CN103523197A - Unmanned aerial vehicle bottom camera cabin - Google Patents
Unmanned aerial vehicle bottom camera cabin Download PDFInfo
- Publication number
- CN103523197A CN103523197A CN201310480641.7A CN201310480641A CN103523197A CN 103523197 A CN103523197 A CN 103523197A CN 201310480641 A CN201310480641 A CN 201310480641A CN 103523197 A CN103523197 A CN 103523197A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- cabin
- phase cabin
- plane machine
- plane body
- 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.)
- Pending
Links
Images
Abstract
The invention relates to an unmanned aerial vehicle component, and in particular relates to an unmanned aerial vehicle bottom camera cabin which structurally comprises a plane body, wherein side wings are arranged on two sides of the middle part of the plane body; side empennages are arranged on two sides of the tail part of the plane body; an empennage is arranged above the tail part of the plane body; a cabin cover is arranged on the lower surface of the middle part of the plane body; a camera cabin is arranged inside the cabin cover; a fixing rod for mounting a holder is arranged inside the camera cabin; and the fixing rod is of a vertical telescopic structure. According to the unmanned aerial vehicle component, the fixing rod for mounting the holder is arranged in the bottom of the middle part of the plane body, the fixing rod is used for mounting the holder and connecting a camera, as the mounting position is at the middle part of the plane body, the counter weight ratio of the front and back parts of the plane body is not affected after the camera is mounted, the stability of an unmanned aerial vehicle in flying is not affected, and the security is improved.
Description
Technical field
The present invention 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 invention provides a kind of can taking photo by plane, can keep again phase cabin at the bottom of fuselage pulsation-free unmanned plane machine.
To achieve these goals, the present invention 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 invention, 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 embodiment of the present invention.
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 the preferred embodiments of the present invention; not thereby limit the scope of the claims of the present invention; every equivalent structure or conversion of equivalent flow process that utilizes specification sheets of the present invention 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 invention.
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 |
|---|---|---|---|
| CN201310480641.7A CN103523197A (en) | 2013-10-15 | 2013-10-15 | Unmanned aerial vehicle bottom camera cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310480641.7A CN103523197A (en) | 2013-10-15 | 2013-10-15 | Unmanned aerial vehicle bottom camera cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103523197A true CN103523197A (en) | 2014-01-22 |
Family
ID=49925650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310480641.7A Pending CN103523197A (en) | 2013-10-15 | 2013-10-15 | Unmanned aerial vehicle bottom camera cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103523197A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103818544A (en) * | 2014-01-24 | 2014-05-28 | 深圳一电科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle body and manufacturing method thereof |
| CN104015916A (en) * | 2014-06-13 | 2014-09-03 | 韩世宇 | Unmanned plane |
| CN106029502A (en) * | 2015-04-24 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| CN106904287A (en) * | 2017-03-21 | 2017-06-30 | 四川智航慧飞无人机科技有限公司 | Take photo by plane the protection structure of unmanned plane camera |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101832771A (en) * | 2010-05-13 | 2010-09-15 | 北京航景创新科技有限公司 | Small-size and high-speed positioning cradle head for aerial survey of unmanned aerial vehicle |
| CN102806990A (en) * | 2012-07-27 | 2012-12-05 | 沈阳航天新光集团有限公司 | Portable mapping unmanned aerial plane |
| CN102923308A (en) * | 2012-08-06 | 2013-02-13 | 吴云东 | Hybrid electric power pilotless remote-sensing airplane |
| CN203486130U (en) * | 2013-10-15 | 2014-03-19 | 江苏艾锐泰克无人飞行器科技有限公司 | Camera cabin at bottom of unmanned aerial vehicle |
-
2013
- 2013-10-15 CN CN201310480641.7A patent/CN103523197A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101832771A (en) * | 2010-05-13 | 2010-09-15 | 北京航景创新科技有限公司 | Small-size and high-speed positioning cradle head for aerial survey of unmanned aerial vehicle |
| CN102806990A (en) * | 2012-07-27 | 2012-12-05 | 沈阳航天新光集团有限公司 | Portable mapping unmanned aerial plane |
| CN102923308A (en) * | 2012-08-06 | 2013-02-13 | 吴云东 | Hybrid electric power pilotless remote-sensing airplane |
| CN203486130U (en) * | 2013-10-15 | 2014-03-19 | 江苏艾锐泰克无人飞行器科技有限公司 | Camera cabin at bottom of unmanned aerial vehicle |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103818544A (en) * | 2014-01-24 | 2014-05-28 | 深圳一电科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle body and manufacturing method thereof |
| CN103818544B (en) * | 2014-01-24 | 2016-05-18 | 深圳一电航空技术有限公司 | Unmanned plane, unmanned aerial vehicle body and manufacture method thereof |
| CN104015916A (en) * | 2014-06-13 | 2014-09-03 | 韩世宇 | Unmanned plane |
| CN106029502A (en) * | 2015-04-24 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| WO2016169035A1 (en) * | 2015-04-24 | 2016-10-27 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| CN106904287A (en) * | 2017-03-21 | 2017-06-30 | 四川智航慧飞无人机科技有限公司 | Take photo by plane the protection structure of unmanned plane camera |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205150264U (en) | Can dismantle unmanned aerial vehicle battery package assembly | |
| CN105966612B (en) | Become posture VTOL unmanned plane | |
| CN103523197A (en) | Unmanned aerial vehicle bottom camera cabin | |
| CN203486130U (en) | Camera cabin at bottom of unmanned aerial vehicle | |
| WO2018148248A1 (en) | Uav booster aircraft for takeoff and climb assist | |
| CN205221105U (en) | Solar energy VTOL fixed wing uavs | |
| 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 | |
| CN103523203A (en) | Front camera cabin of unmanned aerial vehicle | |
| CN203465855U (en) | Obstacle alarm system for unmanned plane | |
| CN103531044A (en) | Barrier alarm system for unmanned aerial vehicle | |
| CN203497173U (en) | Single-interceptor tail wing of unmanned plane | |
| CN206031796U (en) | Unmanned aerial vehicle's parachute structure | |
| CN108657435A (en) | A kind of stability it is good agricultural nobody spill medicine device | |
| CN106965934A (en) | The landing modes and device of a kind of aircraft | |
| CN103786873A (en) | Interceptor for airframe bottom of unmanned plane | |
| 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) | |
| CN106915464A (en) | The landing-gear and mode of a kind of aircraft | |
| CN105129104A (en) | Camera bracket and fixed-wing unmanned aerial vehicle | |
| CN106828914A (en) | A kind of modularization VTOL fixed-wing unmanned vehicle based on culvert type force vector component | |
| CN203497169U (en) | Plane-body-top interceptor of unmanned plane | |
| CN203497172U (en) | Multi-interceptor tail wing of unmanned plane | |
| CN203666975U (en) | Mounting fixing device for steering engine of unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140122 |