CN205396570U - Aerial survey unmanned aerial vehicle's camera installation device - Google Patents
Aerial survey unmanned aerial vehicle's camera installation device Download PDFInfo
- Publication number
- CN205396570U CN205396570U CN201620188623.0U CN201620188623U CN205396570U CN 205396570 U CN205396570 U CN 205396570U CN 201620188623 U CN201620188623 U CN 201620188623U CN 205396570 U CN205396570 U CN 205396570U
- Authority
- CN
- China
- Prior art keywords
- camera
- housing
- unmanned plane
- chamber
- erecting device
- Prior art date
- 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.)
- Expired - Fee Related
Links
Landscapes
- Lens Barrels (AREA)
Abstract
The utility model discloses an aerial survey unmanned aerial vehicle's camera installation device, include: the casing, including first cavity and second cavity, first cavity and second cavity are kept apart by the baffle, first cavity holding camera main part, the camera camera lens passes the baffle and stretches into the second cavity, damping ring, it sets up between baffle and camera main part for camera rocking in the casing alleviate, and lens cap, its and second cavity front end swivelling joint for protection camera camera lens, wherein, the casing is connected with the unmanned aerial vehicle organism. The utility model discloses a be equipped with the convenient lens cap who dismantles on the camera installation device, under the condition of protective glass dust fall or wearing and tearing, change protective glass that can be simple, convenient, and set up damping ring between installation device and the camera, the damping ring design is small and exquisite reliable, solves the unmanned aerial vehicle vibration and the fuzzy problem of shooting that arouses.
Description
Technical field
This utility model relates to unmanned plane aerial camera field.More specifically, this utility model relates to the camera erecting device of a kind of aerial survey unmanned plane.
Background technology
Unmanned plane is to carry out, by radio robot or airborne computer stored program controlled, the not manned vehicle that manipulates.Unmanned plane simple in construction, use cost are low, not only can complete the task that manned aircraft performs, be more suitable for the task that people's aircraft should not perform, be used for now fields such as taking photo by plane.Unmanned plane photography of taking photo by plane is using UAV as aerial platform, with airborne sensory equipment, such as high resolution CCD digital camera, light optical camera, infrared scanner, laser scanner, magnetic determining device etc. obtain information, with computer, image information is processed, and be fabricated to image according to certain required precision.
Use unmanned plane to carry out zonule remote sensing to take photo by plane technology, achieve significant results and experience in practice.The miniature aerial remote sens ing technique being aerial remote sensing platform with unmanned plane, adapts to national economy and the needs of cultural construction development, provides the effective remote sensing technology means of services for the regional economy such as particularly city, small and medium-sized cities, town, county, township and cultural construction.China's expanding economy is had important facilitation by remote sensing technology of taking photo by plane.Unmanned plane takes photo by plane that camera work can be widely applied to country's ecological environmental protection, mineral resources exploration, marine environmental monitoring, land use survey, water resources development, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration, forest disease and pest protects and the field such as monitoring, public safety, Defence business, digital earth and advertisement photography, has the wide market demand.The advantage that unmanned plane aerial images has high-resolution, large scale, little area, high Up-to-date state.It is particularly suitable for obtaining banding area aerial images (highway, railway, river, reservoir, coastline etc.).And UAV provides easy to operate for photography of taking photo by plane, it is easy to the remote sensing platform of transition.Landing of taking off is limited less by place, on playground, highway or other openr ground all can landings, its stability, safety are good, transitions etc. are very easy to, small portable, low-noise energy-saving, efficiently motor-driven, image definition, lightness, miniaturization, the intelligent outstanding feature that unmanned plane is taken photo by plane especially.
Unmanned aerial vehicle remote sensing take photo by plane use photography, apparatus for making a video recording is mainly through the photographing unit of repacking, shooting black and white, colored negative film and reversal film.It is used as small digital camera or video wireless transmission technology carries out colored production.On SUAV, the camera for taking pictures typically directly is arranged on fuselage or is placed in fuselage by damping cotton.But there is problems in that 1, fixing not in place, in-flight easily caused by vibrations, it is impossible to ensure and aircraft abswolute level;2, not having epi mirror to protect, when forward lands, camera is easily contaminated.
Utility model content
A purpose of the present utility model is to solve at least the above and defect, and provides the advantage that at least will be described later.
This utility model is it is also an object that a kind of camera erecting device of design, and the protective glass of its front end can protect the camera lens of camera, and makes the protective glass can rapidly, change easily when dust fall or destruction.
This utility model it is also an object that arrange damping ring between camera and erecting device, and damping ring design is small and exquisite reliably, the problem solving unmanned plane vibration.
In order to realize these purposes according to the present invention and further advantage, it is provided that the camera erecting device of a kind of aerial survey unmanned plane, including:
Housing, including the first chamber and the second chamber, described first chamber and the second chamber are isolated by baffle plate, and described first chamber houses camera main-body, and camera lens stretches into described second chamber through baffle plate;
Damping ring, it is arranged between baffle plate and camera main-body, for alleviating camera rocking in housing;And
Lens cap, it is rotatably connected with the second chamber front end, is used for protecting camera lens;
Wherein, described housing is connected with unmanned plane body.
Preferably, described protective glass is bonding integral by glue with lens cap.
Preferably, also include:
Fastening screw, it is arranged on camera main-body side;
Through hole, it is arranged on housing the position of corresponding fixing threaded hole;
Trip bolt, it is through through hole precession fastening screw, and described trip bolt connects housing and camera for fixing.
Preferably, described damping ring is polystyrene material vibration-dampening bubble.
Preferably, described damping ring is shock-absorbing spring structure.
Preferably, described housing includes:
First housing, is the first chamber inside it;
Second housing, inside is the second chamber;
Wherein, the external diameter of the second housing is little compared with the external diameter of the first housing, connection lens lid after the fixing hole of the second housing traverse unmanned plane body.
Preferably, described first housing is outs open structure, and described outs open structure is used for putting into camera main-body and limiting positioning camera.
This utility model at least includes following beneficial effect: 1, be connected with camera main-body by the second housing, and is positioned at by camera main-body between the first housing and lens cap, makes camera erecting device be connected with unmanned plane more solid and reliable.2, camera erecting device is internally formed the cavity of closing, effectively prevents camera and camera lens to be subject to the pollution of ground dust when landing.3, arranging damping ring between camera and erecting device, damping ring design is small and exquisite reliably, the problem solving unmanned plane vibration.4, protective glass is dismountable with lens cap is connected, and when protective glass dust fall or abrasion, can change protective glass simply and easily.
Part is embodied by further advantage of the present utility model, target and feature by description below, and part also will by being understood by those skilled in the art research of the present utility model and practice.
Accompanying drawing explanation
Fig. 1 is unmanned plane camera erecting device structure chart.
Fig. 2 is camera erecting device and unmanned plane and camera mounting structure figure.
Detailed description of the invention
Below in conjunction with accompanying drawing, this utility model is described in further detail, to make those skilled in the art can implement according to this with reference to description word.
Should be appreciated that used herein such as " have ", existence or the interpolation of other elements one or more or its combination do not allotted in " comprising " and " including " term.
As illustrated in fig. 1 and 2, camera erecting device 100 of the present utility model includes: housing 110, lens cap 120 and trip bolt 130.
As seen from Figure 1, housing 110 includes first housing the 111, second housing 112, baffle plate 113, damping ring 114 and through hole 115.Described housing 110 is metal material or plastic material, and its light quality is carried in unmanned plane.First housing 111 is the outs open structure of cylinder or cuboid, it it is the first chamber in it, described first chamber is identical with camera main-body 210 shape, for housing camera main-body 210, the outs open structure of described first housing 111 is easy to camera 200 and is put into camera erecting device, for preventing camera from departing from erecting device after camera 200 is put into;Wherein, the position of the fastening screw of the corresponding camera 200 of described first housing 111 offers through hole 115, and described through hole 115 is for fixing housing 110 and camera 200 further;Second housing 112 is cylindrical structure, it it is the second chamber in it, described second chamber is identical with camera lens 220 shape, for housing camera lens 220, wherein, described second housing 112 is away from the inner circle sidewall laying screwed hole of baffle plate 113, and the screwed hole of described screwed hole and lens cap 120 matches;Further, the external diameter of described second housing 112 is little compared with the external diameter of the first housing 111, makes the first housing 111 and the second housing 112 junction form top fastening station structure.Described first chamber and the second chamber are cut off by baffle plate 113, and described baffle plate 113 is offered central through hole, and described central through hole size and camera lens 220 match, and described camera lens 220 enters the second chamber after baffle plate 113.Damping ring 114 is the cirque structure with damping effect, in it, ring size matches with the size of camera lens 220, camera lens 220 is after damping ring 114, damping ring 114 above and below is against on camera main-body 210 and baffle plate 113 respectively, for alleviating the camera main-body 210 vibration in camera erecting device.
In another embodiment, described damping ring 114 is polystyrene material vibration-dampening bubble, can not only alleviate the weight of erecting device and have good effectiveness in vibration suppression, reduces in the process of taking photo by plane owing to vibration causes image blurring as far as possible.
In another embodiment, described damping ring 114 is shock-absorbing spring structure, and described shock-absorbing spring is light-weight metal material, alleviates the relative movement between camera erecting device 100 and camera 200, it is to avoid the relative movement impact on taking photo by plane.
Lens cap 120 is the circular screw cap structure with central through hole, and its lid external diameter is big compared with the external diameter of the second housing 112, makes lens cap 120 and the second housing 112 junction form low fastening station structure;Being provided with annulus boss inside lid, the external diameter of described annulus boss and the internal diameter of the second housing 112 match, and further, the excircle of described annulus boss is provided with screwed hole, for second housing 112 that is rotatably connected by the annulus boss of lens cap 120;The central through hole that protective glass 121 is the circular eyeglass that light transmission is good, anti-wear-resisting, its external diameter and lens cap 120 matches, and is connected on lens cap 120 by protective glass 121 with glue, it is simple to the advantage installing, change and having good airproof performance;Protective glass 121 is provided with knob buckle 122 near the side of camera lens 220, is used for the camera lens 220 that is rotatably connected.
Trip bolt 130 is metal material screw, described camera main-body 210 offers the fastening screw for installing spider, when erecting device put into by camera 200, described through hole 115 is corresponding with fastening screw hole site, precession fastening screw after trip bolt 130 traverse through hole 115, is connected fixing with camera 200 for camera erecting device 100.
Unmanned plane 300 is provided with fixing hole for fixed camera erecting device 100, and the external diameter of described fixing hole diameter and the second housing matches, and the height of fixing hole and the height of the second housing 112 are identical;Second housing 112 is carried out limiting and positioning unmanned plane 300 by top fastening station structure after described fixing hole, and after lens cap 120 connects the second housing 112, low fastening station structure carries out limiting and position unmanned plane 300.
The installation process of camera erecting device 100 refers to Fig. 1 and Fig. 2, camera 200 is put into by the outs open structure of the first housing the first chamber of housing 110, camera lens 220 sequentially passes through damping ring 114 and baffle plate 113 enters the second chamber, now, camera main-body about 210 both ends of the surface are against on outs open structure and damping ring 114, play vibration damping and fixing effect, again by precession fastening screw after trip bolt 130 traverse through hole 115, it is connected fixing with camera 200 for camera erecting device 100 further.Now, by the second housing 112 through fixing hole in unmanned plane 300 main body, top fastening station structure carry out above spacing unmanned plane 300, then lens cap 120 is threaded into housing 110, low fastening station structure carry out below spacing unmanned plane 300;Meanwhile, the knob buckle 122 clamping camera lens 220 on protective glass 121, plays the effect of protection camera lens.Abrasion or dust fall occur when protective glass 121, after lens cap 120 is screwed out housing 110, is replaced protective glass 121.
Although embodiment of the present utility model is disclosed as above, but it is not restricted in description and embodiment listed utilization.It can be applied to various applicable field of the present utility model completely.For those skilled in the art, it is easily achieved other amendment.Therefore, under the general concept limited without departing substantially from claim and equivalency range, this utility model is not limited to specific details and shown here as the legend with description.
Claims (7)
1. the camera erecting device of an aerial survey unmanned plane, it is characterised in that including:
Housing, including the first chamber and the second chamber, described first chamber and the second chamber are isolated by baffle plate, and described first chamber houses camera main-body, and camera lens stretches into described second chamber through baffle plate;
Damping ring, it is arranged between baffle plate and camera main-body, for alleviating camera rocking in housing;And
Lens cap, it is rotatably connected with the second chamber front end, is used for protecting camera lens;
Wherein, described housing is connected with unmanned plane body.
2. the camera erecting device of aerial survey unmanned plane as claimed in claim 1, it is characterised in that described protective glass is bonding integral by glue with lens cap.
3. the camera erecting device of aerial survey unmanned plane as claimed in claim 2, it is characterised in that also include:
Fastening screw, it is arranged on camera main-body side;
Through hole, it is arranged on housing the position of corresponding fixing threaded hole;
Trip bolt, it is through through hole precession fastening screw, and described trip bolt connects housing and camera for fixing.
4. the camera erecting device of aerial survey unmanned plane as claimed in claim 3, it is characterised in that described damping ring is polystyrene material vibration-dampening bubble.
5. the camera erecting device of aerial survey unmanned plane as claimed in claim 3, it is characterised in that described damping ring is shock-absorbing spring structure.
6. the camera erecting device of the aerial survey unmanned plane as described in claim 4 or 5, it is characterised in that described housing includes:
First housing, is the first chamber inside it;
Second housing, inside is the second chamber;
Wherein, the external diameter of the second housing is little compared with the external diameter of the first housing, connection lens lid after the fixing hole of the second housing traverse unmanned plane body.
7. the camera erecting device of aerial survey unmanned plane as claimed in claim 6, it is characterised in that described first housing is outs open structure, and described outs open structure is used for putting into camera main-body and limiting positioning camera.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620188623.0U CN205396570U (en) | 2016-03-11 | 2016-03-11 | Aerial survey unmanned aerial vehicle's camera installation device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620188623.0U CN205396570U (en) | 2016-03-11 | 2016-03-11 | Aerial survey unmanned aerial vehicle's camera installation device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205396570U true CN205396570U (en) | 2016-07-27 |
Family
ID=56440290
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201620188623.0U Expired - Fee Related CN205396570U (en) | 2016-03-11 | 2016-03-11 | Aerial survey unmanned aerial vehicle's camera installation device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205396570U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106167102A (en) * | 2016-08-31 | 2016-11-30 | 河南翱翔航空科技有限公司 | Aerial camera shock bracket |
-
2016
- 2016-03-11 CN CN201620188623.0U patent/CN205396570U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106167102A (en) * | 2016-08-31 | 2016-11-30 | 河南翱翔航空科技有限公司 | Aerial camera shock bracket |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11563932B2 (en) | Estimating real-time delay of a video data stream | |
CN204527625U (en) | Multifunctional individual unmanned plane | |
CN105700547B (en) | A kind of aerial three-dimensional video-frequency streetscape system and implementation method based on navigation dirigible | |
US10710707B2 (en) | Unmanned aerial vehicle | |
CN206704529U (en) | A kind of camera oblique photograph unmanned plane of four rotor five | |
CN103438869A (en) | Aerial dynamic large-scale vegetation coverage acquisition system | |
Renwick et al. | Drone-based reconstruction for 3D geospatial data processing | |
CN205396570U (en) | Aerial survey unmanned aerial vehicle's camera installation device | |
CN206544595U (en) | A kind of crash structure of fire-fighting unmanned plane | |
CN110390722A (en) | A kind of Millisecond draws the method and system of real-time live-action map | |
KR102104003B1 (en) | System for constructing spatial data big data platform using sensorless data acquisition and mission equipment | |
CN215639428U (en) | Semi-permanent image control point device based on unmanned aerial vehicle remote sensing monitoring landslide hazard | |
CN109345830A (en) | A kind of intelligent transportation managing and control system based on unmanned plane | |
CN206301209U (en) | A kind of crop straw burning monitoring device based on unmanned plane | |
CN109211911A (en) | Water body environment monitoring method | |
CN103855641B (en) | A kind of Multifunctional power transmission line inspection device | |
CN203385417U (en) | Large-scale aviation dynamic acquisition system for vegetation coverage | |
Salmon et al. | Mobile Bot Swarms: They're closer than you might think! | |
CN205378126U (en) | Spring imager based on cloud computing environment | |
CN110390721A (en) | It is a kind of to be uniformly distributed the method and system for drawing real-time live-action map | |
Zhao et al. | Research on UAV aided earthquake emergency system | |
CN213502905U (en) | Unmanned aerial vehicle who possesses search for and rescue function | |
ES2357743A1 (en) | Platform for the taking of aerial images. (Machine-translation by Google Translate, not legally binding) | |
CN205071162U (en) | Unmanned aerial vehicle image gathering module | |
MUDURA et al. | Calculate the volume of landfill cristeşti, mureş using the classical method and digital terrain model using pictures from UAV |
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: 20160727 Termination date: 20170311 |
|
CF01 | Termination of patent right due to non-payment of annual fee |