CN105270613B - A kind of six axis aircraft of achievable telescopic folding - Google Patents
A kind of six axis aircraft of achievable telescopic folding Download PDFInfo
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- CN105270613B CN105270613B CN201510704049.XA CN201510704049A CN105270613B CN 105270613 B CN105270613 B CN 105270613B CN 201510704049 A CN201510704049 A CN 201510704049A CN 105270613 B CN105270613 B CN 105270613B
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- horn
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Abstract
A kind of six axis aircraft of achievable telescopic folding provided by the invention, including paddle disk, paddle disk is regular hexagon structure, and paddle disk is equipped with the first mounting hole on the center per one side, first mounting hole is equipped with L-type installing plate, L-type installing plate is equipped with horn, and horn includes outer boom, interior horn, sleeve and positioner, simple in structure, design is reasonable, positioner is positioned using ball, frictional force of the horn in telescopic process is reduced to greatest extent, easy to flexible；Outer boom, interior horn and casing are tubular type structure design, more preferable than the mechanical property of square tube under similarity condition, can bear the power of bigger；When horn folds, first the second bolt is taken off, then horn is rolled over downwards to 90 degree, then connected horn and L-type installing plate with the second bolt, step is simple, simple operation, easy to carry, and the scope of application is wider, can more meet the needs of user.
Description
Technical field
The present invention relates to the six axis aircraft in vehicle technology field, particularly a kind of achievable telescopic folding.
Background technology
Aircraft is to be manufactured by the mankind, can fly away from ground, controlled in space flight and by people in endoatmosphere or big
The apparatus flying object of gas-bearing formation external space flight.The referred to as aircraft of flight in endoatmosphere, is known as spacecraft in space flight.
With the development of the times, in order to meet the needs of user, Multi-axis aircraft develops towards maximization direction.And existing multiaxis
Aircraft is largely complicated, not easy to operate when causing to stretch with folding, and is unfavorable for carrying.
The content of the invention
Problem to be solved by this invention is to provide a kind of six axis aircraft of achievable telescopic folding, solves existing more
Axis aircraft is largely complicated, not easy to operate when causing to stretch with folding, the problem of being unfavorable for carrying.
To solve problem above scheme of the present invention：
A kind of six axis aircraft of achievable telescopic folding, including paddle disk, the paddle disk is regular hexagon structure, described
Paddle disk per one side center on be equipped with the first mounting hole, first mounting hole is equipped with L-type installing plate, described
L-type installing plate be two, axisymmetricly set using the center line of paddle disk as symmetry axis, the L-type installing plate is equipped with machine
Arm, the L-type installing plate include the first installing plate and the second installing plate, and first installing plate is vertical with the second installing plate
Set, first installing plate is equipped with the second mounting hole, and the second installing plate is equipped with the 3rd mounting hole, the described second peace
Dress hole is used cooperatively by the first bolt and the first mounting hole, and the horn includes outer boom, interior horn, sleeve and positioning and fills
Put, the interior horn is equipped with location hole, and the outer boom includes the first outer end and the first inner, described interior horn bag
The second outer end and second the inner are included, the positioner is fixed on first the inner of outer boom, and the sleeve is embedded in
On second outer end of interior horn, the positioner includes locating rod, and the locating rod includes installation end and fixing end, institute
The fixing end stated is equipped with mounting groove, is equipped with spring in the mounting groove, and spring is equipped with ball, and the of the outer boom
One inner the second outer end through sleeve and interior horn, makes ball be used cooperatively with location hole, the interior horn second in
End is equipped with the 4th mounting hole, and the 4th mounting hole is used cooperatively by the second bolt and the 3rd mounting hole.
A kind of six axis aircraft of above-mentioned achievable telescopic folding, wherein, the location hole includes the first location hole
With the second location hole, the length between the first location hole and the second location hole is 10-20cm.
A kind of six axis aircraft of above-mentioned achievable telescopic folding, wherein, the outer boom, interior horn and casing are equal
For tubular type structure design.
A kind of six axis aircraft of above-mentioned achievable telescopic folding, wherein, the height R1 of the outer boom is less than interior
The height R2 of horn.
The beneficial effect of this programme：
A kind of six axis aircraft of achievable telescopic folding provided by the invention, simple in structure, design is reasonable, positioner
Positioned using ball, frictional force of the horn in telescopic process is reduced to greatest extent, easy to flexible, interior horn is equipped with
Two location holes, stretch and adjust easy to outer boom；Outer boom, interior horn and casing are tubular type structure design, same
Under the conditions of, it is more preferable than the mechanical property of square tube, the power of bigger can be born；When horn folds, first the second bolt is taken off,
Then horn to be rolled over downwards to 90 degree, then connected horn and L-type installing plate with the second bolt, step is simple,
Simple operation, easy to carry, the scope of application is wider, can more meet the needs of user.
Brief description of the drawings
Fig. 1 is overall structure figure of the present invention.
Fig. 2 is part A enlarged diagram in Fig. 1.
Fig. 3 is horn structure chart of the present invention.
Fig. 4 is the external arm of the present invention, inscribed arm and positioning device structure exploded perspective view.
Fig. 5 is paddle dish structure figure of the present invention.
Fig. 6 is L-type mounting plates structure figure.
Embodiment
As shown in the figure, a kind of six axis aircraft of achievable telescopic folding, including paddle disk 1, the paddle disk 1 are positive six
Side shape structure, the paddle disk 1 are equipped with the first mounting hole 2 on the center per one side, are set on first mounting hole 2
There is L-type installing plate 3, the L-type installing plate 3 is two, is axisymmetricly set using the center line of paddle disk 1 as symmetry axis, described
L-type installing plate 3 be equipped with horn 4, the L-type installing plate 3 includes the first installing plate 5 and the second installing plate 6, described
One installing plate 5 is vertically arranged with the second installing plate 6, and first installing plate 5 is equipped with the second mounting hole 7, the second installing plate 6
The 3rd mounting hole 8 is equipped with, second mounting hole 7 is used cooperatively by the first bolt 9 and the first mounting hole 2, described
Horn 4 includes outer boom 10, interior horn 11, sleeve 12 and positioner 13, the interior horn 11 and is equipped with location hole 14, institute
The outer boom 10 stated includes the first outer end 15 and first the inner 16, and it is inner that the interior horn 11 includes the second outer end 17 and second
18, the positioner 13 is fixed on first the inner 16 of outer boom 10, and the sleeve 12 is embedded in interior horn 11
On second outer end 17, the positioner 13 includes locating rod 19, and the locating rod 19 includes installation end 20 and fixing end
21, the fixing end 21 is equipped with mounting groove 22, is equipped with spring 23 in the mounting groove 22, spring 23 is equipped with ball
24, first the inner 16 of the outer boom 10 makes ball 24 and positioning through the second outer end 17 of sleeve 12 and interior horn 11
Hole 14 is used cooperatively, and second the inner 18 of the interior horn 11 is equipped with the 4th mounting hole 25, the 4th mounting hole 25
It is used cooperatively by the second bolt 111 with the 3rd mounting hole 8, the location hole 14 includes the first location hole 26 and the second positioning
Hole 27, the length between the first location hole 26 and the second location hole 27 are 10-20cm, the outer boom 10, interior horn 11 with
Casing 12 is tubular type structure design, and the height R1 of the outer boom 10 is less than the height R2 of interior horn 11.
A kind of six axis aircraft of achievable telescopic folding provided by the invention, simple in structure, design is reasonable, positioner
Positioned using ball, frictional force of the horn in telescopic process is reduced to greatest extent, easy to flexible, interior horn is equipped with
Two location holes, stretch and adjust easy to outer boom；Outer boom, interior horn and casing are tubular type structure design, same
Under the conditions of, it is more preferable than the mechanical property of square tube, the power of bigger can be born；When horn folds, first the second bolt is taken off,
Then horn to be rolled over downwards to 90 degree, then connected horn and L-type installing plate with the second bolt, step is simple,
Simple operation, easy to carry, the scope of application is wider, can more meet the needs of user.
It is merely preferred embodiments of the present invention, but protection scope of the present invention is not limited thereto, it is any to be familiar with
Those skilled in the art the invention discloses technical scope in, the change or replacement that can readily occur in should all be covered
Within the scope of the present invention.Therefore, protection scope of the present invention should be subject to the protection domain of claims.
Claims (1)
1. a kind of six axis aircraft of achievable telescopic folding, including paddle disk, it is characterized in that, the paddle disk is regular hexagon knot
Structure, the paddle disk are equipped with the first mounting hole on the center per one side, first mounting hole is pacified equipped with L types
Loading board, the L types installing plate are two, are axisymmetricly set using the center line of paddle disk as symmetry axis, L types peace
Loading board is equipped with horn, and the L types installing plate includes the first installing plate and the second installing plate, first installing plate
It is vertically arranged with the second installing plate, first installing plate is equipped with the second mounting hole, and the second installing plate is equipped with the 3rd peace
Fill hole, second mounting hole is used cooperatively by the first bolt and the first mounting hole, the horn including outer boom,
Interior horn, sleeve and positioner, the interior horn are equipped with location hole, and the outer boom includes the first outer end and the
One is inner, and the interior horn includes the second outer end and second the inner, and the positioner is fixed in the first of outer boom
On end, the sleeve is embedded on the second outer end of interior horn, and the positioner includes locating rod, the positioning
Bar includes installation end and fixing end, and the fixing end is equipped with mounting groove, is equipped with spring in the mounting groove, on spring
Equipped with ball, first inner the second outer end through sleeve and interior horn of the outer boom, makes ball coordinate with location hole
Use, second the inner of the interior horn is equipped with the 4th mounting hole, and the 4th mounting hole passes through the second bolt and the
Three mounting holes are used cooperatively；The location hole includes the first location hole and the second location hole, the first location hole and the second positioning
Length between hole is 10-20cm；Outer boom, interior horn and the casing is tubular type structure design, and described is outer
The height R1 of horn is less than the height R2 of interior horn.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510704049.XA CN105270613B (en) | 2015-10-27 | 2015-10-27 | A kind of six axis aircraft of achievable telescopic folding |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510704049.XA CN105270613B (en) | 2015-10-27 | 2015-10-27 | A kind of six axis aircraft of achievable telescopic folding |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105270613A CN105270613A (en) | 2016-01-27 |
| CN105270613B true CN105270613B (en) | 2018-04-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510704049.XA Active CN105270613B (en) | 2015-10-27 | 2015-10-27 | A kind of six axis aircraft of achievable telescopic folding |
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| CN (1) | CN105270613B (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3971084A1 (en) | 2016-02-22 | 2022-03-23 | SZ DJI Technology Co., Ltd. | Aéronef multi-rotor pliable |
| CN106394887B (en) * | 2016-10-24 | 2018-06-26 | 杭州鼎曜信息技术有限公司 | Multi-rotor unmanned aerial vehicle and its control method |
| CN106314783B (en) * | 2016-10-24 | 2018-09-14 | 杭州鼎曜信息技术有限公司 | Anti- hurt sb.'s feelings multi-rotor unmanned aerial vehicle and its control method |
| CN107757913B (en) * | 2017-11-21 | 2020-01-07 | 歌尔科技有限公司 | Load control method and device based on unmanned aerial vehicle and unmanned aerial vehicle |
| CN208325617U (en) * | 2018-04-28 | 2019-01-04 | 上海飞来信息科技有限公司 | The variable multi-rotor aerocraft of wheelbase |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103318405B (en) * | 2013-07-17 | 2015-11-18 | 国家电网公司 | A kind of unmanned plane |
| CN204452930U (en) * | 2014-12-18 | 2015-07-08 | 合肥工业大学 | The four-axle aircraft of telescopic folding |
| CN104648664B (en) * | 2014-12-18 | 2017-02-22 | 合肥工业大学 | Retractable folding quad rotor |
| CN204587297U (en) * | 2015-04-20 | 2015-08-26 | 戴永东 | Unmanned plane and fuselage |
| CN204701765U (en) * | 2015-06-03 | 2015-10-14 | 江苏数字鹰科技发展有限公司 | With the multi-rotor aerocraft of rotor and cantilever folding and unfolding |
| CN205221097U (en) * | 2015-10-27 | 2016-05-11 | 镇江顺宇飞行器有限公司 | Can realize flexible six aircraft of folding |
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| CN105270613A (en) | 2016-01-27 |
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Effective date of registration: 20201217 Address after: No.2 building, medical machinery industrial park, west section of Daxue Road, Wanfu office, hi tech Zone, Heze City, Shandong Province Patentee after: Shandong Green Kairui Precision Instrument Co.,Ltd. Address before: Building 1, No. 33, Yangzijiang Road, Dagang, Zhenjiang New District, Zhenjiang City, Jiangsu Province Patentee before: ZHENJIANG SHUNYU AIRCRAFT Co.,Ltd. |