CN108248877A - A kind of aerial survey unmanned plane task device protective device - Google Patents
A kind of aerial survey unmanned plane task device protective device Download PDFInfo
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- CN108248877A CN108248877A CN201810042537.2A CN201810042537A CN108248877A CN 108248877 A CN108248877 A CN 108248877A CN 201810042537 A CN201810042537 A CN 201810042537A CN 108248877 A CN108248877 A CN 108248877A
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- task
- unmanned plane
- equipment
- control system
- task device
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- 230000001681 protective effect Effects 0.000 title claims abstract description 22
- 238000013016 damping Methods 0.000 claims abstract description 17
- 230000007246 mechanism Effects 0.000 claims abstract description 8
- 238000004891 communication Methods 0.000 claims description 3
- 230000008901 benefit Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000007474 system interaction Effects 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000005856 abnormality Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000003204 osmotic effect Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Feedback Control In General (AREA)
Abstract
The present invention relates to a kind of aerial survey unmanned plane task device protective devices; including device body; described device ontology includes control system, installing mechanism, equipment protecting equipment, power plant and damping device; and device body is equipped with external interface; the external interface connects control system, orders and performs for receiving；The control system connecting power device, the power plant are set on above equipment protecting equipment, and driving equipment protective device is run, and the equipment protecting equipment includes screw and auxiliary rod；It is an advantage of the invention that so that the reasonable folding and unfolding of task device, so as to reduce the resistance of aircraft, improves the pneumatic property of aircraft；Task device will automatically retract body protective device when not working, if there is the problems such as emergency landing, parachuting, exception of taking off in aircraft, the probability that task device will be greatly reduced is damaged.
Description
Technical field
The present invention relates to fixed unmanned plane task device security fields, and in particular to a kind of aerial survey unmanned plane task device is protected
Protection unit.
Background technology
At present, unmanned plane industry in China's is fast-developing, and application range is also in rapid osmotic to all trades and professions.At present
It is mainly used in the industries such as geographical mapping, power-line patrolling, frontier defense patrol, oil-gas pipeline inspection.Unmanned plane during flying safety just into
For the problem that everybody payes attention to, and the task device of UAV flight is of high cost, and safety is just particularly important.
Auxiliary installation for unmanned plane task device is mainly two kinds of holder and gondola.Holder be usually used in more rotors nobody
Machine is broadly divided into two axis, three axis.It, which is acted on, is mainly used to stablize camera lens, eliminates unmanned plane roll, the rolling that pitching is brought to camera lens
It is dynamic.The advantage of gondola just seems more obvious, the work(such as small, light-weight, varifocal, automatically track target, equipment damping
Can, the drawback is that resolution ratio that is expensive, carrying camera is low and can only be compatible with included camera lens.
Fixed-wing conventional equipment volume is larger, and weight is in the slr camera of more than 1kg, laser radar, thermal camera, more
The professional equipments such as spectrum camera, it is all different per money equipment volume size, this is solved the problems, such as there is no corresponding measure, usually at present
It is fixed on body using simple damping processing.Presently, there are following two aspects problems：On the one hand, the image of acquisition can not
Fully meet requirement；Still further aspect, equipment fixation are to allow sensor daylighting aboard, its equipment is mounted on body
Outside affects the aeroperformance of aircraft, increases aircraft drag, reduces cruise duration first；Secondly, task device is flying
Machine takes off to be placed in outside body when landing and is highly prone to damage.
Existing Chinese patent document CN106347643A discloses a kind of unmanned plane automatic protective system, mainly solves
Problem is：Unmanned plane personnel out of control caused on unmanned plane and ground, property, equipment loss problem, solved with the present invention
Problem is different.
Invention content
Present invention aim to address the above problems, provide a kind of aerial survey unmanned plane task device protective device, can subtract
The resistance of few aircraft improves the pneumatic property of aircraft, meanwhile, reduce the probability that task device is damaged.
To achieve the above object, the present invention provides following technical solution：
A kind of aerial survey unmanned plane task device protective device, including device body, described device ontology include control system,
Installing mechanism, equipment protecting equipment, power plant and damping device, and device body is equipped with external interface, it is described to external
Mouth connection control system, orders and performs for receiving；The control system is used to judge that height of the unmanned plane apart from ground is
It is no to meet condition, and send out order command；The control system connecting power device, the power plant are filled set on equipment protection
Top is put, and driving equipment protective device is run, the equipment protecting equipment includes screw and auxiliary rod, the screw and auxiliary
Bar is set on task device surrounding, and the screw outer surface has screw thread, and the task device is slided up and down along screw external screw thread, institute
Auxiliary rod is stated for preventing task device position from shifting；Described installing mechanism one end damping device for connecting, other end connection
Task device, the damping device are set on above task device.
Further, the control system judges that task device meets the standard of condition for 30 meters apart from ground level.
Further, the power plant be motor, and its quantity be two, every portion be equipped with power cord, signal wire and
Communication line.
Further, the damping device is rubber shock-absorbing ball.
Further, the external interface is serial line interface.
The beneficial effects of the present invention are：
The present apparatus is independent Control architecture, can also pass through the instruction of the serial line interface of standard and its without instruction works
Its system interaction.The present apparatus causes the reasonable folding and unfolding of task device, so as to reduce the resistance of aircraft, improves the pneumatic property of aircraft；Appoint
Equipment of being engaged in will automatically retract this protective device when not working；If there is emergency landing, parachuting in aircraft, abnormal etc. ask of taking off
During topic, the probability that task device will be greatly reduced is damaged.The present apparatus does not interfere with the aeroperformance of aircraft, reduces aircraft
Resistance extends aircraft cruise duration.
Description of the drawings
Technical solution in order to illustrate the embodiments of the present invention more clearly, below will be to needed in embodiment description
Attached drawing is briefly described, it should be apparent that, the accompanying drawings in the following description is only the present invention in order to illustrate more clearly of this hair
Bright embodiment or technical solution of the prior art for those of ordinary skill in the art, are not making the creative labor
Under the premise of, it can also be obtained according to these attached drawings other attached drawings.
Fig. 1 is the device of the invention connection diagram；
Fig. 2 is the device of the invention work flow diagram.
Specific embodiment
A kind of aerial survey unmanned plane task device protective device as shown in Figure 1, including device body, described device ontology packet
Control system 1, installing mechanism 2, equipment protecting equipment 4, power plant 5 and damping device 6 are included, and device body is equipped with externally
Interface 3, the external interface 3 connect control system 1, order and perform for receiving；The control system 1 is used to judge nobody
Whether height of the machine apart from ground meets condition, and send out order command；1 connecting power device 5 of control system, it is described dynamic
Power apparatus 5 is set on 4 top of equipment protecting equipment, and driving equipment protective device 4 is run, and the equipment protecting equipment 4 includes silk
Bar 41 and auxiliary rod 42, the screw 41 and auxiliary rod 42 are set on 7 surrounding of task device, and 41 outer surface of screw has spiral shell
Line, the task device 7 are slided up and down along 41 external screw thread of screw, and the auxiliary rod 42 is used to prevent 7 position of task device from occurring
Offset；2 one end damping device for connecting 6 of installing mechanism, other end connection task device 7, the damping device 6 are set on task
7 top of equipment.
Further, the control system 1 judges that task device 7 meets the standard of condition for 30 meters apart from ground level.
Further, the power plant 5 be motor, and its quantity be two, every portion be equipped with power cord, signal wire and
Communication line.
Further, the damping device 6 is rubber shock-absorbing ball.
Further, the external interface 3 is serial line interface.
The present invention the course of work be：
Such as Fig. 2, when the present apparatus receives instruction, control system 1 detects whether to meet condition, and just response refers to when meeting condition
It enables, the condition of being unsatisfactory for can feed back exception information.5 driving equipment protective device 4 of power plant is run simultaneously, and the present apparatus is independent
Control architecture can also be instructed and other system interactions without instruction works by the external interface 3 of standard.Task device 7 exists
When not working, this protective device will be automatically retracted, if the problems such as emergency landing, parachuting, exception of taking off occurs in aircraft, by pole
Big reduces the impaired probability of task device 7.
Embodiment：
The present apparatus receives instruction, and the detection instruction of control system 1 meets condition：It, will be by external when 30 meters high from the ground
The publication of interface 3 performs order, and 5 driving equipment protective device 4 of power plant is run, when 1 testing result of control system is meets item
It during part, performs the receipts of task device 7 or puts, when being unsatisfactory for condition, abnormality code is returned to the present apparatus.Damping device 6 is logical
It crosses and is positioned between installing mechanism 2, the two closely connects, and reduces the shake of task device 7, achievees the effect that damping.
This task device protective device supports common aerial survey slr camera：Canon 5D- II, 5D- III, Sony D800, D810,
D850 flies to think iXU-R1000.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
With within principle, any modification, equivalent replacement, improvement and so on should all be included in the protection scope of the present invention god.
Claims (5)
1. a kind of aerial survey unmanned plane task device protective device, including device body, which is characterized in that described device ontology includes
Control system (1), installing mechanism (2), equipment protecting equipment (4), power plant (5) and damping device (6), and on device body
Equipped with external interface (3), external interface (3) the connection control system (1) is ordered and is performed for receiving；
The control system (1) is for judging whether height of the unmanned plane apart from ground meets condition, and send out order command；Institute
Control system (1) connecting power device (5) is stated, the power plant (5) drives and sets above equipment protecting equipment (4)
Standby protective device (4) is run, and the equipment protecting equipment (4) includes screw (41) and auxiliary rod (42), the screw (41) and
For auxiliary rod (42) set on task device (7) surrounding, screw (41) outer surface has a screw thread, and the task device (7) is along silk
Bar (41) external screw thread slides up and down, and the auxiliary rod (42) is for preventing task device (7) position from shifting；
Installing mechanism (2) one end damping device for connecting (6), other end connection task device (7), the damping device (6)
Above task device (7).
A kind of 2. aerial survey unmanned plane task device protective device according to claim 1, which is characterized in that the control system
System (1) judges that task device (7) meets the standard of condition for 30 meters apart from ground level.
A kind of 3. aerial survey unmanned plane task device protective device according to claim 1, which is characterized in that the power dress
(5) are put as motor, and its quantity is two, every portion is equipped with power cord, signal wire and communication line.
A kind of 4. aerial survey unmanned plane task device protective device according to claim 1, which is characterized in that the damping dress
(6) are put as rubber shock-absorbing ball.
5. according to a kind of aerial survey unmanned plane task device protective device of claim 1-4 any one of them, which is characterized in that institute
External interface (3) is stated as serial line interface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810042537.2A CN108248877A (en) | 2018-01-17 | 2018-01-17 | A kind of aerial survey unmanned plane task device protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810042537.2A CN108248877A (en) | 2018-01-17 | 2018-01-17 | A kind of aerial survey unmanned plane task device protective device |
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| Publication Number | Publication Date |
|---|---|
| CN108248877A true CN108248877A (en) | 2018-07-06 |
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ID=62741008
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810042537.2A Pending CN108248877A (en) | 2018-01-17 | 2018-01-17 | A kind of aerial survey unmanned plane task device protective device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111114808A (en) * | 2020-01-13 | 2020-05-08 | 西安深瞳智控技术有限公司 | Photoelectric pod retraction mechanism |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120025021A1 (en) * | 2010-07-16 | 2012-02-02 | James Jorgensen | Payload door and elevator system |
| CN205615730U (en) * | 2016-05-19 | 2016-10-05 | 四川建筑职业技术学院 | Unmanned aerial vehicle's receive and release cloud platform |
| CN205770191U (en) * | 2016-05-25 | 2016-12-07 | 浙江安迪信信息技术有限公司 | One is taken photo by plane unmanned plane |
| CN206520749U (en) * | 2017-02-13 | 2017-09-26 | 李昌邦 | One kind is taken photo by plane unmanned plane |
-
2018
- 2018-01-17 CN CN201810042537.2A patent/CN108248877A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120025021A1 (en) * | 2010-07-16 | 2012-02-02 | James Jorgensen | Payload door and elevator system |
| CN205615730U (en) * | 2016-05-19 | 2016-10-05 | 四川建筑职业技术学院 | Unmanned aerial vehicle's receive and release cloud platform |
| CN205770191U (en) * | 2016-05-25 | 2016-12-07 | 浙江安迪信信息技术有限公司 | One is taken photo by plane unmanned plane |
| CN206520749U (en) * | 2017-02-13 | 2017-09-26 | 李昌邦 | One kind is taken photo by plane unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111114808A (en) * | 2020-01-13 | 2020-05-08 | 西安深瞳智控技术有限公司 | Photoelectric pod retraction mechanism |
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| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20190418 Address after: 710000 Room IBCA-2103, Huixin, Bayi Road, Zhangba Street, Xi'an High-tech Zone, Shaanxi Province Applicant after: Nine-day Infinite Intelligent Technology Co., Ltd. Address before: 710000 Room IBCA-2102, Huixin, Zhangbayi Road, Xi'an High-tech Zone, Shaanxi Province Applicant before: Xi'an nine days limitless Intelligent Technology Co., Ltd. |
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180706 |