CN106628210B - A kind of unmanned plane Shatter-resistant device - Google Patents
A kind of unmanned plane Shatter-resistant device Download PDFInfo
- Publication number
- CN106628210B CN106628210B CN201710105139.6A CN201710105139A CN106628210B CN 106628210 B CN106628210 B CN 106628210B CN 201710105139 A CN201710105139 A CN 201710105139A CN 106628210 B CN106628210 B CN 106628210B
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- Prior art keywords
- vertical
- horizontal
- unmanned plane
- buffer
- yielding rubber
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
- B64D45/06—Landing aids; Safety measures to prevent collision with earth's surface mechanical
Abstract
The present invention discloses a kind of unmanned plane Shatter-resistant device, including unmanned plane main body, four vertical sliding cylinders and four vertical sliding bars, four horizontal sliding cylinders and four horizontal slide rods, two vertical bumper brackets, two horizontal bumper brackets, four vertical buffer rolls, two horizontal buffer rolls, two yielding rubber coverings, four wind springs, two gas receivers.The present invention realizes self-protection function when accidental falling situation occurs in unmanned plane by being provided with yielding rubber covering；By setting vertical sliding cylinder and vertical sliding bar and horizontal sliding cylinder and horizontal slide rod, the function of the multi-faceted protection of unmanned plane is realized；The gas receiver covered by setting elastic film carries out multiple protective to unmanned plane.
Description
Technical field
The present invention relates to a kind of unmanned plane auxiliary devices, particularly disclose a kind of unmanned plane Shatter-resistant device, belong to unmanned plane
Technical field.
Background technique
Unmanned air vehicle technique is quickly grown in recent years, and a variety of rotor crafts appear on the market, although unmanned air vehicle technique obtained compared with
Great development, but existing unmanned air vehicle technique relies primarily on battery as power often will appear in the use process of unmanned plane
Accidental falling due to occurring interrupting etc. powerup issue and communication system, and once there are accidental falling feelings in unmanned plane
Condition, unmanned plane will be faced with the misfortune of damage, cause damages to user.
Summary of the invention
In view of the above-mentioned problems, the present invention provides a kind of unmanned plane Shatter-resistant device, it can be safe with effective protection unmanned plane during flying,
The occurrence of preventing accidental falling from damaging.
Technical solution used in the present invention is: a kind of unmanned plane Shatter-resistant device, including unmanned plane main body, four vertical cunnings
Dynamic cylinder and four vertical sliding bars, four horizontal sliding cylinders and four horizontal slide rods, two vertical bumper brackets, two levels are delayed
Frame, four vertical buffer rolls, two horizontal buffer rolls, two yielding rubber coverings, four wind springs, two gas receivers are rushed, in nothing
Man-machine body top is vertically-mounted, and there are two vertical sliding cylinders, while being symmetrically installed in unmanned plane lower body part and sliding there are two vertical
Dynamic cylinder, four vertical sliding bars are slidably mounted on respectively in four vertical sliding cylinders, each vertical sliding boom end with
Buffer spring, the other end of two vertical sliding bars of unmanned plane body top are provided between the bottom of corresponding vertical sliding cylinder
It is provided with a vertical bumper bracket, the other end of two vertical sliding bars of unmanned plane lower body part is provided with another vertical buffering
Frame；Horizontal sliding cylinder there are two being horizontally mounted in unmanned plane body front part, while two are symmetrically installed in unmanned plane back body
A horizontal sliding cylinder, four horizontal slide rods are slidably mounted on respectively in four horizontal sliding cylinders, each horizontal sliding
Buffer spring, two horizontal slide rods of unmanned plane body front part are provided between boom end and the bottom of corresponding horizontal sliding cylinder
The other end be provided with a horizontal bumper bracket, the other end of two horizontal slide rods of unmanned plane back body is provided with another
Horizontal bumper bracket；Vertical buffer roll there are two being symmetrically arranged on the inside of each of described vertical bumper bracket, vertical buffer roll
Both ends be rotatably installed in the inside of vertical bumper bracket respectively；A level is rotatably equipped on each of described horizontal bumper bracket
Buffer roll；One end of the yielding rubber covering is fixed on the vertical buffer roll circumference of upper front, and the other end is fixed on
On the vertical buffer roll circumference of lower front side, the horizontal buffer roll of the front is located on the inside of yielding rubber covering, and and its
It is in contact；One end of another yielding rubber covering is fixed on the vertical buffer roll circumference on rear side of top, and the other end is fixed on
On the vertical buffer roll circumference of lower rearward side, the horizontal buffer roll at the rear portion is located on the inside of yielding rubber covering, and and its
It is in contact；One end of vertical bumper bracket is symmetrical arranged there are two wind spring, and one end of the wind spring is fixed on vertical bumper bracket,
The other end of each wind spring is connected with one end of a vertical buffer roll；Wind spring controls vertical buffer roll by spring force and revolves
Turn, yielding rubber covering is made to be in tensioning state always；When vertical sliding bar is to vertical sliding cylinder inner end sliding compression buffering elastic
When spring or horizontal slide rod are to horizontal sliding cylinder inner end sliding compression buffer spring, wind spring controls yielding rubber by spring force
The both ends of covering are wound in vertical buffer roll, so that yielding rubber covering be made to be in tensioning state；Two vertical bumper brackets
Outside is respectively arranged with a gas receiver, and the gas receiver is cylindrical body uncovered structure, and is covered by elastic film.
Further, ventilative in order to mitigate weight and realization, it is saturating that loss of weight is provided on two yielding rubber coverings
Stomata.
Beneficial effects of the present invention: the present invention realizes unmanned plane and unexpected pendant occurs by being provided with yielding rubber covering
Fall self-protection function when situation；It is sliding by setting vertical sliding cylinder and vertical sliding bar and horizontal sliding cylinder and level
Lever realizes the function of the multi-faceted protection of unmanned plane；The gas receiver covered by setting elastic film carries out unmanned plane more
It protects again.
Detailed description of the invention
Fig. 1 is integral installation distribution structure schematic diagram of the invention.
Fig. 2 is the integral installation distribution structure schematic diagram of another angle of the present invention.
Fig. 3 is the assembling structure schematic diagram after hidden parts part of the present invention.
Fig. 4 is the assembling structure schematic diagram after hidden parts part of the present invention.
Fig. 5 is the assembling structure schematic diagram of part in the present invention.
Drawing reference numeral: 1- unmanned plane main body, the horizontal sliding cylinder of 2-, 3- yielding rubber covering, the vertical bumper bracket of 4-, 5- elasticity
Film, 6- gas receiver, 7- vertical sliding cylinder, 8- wind spring, 9- horizontal slide rod, the horizontal buffer roll of 10-, the horizontal bumper bracket of 11-,
12- vertical sliding bar, the vertical buffer roll of 13-, 14- buffer spring.
Specific embodiment
The invention will be further described combined with specific embodiments below, in the illustrative examples and explanation of the invention
For explaining the present invention, but it is not as a limitation of the invention.
Embodiment is a kind of unmanned plane Shatter-resistant device of the invention, in unmanned plane as shown in figure 1, figure 2, figure 3, figure 4 and figure 5
There are two vertical sliding cylinders 7 for the installation of 1 Upper vertical of main body, while being symmetrically installed in 1 lower part of unmanned plane main body and sliding there are two vertical
Dynamic cylinder 7, four vertical sliding bars 12 are slidably mounted on respectively in four vertical sliding cylinders 7, each 12 end of vertical sliding bar with
Buffer spring 14 is provided between the bottom of corresponding vertical sliding cylinder 7, two, 1 top of unmanned plane main body vertical sliding bar 12
The other end is provided with a vertical bumper bracket 4, and the other end of the 1 two vertical sliding bars 12 in lower part of unmanned plane main body is provided with another
A vertical bumper bracket 4.
Horizontal sliding cylinder 2 there are two being horizontally mounted in 1 front of unmanned plane main body, at the same it is symmetrical at 1 rear portion of unmanned plane main body
There are two horizontal sliding cylinder 2, four horizontal slide rods 9 is slidably mounted in four horizontal sliding cylinders 2 respectively for installation, often
Buffer spring 14 is provided between a 9 end of horizontal slide rod and the bottom of corresponding horizontal sliding cylinder 2, before unmanned plane main body 1
The other end of two horizontal slide rods 9 in portion is provided with a horizontal bumper bracket 11, two, 1 rear portion of unmanned plane main body horizontal slide rod
9 other end is provided with another horizontal bumper bracket 11.The inside of each vertical bumper bracket 4 is symmetrically arranged that there are two vertical
Buffer roll 13, the both ends of vertical buffer roll 13 are rotatably installed in the inside of vertical bumper bracket 4 respectively.On each horizontal bumper bracket 11
It is rotatably equipped with a horizontal buffer roll 10.
One end of yielding rubber covering 3 is fixed on 13 circumference of vertical buffer roll of upper front, and the other end is fixed on down
On 13 circumference of vertical buffer roll on front side of portion, the horizontal buffer roll 10 of front is located at 3 inside of yielding rubber covering, and connects with it
Touching.One end of another yielding rubber covering 3 is fixed on 13 circumference of vertical buffer roll on rear side of top, and the other end is fixed on down
On 13 circumference of vertical buffer roll on rear side of portion, the horizontal buffer roll 10 at rear portion is located at 3 inside of yielding rubber covering, and connects with it
Touching.One end of vertical bumper bracket 4 is symmetrical arranged there are two wind spring 8, and one end of wind spring 8 is fixed on vertical bumper bracket 4, Mei Gejuan
The other end of spring 8 is connected with one end of a vertical buffer roll 13.Wind spring 8 controls vertical buffer roll 13 by spring force and revolves
Turn, makes yielding rubber covering 3 always in tensioning state.When vertical sliding bar 12 is slow to 7 inner end sliding compression of vertical sliding cylinder
When rushing spring 14 or horizontal slide rod 9 to horizontal 2 inner end sliding compression buffer spring 14 of sliding cylinder, wind spring 8 passes through spring force
The both ends of control yielding rubber covering 3 are wound in vertical buffer roll 13, so that yielding rubber covering 3 be made to be in tensioning state.
The outside of two vertical bumper brackets 4 is respectively arranged with a gas receiver 6, and the gas receiver 6 is cylindrical body uncovered structure, and is led to
Elastic film 5 is crossed to be covered.
Working principle of the present invention: the present invention is by the way that unmanned plane main body 1 to be placed into inside the present invention to realize protection
Unmanned plane, the purpose for preventing unmanned plane from breaking.When accidental falling occurs in unmanned plane, if unmanned plane falls straight down, pacify
The elastic film 5 of 6 end of gas receiver on the outside of vertical bumper bracket 4 ruptures after being hit, the compressed air in gas receiver 6
It quickly releases, to give 1 one upward oppositions of unmanned plane main body, mitigates the dynamics that a part of unmanned plane falls；When
It is vertical sliding by two after vertical bumper bracket 4 is hit when the dynamics that unmanned plane falls is not eliminated by gas receiver 6 completely
Lever 12 is slided to 7 inner end of vertical sliding cylinder, to compress buffer spring 14, realizes that buffering, the dynamics that unmanned plane is fallen are complete
Complete to offset, wind spring 8 is wound by the both ends that spring force controls yielding rubber covering 3 in vertical buffer roll 13 at this time, to make
Yielding rubber covering 3 remains tensioning state.When ground is fallen at the front of unmanned plane or rear portion, shatter-resistant cushioning principle is same
It is upper described.
Claims (2)
1. a kind of unmanned plane Shatter-resistant device, including unmanned plane main body (1), four vertical sliding cylinders (7) and four vertical sliding bars
(12), four horizontal sliding cylinders (2) and four horizontal slide rods (9), two vertical bumper brackets (4), two horizontal bumper brackets
(11), four vertical buffer rolls (13), two horizontal buffer rolls (10), two yielding rubber coverings (3), four wind springs (8), two
A gas receiver (6), it is characterised in that: in the installation of unmanned plane main body (1) Upper vertical, there are two vertical sliding cylinder (7), while
Unmanned plane main body (1) lower part is symmetrically installed there are two vertical sliding cylinder (7), and four vertical sliding bars (12) are slided respectively
Be mounted in four vertical sliding cylinders (7), each vertical sliding bar (12) end and the bottom of corresponding vertical sliding cylinder (7) it
Between be provided with buffer spring (14), the other end of the two vertical sliding bars (12) in unmanned plane main body (1) top be provided with one it is perpendicular
Straight bumper bracket (44), it is vertical slow that the other end of the two vertical sliding bars (12) in unmanned plane main body (1) lower part is provided with another
Rush frame 4；There are two being horizontally mounted in unmanned plane main body (1) front horizontal sliding cylinder (2), while at unmanned plane main body (1) rear portion
It is symmetrically installed there are two horizontal sliding cylinder (2), four horizontal slide rods (9) are slidably mounted on four horizontal slidings respectively
In cylinder (2), buffer spring is provided between each horizontal slide rod (9) end and the bottom of corresponding horizontal sliding cylinder (2)
(14), the other end of two horizontal slide rods (9) in unmanned plane main body (1) front is provided with a horizontal bumper bracket (11), nobody
The other end of two horizontal slide rods (9) in owner's body (1) rear portion is provided with another horizontal bumper bracket (11)；It is each of described perpendicular
There are two being symmetrically arranged on the inside of straight bumper bracket (4) vertical buffer roll (13), the both ends of vertical buffer roll (13) turn respectively
The dynamic inside for being mounted on vertical bumper bracket (4)；A horizontal buffering is rotatably equipped on each of described horizontal bumper bracket (11)
Roller (10)；One end of the yielding rubber covering (3) is fixed on vertical buffer roll (13) circumference of upper front, the other end
It is fixed on vertical buffer roll (13) circumference of lower front side, the horizontal buffer roll (10) of the front is located at yielding rubber illiteracy
On the inside of skin (3), and contact；One end of another yielding rubber covering (3) is fixed on the vertical buffer roll on rear side of top
(13) on circumference, the other end is fixed on vertical buffer roll (13) circumference of lower rearward side, the horizontal buffer roll at the rear portion
(10) it is located on the inside of yielding rubber covering (3), and contacts；It is rolled up there are two being symmetrical arranged one end of vertical bumper bracket (4)
Spring (8), one end of the wind spring (8) are fixed on vertical bumper bracket (4), and the other end of each wind spring (8) and one are vertical
One end of buffer roll (13) is connected；Wind spring (8) controls vertical buffer roll (13) rotation by spring force, makes rubber covering (3)
Always it is in tensioning state；When vertical sliding bar (12) to vertical sliding cylinder (7) inner end sliding compression buffer spring (14) or
When horizontal slide rod (9) is to horizontal sliding cylinder (2) inner end sliding compression buffer spring (14), wind spring (8) passes through spring force and controls
The both ends of yielding rubber covering (3) are wound on vertical buffer roll (13), so that yielding rubber covering (3) be made to be in tensioning shape
State；A gas receiver (6) is respectively arranged on the outside of two vertical bumper brackets (4), the gas receiver (6) is cylindrical body uncovered
Structure, and covered by elastic film (5).
2. a kind of unmanned plane Shatter-resistant device as described in claim 1, it is characterised in that: two yielding rubber coverings
(3) loss of weight air hole is provided on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710105139.6A CN106628210B (en) | 2017-02-25 | 2017-02-25 | A kind of unmanned plane Shatter-resistant device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710105139.6A CN106628210B (en) | 2017-02-25 | 2017-02-25 | A kind of unmanned plane Shatter-resistant device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106628210A CN106628210A (en) | 2017-05-10 |
| CN106628210B true CN106628210B (en) | 2019-01-08 |
Family
ID=58846793
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710105139.6A Active CN106628210B (en) | 2017-02-25 | 2017-02-25 | A kind of unmanned plane Shatter-resistant device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106628210B (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204250378U (en) * | 2014-10-27 | 2015-04-08 | 成都好飞机器人科技有限公司 | There are four rotor wing unmanned aerial vehicles of anti-collision protection device |
| CN205524973U (en) * | 2016-01-30 | 2016-08-31 | 周倜 | Aircraft buffer protection cover |
| CN205574291U (en) * | 2016-02-23 | 2016-09-14 | 周倜 | Double -deck aircraft protection device |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9725170B2 (en) * | 2013-06-11 | 2017-08-08 | Ecole Polytechnique Federale De Lausanne (Epfl) | Vertical take-off and landing aerial vehicle |
-
2017
- 2017-02-25 CN CN201710105139.6A patent/CN106628210B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204250378U (en) * | 2014-10-27 | 2015-04-08 | 成都好飞机器人科技有限公司 | There are four rotor wing unmanned aerial vehicles of anti-collision protection device |
| CN205524973U (en) * | 2016-01-30 | 2016-08-31 | 周倜 | Aircraft buffer protection cover |
| CN205574291U (en) * | 2016-02-23 | 2016-09-14 | 周倜 | Double -deck aircraft protection device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106628210A (en) | 2017-05-10 |
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| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181123 Address after: Room 608, Block J, Haitai Green Industrial Base, No. 6 Haitai Development Six Road, Huayuan Industrial Zone, Nankai District, Tianjin Applicant after: Tianjin Puxun Power Information Technology Co., Ltd. Applicant after: STATE GRID INFORMATION & TELECOMMUNICATION GROUP CO., LTD. Address before: 054999 Luzhai Township, Linxi County, Xingtai, Hebei Applicant before: Wei Ailing |
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| GR01 | Patent grant |