CN209617462U - A kind of remote sensing unmanned plane buffering landing - Google Patents
A kind of remote sensing unmanned plane buffering landing Download PDFInfo
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- CN209617462U CN209617462U CN201822272814.7U CN201822272814U CN209617462U CN 209617462 U CN209617462 U CN 209617462U CN 201822272814 U CN201822272814 U CN 201822272814U CN 209617462 U CN209617462 U CN 209617462U
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- fixedly connected
- unmanned plane
- bracket
- drone body
- remote sensing
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Abstract
The utility model discloses the remote sensing unmanned planes that one kind can buffer landing, including drone body and u-bracket, the drone body is located at the top of u-bracket, the two sides of the drone body, front and back are fixedly connected to support rod, the support rod is fixedly connected with vertical tube far from one end of drone body, the inner cavity of the vertical tube, which is fixed by the bracket, is connected with motor, is fixedly connected with flabellum at the top of the machine shaft.The utility model can make unmanned plane buffering landing; reduce the inertia of unmanned plane in descent; to carry out buffer protection to drone body internal part; extend the service life of unmanned plane; the bracket for solving remote sensing unmanned plane bottom during landing can make impact with the ground; bracket does not have pooling feature, causes unmanned plane inertia is excessive to be easy to damage internal part in knockout process, thus the problem of reducing remote sensing unmanned plane service life.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of remote sensing unmanned plane that can buffer landing.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer, compared with manned aircraft, nobody
Machine is often more suitable for the task of those too " slow-witted, dirty or dangerous ", and unmanned plane presses application field, can be divided into it is military with it is civilian,
Military aspect, unmanned plane are divided into reconnaissance plane and target drone, civilian aspect, and unmanned plane+industrial application is that unmanned plane has really just needed；
At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping,
The application in news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded unmanned plane itself
Purposes, developed country also actively extension industrial application and develop unmanned air vehicle technique.
The bracket of remote sensing unmanned plane bottom during landing can make impact with the ground, and bracket does not have pooling feature, hit
Cause unmanned plane inertia is excessive to be easy to damage internal part during hitting, to reduce the service life of remote sensing unmanned plane.
Utility model content
The purpose of this utility model is to provide the remote sensing unmanned planes that one kind can buffer landing, and the excellent of landing can be buffered by having
Point, the bracket for solving remote sensing unmanned plane bottom during landing can make impact with the ground, and bracket does not have pooling feature, hit
Cause unmanned plane inertia is excessive to be easy to damage internal part during hitting, to reduce asking for remote sensing unmanned plane service life
Topic.
To achieve the above object, the utility model provides the following technical solutions: one kind can buffer the remote sensing unmanned plane of landing,
Including drone body and u-bracket, the drone body is located at the top of u-bracket, the two sides of the drone body,
Front and back is fixedly connected to support rod, and the support rod is fixedly connected with vertical tube far from one end of drone body, institute
The inner cavity for stating vertical tube, which is fixed by the bracket, is connected with motor, is fixedly connected with flabellum at the top of the machine shaft, it is described nobody
The two sides of machine body bottom portion are fixedly connected to the first link block, and the bottom of first link block is connected with by shaft
Connecting rod, the one end of the connecting rod far from the first link block are connected with the second link block, the u-bracket by shaft
Inner cavity be fixedly connected with cross bar, the surface of the cross bar is arranged with casing and the first spring respectively, the top of described sleeve pipe with
The bottom of second link block is fixedly connected, and one end of first spring is fixedly connected with casing, first spring it is another
End is fixedly connected with the inner wall of u-bracket, signal receiver is fixedly connected at the top of the drone body, the signal connects
The output end of receipts device is two-way to be electrically connected with processor, and the input terminal of the processor is electrically connected with power module, the processor
The inner cavity of drone body is respectively positioned on power module, the power module is located at battery, the input of the signal receiver
End is electrically connected with signal projector, and the input terminal of the signal projector is electrically connected with remote control terminal.
Preferably, the bottom of the u-bracket inner cavity is fixedly connected with long tube, and the bottom of the long tube cavity is fixedly connected
There is second spring, vertical bar is fixedly connected at the top of the second spring, the outside of long tube is through at the top of the vertical bar simultaneously
It is fixedly connected with the bottom of drone body.
Preferably, the two sides of the long tube cavity offer sliding slot, and the bottom of the vertical bar two sides is fixedly connected to
Slide bar, the slide bar extend to the inner cavity of sliding slot far from one end of vertical bar and are connected with pulley, the pulley by shaft
Side far from slide bar is contacted with the inner wall of sliding slot.
Preferably, the bottom of the u-bracket is fixedly connected with cushion, and the inside of the cushion offers through-hole.
Compared with prior art, the beneficial effects of the utility model are as follows:
1, the utility model by drone body, u-bracket, support rod, vertical tube, motor, flabellum, the first link block,
Connecting rod, the second link block, cross bar, casing and the first spring are cooperated, and unmanned plane buffering can be made to land, in descent
Reduce the inertia of unmanned plane, to carry out buffer protection to drone body internal part, extend the service life of unmanned plane,
The bracket for solving remote sensing unmanned plane bottom during landing can make impact with the ground, and bracket does not have pooling feature, hit
Cause unmanned plane inertia is excessive to be easy to damage internal part in the process, to reduce asking for remote sensing unmanned plane service life
Topic.
2, the utility model is by long tube, second spring and vertical bar, can the bottom to drone body carry out buffering branch
Support, good buffer effect can be balanced support, to vertical bar by setting sliding slot, slide bar and pulley convenient for the vertical shifting of vertical bar
Dynamic, the setting of pulley reduces the frictional force between slide bar and sliding slot, can be to the bottom of u-bracket by the way that cushion is arranged
Buffer protection is carried out, it, can be with by setting signal receiver, processor, power module, signal projector and remote control terminal
Realize remote controlled unmanned machine.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 connects schematic cross-sectional view with second spring for the utility model long tube；
Fig. 3 connects schematic top plan view with support rod for the utility model structure drone body；
Fig. 4 is Tthe utility model system schematic diagram.
In figure: 1 drone body, 2U type bracket, 3 support rods, 4 vertical tubes, 5 motors, 6 flabellums, 7 first link blocks, 8 connect
Extension bar, 9 second link blocks, 10 cross bars, 11 casings, 12 first springs, 13 long tubes, 14 second springs, 15 vertical bars, 16 sliding slots, 17
It is slide bar, 18 pulleys, 19 cushions, 20 signal receivers, 21 processors, 22 power modules, 23 signal projectors, 24 long-range distant
Control terminal.
Specific embodiment
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
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-4, a kind of remote sensing unmanned plane buffering landing, including drone body 1 and u-bracket 2 are please referred to, nobody
Machine ontology 1 is located at the top of u-bracket 2, and the two sides of drone body 1, front and back are fixedly connected to support rod 3, branch
Strut 3 is fixedly connected with vertical tube 4 far from one end of drone body 1, and the inner cavity of vertical tube 4, which is fixed by the bracket, is connected with motor 5,
Flabellum 6 is fixedly connected at the top of 5 shaft of motor, the two sides of 1 bottom of drone body are fixedly connected to the first link block 7,
The bottom of first link block 7 is connected with connecting rod 8 by shaft, and connecting rod 8 passes through far from one end of the first link block 7
Shaft is connected with the second link block 9, and the inner cavity of u-bracket 2 is fixedly connected with cross bar 10, and the surface of cross bar 10 covers respectively
Equipped with casing 11 and the first spring 12, the top of casing 11 is fixedly connected with the bottom of the second link block 9, the first spring 12
One end is fixedly connected with casing 11, and the other end of the first spring 12 is fixedly connected with the inner wall of u-bracket 2,2 inner cavity of u-bracket
Bottom be fixedly connected with long tube 13, the bottom of 13 inner cavity of long tube is fixedly connected with second spring 14, the top of second spring 14
It is fixedly connected with vertical bar 15, the top of vertical bar 15 is through to the outside of long tube 13 and is fixedly connected with the bottom of drone body 1,
The two sides of 13 inner cavity of long tube offer sliding slot 16, and the bottom of 15 two sides of vertical bar is fixedly connected to slide bar 17, and slide bar 17 is separate
One end of vertical bar 15 extends to the inner cavity of sliding slot 16 and is connected with pulley 18 by shaft, pulley 18 far from slide bar 17 one
Side is contacted with the inner wall of sliding slot 16, and the bottom of u-bracket 2 is fixedly connected with cushion 19, and the inside of cushion 19 offers logical
Hole, the top of drone body 1 are fixedly connected with signal receiver 20, and the output end of signal receiver 20 is two-way to be electrically connected with place
Device 21 is managed, the input terminal of processor 21 is electrically connected with power module 22, and processor 21 and power module 22 are respectively positioned on unmanned plane sheet
The inner cavity of body 1, power module 22 are located at battery, and the input terminal of signal receiver 20 is electrically connected with signal projector 23, signal
The input terminal of transmitter 23 is electrically connected with remote control terminal 24, can be to nothing by long tube 13, second spring 14 and vertical bar 15
The bottom of man-machine ontology 1 carries out cushioning supportive, and good buffer effect can be to perpendicular by setting sliding slot 16, slide bar 17 and pulley 18
Bar 15 is balanced support, and convenient for the vertically movable of vertical bar 15, the setting of pulley 18 is reduced between slide bar 17 and sliding slot 16
Frictional force can carry out buffer protection to the bottom of u-bracket 2, pass through setting signal receiver by the way that cushion 19 is arranged
20, processor 21, power module 22, signal projector 23 and remote control terminal 24, may be implemented remote controlled unmanned machine,
Connected by drone body 1, u-bracket 2, support rod 3, vertical tube 4, motor 5, flabellum 6, the first link block 7, connecting rod 8, second
It connects block 9, cross bar 10, casing 11 and the first spring 12 to be cooperated, unmanned plane buffering landing can be made, reduce nothing in descent
Man-machine inertia extends the service life of unmanned plane to carry out buffer protection to 1 internal part of drone body, solves
The bracket of remote sensing unmanned plane bottom during landing can make impact with the ground, and bracket does not have pooling feature, knockout process
In cause unmanned plane inertia is excessive to be easy to damage internal part, thus the problem of reducing remote sensing unmanned plane service life.
In use, power module 22 provides electric energy for unmanned plane, remote control terminal 24 operates instruction of taking off and passes through signal
Transmitter 23 is sent to signal receiver 20, and signal receiver 20 sends instructions to processor 21, and processor 21 passes through motor 5
The shaft of operation, motor 5 drives flabellum 6 to rotate, and unmanned plane is made to take off, u-bracket 2 and ground face contact when unmanned plane lands, by
In inertia u-bracket 2 by upward power, drone body 1 is subject to downward force, and drone body 1 drives the first link block 7
It moves down, the first link block 7 pushes connecting rod 8 mobile, and the bottom of connecting rod 8 pushes the second link block 9 mobile, and second connects
It connects block 9 and squeezes the movement of the first spring 12, buffer shock-absorbing is carried out to unmanned plane by the first spring 12, while vertical bar 15 moves down
Second spring 14 is compressed, buffer shock-absorbing can also be carried out to drone body 1 by second spring 14.
In summary: this can buffer the remote sensing unmanned plane of landing, by drone body 1, u-bracket 2, support rod 3, erect
Pipe 4, motor 5, flabellum 6, the first link block 7, connecting rod 8, the second link block 9, cross bar 10, casing 11 and the first spring 12 carry out
Cooperation, the bracket for solving remote sensing unmanned plane bottom during landing can make impact with the ground, and bracket does not have pooling feature,
Cause unmanned plane inertia is excessive to be easy to damage internal part in knockout process, to reduce remote sensing unmanned plane service life
Problem.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (4)
1. one kind can buffer the remote sensing unmanned plane of landing, including drone body (1) and u-bracket (2), it is characterised in that: institute
The top that drone body (1) is located at u-bracket (2) is stated, the two sides of the drone body (1), front and back are fixed
It is connected with support rod (3), the support rod (3) is fixedly connected with vertical tube (4) far from the one end of drone body (1), described perpendicular
The inner cavity of pipe (4), which is fixed by the bracket, to be connected with motor (5), is fixedly connected with flabellum (6) at the top of motor (5) shaft,
The two sides of drone body (1) bottom are fixedly connected to the first link block (7), the bottom of first link block (7)
It is connected with connecting rod (8) by shaft, the connecting rod (8) passes through shaft activity far from the one end of the first link block (7)
It is connected with the second link block (9), the inner cavity of the u-bracket (2) is fixedly connected with cross bar (10), the surface of the cross bar (10)
It is arranged with casing (11) and the first spring (12) respectively, the top of described sleeve pipe (11) and the bottom of the second link block (9) are fixed
Connection, one end of first spring (12) are fixedly connected with casing (11), the other end of first spring (12) and U-shaped branch
The inner wall of frame (2) is fixedly connected, and is fixedly connected with signal receiver (20), the signal at the top of the drone body (1)
The output end of receiver (20) is two-way to be electrically connected with processor (21), and the input terminal of the processor (21) is electrically connected with power supply mould
Block (22), the processor (21) and power module (22) are respectively positioned on the inner cavity of drone body (1), the power module (22)
Positioned at battery, the input terminal of the signal receiver (20) is electrically connected with signal projector (23), the signal projector
(23) input terminal is electrically connected with remote control terminal (24).
2. the remote sensing unmanned plane that one kind according to claim 1 can buffer landing, it is characterised in that: the u-bracket (2)
The bottom of inner cavity is fixedly connected with long tube (13), and the bottom of long tube (13) inner cavity is fixedly connected with second spring (14), institute
It states and is fixedly connected at the top of second spring (14) vertical bar (15), the outside of long tube (13) is through at the top of the vertical bar (15)
And it is fixedly connected with the bottom of drone body (1).
3. the remote sensing unmanned plane that one kind according to claim 2 can buffer landing, it is characterised in that: in the long tube (13)
The two sides of chamber offer sliding slot (16), and the bottom of vertical bar (15) two sides is fixedly connected to slide bar (17), the slide bar
(17) one end far from vertical bar (15) extends to the inner cavity of sliding slot (16) and is connected with pulley (18), the cunning by shaft
Wheel (18) is contacted far from the side of slide bar (17) with the inner wall of sliding slot (16).
4. the remote sensing unmanned plane that one kind according to claim 1 can buffer landing, it is characterised in that: the u-bracket (2)
Bottom be fixedly connected with cushion (19), the inside of the cushion (19) offers through-hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822272814.7U CN209617462U (en) | 2018-12-29 | 2018-12-29 | A kind of remote sensing unmanned plane buffering landing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822272814.7U CN209617462U (en) | 2018-12-29 | 2018-12-29 | A kind of remote sensing unmanned plane buffering landing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209617462U true CN209617462U (en) | 2019-11-12 |
Family
ID=68448493
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822272814.7U Expired - Fee Related CN209617462U (en) | 2018-12-29 | 2018-12-29 | A kind of remote sensing unmanned plane buffering landing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209617462U (en) |
-
2018
- 2018-12-29 CN CN201822272814.7U patent/CN209617462U/en not_active Expired - Fee Related
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191112 Termination date: 20201229 |