CN107284681A - A kind of shockproof unmanned plane of anticollision - Google Patents
A kind of shockproof unmanned plane of anticollision Download PDFInfo
- Publication number
- CN107284681A CN107284681A CN201710600409.0A CN201710600409A CN107284681A CN 107284681 A CN107284681 A CN 107284681A CN 201710600409 A CN201710600409 A CN 201710600409A CN 107284681 A CN107284681 A CN 107284681A
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- China
- Prior art keywords
- flap
- rotating shaft
- torque spring
- unmanned plane
- adjacent
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- 239000012528 membrane Substances 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims 1
- 230000003139 buffering effect Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Vibration Dampers (AREA)
Abstract
The invention discloses a kind of shockproof unmanned plane of anticollision, including body, body both sides left and right ends have been fixedly connected with connecting plate, two adjacent connecting plates are rotatably connected to same first rotating shaft, the equal movable sleeve in first rotating shaft left and right ends is connected to the first flap, two adjacent first flap opposite sides are equipped with the second flap, and two equal pivot bush units of the second flap are in first rotating shaft.The present invention is cased with the first flap, the second flap by setting in first rotating shaft, three is connected with each other by the first torque spring, the second torque spring, the 3rd torque spring simultaneously, make the first flap, the second flap in the case where being hit, with certain elastic deformability, it is to avoid body is directly damaged；The elastic flap of body both sides is connected as one by setting resilient sleeve, makes to be wrapped in elastic device support body on the outside of body, makes body avoid, directly with ground contact, buffering certain inertial impact force, improving body service life when landing.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, the shockproof unmanned plane of specially a kind of anticollision.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated, or fully or intermittently independently operated by car-mounted computer.With someone
Drive an airplane and compare, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane presses application field,
Can be divided into it is military with it is civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application is
Unmanned plane has really just been needed；At present taking photo by plane, agricultural, plant protection, miniature auto heterodyne, express transportation, disaster relief, observe wild move
The application in thing, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
Big has expanded the purposes of unmanned plane in itself, and developed country is also in actively extension sector application and development unmanned air vehicle technique.
Unmanned plane in the process of moving, by its external environment condition travelled not can determine that, in operation may by unmanned plane
It can be collided by outside material object, under the protection of unshielded device, unmanned plane is likely to greatly be damaged；While nothing
Man-machine when dropping to ground, body directly rushes at ground under effect of inertia, it is easy to damage body, and influence body is used
Life-span, in consideration of it, the present invention proposes that a kind of shockproof unmanned plane of anticollision solves the above problems.
The content of the invention
It is an object of the invention to provide a kind of shockproof unmanned plane of anticollision, with asking for solving to propose in above-mentioned background technology
Topic.
To achieve the above object, the present invention provides following technical scheme：A kind of shockproof unmanned plane of anticollision, including body,
Body both sides left and right ends have been fixedly connected with connecting plate, and two adjacent connecting plates are rotatably connected to same first turn
Axle, the equal movable sleeve in first rotating shaft left and right ends is connected to the first flap, and two adjacent first flap opposite sides are equipped with
Two flaps, two equal pivot bush units of the second flap are in first rotating shaft, and first flap, the second flap are away from adjacent first
One end of rotating shaft, which is run through, the second rotating shaft, and the second rotating shaft extends laterally, and one end of the second rotating shaft extension, which is rotated, to be connected
The 3rd flap is connected to, same elastic membrane is fixedly connected with four the 3rd flaps of homonymy, the 3rd flap is away from phase
Second adjacent rotating shaft one end detachable interposing is connected to inflatable cover, and two relative inflatable covers of homonymy are connected with same resilient sleeve, and bullet
Property set and elastic membrane set in vertical direction.
It is preferred that, the first torque spring is socketed with the first rotating shaft, the first torque spring two ends are fixed respectively
In in first rotating shaft and the second flap.
It is preferred that, the second torque spring is socketed with the first rotating shaft, the second torque spring two ends are fixed respectively
In on the first flap and the second flap adjacent thereto.
It is preferred that, the 3rd torque spring is socketed with the first rotating shaft, the 3rd torque spring two ends are fixed respectively
In in first rotating shaft and the first flap.
It is preferred that, back-moving spring is provided with the resilient sleeve, the back-moving spring two ends are individually fixed in adjacent with its
On inflatable cover.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention is rational in infrastructure, practical, with following excellent
Point：
1. the first flap, the second flap are cased with first rotating shaft by setting, while passing through the first torque spring, the second torsion
Three is connected with each other by spring, the 3rd torque spring, makes the first flap, the second flap in the case where being hit, with one
Fixed elastic deformability, it is to avoid body is directly damaged；
2. connecting as one the elastic flap of body both sides by setting resilient sleeve, make to be wrapped in elastic device on the outside of body
In support body, body is set to avoid, directly with ground contact, buffering certain inertial impact force, improving the use longevity of body when landing
Life.
Brief description of the drawings
Fig. 1 is cross-sectional view of the present invention；
Fig. 2 is first rotating shaft of the present invention and two flap attachment structure schematic diagrams.
In figure：1 body, 2 connecting plates, 3 first rotating shafts, 4 first flaps, 5 second flaps, 6 elastic membranes, 7 the 3rd flaps, 8
Inflatable cover, 9 resilient sleeves, 10 back-moving springs, 11 first torque springs, 12 second torque springs, 13 the 3rd torque springs, 14 second
Rotating shaft.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Fig. 1-2 is referred to, the present invention provides a kind of technical scheme：A kind of shockproof unmanned plane of anticollision, including body 1, machine
The both sides left and right ends of body 1 have been fixedly connected with connecting plate 2, and two adjacent connecting plates 2 are rotatably connected to same first rotating shaft 3,
The equal movable sleeve in the left and right ends of first rotating shaft 3 is connected to the first flap 4, and two adjacent opposite sides of first flap 4 are equipped with second turn
Plate 5, two equal pivot bush units of the second flap 5 are in first rotating shaft 3, being socketed with the first torque spring 11, first in first rotating shaft 3
The two ends of torque spring 11 are individually fixed on the flap 5 of first rotating shaft 3 and second, and the second torque spring is socketed with first rotating shaft 3
12, the two ends of the second torque spring 12 be individually fixed in the first flap 4 and the second flap 5 adjacent thereto on, in first rotating shaft 3 cover
The 3rd torque spring 12 is connected to, the two ends of the 3rd torque spring 12 are individually fixed on the flap 4 of first rotating shaft 3 and first, in body 1
When being hit, the elastic support body that the outside of body 1 is provided with ensures certain bumper and absorbing shock ability, the first flap 4, the second flap 5
One end away from adjacent first rotating shaft 3, which is run through, the second rotating shaft 14, and the second rotating shaft 14 extends laterally, the second rotating shaft 14
One end of extension is rotatably connected to the 3rd flap 7, and same elastic membrane 6 is fixedly connected with four the 3rd flaps 7 of homonymy,
3rd flap 7 is connected to inflatable cover 8 away from the adjacent one end detachable interposing of the second rotating shaft 14, and two relative inflatable covers 8 of homonymy connect
Same resilient sleeve 9 is connected to, and resilient sleeve 9 and elastic membrane 6 are set in vertical direction, and back-moving spring 10 is provided with resilient sleeve 9, are resetted
The two ends of spring 10 are individually fixed on the inflatable cover 8 adjacent with its, are improved the elastic performance of the elastic support body of body 1, are improved it
The effect of damping anticollision.
Operation principle：The first flap 4, the second flap 5 are cased with first rotating shaft 3 by setting, while passing through the first torsion bullet
Three is connected with each other by spring 12, the second torque spring 13, the 3rd torque spring 14, make the first flap 4, the second flap 5 by
In the case of shock, with certain elastic deformability, it is to avoid body 1 is directly damaged；By setting resilient sleeve 9 by body
The elastic flap of 1 both sides is connected as one, and the outside of body 1 is wrapped in elastic device support body, is avoided when body 1 is landed straight
Connect with ground contact, buffer certain inertial impact force.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of changes, modification can be carried out to these embodiments, replace without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (5)
1. a kind of shockproof unmanned plane of anticollision, including body (1), it is characterised in that：Body (1) the both sides left and right ends are solid
Surely connecting plate (2) is connected with, two adjacent connecting plates (2) are rotatably connected to same first rotating shaft (3), the first rotating shaft
(3) the equal movable sleeve in left and right ends is connected to the first flap (4), and two adjacent first flap (4) opposite sides are equipped with the second flap
(5), two the second flap (5) pivot bush units are in first rotating shaft (3), and first flap (4), the second flap (5) are remote
One end of adjacent first rotating shaft (3), which is run through, the second rotating shaft (14), and the second rotating shaft (14) extends laterally, and described second
One end of rotating shaft (14) extension is rotatably connected to the 3rd flap (7), is fixedly connected with four the 3rd flaps (7) of homonymy
Same elastic membrane (6), the 3rd flap (7) is connected to inflatable cover (8) away from adjacent the second rotating shaft (14) one end detachable interposing,
Two relative inflatable covers (8) of homonymy are connected with same resilient sleeve (9), and resilient sleeve (9) and elastic membrane (6) are set in vertical direction
Put.
2. a kind of shockproof unmanned plane of anticollision according to claim 1, it is characterised in that：Covered on the first rotating shaft (3)
The first torque spring (11) is connected to, the first torque spring (11) two ends are individually fixed in first rotating shaft (3) and the second flap
(5) on.
3. a kind of shockproof unmanned plane of anticollision according to claim 1, it is characterised in that：Covered on the first rotating shaft (3)
The second torque spring (12) is connected to, the second torque spring (12) two ends are individually fixed in the first flap (4) and adjacent thereto
The second flap (5) on.
4. a kind of shockproof unmanned plane of anticollision according to claim 3, it is characterised in that：Covered on the first rotating shaft (3)
The 3rd torque spring (12) is connected to, the 3rd torque spring (12) two ends are individually fixed in first rotating shaft (3) and the first flap
(4) on.
5. a kind of shockproof unmanned plane of anticollision according to claim 3, it is characterised in that：It is provided with the resilient sleeve (9)
Back-moving spring (10), back-moving spring (10) two ends are individually fixed on the inflatable cover adjacent with its (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710600409.0A CN107284681A (en) | 2017-07-21 | 2017-07-21 | A kind of shockproof unmanned plane of anticollision |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710600409.0A CN107284681A (en) | 2017-07-21 | 2017-07-21 | A kind of shockproof unmanned plane of anticollision |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107284681A true CN107284681A (en) | 2017-10-24 |
Family
ID=60102027
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710600409.0A Withdrawn CN107284681A (en) | 2017-07-21 | 2017-07-21 | A kind of shockproof unmanned plane of anticollision |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107284681A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108327910A (en) * | 2018-03-31 | 2018-07-27 | 苏州声婉智能科技有限公司 | A kind of agricultural plant protection drone |
-
2017
- 2017-07-21 CN CN201710600409.0A patent/CN107284681A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108327910A (en) * | 2018-03-31 | 2018-07-27 | 苏州声婉智能科技有限公司 | A kind of agricultural plant protection drone |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20171024 |
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| WW01 | Invention patent application withdrawn after publication |