanned aerial vehicle aerial shooting device Granted publication date: 20160323 License type: Exclusive License Record date: 20170314 |
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Effective date of registration: 20170418 Address after: 300000 Tianjin city Dongli District Junliangcheng Tengfei Road No. 3 floor of building B Patentee after: TIANJIN SHUGUANG TIANCHENG TECHNOLOGY Co.,Ltd. Address before: No. 300151 Tianjin road Hebei District City, Wang Chuanchang Hospital No. 62 Patentee before: TIANJIN AURORA UAV TECHNOLOGY Co.,Ltd. |
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Effective date of registration: 20221010 Address after: 300457 No. 105, Building 9, Zone B3 (formerly Zone 2 of Ronghui Business Park), Binhai Zhongguancun Science and Technology Park, Tianjin Economic and Technological Development Zone, Binhai New Area, Tianjin Patentee after: Tianjin Phoenix Intelligent Technology Co.,Ltd. Address before: Floor 1, block B, No.3, Tengfei Road, Junliang City, Dongli District, Tianjin Patentee before: TIANJIN SHUGUANG TIANCHENG TECHNOLOGY Co.,Ltd. |
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