CN107539490A - A kind of unmanned plane with lower cover - Google Patents
A kind of unmanned plane with lower cover Download PDFInfo
- Publication number
- CN107539490A CN107539490A CN201610499600.6A CN201610499600A CN107539490A CN 107539490 A CN107539490 A CN 107539490A CN 201610499600 A CN201610499600 A CN 201610499600A CN 107539490 A CN107539490 A CN 107539490A
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- China
- Prior art keywords
- lower cover
- unmanned plane
- shell
- video camera
- foam
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Abstract
The present invention discloses a kind of unmanned plane with lower cover; including shell and the main element being contained in shell; the shell outline is that arc bus rotates about the axis the cydariform to be formed; shell lower end section part is additionally provided with the lower cover of one and the smooth split of case surface; the lower cover is detachably arranged on shell, and the lower cover also includes being laid in the video camera protective layer being bonded with lower cover inwall in lower cover.The lower cover of the present invention can be protected to the video camera of unmanned plane, and match adaptation with the shell structure of unmanned plane.
Description
Technical field
The present invention relates to unmanned plane field, especially a kind of unmanned plane with lower cover.
Background technology
At present, unmanned plane is applied in social life more and more widely, and the place for being difficult to reach for people is carried out
Closely observe, or carry out high-altitude and take a crane shot, and then provided convenience for observation, shooting.
Existing unmanned plane lower end is provided with foot stool in order to which the landing of unmanned plane, upper end are provided with horn, still, existing nothing
Foot stool and horn in man-machine be with fuselage in a manner of being fixedly connected, after use, it is necessary to unmanned plane deposit, then due to
Foot stool space-consuming is larger so that storage is inconvenient, and easily causes the damage to unmanned plane.Therefore, design one kind does not make
The unmanned plane that used time is easy to deposit safely is become for an important research direction, such as designs streamline outward appearance nobody
Machine, such as egg type unmanned plane, deployable foot stool and horn when in use, after use, recoverable foot stool and horn formed once
In carrying and have the egg type structure of beauty function.Unmanned plane lower end would generally be provided with video camera, therefore on the basis of egg type unmanned plane
Upper design one kind can protect video camera, and turn into a new research topic with the lower cover of unmanned plane Structure adaptation.
In view of this it is special to propose the present invention.
The content of the invention
The technical problem to be solved in the present invention is overcome the deficiencies in the prior art, there is provided a kind of unmanned plane with lower cover,
The video camera of unmanned plane can be protected by lower cover during using and depositing unmanned plane, the lower cover and nobody
The shell structure matching of machine adapts to, and has effect attractive in appearance.
In order to solve the above technical problems, the basic conception of the technical solution adopted by the present invention is：
A kind of unmanned plane with lower cover, including shell and the main element that is contained in shell, the shell outline be
Arc bus rotates about the axis the cydariform to be formed, and shell lower end section part is additionally provided with one and the smooth split of case surface
Lid, the lower cover are detachably arranged on shell.
In such scheme, lower cover and unmanned plane case surface split, and complete smooth curved surface is formed in mosaic, make
It is streamlined structure to obtain whole unmanned plane, and aesthetic is good.
Preferably, the lower cover also includes being laid in the video camera protective layer being bonded with lower cover inwall in lower cover.
Preferably, the unmanned plane also includes the unmanned plane horn that opposite shell is deployed and reclaimed, the unmanned plane horn
When the state of recovery, section under shell is stretched out in horn lower end, and the lower cover edge of opening is provided with what is coordinated with horn external part
Breach.
Preferably, the breach is set with horn to correspond.
Preferably, breach lower edge is placed under described has button hand position, and the button hand position is that lower lid housing is following in breach
Edge caves inward the face of caving in be formed.
In such scheme, increase button hand position can be easy to user to unload lower cover manually.
Preferably, the lower cover is provided with bayonet connection on the inwall of openend, shell lower end section part it is interior
Wall is provided with the snap seats being detachably connected with the bayonet connection.
Preferably, the bayonet connection is fixedly connected with a button, and the button drives bayonet connection up and down
Lower cover surface of shell is arranged on, the button position is not higher by lower cover surface of shell.
In such scheme, the button for causing bayonet connection and snap seats Joint failure is added, by using button
It is more convenient for dismounting of the user to lower cover.
Preferably, the video camera protective layer is foam, and the foam is crown less than the hollow ball of lower cover depth for height
Structure, the foam mass axis overlaps with lower cover mass axis and plane of the opening is perpendicular to lower cover mass axis, the foam
Bulge loop is provided with the upside of open end, the lower cover inner walls, which are correspondingly provided with, acts on bulge loop to fix the limit convex of foam
Circle.
It is video camera protective layer from foam in such scheme, foam elasticity gets well the protecting effect having had to video camera
And in light weight it is easy to carry.
Preferably, the lower cover inner walls are provided with annular convex rib on the upside of spacing flange collar, are put down where the annular convex rib
Face is perpendicular to lower cover mass axis.
Preferably, it is provided with and strengthens along lower cover mass axis direction on the inwall of the housing between each breach of the lower cover
Muscle.
In such scheme, lower cover inner walls are provided with annular convex rib and reinforcement adds the intensity of lower cover, are not easy
Damage
Preferably, the unmanned plane also includes a shooting movable up and down being arranged on the main element of shell lower end
Machine, the lower cover bottom open up an opening for being available for video camera to stretch out or be recovered in lower cover.
After adopting the above technical scheme, the present invention has the advantages that compared with prior art：
1st, unmanned plane lower cover of the invention is detachably arranged on unmanned plane shell, is easy to enter the video camera in shell
Row operation is handled.The lower cover also includes being laid in the video camera protective layer being bonded with lower cover inwall in lower cover.Lower cover is using
After video camera can be protected, and with the smooth split of unmanned plane main casing.
2nd, lower cover of the invention and unmanned plane case surface split, and complete smooth curved surface is formed in mosaic so that
Whole unmanned plane is streamlined structure, and aesthetic is good.
3rd, it is video camera protective layer from foam, the good protecting effect having had to video camera of elasticity is in light weight to be easy to carry.
4th, lower cover inner walls are provided with annular convex rib and reinforcement adds the intensity of lower cover, are hardly damaged.
The embodiment of the present invention is described in further detail below in conjunction with the accompanying drawings.
Brief description of the drawings
A part of the accompanying drawing as the application, for providing further understanding of the invention, of the invention is schematic
Embodiment and its illustrate to be used to explain the present invention, but do not form inappropriate limitation of the present invention.Obviously, drawings in the following description
Only some embodiments, to those skilled in the art, on the premise of not paying creative work, can be with
Other accompanying drawings are obtained according to these accompanying drawings.In the accompanying drawings：
Fig. 1 is the schematic diagram of the complete split of unmanned plane housing of the present invention；
Fig. 2 is the unmanned plane shell structure explosive view of the present invention；
Fig. 3 is the unmanned plane lower cover structure explosive view of the present invention；
Fig. 4 is the unmanned plane lower cover and foam installation diagram of the present invention；
In figure：1st, shell；11st, unmanned plane horn；2nd, lower cover；21st, breach；22nd, bayonet connection；23rd, reinforcement；3rd, on
Lid；4th, video camera；5th, button；6th, button hand position；7th, foam；71st, double faced adhesive tape；711st, bulge loop；712nd, spacing flange collar；713rd, convex annular
Muscle.
It should be noted that these accompanying drawings and word description are not intended as the design model limiting the invention in any way
Enclose, but be that those skilled in the art illustrate idea of the invention by reference to specific embodiment.
Embodiment
To make the purpose, technical scheme and advantage of the embodiment of the present invention clearer, below in conjunction with the embodiment of the present invention
In accompanying drawing, the technical scheme in embodiment is clearly and completely described, following examples be used for illustrate the present invention, but
It is not limited to the scope of the present invention.
In the description of the invention, it is necessary to explanation, the orientation or position of the instruction such as term " on ", " under ", " interior ", " outer "
It is based on orientation shown in the drawings or position relationship to put relation, is for only for ease of the description present invention and simplifies description, rather than
Indicate or imply that signified device or element there must be specific orientation, with specific azimuth configuration and operation, therefore can not
It is interpreted as limitation of the present invention.
In the description of the invention, it is necessary to which explanation, unless otherwise clearly defined and limited, term " installation ", " connects
Connect " it should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or it is integrally connected；It can be machine
Tool connects or electrical connection；Can be joined directly together, can also be indirectly connected by intermediary.For this area
For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Embodiment one
Unmanned plane housing as shown in Figures 1 to 4, and lower cover structure figure, the unmanned plane of the present invention with lower cover, bag
Include shell 1 and the main element being contained in shell, it is characterised in that the outline of shell 1 is that arc bus revolves around axis
Turn the cydariform formed, the lower end section part of shell 1 is additionally provided with the lower cover 2 of one and the smooth surface split of shell 1, the lower cover 2
It is detachably arranged on shell 1, the lower cover 2 also includes being laid in the video camera protection being bonded with lower cover inwall in lower cover 2
Layer, section is additionally provided with lid 3 on one, the upper lid 3 and the smooth split of section on shell 1 on the shell 1, upper lid 3, lower cover 2 with
And the three of shell 1 is combined and spliced so that whole unmanned plane is in an egg type structure.
The unmanned plane with lower cover also includes the unmanned plane horn 11 that opposite shell 1 is deployed and reclaimed, the unmanned plane
Horn 11 when the state of recovery, the lower end of unmanned plane horn 11 stretch out 1 time section of shell, the edge of opening of lower cover 2 be provided with and
The breach 21 that the external part of unmanned plane horn 11 coordinates.The breach 21 is set with unmanned plane horn 11 to correspond, breach 21
It is identical with the quantity of unmanned plane horn 11, preferably four.
The lower cover 2 has button hand position 6 in the lower edge of breach 21, and the button hand position 6 is lower lid housing in breach lower edge
Cave inward the face of caving in be formed.By setting lower cover button hand position on each breach, hand disassembly of the user to lower cover is facilitated.
The lower cover 2 is provided with the bayonet connection 22 of protrusion on the inwall of openend, the lower end section part of shell 1
Inner walls are provided with snap seats, and the bayonet connection 22 cooperatively forms the buckle structure being detachably connected with snap seats.
As further optimization, the bayonet connection 22 is fixedly connected with a button 5 for being located at lower cap surface, described to press
The position of button 5 is not higher by lower cover surface of shell, it is preferred that when not applying external force, the outer surface of button 5 is spelled with the smooth surface of lower cover 2
Close, the button 5 can be up and down by external force by stopping means control, and the stopping means includes a restraint slot and two limits
Position portion, the fiting constraint groove inwall of button 5 is up and down, and movable between two limiting sections, and two limiting sections include limit
Button 5 processed protrudes the first limiting section of surface of shell and causes bayonet connection to depart from the second limiting section of snap seats, described
First time limiting section and the second limiting section between be additionally provided with a spring to the first limiting section ejection button 5, button 5 can be outside
The lower against the force of the spring of power effect reaches the second limiting section to cause bayonet connection 22 to depart from snap seats.
Embodiment two
Unmanned plane housing as shown in Figures 1 to 4, and lower cover structure figure, unmanned plane lower cover 2 of the invention also include tiling
The video camera protective layer being bonded in lower cover 2 with the inwall of lower cover 2.Preferably, the video camera protective layer is foam 7, the bubble
Cotton 7 is fixed with lower cover inwall and is bonded, it is preferred that foam 7 is fixed with the inwall of lower cover 2 by double faced adhesive tape 71 and is bonded.In the present embodiment
It is that video camera protective layer has the advantages of notable, the curved inner wall of the flexible suitable lower cover of foam material from foam, foam has
Elasticity has preferable protective effect to video camera 4, and foam light weight is easy to carry.
The foam 7 is less than the hollow ball Crown structure of lower cover depth, the mass axis of foam 7 and lower cover weight for height
Mandrel line overlaps and plane of the opening is perpendicular to the mass axis of lower cover 2, and the foam 7 is provided with bulge loop 711, institute on the upside of open end
State lower cover inner walls and be correspondingly provided with and act on bulge loop to fix the spacing flange collar 712 of foam.
The inner walls of lower cover 2 are provided with annular convex rib 713, the place of annular convex rib 713 in the spacing upside of flange collar 712
Plane it is vertical with the mass axis of lower cover 2.The inwall of housing parts between each breach 21 of lower cover 2 is provided with along lower cover weight
The reinforcement 23 being distributed on heart axis direction.The inner walls of lower cover 2 are provided with annular convex rib 713 and reinforcement 23 adds lower cover
2 intensity so that lower cover 2 is hardly damaged in routine use.
Embodiment three
In the present embodiment, a video camera is set on the main element of the shell lower end of unmanned plane, and the video camera can lead to
Cross an apparatus for adjusting position and carry out the regulation of upper-lower position to it, the lower cover bottom opens up opening for a size and Camera Match
Mouthful, the video camera is extended in the presence of apparatus for adjusting position or is recovered in lower cover.
Described above is only presently preferred embodiments of the present invention, not makees any formal limitation to the present invention, though
So the present invention is disclosed above with preferred embodiment, but is not limited to the present invention, any technology people for being familiar with this patent
Member without departing from the scope of the present invention, when the technology contents using above-mentioned prompting make it is a little change or be modified to
The equivalent embodiment of equivalent variations, as long as being the content without departing from technical solution of the present invention, the technical spirit pair according to the present invention
Any simple modification, equivalent change and modification that above example is made, in the range of still falling within the present invention program.
Claims (10)
1. a kind of unmanned plane with lower cover, including shell and the main element that is contained in shell, it is characterised in that the shell
Outline is that arc bus rotates about the axis the cydariform to be formed, and it is smooth with case surface that shell lower end section part is additionally provided with one
The lower cover of split, the lower cover are detachably arranged on shell.
2. the unmanned plane according to claim 1 with lower cover, it is characterised in that the lower cover also includes being laid in lower cover
The video camera protective layer being bonded with lower cover inwall.
3. the unmanned plane according to claim 2 with lower cover, it is characterised in that also deploy including opposite shell and reclaim
Unmanned plane horn, for the unmanned plane horn when state of recovery, section under shell, the lower cover edge of opening are stretched out in horn lower end
It is provided with the breach coordinated with horn external part.
4. the unmanned plane according to claim 3 with lower cover, it is characterised in that breach lower edge is placed under described has button
Hand position, the button hand position are that lower lid housing caves inward the face of caving in be formed in breach lower edge.
5. the unmanned plane according to claim 1 with lower cover, it is characterised in that the lower cover is set on the inwall of openend
There is bayonet connection, the inwall of shell lower end section part is provided with the buckle being detachably connected with the bayonet connection
Seat.
6. the unmanned plane according to claim 5 with lower cover, it is characterised in that the bayonet connection be fixedly connected one by
Button, the button drive bayonet connection it is up and down be arranged on lower cover surface of shell, the button position is not higher by lower cover
Surface of shell.
7. the unmanned plane according to claim 2 with lower cover, it is characterised in that the video camera protective layer is foam, institute
State foam for height be less than lower cover depth hollow ball Crown structure, the foam mass axis overlapped with lower cover mass axis and
For plane of the opening perpendicular to lower cover mass axis, the foam is provided with bulge loop, the lower cover inner walls pair on the upside of open end
It should be provided with and act on bulge loop to fix the spacing flange collar of foam.
8. the unmanned plane according to claim 7 with lower cover, it is characterised in that the lower cover inner walls are in spacing flange collar
Upside is provided with annular convex rib, and plane is perpendicular to lower cover mass axis where the annular convex rib.
9. the unmanned plane according to claim 3 with lower cover, it is characterised in that housing between each breach of lower cover
On inwall reinforcement is provided with along lower cover mass axis direction.
10. the unmanned plane according to claim 1 with lower cover, it is characterised in that also including a setting movable up and down
Video camera on the main element of shell lower end, the lower cover bottom open up one and are available for video camera to stretch out or be recovered in lower cover
Opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610499600.6A CN107539490A (en) | 2016-06-29 | 2016-06-29 | A kind of unmanned plane with lower cover |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610499600.6A CN107539490A (en) | 2016-06-29 | 2016-06-29 | A kind of unmanned plane with lower cover |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107539490A true CN107539490A (en) | 2018-01-05 |
Family
ID=60965928
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610499600.6A Pending CN107539490A (en) | 2016-06-29 | 2016-06-29 | A kind of unmanned plane with lower cover |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107539490A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109981788A (en) * | 2019-04-03 | 2019-07-05 | 安徽中科智能感知产业技术研究院有限责任公司 | A kind of communication management method of agricultural Internet of Things virtual terminal |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2472610Y (en) * | 2001-04-12 | 2002-01-23 | 广东美的集团股份有限公司 | Electric rice cooker |
| US8137007B1 (en) * | 2008-01-11 | 2012-03-20 | Brandebury Tool Company, Inc. | Miniaturized turret-mounted camera assembly |
| CN102745273A (en) * | 2012-05-31 | 2012-10-24 | 北京航空航天大学 | Miniature throwable deformation reconnaissance ball |
| CN203084400U (en) * | 2012-05-23 | 2013-07-24 | 吴日开 | Universal camera protective housing |
| CN203609298U (en) * | 2013-10-28 | 2014-05-28 | 美的集团股份有限公司 | Press button assembly of electric rice cooker and electric rice cooker adopting press button assembly |
| EP2132527B1 (en) * | 2007-04-02 | 2014-10-22 | Embraer S.A. | Retractable system for aeronautical sensors |
| CN105193277A (en) * | 2015-10-15 | 2015-12-30 | 珠海格力电器股份有限公司 | Detachable hinge structure and kitchen appliance with same |
| CN105584621A (en) * | 2015-12-25 | 2016-05-18 | 北京臻迪机器人有限公司 | Aircraft |
-
2016
- 2016-06-29 CN CN201610499600.6A patent/CN107539490A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2472610Y (en) * | 2001-04-12 | 2002-01-23 | 广东美的集团股份有限公司 | Electric rice cooker |
| EP2132527B1 (en) * | 2007-04-02 | 2014-10-22 | Embraer S.A. | Retractable system for aeronautical sensors |
| US8137007B1 (en) * | 2008-01-11 | 2012-03-20 | Brandebury Tool Company, Inc. | Miniaturized turret-mounted camera assembly |
| CN203084400U (en) * | 2012-05-23 | 2013-07-24 | 吴日开 | Universal camera protective housing |
| CN102745273A (en) * | 2012-05-31 | 2012-10-24 | 北京航空航天大学 | Miniature throwable deformation reconnaissance ball |
| CN203609298U (en) * | 2013-10-28 | 2014-05-28 | 美的集团股份有限公司 | Press button assembly of electric rice cooker and electric rice cooker adopting press button assembly |
| CN105193277A (en) * | 2015-10-15 | 2015-12-30 | 珠海格力电器股份有限公司 | Detachable hinge structure and kitchen appliance with same |
| CN105584621A (en) * | 2015-12-25 | 2016-05-18 | 北京臻迪机器人有限公司 | Aircraft |
Non-Patent Citations (2)
| Title |
|---|
| 上海科学技术文献出版社等编辑: "《专利文献通报 建筑、给排水》", 31 December 1985, 上海科学技术文献出版社 * |
| 中一: "《摄像知识一本通》", 30 June 2013, 企业管理出版社 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109981788A (en) * | 2019-04-03 | 2019-07-05 | 安徽中科智能感知产业技术研究院有限责任公司 | A kind of communication management method of agricultural Internet of Things virtual terminal |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180105 |
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| RJ01 | Rejection of invention patent application after publication |