CN103523203A - Front camera cabin of unmanned aerial vehicle - Google Patents
Front camera cabin of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN103523203A CN103523203A CN201310480536.3A CN201310480536A CN103523203A CN 103523203 A CN103523203 A CN 103523203A CN 201310480536 A CN201310480536 A CN 201310480536A CN 103523203 A CN103523203 A CN 103523203A
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- Prior art keywords
- unmanned plane
- cloud terrace
- adapter plate
- plane body
- before unmanned
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Abstract
The invention relates to an unmanned aerial vehicle component, and in particular relates to a front camera cabin of an unmanned aerial vehicle. The front camera cabin 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 holder fixing plate is arranged at the head part of the plane body; and a transparent hood is arranged outside the holder fixing plate. According to the front camera cabin of the unmanned aerial vehicle, as a camera cabin is arranged at the head part of the plane body in advance, the holder fixing plate is arranged inside the camera cabin and is used for mounting a holder and connecting a camera, the camera mounting structure is one part of the whole unmanned aerial vehicle, the counter weight ratio of the front and back parts of the plane body can be calculated in advance, and subsequently components are configured, therefore, 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 the 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 before especially a kind of unmanned plane.
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 the front phase cabin of fuselage pulsation-free unmanned plane.
To achieve these goals, the present invention adopts following technical scheme:
Comprise a fuselage, described waist both sides are provided with flank, and afterbody both sides are provided with tail flank, and afterbody top is provided with empennage, and its improvement is: described fuselage head is provided with a The Cloud Terrace adapter plate, and described The Cloud Terrace adapter plate outside is provided with a translucent cover.
Preferably, described The Cloud Terrace adapter plate is vertical setting.
Preferably, described The Cloud Terrace adapter plate is installed on the turning cylinder of a level.
Preferably, described The Cloud Terrace adapter plate is rectangle or square.
Preferably, described translucent cover is the curved-surface structure adapting with front fuselage profile.
Preferably, between described translucent cover and fuselage, be provided with seal ring.
Preferably, described translucent cover is aeronautical glasses cover.
Preferably, described turning cylinder is a hollow tube.
Preferably, described hollow tube is a circular body.
Preferably, described The Cloud Terrace adapter plate and turning cylinder are aluminum alloy integral structure.
Owing to having adopted said structure, before unmanned plane of the present invention, phase cabin arranges a phase cabin at fuselage head in advance, The Cloud Terrace adapter plate is set in phase cabin, for The Cloud Terrace is installed, connects camera, camera mounting structure is unmanned plane part of the whole, can precalculated front and back counterweight ratio, carrying out component configuration, so being installed, camera can not destroy the counterweight ratio before and after fuselage later yet, the stability that does not affect unmanned plane during flying, has 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, before the unmanned plane 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, described fuselage 1 head is provided with a The Cloud Terrace adapter plate 5, and described The Cloud Terrace adapter plate 5 outsides are provided with a translucent cover 6.
In the present embodiment, described The Cloud Terrace adapter plate 5 is vertical setting.
Because camera need to rotate adjusting angle when taking pictures, in order to coordinate the adjusting of The Cloud Terrace, in the present embodiment, described The Cloud Terrace adapter plate 5 is installed on the turning cylinder 7 of a level.
In the present embodiment, described The Cloud Terrace adapter plate 5 is rectangle or square.
In order to keep unmanned plane overall profile integraty, in the present embodiment, described translucent cover 6 is the curved-surface structure adapting with fuselage 1 front end profile.
In order to play the effect of sealing, in the present embodiment, between described translucent cover 6 and fuselage 1, be provided with seal ring 8.
In the present embodiment, described translucent cover 6 is aeronautical glasses cover.
In the present embodiment, described turning cylinder 7 is a hollow tube.
In the present embodiment, described hollow tube is a circular body.
In the present embodiment, described The Cloud Terrace adapter plate 5 is aluminum alloy integral structure with turning cylinder 7.
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 before unmanned plane, comprises a fuselage, and 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 fuselage head is provided with a The Cloud Terrace adapter plate, and described The Cloud Terrace adapter plate outside is provided with a translucent cover.
2. phase cabin before unmanned plane as claimed in claim 1, is characterized in that: described The Cloud Terrace adapter plate arranges for vertical.
3. phase cabin before unmanned plane as claimed in claim 2, is characterized in that: described The Cloud Terrace adapter plate is installed on the turning cylinder of a level.
4. phase cabin before unmanned plane as claimed in claim 3, is characterized in that: described The Cloud Terrace adapter plate is rectangle or square.
5. phase cabin before unmanned plane as claimed in claim 4, is characterized in that: described translucent cover is the curved-surface structure adapting with front fuselage profile.
6. phase cabin before unmanned plane as claimed in claim 5, is characterized in that: between described translucent cover and fuselage, be provided with seal ring.
7. phase cabin before unmanned plane as claimed in claim 6, is characterized in that: described translucent cover is aeronautical glasses cover.
8. phase cabin before unmanned plane as claimed in claim 7, is characterized in that: described turning cylinder is a hollow tube.
9. phase cabin before unmanned plane as claimed in claim 8, is characterized in that: described hollow tube is a circular body.
10. phase cabin before unmanned plane as claimed in claim 9, is characterized in that: described The Cloud Terrace adapter plate and turning cylinder are aluminum alloy integral structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310480536.3A CN103523203A (en) | 2013-10-15 | 2013-10-15 | Front camera cabin of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310480536.3A CN103523203A (en) | 2013-10-15 | 2013-10-15 | Front camera cabin of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103523203A true CN103523203A (en) | 2014-01-22 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310480536.3A Pending CN103523203A (en) | 2013-10-15 | 2013-10-15 | Front camera cabin of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN103523203A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103803093A (en) * | 2014-03-03 | 2014-05-21 | 天津曙光敬业科技有限公司 | Fixed-wing unmanned aerial vehicle aerial shooting device |
| CN107585305A (en) * | 2017-10-10 | 2018-01-16 | 王根英 | A kind of light and handy unmanned plane |
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| CN202170018U (en) * | 2011-07-15 | 2012-03-21 | 东华大学 | Small-sized perpendicular taking off and landing unmanned plane for monitoring and fire fighting |
| CN102490904A (en) * | 2010-03-16 | 2012-06-13 | 北京航空航天大学 | Small multipurpose unmanned plane |
| CN202414153U (en) * | 2011-12-21 | 2012-09-05 | 天津风之翼科技有限公司 | Multi-purpose unmanned aerial vehicle airframe |
| CN103241380A (en) * | 2012-02-03 | 2013-08-14 | 伊德斯德国股份有限公司 | Surveillance and/or weapons system and method for objects on land or sea |
| CN203497168U (en) * | 2013-10-15 | 2014-03-26 | 江苏艾锐泰克无人飞行器科技有限公司 | Front camera bin of unmanned plane |
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2013
- 2013-10-15 CN CN201310480536.3A patent/CN103523203A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102490904A (en) * | 2010-03-16 | 2012-06-13 | 北京航空航天大学 | Small multipurpose unmanned plane |
| CN202170018U (en) * | 2011-07-15 | 2012-03-21 | 东华大学 | Small-sized perpendicular taking off and landing unmanned plane for monitoring and fire fighting |
| CN202414153U (en) * | 2011-12-21 | 2012-09-05 | 天津风之翼科技有限公司 | Multi-purpose unmanned aerial vehicle airframe |
| CN103241380A (en) * | 2012-02-03 | 2013-08-14 | 伊德斯德国股份有限公司 | Surveillance and/or weapons system and method for objects on land or sea |
| CN203497168U (en) * | 2013-10-15 | 2014-03-26 | 江苏艾锐泰克无人飞行器科技有限公司 | Front camera bin of unmanned plane |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103803093A (en) * | 2014-03-03 | 2014-05-21 | 天津曙光敬业科技有限公司 | Fixed-wing unmanned aerial vehicle aerial shooting device |
| CN103803093B (en) * | 2014-03-03 | 2016-03-23 | 天津曙光敬业科技有限公司 | Fixed-wing unmanned plane aerial device |
| CN107585305A (en) * | 2017-10-10 | 2018-01-16 | 王根英 | A kind of light and handy unmanned plane |
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| 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 |