CN206766371U - A kind of fixed-wing unmanned plane auxiliary takeoff apparatus - Google Patents
A kind of fixed-wing unmanned plane auxiliary takeoff apparatus Download PDFInfo
- Publication number
- CN206766371U CN206766371U CN201720642661.3U CN201720642661U CN206766371U CN 206766371 U CN206766371 U CN 206766371U CN 201720642661 U CN201720642661 U CN 201720642661U CN 206766371 U CN206766371 U CN 206766371U
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- fixed
- unmanned plane
- block
- baffle plate
- fix bar
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Abstract
The utility model discloses a kind of fixed-wing unmanned plane auxiliary takeoff apparatus, including two carrying platforms be arrangeding in parallel, the upper surface of each carrying platform is inclined plane, the side of each carrying platform is equipped with some holders, fixed cover block is equipped with the relative side side wall of two carrying platforms, each relative side of the fixed cover block is inserted with inserted block, connected between two inserted blocks by a rotating bar being vertically arranged, unmanned plane is provided between the upside of two carrying platforms, fixed block is equipped with the bottom incline of the carrying platform, the upper end of each fixed block is equipped with fix bar, the each one end of the fix bar away from fixed block is equipped with the connecting rod vertical with fix bar.The utility model is simple in construction, is easy to use quick, by the setting of carrying platform can unmanned plane adapt to a variety of landform, facilitate Assisted Take Off.
Description
Technical field
It the utility model is related to unmanned plane auxiliary takeoff apparatus technical field, more particularly to a kind of fixed-wing unmanned plane auxiliary
Launching apparatus.
Background technology
Fixed-wing unmanned plane, it is that wing outer end angle of sweep can be with a kind of nothing for the wing fixation that speed automatic or manual adjusts
It is man-machine.Blackhawk, wasp series fixed-wing UAS are developed by the carbon-based company in Taiwan, because of its excellent performance, modularization collection
Into, the industries such as mapping, geology, oil, agricultural have been widely used at present, and there is wide market application foreground, at present,
Fixed-wing unmanned plane needs certain speed when taking off, as still using by the way of routinely taking off, pair with often each
It is impossible for the unmanned plane of kind landform operation, so having expedited the emergence of various forms of takeoff auxiliary devices.
Utility model content
The purpose of this utility model be in order to solve shortcoming present in prior art, and a kind of fixed-wing proposed nobody
Machine auxiliary takeoff apparatus.
To achieve these goals, the utility model employs following technical scheme：
A kind of fixed-wing unmanned plane auxiliary takeoff apparatus, including two carrying platforms be arrangeding in parallel, each carrying
The upper surface of platform is inclined plane, and the side of each carrying platform is equipped with some holders, and two carryings are flat
Fixed cover block is equipped with the relative side side wall of platform, each relative side of the fixed cover block is inserted with inserted block, two
Connected between the inserted block by a rotating bar being vertically arranged, nobody is provided between the upside of two carrying platforms
Machine, fixed block is equipped with the bottom incline of the carrying platform, the upper end of each fixed block is equipped with fix bar, each
The one end of the fix bar away from fixed block is equipped with the connecting rod vertical with fix bar, the connecting rod away from fix bar one
End is connected with baffle plate by rotary shaft, and the baffle plate is provided with the first spring close to the side of connecting rod, and is set on the downside of connecting rod
There is the first contiguous block being connected with the first spring, connected between the baffle plate and fix bar by rotating kelly, the carrying is flat
The upper surface of platform is additionally provided with the second contiguous block, is arranged with second spring on second contiguous block, under the unmanned airplane empennage
Side is provided with the hook that radian is 90 °, and the other end of second spring connects with hook.
Preferably, the baffle plate is provided with rubber blanket close to the side of fix bar, and the side wall of the baffle plate is provided with fixture block, and
Rotate kelly and be provided with some necks to match with fixture block.
Preferably, shift(ing) ring is arranged with the hook, and the end of second spring is connected with shift(ing) ring.
Preferably, the baffle plate setting is in side of the unmanned plane host wing away from fixed block.
Preferably, two symmetrical shifting rollers are equipped with the downside of each carrying platform.
Preferably, the rotation kelly is made up of vulcanie.
In the utility model, when using the device, unmanned plane is placed on carrying platform, blocked by baffle plate
Host wing, progress is spacing, pulls down unmanned plane by the effect of the first contiguous block and the first spring, then drives the second bullet
Spring drawstring, the neck rotated on kelly snaps on fixture block baffle plate and unmanned plane is fixed, when being pressed onto to a certain degree,
It can will rotate kelly to take away from fixture block, one elastic force of aircraft, Assisted Take Off be given under the elastic reaction of spring, and carry
Platform is the structure that can be extended, and is adapted to different size of unmanned plane, the utility model is simple in construction, is easy to use
Fast, by the setting of carrying platform can unmanned plane adapt to a variety of landform, facilitate Assisted Take Off.
Brief description of the drawings
Fig. 1 be the utility model proposes a kind of fixed-wing unmanned plane auxiliary takeoff apparatus structural representation；
Fig. 2 be the utility model proposes a kind of fixed-wing unmanned plane auxiliary takeoff apparatus carrying platform side view.
In figure：1 carrying platform, 2 fixed blocks, 3 unmanned planes, 4 fix bars, 5 connecting rods, 6 rotate kellies, 7 first contiguous blocks,
8 rotary shafts, 9 baffle plates, 10 first springs, 11 shifting rollers, 12 hooks, 13 second springs, 14 second contiguous blocks, 15 holders,
16 fixed cover blocks, 17 inserted blocks, 18 rotating bars.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.
Reference picture 1-2, a kind of fixed-wing unmanned plane auxiliary takeoff apparatus, including two carrying platforms 1 be arrangeding in parallel, often
The upper surface of individual carrying platform 1 is inclined plane, and the side of each carrying platform 1 is equipped with some holders 15, two carryings
Fixed cover block 16 is equipped with the relative side side wall of platform 1, the relative side of each fixed cover block 16 is inserted with inserted block 17,
Connected between two inserted blocks 17 by a rotating bar being vertically arranged 18, nobody is provided between the upside of two carrying platforms 1
Machine 3, fixed block 2 is equipped with the bottom incline of carrying platform 1, the upper end of each fixed block 2 is equipped with fix bar 4, Mei Gegu
The one end of fixed pole 4 away from fixed block 2 is equipped with the connecting rod 5 vertical with fix bar 4, and the one end of connecting rod 5 away from fix bar 4 leads to
Cross rotary shaft 8 and be connected with baffle plate 9, baffle plate 9 is provided with the first spring 10 close to the side of connecting rod 5, and the downside of connecting rod 5 is provided with
The first contiguous block 7 being connected with the first spring 10, is connected between baffle plate 9 and fix bar 4 by rotating kelly 6, and the rotation
Kelly 6 is made up of vulcanie, both the effect with clamping, and again convenient to rotate, the upper surface of carrying platform 1 is additionally provided with the second company
Block 14 is connect, second spring 13 is arranged with the second contiguous block 14, the downside of the empennage of unmanned plane 3 is provided with the hook 12 that radian is 90 °,
And the other end of second spring 13 12 is connected with hook, baffle plate 9 is provided with rubber blanket close to the side of fix bar 4, and rubber blanket can be with
The wing of unmanned plane 3 is protected, the side wall of baffle plate 9 is provided with fixture block, and rotates kelly 6 and be provided with what is matched with fixture block
Some necks, link up with and be arranged with shift(ing) ring on 12, and the end of second spring 13 is connected with shift(ing) ring, baffle plate 9 is arranged on nobody
Side of the host wing of machine 3 away from fixed block 2, the downside of each carrying platform 1 are equipped with two symmetrical shifting rollers 11.
In the utility model, when using the device, unmanned plane is placed on carrying platform 1, kept off by baffle plate 9
Firmly host wing, progress is spacing, pulls down unmanned plane 3 by the effect of the first contiguous block 7 and the first spring 10, then drives
The drawstring of second spring 13, the neck rotated on kelly 6 snap on fixture block baffle plate 9 and unmanned plane 3 are fixed, certain when being pressed onto
When degree, it can will rotate kelly 6 and be taken away from fixture block, one elastic force of aircraft is given under the elastic reaction of spring, is aided in
Take off, and the setting of 90 ° of hook 12 and shift(ing) ring avoids the risk that hook 12 is tangled, and does not interfere with unmanned plane 3
Take off, and carrying platform 1 is the structure that can be extended, and is adapted to different size of unmanned plane.
It is described above, the only preferable embodiment of the utility model, but the scope of protection of the utility model is not
This is confined to, any one skilled in the art is in the technical scope that the utility model discloses, according to this practicality
New technical scheme and its utility model design are subject to equivalent substitution or change, should all cover in protection model of the present utility model
Within enclosing.
Claims (6)
1. a kind of fixed-wing unmanned plane auxiliary takeoff apparatus, including two carrying platforms (1) be arrangeding in parallel, it is characterised in that
The upper surface of each carrying platform (1) is inclined plane, and the side of each carrying platform (1) is equipped with some placements
Box (15), fixed cover block (16) is equipped with the relative side side wall of two carrying platforms (1), each fixed cover block
(16) relative side is inserted with inserted block (17), passes through a rotating bar being vertically arranged between two inserted blocks (17)
(18) connect, unmanned plane (3), the bottom incline of the carrying platform (1) are provided between the upside of two carrying platforms (1)
On be equipped with fixed block (2), the upper end of each fixed block (2) is equipped with fix bar (4), and each fix bar (4) is remote
One end from fixed block (2) is equipped with the connecting rod (5) vertical with fix bar (4), and the connecting rod (5) is away from fix bar (4)
One end baffle plate (9) is connected with by rotary shaft (8), the baffle plate (9) is provided with the first spring close to the side of connecting rod (5)
(10), and the downside of connecting rod (5) is provided with the first contiguous block (7) for be connected with the first spring (10), the baffle plate (9) and fixation
Connected between bar (4) by rotating kelly (6), the upper surface of the carrying platform (1) is additionally provided with the second contiguous block (14), described
Second spring (13) is arranged with second contiguous block (14), the downside of unmanned plane (3) empennage is provided with the hook that radian is 90 °
(12), and the other end of second spring (13) is connected with hook (12).
A kind of 2. fixed-wing unmanned plane auxiliary takeoff apparatus according to claim 1, it is characterised in that the baffle plate (9)
Rubber blanket is provided with close to the side of fix bar (4), the side wall of the baffle plate (9) is provided with fixture block, and rotates kelly (6) and be provided with
Some necks to match with fixture block.
A kind of 3. fixed-wing unmanned plane auxiliary takeoff apparatus according to claim 1, it is characterised in that the hook (12)
On be arranged with shift(ing) ring, and the end of second spring (13) is connected with shift(ing) ring.
A kind of 4. fixed-wing unmanned plane auxiliary takeoff apparatus according to claim 1, it is characterised in that the baffle plate (9)
It is arranged on side of unmanned plane (3) host wing away from fixed block (2).
A kind of 5. fixed-wing unmanned plane auxiliary takeoff apparatus according to claim 1, it is characterised in that each carrying
Two symmetrical shifting rollers (11) are equipped with the downside of platform (1).
A kind of 6. fixed-wing unmanned plane auxiliary takeoff apparatus according to claim 1, it is characterised in that the rotation kelly
(6) it is made up of vulcanie.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720642661.3U CN206766371U (en) | 2017-06-05 | 2017-06-05 | A kind of fixed-wing unmanned plane auxiliary takeoff apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720642661.3U CN206766371U (en) | 2017-06-05 | 2017-06-05 | A kind of fixed-wing unmanned plane auxiliary takeoff apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206766371U true CN206766371U (en) | 2017-12-19 |
Family
ID=60635860
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720642661.3U Expired - Fee Related CN206766371U (en) | 2017-06-05 | 2017-06-05 | A kind of fixed-wing unmanned plane auxiliary takeoff apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206766371U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111717409A (en) * | 2020-06-23 | 2020-09-29 | 长沙航华电子科技有限公司 | High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle |
-
2017
- 2017-06-05 CN CN201720642661.3U patent/CN206766371U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111717409A (en) * | 2020-06-23 | 2020-09-29 | 长沙航华电子科技有限公司 | High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle |
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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: 20171219 Termination date: 20180605 |