CN207758989U - A kind of unmanned plane wing protective device - Google Patents
A kind of unmanned plane wing protective device Download PDFInfo
- Publication number
- CN207758989U CN207758989U CN201820084105.3U CN201820084105U CN207758989U CN 207758989 U CN207758989 U CN 207758989U CN 201820084105 U CN201820084105 U CN 201820084105U CN 207758989 U CN207758989 U CN 207758989U
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- China
- Prior art keywords
- unmanned plane
- wing
- bearing
- connecting rod
- connecting plate
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Abstract
The utility model discloses a kind of unmanned plane wing protective devices, including body assembly and guard assembly, the body assembly includes unmanned plane and connecting rod, the connecting rod is located above the right side of the unmanned plane, and it is welded and fixed with the unmanned plane, the unmanned plane is electrically connected with external power supply, the guard assembly includes wing, fender bracket, bearing and interior connecting plate, the bearing is located at the one end of the connecting rod far from the unmanned plane, and it is fixedly connected with the unmanned plane, the bottom surface of the bearing is fixedly installed the fender bracket, the wing is located at the upper surface of the bearing；If wing collides, increase the hardness of wing by protective plate, wing is avoided to damage, if unmanned plane lands, the bottom surface both side of unmanned plane is provided with cushioning supportive, spring is internally provided in buffering stand, if misoperation when landing, by shock bracket, the weight of itself when buffering unmanned plane lands offers convenience to user.
Description
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of unmanned plane wing protective device.
Background technology
Wing is one of important component of unmanned plane, is mounted on fuselage.Its main effect is to generate lift, in wing
On be also equipped with the wing flap for improving take-off and landing performance and aileron for aircraft lateral control, some is also filled in the leading edge of a wing
There is slat etc. to increase the device of lift.
Original unmanned plane wing protective device, unmanned plane are operated in lift-off when if colliding aerial flying bird or landing
It is improper, it is be easy to cause the damage of unmanned plane wing, property loss is brought to user.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane wing protective devices, to solve to carry in above-mentioned background technology
The original unmanned plane wing protective device gone out, unmanned plane is in lift-off, if misoperation when colliding aerial flying bird or landing,
The problem of be easy to causeing the damage of unmanned plane wing, property loss brought to user.
To achieve the above object, the utility model provides the following technical solutions：A kind of unmanned plane wing protective device, including
Body assembly and guard assembly, the body assembly include unmanned plane and connecting rod, and the connecting rod is located at the unmanned plane
It above right side, and is welded and fixed with the unmanned plane, the unmanned plane is electrically connected with external power supply, and the guard assembly includes
Wing, fender bracket, bearing and interior connecting plate, the bearing are located at the one end of the connecting rod far from the unmanned plane, and with it is described
Unmanned plane is fixedly connected, and the bottom surface of the bearing is fixedly installed the fender bracket, and the wing is located at the upper table of the bearing
Face, and be rotatablely connected with the bearing, the inside of the wing offers the first vessel, and the interior connecting plate is contained in described first
The inside of vessel, and be fixedly connected with the wing, the interior connecting plate includes protective plate and weighted plate, the inside of the interior connecting plate
The second vessel is offered, the protective plate is contained in the inside of second vessel, and is fixed with the madial wall of the interior connecting plate
Connection, the weighted plate is located at the upper surface of the interior connecting plate, and is fixedly connected with the interior connecting plate.
Preferably, the connecting rod quantity is four, and four connecting rods are symmetrically distributed in the cross of the unmanned plane
Section.
Preferably, the wing and the connecting rod are rotatablely connected by the bearing.
Preferably, the unmanned plane further includes having buffering stand, and the buffering stand quantity is two, two bufferings
Holder is symmetrically distributed at left and right sides of the bottom surface of the unmanned plane.
Preferably, the inside of the buffering stand offers third vessel, and external springs are contained in the third vessel
Inside, and be fixedly connected with the buffering stand.
Compared with prior art, the utility model has the beneficial effects that：It is internally provided with interior connecting plate in wing, if nobody
Machine is fixedly installed protective plate on the inside of interior connecting plate, if wing collides, increases wing by protective plate in lift-off
Hardness, avoid wing from damaging, if unmanned plane land, the bottom surface both side of unmanned plane is provided with cushioning supportive, buffering branch
Frame is internally provided with spring, if misoperation when landing, by shock bracket, and the weight of itself when buffering unmanned plane lands,
It offers convenience to user.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the wing structure schematic diagram in the utility model；
Fig. 3 is the interior link configuration schematic diagram in the utility model；
In figure：10- body assemblies, 11- unmanned planes, 12- buffering stands, 13- connecting rods, 20- guard assemblies, 21- wings,
22- fender brackets, 23- bearings, connecting plate, 241- protective plates, 242- weighted plates in 24-.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
- 3 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of unmanned plane wing protective device, including this
Body component 10 and guard assembly 20, body assembly 10 include unmanned plane 11 and connecting rod 13, and connecting rod 13 is located at unmanned plane 11
It above right side, and is welded and fixed with unmanned plane 11, unmanned plane 11 is electrically connected with external power supply, and guard assembly 20 includes wing
21, fender bracket 22, bearing 23 and interior connecting plate 24, bearing 23 are located at the one end of connecting rod 13 far from unmanned plane 11, and and unmanned plane
11 are fixedly connected, and the bottom surface of bearing 23 is fixedly installed fender bracket 22, and wing 21 is located at the upper surface of bearing 23, and with bearing 23
The inside of rotation connection, wing 21 offers the first vessel, and interior connecting plate 24 is contained in the inside of the first vessel, and solid with wing 21
Fixed connection, interior connecting plate 24 include protective plate 241 and weighted plate 242, and the inside of interior connecting plate 24 offers the second vessel, protective plate
241 are contained in the inside of the second vessel, and are fixedly connected with the madial wall of interior connecting plate 24, and weighted plate 242 is located at interior connecting plate 24
Upper surface, and be fixedly connected with interior connecting plate 24.
In the present embodiment, protective plate 241 is that high density material is increased if wing 21 collides by protective plate 241
The hardness of wing 21 avoids wing 21 from damaging.
In the present embodiment, unmanned plane 11 is placed into job site, because four connecting rods 13 are symmetrically distributed in nobody
The cross section of machine 11 so that in lifting, faster, wing 21 and connecting rod 13 are rotatablely connected speed unmanned plane 11 by bearing 23,
When wing 21 rotates, generates negative pressure and then unmanned plane 11 is driven to go up to the air, interior connecting plate 24 is internally provided in wing 21, if nobody
Machine 11 is fixedly installed protective plate 241 in the inside of interior connecting plate 24, if wing 21 collides, passes through protection in lift-off
Plate 241 increases the hardness of wing 21, and wing 21 is avoided to damage, if unmanned plane 11 lands, is set in the bottom surface both side of unmanned plane 11
It is equipped with cushioning supportive 12, spring is internally provided in buffering stand 12, it is slow by shock bracket 12 if misoperation when landing
The weight of itself when unmanned plane 11 lands is rushed, is offered convenience to user.
Further, 13 quantity of connecting rod is four, and four connecting rods 13 are symmetrically distributed in the cross section of unmanned plane 11.
In the present embodiment, 13 quantity of connecting rod is four, and four connecting rods 13 are symmetrically distributed in the transversal of unmanned plane 11
Face so that unmanned plane 11 lifting when speed faster.
Further, wing 21 and connecting rod 13 are rotatablely connected by bearing 23.
In the present embodiment, wing 21 and connecting rod 13 are rotatablely connected by bearing 23, wing 21 rotate when, generate negative pressure into
And unmanned plane 11 is driven to go up to the air.
Further, unmanned plane 11 further includes having buffering stand 12, and 12 quantity of buffering stand is two, two buffering stands
12 are symmetrically distributed at left and right sides of the bottom surface of unmanned plane 11.
In the present embodiment, if unmanned plane 11 lands, the bottom surface both side of unmanned plane 11 is provided with cushioning supportive 12, slow
That rushes holder 12 is internally provided with spring, if misoperation when landing, is buffered when unmanned plane 11 lands certainly by shock bracket 12
The weight of body, offers convenience to user.
Further, the inside of buffering stand 12 offers third vessel, and external springs are contained in the inside of third vessel,
And it is fixedly connected with buffering stand 12.
In the present embodiment, it is internally provided with spring in buffering stand 12, if misoperation when landing, passes through shock bracket
The weight of itself when 12 buffering unmanned planes 11 land, offers convenience to user.
The operation principle and process for using of the utility model：After the utility model installs, accumulator is placed into nothing
Unmanned plane 11 is placed into job site by man-machine 11 inside, because four connecting rods 13 are symmetrically distributed in the cross of unmanned plane 11
Section so that faster, wing 21 and connecting rod 13 are rotatablely connected speed unmanned plane 11 by bearing 23,21 turns of wing in lifting
When dynamic, generate negative pressure and then unmanned plane 11 is driven to go up to the air, interior connecting plate 24 is internally provided in wing 21, if unmanned plane 11 is rising
When empty, it is fixedly installed protective plate 241 in the inside of interior connecting plate 24, if wing 21 collides, is increased by protective plate 241
The hardness of wing 21 avoids wing 21 from damaging, if unmanned plane 11 lands, the bottom surface both side of unmanned plane 11 is provided with buffering branch
Support 12, spring is internally provided in buffering stand 12, if misoperation when landing, unmanned plane 11 is buffered by shock bracket 12
The weight of itself, offers convenience to user when landing, and after completing work, whether the wing 21 of regular price differential unmanned plane 11 occurs
Damage, so that unmanned plane 11 is used for a long time.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of unmanned plane wing protective device, it is characterised in that：Including body assembly（10）And guard assembly（20）, described
Body component（10）Including unmanned plane（11）And connecting rod（13）, the connecting rod（13）Positioned at the unmanned plane（11）Right side on
Side, and with the unmanned plane（11）It is welded and fixed, the unmanned plane（11）It is electrically connected with external power supply, the guard assembly
（20）Including wing（21）, fender bracket（22）, bearing（23）With interior connecting plate（24）, the bearing（23）Positioned at the connecting rod
（13）Far from the unmanned plane（11）One end, and with the unmanned plane（11）It is fixedly connected, the bearing（23）Bottom surface it is solid
Surely it is provided with the fender bracket（22）, the wing（21）Positioned at the bearing（23）Upper surface, and with the bearing（23）
Rotation connection, the wing（21）Inside offer the first vessel, the interior connecting plate（24）It is contained in first vessel
Inside, and with the wing（21）It is fixedly connected, the interior connecting plate（24）Including protective plate（241）And weighted plate（242）, described
Interior connecting plate（24）Inside offer the second vessel, the protective plate（241）Be contained in the inside of second vessel, and with institute
State interior connecting plate（24）Madial wall be fixedly connected, the weighted plate（242）Positioned at the interior connecting plate（24）Upper surface, and with institute
State interior connecting plate（24）It is fixedly connected.
2. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that：The connecting rod（13）Quantity
It is four, four connecting rods（13）It is symmetrically distributed in the unmanned plane（11）Cross section.
3. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that：The wing（21）With it is described
Connecting rod（13）Pass through the bearing（23）Rotation connection.
4. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that：The unmanned plane（11）Also wrap
Buffering stand is included（12）, the buffering stand（12）Quantity is two, two buffering stands（12）It is symmetrically distributed in
The unmanned plane（11）Bottom surface at left and right sides of.
5. a kind of unmanned plane wing protective device according to claim 4, it is characterised in that：The buffering stand（12）'s
Inside offers third vessel, and external springs are contained in the inside of the third vessel, and with the buffering stand（12）It is fixed
Connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820084105.3U CN207758989U (en) | 2018-01-18 | 2018-01-18 | A kind of unmanned plane wing protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820084105.3U CN207758989U (en) | 2018-01-18 | 2018-01-18 | A kind of unmanned plane wing protective device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207758989U true CN207758989U (en) | 2018-08-24 |
Family
ID=63180814
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820084105.3U Expired - Fee Related CN207758989U (en) | 2018-01-18 | 2018-01-18 | A kind of unmanned plane wing protective device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207758989U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979704A (en) * | 2019-11-07 | 2020-04-10 | 刘创 | Logistics distribution unmanned aerial vehicle |
| CN111559503A (en) * | 2020-05-27 | 2020-08-21 | 鑫亿智慧科技有限公司 | Unmanned aerial vehicle body temperature measuring device and method for smart city |
-
2018
- 2018-01-18 CN CN201820084105.3U patent/CN207758989U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979704A (en) * | 2019-11-07 | 2020-04-10 | 刘创 | Logistics distribution unmanned aerial vehicle |
| CN110979704B (en) * | 2019-11-07 | 2021-08-20 | 陕西蓝天上航空俱乐部有限公司 | Logistics distribution unmanned aerial vehicle |
| CN111559503A (en) * | 2020-05-27 | 2020-08-21 | 鑫亿智慧科技有限公司 | Unmanned aerial vehicle body temperature measuring device and method for smart city |
| CN111559503B (en) * | 2020-05-27 | 2022-07-01 | 鑫亿智慧科技有限公司 | Unmanned aerial vehicle body temperature measuring device and method for smart city |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180824 Termination date: 20200118 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |