CN204331478U - Unmanned plane is left a blank supervisory system - Google Patents
Unmanned plane is left a blank supervisory system Download PDFInfo
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- CN204331478U CN204331478U CN201420851754.3U CN201420851754U CN204331478U CN 204331478 U CN204331478 U CN 204331478U CN 201420851754 U CN201420851754 U CN 201420851754U CN 204331478 U CN204331478 U CN 204331478U
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Abstract
A kind of unmanned plane is left a blank supervisory system, and emergent buffering parachute being housed at unmanned plane top; Semicircle screw propeller protector is installed additional between often pair of upper and lower two screw propellers; On carry bar, carry the LED of two video cameras and four 100 watts; The high definition minisize pick-up head of two adjustable-angles is also housed in unmanned plane bottom; In the bottom of unmanned plane, circular unmanned plane base is housed; The launching platform frame being positioned at ground is dock shape with unmanned plane base; In the bottom of launching platform frame, power supply is housed and video line rolls frame, the power lead end of incoming cables of rolling on frame at power supply and video line is connected to direct current voltage regulator; It is also provided with induction motor and remote pilot box.The utility model has good illumination functions, and shooting picture is clear; Adopt ground power supply system and audio video synchronization download system, monitoring of can leaving a blank for a long time; Adopt induction motor device, motor can be allowed automatically to respond to unmanned plane height and automatically rotate, folding and unfolding electric wire, make electric wire obtain reasonable maximization and use.
Description
Technical field
The utility model belongs to monitoring field of taking photo by plane, and more particularly, relates to a kind of unmanned plane and to leave a blank supervisory system.
Background technology
Along with advancing by leaps and bounds of national economic development, resource exploration and environmental monitoring work more and more important, duty cycle is shorter and shorter, and conventional satellite and airborne remote sensing means have been difficult to meet application demand.In recent years, low-altitude remote sensing dynamic monitoring and emergency monitoring are mainly used among a small circle repeatedly the emergency monitoring etc. of dynamic monitoring and unexpected incidents repeatedly, and the demand of large-scale cartography, these detection requirement remote sensing obtains system to be possessed: 1, coverage count ability; 2, wave band, resolution and time suitable Spatial data capture ability; 3, the providing capability of quantitative data; 4, high-precision fixed capability.This target realize non-single platform or sensor can be competent at.Due to the impact by factors such as satellite recursion period, spatial domain use and weathers, the guarantee in remotely-sensed data source has become bottleneck problem of its application of restriction.
All kinds of disaster of modern society and accident take place frequently, if state of affairs progress can not be understood in time, can seriously limit the rescue assessment of disaster and the control treatment to accident, thus cause even more serious casualties and economic loss, therefore wide in the urgent need to a kind of scope, without dead angle, mobility strong, tracking system real-time dynamic that synchronizing information is high.The development of unmanned air vehicle technique, its application surface is more and more wider, all embody indispensable importance at civil area and military domain, the application especially in aeroplane photography is more and more extensive, adopts unmanned plane to become the main flow of development at present as aeroplane photography platform.But existing unmanned plane does not possess the function of illumination, the picture taking out under night or the bad condition of light is fuzzyyer, brings very large trouble to taking photo by plane; Simultaneously unmanned plane is in flight course, and monitoring equipment is easily subject to windage thus changes camera lens orientation, affect shooting effect, for the electric wire of powering also along with the change of unmanned plane height is stretched back and forth, can not get reasonable maximization use.
Utility model content
The purpose of this utility model will overcome the above problems exactly, and provide a kind of unmanned plane to leave a blank supervisory system, it has good illumination functions, and shooting picture is clear; Supervisory system can steadily be taken for a long time, simultaneously can by the highly automated folding and unfolding electric wire of induction unmanned plane, make unmanned plane can meet scope wide, without dead angle, mobility strong, real-time dynamic monitoring that synchronizing information is high.
The technical scheme that the utility model provides is: a kind of unmanned plane is left a blank supervisory system, and it comprises the tilt-top of unmanned plane, GPS positioning system, screw propeller, gyro sensor, video camera, fixing camera; Be characterized in: each screw propeller of unmanned plane is designed to upper and lower two screw propellers, driven by upper and lower screw propeller motor respectively; Emergent buffering parachute is housed at unmanned plane top; Outside semicircle screw propeller protector is installed additional between often pair of upper and lower two screw propellers; Be provided with carry bar in unmanned plane the latter half, on carry bar, carry the LED of two video cameras and four 100 watts; Camera lens wiper is provided with outside camera lens; The high definition minisize pick-up head of two adjustable-angles is also housed in unmanned plane bottom, 30 watts of spotlight LED lamps of adjustable-angle are housed on high definition minisize pick-up head both sides; In the bottom of unmanned plane, circular unmanned plane base is housed; The launching platform frame being positioned at ground is round table-like, and the upper plane of round platform is fluted body ring-type, with the circular unmanned plane base of aircraft in docking shape; In the bottom of launching platform frame, power supply is housed and video line rolls frame, power supply and video line roll power supply that frame is wound around and video line are connected unmanned plane with unmanned plane base holes power input and camera video output terminal through the upper hole of launching platform frame; The side of rolling frame at power supply and video line is provided with video transmission interface, and the power lead end of incoming cables of rolling on frame at power supply and video line is connected to direct current voltage regulator; It is also provided with induction motor and remote pilot box; Induced electricity arbor is contained in rotating shaft place that power supply and video line roll frame.
The technical scheme adopting the utility model to provide, compared with prior art, has following remarkable result:
(1) the utility model adopts illumination aircraft device, and have good illumination functions, shooting picture is clear;
(2) the utility model adopts ground power supply system and audio video synchronization download system, monitoring of can leaving a blank for a long time;
(3) the utility model adopts induction motor device, motor can be allowed automatically to respond to unmanned plane height and automatically rotate, folding and unfolding electric wire, makes electric wire obtain reasonable maximization and uses.By above device make unmanned plane can realize scope wide, without dead angle, mobility strong, real-time dynamic monitoring that synchronizing information is high.
Accompanying drawing explanation
Fig. 1 is superstructure schematic diagram of the present utility model.
Fig. 2 is substructure schematic diagram of the present utility model.
In figure: 1, emergent buffering parachute; 2, upper and lower screw propeller motor; 3, screw propeller protector; 4, carry bar; 5, power supply and video line; 6, unmanned plane base; 7, camera lens wiper; 8,100 watts of LED; 9, high definition minisize pick-up head; 10,30 watts of spotlight LED lamps; 11, launching platform frame; 12, video transmission interface; 13, power supply and video line roll frame; 14, direct current voltage regulator; 15, remote pilot box; 16, a key takes off and lifting key; 17, decline key; 18, a key return key; 19, induced electricity arbor.
Embodiment
As can be seen from Fig. 1 and Fig. 2, a kind of unmanned plane of the present utility model is left a blank supervisory system, and it comprises the tilt-top of unmanned plane, GPS positioning system, screw propeller, gyro sensor, video camera, fixing camera.Unmanned plane adopts upper and lower double dynamical design, and each screw propeller is designed to upper and lower two screw propellers, is driven respectively by upper and lower screw propeller motor 2; One is enhance aircraft lifting capacity, and two is reduce frame further, improves the portability of transporting transport; Three is the stability that improve attitude of leaving a blank, and guarantees that monitor video is smooth; Four is improve aircraft safety, and the aircraft avoiding a certain electrical fault to cause is unbalance to fall.Emergent buffering parachute 1 is housed at unmanned plane top, when aircraft occurs abnormal, automatically identifies and launch out parachute, the crowd on ground more protected by protection aircraft.Outside semicircle screw propeller protector 3 is installed additional between often pair of upper and lower two screw propellers; one is guarantee that in transport, screw propeller is not by accidental damage; two is ensure that screw propeller does not touch foreign matter awing, and three is avoid unmanned plane burst accidental falling to cause the oar of High Rotation Speed to injure ground staff.Be provided with carry bar 4 in unmanned plane the latter half, on carry bar, carry the LED 8 of two video cameras and four 100 watts, and carry bar plays a part to form a connecting link, and is also simultaneously in order to can conveniently fast disassembling; 100 watts of LED adjustable-angles, search and rescue for ground and provide visible light source, unmanned plane is also provided with the patten transformation program of lamp simultaneously, is scattering search pattern respectively; Optically focused locking mode; Rescue quick-fried sudden strain of a muscle pattern.Outside camera lens, be provided with camera lens wiper 7, unmanned plane overhead rear lens has foreign matter or has fog, or When the Rain Comes, uses camera lens windscreen wiper, can remove foreign material or rainwater.The high definition minisize pick-up head 9 of two adjustable-angles is also housed in unmanned plane bottom, 30 watts of spotlight LED lamps 10 of adjustable-angle are housed on high definition minisize pick-up head 9 both sides, high definition minisize pick-up head 9 and 30 watts of spotlight LED lamps 10 can adjusted in concert angles, ensure camera shooting effect.In the bottom of unmanned plane, circular unmanned plane base 6 is housed, the frame that just in time falls during for landing is being positioned at the launching platform frame 11 on ground; Launching platform frame 11 is in round table-like, and the upper plane of round platform is fluted body ring-type, and with the circular unmanned plane base 6 of aircraft in docking shape, automatically lock after being convenient to unmanned plane landing, unmanned plane is not easily tumbled, and ensures unmanned plane and airborne electric equipment safety; Launching platform frame is integrated with electric power system further in addition, carries more convenient.In the bottom of launching platform frame 11, power supply is housed and video line rolls frame 13, power supply and video line roll power supply that frame 13 is wound around and video line 5 are connected unmanned plane with unmanned plane base 6 hole power input and camera video output terminal through the upper hole of launching platform frame 11.The side of rolling frame 13 at power supply and video line is provided with video transmission interface 10, for exporting camera shooting and video signal.The power lead end of incoming cables of rolling on frame 13 at power supply and video line is connected to direct current voltage regulator 14, according to the height of the height regulating power source voltage of electric wire lift-off.Also be provided with induction motor and remote pilot box 15 in addition; Induced electricity arbor 19 is contained in rotating shaft place that power supply and video line roll frame 13, induction motor by the receipts that can respond to unmanned plane height and control power supply and video line 5 with put.Remote pilot box 15 is provided with a key and takes off and lifting key 16, decline key 17, key return key 18.
Claims (3)
1. unmanned plane is left a blank a supervisory system, and it comprises the tilt-top of unmanned plane, GPS positioning system, screw propeller, gyro sensor, video camera, fixing camera; It is characterized in that: each screw propeller of unmanned plane is designed to upper and lower two screw propellers, driven by upper and lower screw propeller motor (2) respectively; Emergent buffering parachute (1) is housed at unmanned plane top; Outside semicircle screw propeller protector (3) is installed additional between often pair of upper and lower two screw propellers; Be provided with carry bar (4) in unmanned plane the latter half, on carry bar, carry the LED (8) of two video cameras and four 100 watts; Camera lens wiper (7) is provided with outside camera lens; The high definition minisize pick-up head (9) of two adjustable-angles is also housed in unmanned plane bottom, 30 watts of spotlight LED lamps (10) of adjustable-angle are housed on high definition minisize pick-up head both sides; Circular unmanned plane base (6) is housed in the bottom of unmanned plane; Be positioned at the launching platform frame (11) on ground in round table-like, the upper plane of round platform is fluted body ring-type, with the circular unmanned plane base (6) of aircraft in docking shape; In the bottom of launching platform frame (11), power supply is housed and video line rolls frame (13), power supply and video line roll power supply that frame is wound around and video line (5) the upper hole through launching platform frame is connected unmanned plane power input and camera video output terminal with unmanned plane base holes; The side of rolling frame at power supply and video line is provided with video transmission interface (10), is connected to direct current voltage regulator (14) in the power lead end of incoming cables that power supply and video line roll on frame; It is also provided with induction motor and remote pilot box (15); Induced electricity arbor (19) is contained in rotating shaft place that power supply and video line roll frame.
2. a kind of unmanned plane according to claim 1 is left a blank supervisory system, it is characterized in that: LED (8) adjustable-angle of described 100 watts, is also provided with the patten transformation program of lamp, is scattering search pattern respectively; Optically focused locking mode; Rescue quick-fried sudden strain of a muscle pattern.
3. a kind of unmanned plane according to claim 1 and 2 is left a blank supervisory system, it is characterized in that: described remote pilot box (15) is provided with a key and takes off and lifting key (16), decline key (17), a key return key (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420851754.3U CN204331478U (en) | 2014-12-29 | 2014-12-29 | Unmanned plane is left a blank supervisory system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420851754.3U CN204331478U (en) | 2014-12-29 | 2014-12-29 | Unmanned plane is left a blank supervisory system |
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| Publication Number | Publication Date |
|---|---|
| CN204331478U true CN204331478U (en) | 2015-05-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201420851754.3U Expired - Fee Related CN204331478U (en) | 2014-12-29 | 2014-12-29 | Unmanned plane is left a blank supervisory system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104483987A (en) * | 2014-12-29 | 2015-04-01 | 马鞍山市赛迪智能科技有限公司 | Drone airborne monitoring system |
| US20210066995A1 (en) * | 2017-12-25 | 2021-03-04 | Guangzhou Xaircraft Technology Co., Ltd | Driving device, spraying device, and unmanned aerial vehicle |
-
2014
- 2014-12-29 CN CN201420851754.3U patent/CN204331478U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104483987A (en) * | 2014-12-29 | 2015-04-01 | 马鞍山市赛迪智能科技有限公司 | Drone airborne monitoring system |
| US20210066995A1 (en) * | 2017-12-25 | 2021-03-04 | Guangzhou Xaircraft Technology Co., Ltd | Driving device, spraying device, and unmanned aerial vehicle |
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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: 20150513 Termination date: 20151229 |
|
| EXPY | Termination of patent right or utility model |