CN203486130U - Camera cabin at bottom of unmanned aerial vehicle - Google Patents
Camera cabin at bottom of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN203486130U CN203486130U CN201320634726.1U CN201320634726U CN203486130U CN 203486130 U CN203486130 U CN 203486130U CN 201320634726 U CN201320634726 U CN 201320634726U CN 203486130 U CN203486130 U CN 203486130U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- cabin
- fuselage
- phase cabin
- plane machine
- 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
Images
Abstract
The utility model relates to an unmanned aerial vehicle assembly, and particularly relates to a camera cabin at the bottom of an unmanned aerial vehicle. The unmanned aerial vehicle structurally comprises a fuselage, wherein flanks are respectively arranged at two sides of the middle of the fuselage, tail flanks are respectively arranged at two sides of the tail of the fuselage, an empennage is arranged above the tail of the fuselage, a cabin cover is arranged on the lower surface of the middle part of the fuselage, the camera cabin is arranged in the cabin cover, and a fixed rod for installing a holder is arranged in the camera cabin and has a vertically telescopic structure. According to the camera cabin at the bottom of the unmanned aerial vehicle, the fixed rod is arranged at the bottom of the middle of the fuselage and is used for installing the holder and connecting a camera; as the installation position is in the middle of the fuselage, the balance weight of the front and the rear of the fuselage is not affected even if the camera is installed on the fuselage, the flying stability of the unmanned aerial vehicle is not affected, and the safety is improved.
Description
Technical field
The utility model relates to a kind of unmanned plane assembly, phase cabin at the bottom of especially a kind of unmanned plane machine.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft that utilizes radio robot and the process controller of providing for oneself to handle.On machine, without driving compartment, but the equipment such as autopilot, process controller are installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, to its follow the tracks of, location, remote control, remote measurement and digital communication.Can under radio telecommand, as conventional airplane, take off or launch with booster rocket, also can take aerial input to by machine tool and fly.During recovery, the available mode automatic Landing the same with conventional airplane landing mission, also can reclaim with parachute or block by remote control.
An important purposes of existing unmanned plane is taken photo by plane exactly, a support is generally set on unmanned plane head The Cloud Terrace is installed, camera is installed on The Cloud Terrace, and due to general Design and manufacture unmanned plane of unmanned plane maker, The Cloud Terrace is installed under user's requirement again, because aircraft has carried out front and back counterbalance design to keep the steady of aircraft operation when designing, after install support and The Cloud Terrace additional and the front and back counterweight ratio that phase chance is destroyed aircraft be installed, reduce aircraft traveling comfort, have potential safety hazard.
Summary of the invention
The utility model provides a kind of and can take photo by plane, and can keep again phase cabin at the bottom of fuselage pulsation-free unmanned plane machine.
To achieve these goals, the utility model adopts following technical scheme:
Comprise a fuselage, described waist both sides are provided with flank, afterbody both sides are provided with tail flank, afterbody top is provided with empennage, its improvement is: described waist lower surface is provided with a Cang Gai, in the lid of storehouse, be provided with a phase cabin, in described phase cabin, one for installing the fixed link of The Cloud Terrace, and fixed link is vertical telescopic structure.
Preferably, described Cang Gai is to opening structure.
Preferably, described Cang Gai is slab construction.
Preferably, described bottom of fixed is provided with a The Cloud Terrace adapter plate.
Preferably, described The Cloud Terrace adapter plate is perpendicular to fixed link.
Preferably, described The Cloud Terrace adapter plate is rectangle or square.
Preferably, described fixed link is multi-joint telescoping structure.
Preferably, described storehouse covers and is provided with many drive spindles.
Preferably, described drive spindle is connected in the edge of Cang Gai.
Preferably, described drive spindle is hydraulic stem.
Owing to having adopted said structure, at the bottom of unmanned plane machine of the present utility model, the bottom position of phase cabin in the middle of fuselage arranges one the fixed link that The Cloud Terrace can be installed is installed, be used for installing The Cloud Terrace, connect camera, because its installation position is at waist, so installation camera can not destroy the counterweight ratio before and after fuselage later yet, do not affect the stability of unmanned plane during flying, improved safety.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model embodiment.
The specific embodiment
As shown in Figure 1, at the bottom of the unmanned plane machine of the present embodiment, phase cabin comprises a fuselage 1, described fuselage 1 both sides, middle part are provided with flank 2, fuselage 1 two sides of tail is provided with tail flank 3, fuselage 1 afterbody top is provided with empennage 4, and described fuselage 1 middle part lower surface is provided with a storehouse lid 5, in storehouse lid 5, is provided with a phase cabin, in described phase cabin, one for installing the fixed link 6 of The Cloud Terrace, and fixed link 6 is vertical telescopic structure.
In order to keep having a smooth flight, in the present embodiment, described storehouse lid 5 is to opening structure.
In the present embodiment, described storehouse lid 5 is slab construction.
For the ease of parts connection, in the present embodiment, described fixed link 6 bottoms are provided with a The Cloud Terrace adapter plate 7.
In the present embodiment, described The Cloud Terrace adapter plate 7 is perpendicular to fixed link.
In the present embodiment, described The Cloud Terrace adapter plate 7 is rectangle or square.
In order to save the space in fuselage 1, in the present embodiment, described fixed link 6 is multi-joint telescoping structure.
In the present embodiment, described storehouse lid 5 is provided with many drive spindles 8.
In the present embodiment, described drive spindle 8 is connected in the edge of Cang Gai.
In the present embodiment, described drive spindle 8 is hydraulic stem.
The foregoing is only preferred embodiment of the present utility model; not thereby limit the scope of the claims of the present utility model; every equivalent structure or conversion of equivalent flow process that utilizes the utility model specification sheets and accompanying drawing content to do; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (10)
1. phase cabin at the bottom of unmanned plane machine, comprise a fuselage, described waist both sides are provided with flank, afterbody both sides are provided with tail flank, afterbody top is provided with empennage, it is characterized in that: described waist lower surface is provided with a Cang Gai, and Cang Gaizhong is provided with a phase cabin, in described phase cabin, one for installing the fixed link of The Cloud Terrace, and fixed link is vertical telescopic structure.
2. phase cabin at the bottom of unmanned plane machine as claimed in claim 1, is characterized in that: described Cang Gai is to opening structure.
3. phase cabin at the bottom of unmanned plane machine as claimed in claim 2, is characterized in that: described Cang Gai is slab construction.
4. phase cabin at the bottom of unmanned plane machine as claimed in claim 3, is characterized in that: described bottom of fixed is provided with a The Cloud Terrace adapter plate.
5. phase cabin at the bottom of unmanned plane machine as claimed in claim 4, is characterized in that: described The Cloud Terrace adapter plate is perpendicular to fixed link.
6. phase cabin at the bottom of unmanned plane machine as claimed in claim 5, is characterized in that: described The Cloud Terrace adapter plate is rectangle or square.
7. phase cabin at the bottom of unmanned plane machine as claimed in claim 6, is characterized in that: described fixed link is multi-joint telescoping structure.
8. phase cabin at the bottom of unmanned plane machine as claimed in claim 7, is characterized in that: described storehouse covers and is provided with many drive spindles.
9. phase cabin at the bottom of unmanned plane machine as claimed in claim 8, is characterized in that: described drive spindle is connected in the edge of Cang Gai.
10. phase cabin at the bottom of unmanned plane machine as claimed in claim 9, is characterized in that: described drive spindle is hydraulic stem.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320634726.1U CN203486130U (en) | 2013-10-15 | 2013-10-15 | Camera cabin at bottom of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320634726.1U CN203486130U (en) | 2013-10-15 | 2013-10-15 | Camera cabin at bottom of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203486130U true CN203486130U (en) | 2014-03-19 |
Family
ID=50256976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320634726.1U Expired - Fee Related CN203486130U (en) | 2013-10-15 | 2013-10-15 | Camera cabin at bottom of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203486130U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103523197A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Unmanned aerial vehicle bottom camera cabin |
| CN106005454A (en) * | 2016-06-23 | 2016-10-12 | 杨珊珊 | Audio acquisition system and audio collecting method for UAV (unmanned aerial vehicle) |
| CN107499526A (en) * | 2017-07-19 | 2017-12-22 | 深圳市雷凌广通技术研发有限公司 | A kind of unmanned plane of taking photo by plane of 360 degree of pan-shots for mountain area |
-
2013
- 2013-10-15 CN CN201320634726.1U patent/CN203486130U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103523197A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Unmanned aerial vehicle bottom camera cabin |
| CN106005454A (en) * | 2016-06-23 | 2016-10-12 | 杨珊珊 | Audio acquisition system and audio collecting method for UAV (unmanned aerial vehicle) |
| CN107499526A (en) * | 2017-07-19 | 2017-12-22 | 深圳市雷凌广通技术研发有限公司 | A kind of unmanned plane of taking photo by plane of 360 degree of pan-shots for mountain area |
| CN107499526B (en) * | 2017-07-19 | 2020-04-10 | 王政 | A unmanned aerial vehicle that takes photo by plane for 360 degrees panorama shooting in mountain area |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102806990B (en) | Portable type mapping unmanned plane | |
| CN105966612B (en) | Become posture VTOL unmanned plane | |
| CN205293106U (en) | Novel unmanned aerial vehicle nacelle mounting structure | |
| CN103523197A (en) | Unmanned aerial vehicle bottom camera cabin | |
| CN203486130U (en) | Camera cabin at bottom of unmanned aerial vehicle | |
| CN205221105U (en) | Solar energy VTOL fixed wing uavs | |
| WO2018148248A1 (en) | Uav booster aircraft for takeoff and climb assist | |
| CN202935570U (en) | Portable mapping unmanned aerial plane | |
| CN204916155U (en) | Multipurpose unmanned aerial vehicle | |
| CN203497168U (en) | Front camera bin of unmanned plane | |
| CN205293058U (en) | Conveniently carry on fixed wing uavs of jumbo size loading device | |
| CN204937485U (en) | Unmanned aerial vehicle round trip flight control switching system | |
| CN203465855U (en) | Obstacle alarm system for unmanned plane | |
| CN103523203A (en) | Front camera cabin of unmanned aerial vehicle | |
| CN203497173U (en) | Single-interceptor tail wing of unmanned plane | |
| CN206031796U (en) | Unmanned aerial vehicle's parachute structure | |
| CN106965934A (en) | The landing modes and device of a kind of aircraft | |
| CN205971889U (en) | Automatic structure of continuing a journey of unmanned aerial vehicle | |
| CN106828914A (en) | A kind of modularization VTOL fixed-wing unmanned vehicle based on culvert type force vector component | |
| CN106915464A (en) | The landing-gear and mode of a kind of aircraft | |
| CN107150806A (en) | It is a kind of can VTOL fixed-wing unmanned plane | |
| CN103803056A (en) | Interceptor arranged on top of fuselage of unmanned aerial vehicle (UAV) | |
| CN105129104A (en) | Camera bracket and fixed-wing unmanned aerial vehicle | |
| CN203497172U (en) | Multi-interceptor tail wing of unmanned plane | |
| CN203497169U (en) | Plane-body-top interceptor of unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140319 Termination date: 20141015 |
|
| EXPY | Termination of patent right or utility model |