CN105460229B - A kind of aircraft antidetonation camera - Google Patents
A kind of aircraft antidetonation camera Download PDFInfo
- Publication number
- CN105460229B CN105460229B CN201510931764.7A CN201510931764A CN105460229B CN 105460229 B CN105460229 B CN 105460229B CN 201510931764 A CN201510931764 A CN 201510931764A CN 105460229 B CN105460229 B CN 105460229B
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- CN
- China
- Prior art keywords
- camera
- battery storage
- detection control
- shell
- microcontroller
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B17/00—Details of cameras or camera bodies; Accessories therefor
- G03B17/56—Accessories
- G03B17/561—Support related camera accessories
Abstract
The invention discloses a kind of aircraft antidetonation cameras,Including driving box,Universal shaft,Camera,Battery storage shell,Loud speaker and detection control shell,Battery storage shell upper end drives box by universal axis connection,Driving box is arranged in the bottom of mounting plate,Battery storage housing forward end is threadedly coupled detection control shell,Detection control housing forward end is threadedly coupled camera mounting cup,Battery storage housing rear end connects loud speaker,Camera mounting cup is circular configuration,Camera mounting cup circle centre position is equipped with camera,A kind of aircraft antidetonation camera,Realize the shooting or camera shooting of different angle,Flexibility is good,And can be dark under light environment under normal photographing,Play good cushioning effect,And alarm is sent out in time when shaking larger,Carry out early warning,Prevent the damage of camera,Stablizing effect is good,Shooting quality is high,It is easily installed and uses and repair.
Description
Technical field
The present invention relates to vehicle technology field, specifically a kind of aircraft antidetonation camera.
Background technology
It takes photo by plane also known as aerophotography or aeroplane photography, refers to obtaining vertical view from aerial photographing earth landforms, this figure is
Photo map.The video camera taken photo by plane can be controlled by photographer, can also be automatically snapped or remote control.Platform packet used in taking photo by plane
Include aircraft, helicopter, fire balloon, blimp, rocket, kite, parachute etc..In order to allow aerial photograph to stablize, need to use
Advanced photographic equipment, it utilizes three axis or five axis Gyroscopic stabilization functions, so that camera is stablized during taking photo by plane, provides high-quality
The stabilization picture of amount, in addition under long focal length lens it is also highly stable.Figure of taking photo by plane can clearly show ground object, therefore remove
As except photography art, it is also applied to military affairs, transport development, hydraulic engineering, ecological Studies, urban planning etc..
Currently, conventional aircraft aerial device often needs to lock the target of taking photo by plane in the visual field, different angle and range are realized
Target take photo by plane, need to adjust the different shooting angles for changing camera constantly, the usually indefinite installation of existing aerial device, no
Have the function of rotation adjustment, so that shooting angle is received limitation, and in the environment of dark, it is difficult to realize normal photographing.
Especially in aircraft motion process, camera is vulnerable to strong vibrations, influences the stability of camera, to influence to clap
Take the photograph the quality of picture.
Invention content
It is mentioned above in the background art to solve the purpose of the present invention is to provide a kind of aircraft antidetonation camera
Problem.
To achieve the above object, the present invention provides the following technical solutions：
A kind of aircraft antidetonation camera, including driving box, universal shaft, camera, battery storage shell, loud speaker and
Detection control shell, battery storage shell upper end drive box, driving box to be arranged at the bottom of mounting plate by universal axis connection
Portion, battery storage housing forward end are threadedly coupled detection control shell, and detection control housing forward end is threadedly coupled camera mounting cup,
Battery storage housing rear end connects loud speaker, and camera mounting cup is circular configuration, and camera mounting cup circle centre position, which is equipped with, to be taken the photograph
As head, multiple infrared lamps and photosensitive sensor, the camera, infrared lamp and light are equidistantly provided in camera circumferential direction
Dependent sensor is by conducting wire connecting wiring plate, and in detection control shell, wiring plate connects microcontroller for wiring plate setting,
Microcontroller rear end connects magnification circuit plate, and magnification circuit plate is fixed on by fixed pin on detection control shell, amplification electricity
Road plate connects alert receipt end by conducting wire, and alert receipt end is arranged on expelling plate, expelling plate connection loud speaker, on expelling plate
Equipped with alarm sound chip, shock sensor and power pin, power pin connects accumulator, and universal shaft is internally provided with buffering elastic
Spring, buffer spring both ends are arranged with spring bracket and lower spring bracket, and upper spring bracket is connect with upper connecting rod integral type, the top of upper connecting rod
Ball-joint is connected, universal shaft both ends are threaded with upper limit lid and lower limit lid, and driving cassette bottom portion is equipped with spherical groove, spherical
Ball-joint is arranged in groove, ball-joint both sides contradict respectively zigzag tread patterns wheel and laterally driven wheel, the connection of zigzag tread patterns wheel
Vertical drive motor, laterally driven wheel connect horizontal drive motor.
As a further solution of the present invention：It is pasted with rubber pad at the top of the mounting plate, the quadrangle of mounting plate is equipped with
Fastening bolt.
As a further solution of the present invention：The microcontroller is embedded in detection control shell, microcontroller
Outside is provided with rubber buffer ring.
As a further solution of the present invention：The accumulator connects microcontroller by conducting wire, on microcontroller
Equipped with memory.
As a further solution of the present invention：The lower spring bracket is connect with lower connecting rod integral type, and lower connecting rod is fixed on
On battery storage shell.
As a further solution of the present invention：The upper spring bracket and lower spring bracket be arranged universal shaft both ends upper limit lid and
In lower limit lid.
Compared with prior art, the beneficial effects of the invention are as follows：A kind of aircraft antidetonation camera, structure letter
Single, easy to use, by driving box to adjust shooting or camera shooting that universal shaft realizes different angle, flexibility is good, and can be under light
Normal photographing under dark environment plays good cushioning effect by rubber pad, rubber buffer ring and buffer spring, and is shaking
Alarm is sent out in time when dynamic larger, early warning is carried out, prevents the damage of camera, and stablizing effect is good, and shooting quality is high, is easily installed
It uses and repairs.
Description of the drawings
Fig. 1 is the structural diagram of the present invention.
Fig. 2 is the schematic cross-section of the present invention.
Fig. 3 is the structural schematic diagram of universal shaft in the present invention.
Fig. 4 is the structural schematic diagram that box is driven in the present invention.
In figure：1- rubber pads, 2- fastening bolts, 3- mounting plates, 4- drivings box, 5- universal shafts, 6- infrared lamps, 7- camera shootings
Head, 8- cameras mounting cup, 9- photosensitive sensors, 10- battery storages shell, 11- loud speakers, 12- wiring plates, 13- buffer rubber
Cushion rubber, 14- magnification circuit plates, 15- accumulators, 16- alarms sound chip, 17- shock sensors, 18- alert receipts end, 19- hairs
It penetrates plate, 20- power pins, 21- detection controls shell, 22- microcontrollers, 23- fixed pins, 24- ball-joints, connect on 25-
Spring bracket, 30- lower limits lid, 31- lower connecting rods, 32- balls under bar, 26- upper limits lid, the upper spring brackets of 27-, 28- buffer springs, 29-
Connected in star, 33- vertical drive motors, 34- zigzag tread patterns wheel, 35- horizontal drive motors, the laterally driven wheels of 36-.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig.1~4, in the embodiment of the present invention, a kind of aircraft antidetonation camera, including driving box 4, universal shaft
5, camera 7, battery storage shell 10, loud speaker 11 and detection control shell 21,10 upper end of battery storage shell passes through
The connection driving box 4 of universal shaft 5, driving box 4 are arranged in the bottom of mounting plate 3, and 3 top of mounting plate is pasted with rubber pad 1, mounting plate
3 quadrangle is equipped with fastening bolt 2, and mounting plate 3 is fixed on the bottom of aircraft, rubber by the fastening bolt 2 that quadrangle is arranged
There is pad 1 certain cushioning effect, 10 nose threads connecting detection of battery storage shell to control shell 21, detection control shell 21
Nose threads connect camera mounting cup 8, and 10 rear end of battery storage shell connects loud speaker 11.
The camera mounting cup 8 is circular configuration, and 8 circle centre position of camera mounting cup is equipped with camera 7, camera 7
Multiple infrared lamps 6 and photosensitive sensor 9, the camera 7, infrared lamp 6 and light sensor are equidistantly provided in circumferential direction
Device 9 is by conducting wire connecting wiring plate 12, and for the setting of wiring plate 12 in detection control shell 21, wiring plate 12 connects miniature control
Device 22, microcontroller 22 are embedded in detection control shell 21, and 22 outside of microcontroller is provided with rubber buffer ring 13, micro-
22 rear end of type controller connects magnification circuit plate 14, and magnification circuit plate 14 is fixed on detection control shell 21 by fixed pin 23
On, magnification circuit plate 14 connects alert receipt end 18 by conducting wire, and alert receipt end 18 is arranged on expelling plate 19, expelling plate 19
Loud speaker 11 is connected, expelling plate 19 is equipped with alarm sound chip 16, shock sensor 17 and power pin 20, and power pin 20 connects
Accumulator 15 is connect, accumulator 15 connects microcontroller 22 by conducting wire, and microcontroller 22 is equipped with memory, camera 7
By the video signal transmission of shooting to microcontroller 22, it is stored in memory after the processing of microcontroller 22, light sensor
External optical signals are transmitted to microcontroller 22 by device 9, and controlling to adjust infrared lamp 6 after the processing of microcontroller 22 illuminates, just
In aircraft under dark illumination condition normal photographing, when battery storage shell 10 receives significant shock, shock sensor 17
Vibration signal is transmitted to microcontroller 22, controlling loudspeaker 11 sends out alarm after the processing of microcontroller 22.
The universal shaft 5 is internally provided with buffer spring 28, and 28 both ends of buffer spring are arranged with spring bracket 27 and lower spring bracket 29,
Upper spring bracket 27 is connect with 25 integral type of upper connecting rod, and the top of upper connecting rod 25 connects ball-joint 24, lower spring bracket 29 and lower connection
31 integral type of bar connects, and lower connecting rod 31 is fixed on battery storage shell 10, and 5 both ends of universal shaft are threaded with upper limit lid
26 and lower limit lid 30, upper spring bracket 27 and lower spring bracket 29 be arranged in the upper limit lid 26 and lower limit lid 30 at 5 both ends of universal shaft,
In use, when upper connecting rod 25 is given a shock, the upper spring bracket 27 of 25 bottom of upper connecting rod connection squeezes buffer spring 28, buffering elastic
Spring 28 is flexible to slow down vibrating effect, so that the battery storage shell 10 that lower connecting rod 31 connects is mitigated vibrations, plays good damping
Effect.
4 bottom of driving box is equipped with spherical groove 32, and ball-joint 24,24 both sides of ball-joint are arranged in spherical groove 32
Contradicting respectively has zigzag tread patterns wheel 34 and laterally driven wheel 36, and zigzag tread patterns wheel 34 connects vertical drive motor 33, laterally driven
36 connection horizontal drive motor 35 of wheel drives ball-joint in use, by the rotation of zigzag tread patterns wheel 34 and laterally driven wheel 36
The rotation of 24 different directions, so as to adjust the direction of universal shaft 5 and camera 7.
The present invention operation principle be：A kind of aircraft antidetonation camera, it is simple in structure, it is easy to use, pass through
Drive box 4 adjust universal shaft 5 realize different angle shooting or camera shooting, flexibility is good, and can be dark under light environment under just
Often shooting plays good cushioning effect by rubber pad 1, rubber buffer ring 13 and buffer spring 28, and when shaking larger
Send out alarm in time, carry out early warning, prevent the damage of camera 7, stablizing effect is good, and shooting quality is high, be easily installed use and
Repair.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, Er Qie
In the case of without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Profit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent requirements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (6)
1. a kind of aircraft antidetonation camera, including driving box, universal shaft, camera, battery storage shell, loud speaker and inspection
Observing and controlling shell, which is characterized in that battery storage shell upper end drives box, driving box setting pacifying by universal axis connection
The bottom of loading board, battery storage housing forward end are threadedly coupled detection control shell, and detection control housing forward end is threadedly coupled camera shooting
Head mounting cup, battery storage housing rear end connect loud speaker, and camera mounting cup is circular configuration, camera mounting cup circle centre position
Camera is installed, is equidistantly provided with multiple infrared lamps and photosensitive sensor in camera circumferential direction, it is the camera, infrared
Line lamp and photosensitive sensor are by conducting wire connecting wiring plate, and in detection control shell, wiring plate connection is micro- for wiring plate setting
Type controller, microcontroller rear end connect magnification circuit plate, and magnification circuit plate is fixed on detection control shell by fixed pin
On, magnification circuit plate connects alert receipt end by conducting wire, and alert receipt end is arranged on expelling plate, and expelling plate connection is raised one's voice
Device, expelling plate are equipped with alarm sound chip, shock sensor and power pin, and power pin connects accumulator, inside universal shaft
Equipped with buffer spring, buffer spring both ends are arranged with spring bracket and lower spring bracket, and upper spring bracket is connect with upper connecting rod integral type, upper company
The top of extension bar connects ball-joint, and universal shaft both ends are threaded with upper limit lid and lower limit lid, and driving cassette bottom portion is equipped with ball
Connected in star, inside of spherical groove are arranged with ball-joint, and ball-joint both sides contradict respectively zigzag tread patterns wheel and laterally driven wheel, longitudinal
Driving wheel connects vertical drive motor, and laterally driven wheel connects horizontal drive motor.
2. a kind of aircraft antidetonation camera according to claim 1, which is characterized in that pasted at the top of the mounting plate
There are rubber pad, the quadrangle of mounting plate to be equipped with fastening bolt.
3. a kind of aircraft antidetonation camera according to claim 1, which is characterized in that the microcontroller is inlayed
In detection control shell, rubber buffer ring is provided on the outside of microcontroller.
4. a kind of aircraft antidetonation camera according to claim 1, which is characterized in that the accumulator passes through conducting wire
Microcontroller is connected, microcontroller is equipped with memory.
5. a kind of aircraft antidetonation camera according to claim 1, which is characterized in that the lower spring bracket and lower connection
Bar integral type connects, and lower connecting rod is fixed on battery storage shell.
6. a kind of aircraft antidetonation camera according to claim 1, which is characterized in that the upper spring bracket and lower spring bracket
It is arranged in the upper limit lid and lower limit lid at universal shaft both ends.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710284406.0A CN106965949B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
| CN201510931764.7A CN105460229B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
| CN201710284423.4A CN107089344B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510931764.7A CN105460229B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
Related Child Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710284423.4A Division CN107089344B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
| CN201710284406.0A Division CN106965949B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105460229A CN105460229A (en) | 2016-04-06 |
| CN105460229B true CN105460229B (en) | 2018-08-10 |
Family
ID=55598484
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710284423.4A Active CN107089344B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
| CN201710284406.0A Active CN106965949B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
| CN201510931764.7A Active CN105460229B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
Family Applications Before (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710284423.4A Active CN107089344B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
| CN201710284406.0A Active CN106965949B (en) | 2015-12-10 | 2015-12-10 | A kind of aircraft antidetonation camera |
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| Country | Link |
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| CN (3) | CN107089344B (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106364671B (en) * | 2016-10-12 | 2019-01-25 | 江苏锦程航空科技有限公司 | A kind of unmanned minute vehicle |
| US10321029B2 (en) * | 2017-05-01 | 2019-06-11 | Logitech Europe S.A. | Modular coupling for a video camera system |
| US10048570B1 (en) * | 2017-05-01 | 2018-08-14 | Logitech Europe S.A. | Adjustable modular attachment for a video camera system |
| CN109298269A (en) * | 2018-11-16 | 2019-02-01 | 中铁局集团有限公司 | A kind of sliding detection device of urban track traffic heat |
| CN109729247B (en) * | 2018-11-30 | 2021-01-01 | 北京中科时空信息技术有限公司 | Video pixel control array camera device |
| CN112161656B (en) * | 2020-09-30 | 2022-09-06 | 深圳市宝信欣旺科技有限公司 | Optical detection system and detection method for circular PCB |
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- 2015-12-10 CN CN201710284423.4A patent/CN107089344B/en active Active
- 2015-12-10 CN CN201710284406.0A patent/CN106965949B/en active Active
- 2015-12-10 CN CN201510931764.7A patent/CN105460229B/en active Active
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| CN101923213A (en) * | 2010-07-13 | 2010-12-22 | 山东神戎电子股份有限公司 | Laser high-speed spherical night-vision device |
| CN202392373U (en) * | 2011-09-09 | 2012-08-22 | 深圳市大疆创新科技有限公司 | Gyroscopic dynamic self-balancing pan/tilt/zoom (PTZ) |
| CN202349521U (en) * | 2011-12-13 | 2012-07-25 | 河南科技大学 | Pod |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107089344A (en) | 2017-08-25 |
| CN107089344B (en) | 2019-10-11 |
| CN105460229A (en) | 2016-04-06 |
| CN106965949B (en) | 2019-04-19 |
| CN106965949A (en) | 2017-07-21 |
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Effective date of registration: 20180612 Address after: 100000 West Chang'an Avenue, Xicheng District, Xicheng District, Beijing Applicant after: State Grid Corporation of China Applicant after: SHIYAN POWER SUPPLY COMPANY OF STATE GRID HUBEI ELECTRIC POWER COMPANY Address before: 236600 Liu Yang village, Nan Yang village, Miao Lao Town, Taihe County, Fuyang, Anhui Applicant before: Liu Cao |
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