CN206141831U - Unmanned aerial vehicle buffering protection device - Google Patents
Unmanned aerial vehicle buffering protection device Download PDFInfo
- Publication number
- CN206141831U CN206141831U CN201620859058.6U CN201620859058U CN206141831U CN 206141831 U CN206141831 U CN 206141831U CN 201620859058 U CN201620859058 U CN 201620859058U CN 206141831 U CN206141831 U CN 206141831U
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- CN
- China
- Prior art keywords
- buffer protection
- unmanned plane
- aerial vehicle
- unmanned aerial
- umbrella
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
The utility model discloses an unmanned aerial vehicle buffering protection device, include unmanned aerial vehicle, buffer protection case, buffering and decelerating umbrella, timer and subtract the gravity umbrella, unmanned aerial vehicle's upper end is provided with the buffer protection case, the inside of buffer protection case is provided with drag parachute parcel case and subtracts the gravity pack wraps up in the case, drag parachute parcel case is installed in the rear end of buffer protection case, and just the buffering and decelerating umbrella is being placed to inside the compression, subtracting the gravity pack and wrapping up in the upper end that the buffer protection case was being installed to the case, just inside is compressed placing and is subtracted the gravity umbrella, the one side that subtracts the gravity umbrella is provided with and subtracts the gravity switch, it passes through the wire and is connecting the timer to subtract the gravity switch, the utility model discloses can cushion unmanned aerial vehicle's impulsive force when unmanned aerial vehicle descends, it can not be because of speed be too big when descending to prevent, the incessantly machine of stopping to in can shortening the line of unmanned aerial vehicle descending, help unmanned aerial vehicle descend fast, and launching appliance simple structure, light in weight, it is little in unmanned aerial vehicle's flight in -process influence.
Description
Technical field
This utility model is related to a kind of unmanned plane auxiliary equipment, more particularly to a kind of unmanned plane buffer protection device.
Background technology
Current military affairs development in science and technology is rapid, unmanned plane as information weapon equipment, in closely High-technology local war several times
Middle to play more and more important effect, the flat pad of unmanned plane is also increasingly paid attention to by countries in the world.Now nobody
Machine emission system has become the important step in unmanned plane Campaign Process, and progressively developing into carry out an urgent task, and has again
There is the advanced weaponry equipment of adaptability.For this purpose, a kind of it is proposed that unmanned plane buffer protection device.
Utility model content
Main purpose of the present utility model is to provide a kind of unmanned plane buffer protection device, when unmanned plane lands
The impulse force of unmanned plane can be buffered, preventing will not be because speed be too big when landing, incessantly machine of stopping, and can shorten nobody
In the row of machine landing, unmanned plane rapid descent, and landing-gear simple structure are helped, it is lightweight, in the flight of unmanned plane
Affect little in journey, can be with the problem in effectively solving background technology.
For achieving the above object, the technical scheme that this utility model is taken is：
A kind of unmanned plane buffer protection device, including unmanned plane, buffer protection case, buffer deceleration umbrella, intervalometer and loss of weight
Power umbrella, the upper end of the unmanned plane is provided with buffer protection case, and the buffer protection case is internally provided with drag parachute package bin
With loss of weight power umbrella package bin, the drag parachute package bin is arranged on the rear end of buffer protection case, and internal compression is placed buffering
Drag parachute, the loss of weight power umbrella package bin is installed with the upper end of buffer protection case, and internal compression is placed loss of weight power umbrella, described
The side of loss of weight power umbrella is provided with and subtracts gravity switch, and the gravity switch that subtracts is connected to intervalometer, the intervalometer by wire
One end speed reducing switch is connected to by wire, the speed reducing switch is arranged on one end of drag parachute package bin, the intervalometer
Wheel switch is connected to by wire, the wheel switch is arranged on one end of wheel.
Further, the unmanned plane is internally provided with control chamber, and the control chamber is connected to intervalometer by wire.
Further, the two ends of the unmanned plane are provided with all-wing aircraft.
Further, the speed reducing switch, intervalometer and the inside that gravity switch is placed on buffer protection case is subtracted.
Compared with prior art, this utility model has the advantages that：This utility model is when unmanned plane lands
Time can buffer the impulse force of unmanned plane, and preventing will not be because speed be too big when landing, incessantly machine of stopping, and can shorten nothing
In the row of man-machine landing, unmanned plane rapid descent, and landing-gear simple structure are helped, it is lightweight, in the flight of unmanned plane
During affect little.
Description of the drawings
Fig. 1 is a kind of inside overall structure diagram of unmanned plane buffer protection device of this utility model；
Fig. 2 is a kind of overlooking the structure diagram of unmanned plane buffer protection device of this utility model.
In figure：1st, unmanned plane；2nd, all-wing aircraft；3rd, buffer protection case；4th, wheel；5th, wheel switch；6th, control chamber；7th, buffering subtracts
Fast umbrella；8th, drag parachute package bin；9th, speed reducing switch；10th, intervalometer；11st, gravity switch is subtracted；12nd, loss of weight power umbrella package bin；13、
Loss of weight power umbrella.
Specific embodiment
Technological means, creation characteristic, reached purpose and effect to realize this utility model is easy to understand, below
With reference to specific embodiment, this utility model is expanded on further.
As shown in Figure 1-2, a kind of unmanned plane buffer protection device, including unmanned plane 1, buffer protection case 3, buffer deceleration umbrella
7th, intervalometer 10 and loss of weight power umbrella 13, the upper end of the unmanned plane 1 is provided with buffer protection case 3, the buffer protection case 3 it is interior
Portion is provided with drag parachute package bin 8 and loss of weight power umbrella package bin 12, and the drag parachute package bin 8 is arranged on buffer protection case 3
Rear end, and internal compression is placed buffer deceleration umbrella 7, the loss of weight power umbrella package bin 12 is installed with the upper end of buffer protection case 3,
And internal compression is placed loss of weight power umbrella 13, the side of the loss of weight power umbrella 13 is provided with and subtracts gravity switch 11, the loss of weight power
Switch 11 is connected to intervalometer 10 by wire, and one end of the intervalometer 10 is connected to speed reducing switch 9 by wire, described to subtract
Speed switch 9 is arranged on one end of drag parachute package bin 8, and the intervalometer 10 is connected to wheel switch 5, the wheel by wire
Switch 5 is arranged on one end of wheel 4 so that buffer deceleration umbrella 7 first slows down when landing, loss of weight power umbrella after certain hour
13 open, and fall the speed for falling, and wheel 4 is opened when close from the ground.
A kind of unmanned plane buffer protection device of this utility model, passes through the He of buffer deceleration umbrella 7 when unmanned plane lands
Loss of weight power umbrella 13 can buffer the speed of the advance of unmanned plane and because gravity is toward the speed for falling, and preventing will not when landing
Because speed is too big, incessantly machine of stopping so that fuselage is damaged, and can shorten in the row of unmanned plane landing, help unmanned plane quick
Landing, and landing-gear simple structure, it is lightweight, affect little in the flight course of unmanned plane.
Wherein, the unmanned plane 1 is internally provided with control chamber 6, and the control chamber 6 is connected to intervalometer by wire
10 so that can be with remotely control unmanned plane.
Wherein, the two ends of the unmanned plane 1 are provided with all-wing aircraft 2, can help unmanned plane during flying.
Wherein, the speed reducing switch 9, intervalometer 10 and subtract the inside that gravity switch 11 is placed on buffer protection case 3, prevent
Inner body exposes, and affects the flight of unmanned plane.
Ultimate principle of the present utility model and principal character and advantage of the present utility model has been shown and described above.One's own profession
The technical staff of industry it should be appreciated that this utility model is not restricted to the described embodiments, described in above-described embodiment and description
Simply illustrate principle of the present utility model, on the premise of without departing from this utility model spirit and scope, this utility model is also
Various changes and modifications are had, these changes and improvements are both fallen within the range of claimed this utility model.This utility model
Claimed scope is by appending claims and its equivalent thereof.
Claims (4)
1. a kind of unmanned plane buffer protection device, including unmanned plane (1), buffer protection case (3), buffer deceleration umbrella (7), intervalometer
And loss of weight power umbrella (13) (10), it is characterised in that：The upper end of the unmanned plane (1) is provided with buffer protection case (3), the buffering
Guard box (3) is internally provided with drag parachute package bin (8) and loss of weight power umbrella package bin (12), the drag parachute package bin (8)
Installed in the rear end of buffer protection case (3), and internal compression is placed buffer deceleration umbrella (7), the loss of weight power umbrella package bin
(12) upper end of buffer protection case (3) is installed, and internal compression is placed loss of weight power umbrella (13), the loss of weight power umbrella (13)
Side is provided with and subtracts gravity switch (11), and the gravity switch (11) that subtracts is connected to intervalometer (10), the timing by wire
One end of device (10) is connected to speed reducing switch (9) by wire, and the speed reducing switch (9) is arranged on drag parachute package bin (8)
One end, the intervalometer (10) is connected to wheel switch (5) by wire, and wheel switch (5) is arranged on the one of wheel (4)
End.
2. a kind of unmanned plane buffer protection device according to claim 1, it is characterised in that：The unmanned plane (1) it is interior
Portion is provided with control chamber (6), and the control chamber (6) is connected to intervalometer (10) by wire.
3. a kind of unmanned plane buffer protection device according to claim 1, it is characterised in that：The two of the unmanned plane (1)
End is provided with all-wing aircraft (2).
4. a kind of unmanned plane buffer protection device according to claim 1, it is characterised in that：It is the speed reducing switch (9), fixed
When device (10) and subtract the inside that gravity switch (11) is placed on buffer protection case (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620859058.6U CN206141831U (en) | 2016-08-09 | 2016-08-09 | Unmanned aerial vehicle buffering protection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620859058.6U CN206141831U (en) | 2016-08-09 | 2016-08-09 | Unmanned aerial vehicle buffering protection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206141831U true CN206141831U (en) | 2017-05-03 |
Family
ID=58627853
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620859058.6U Expired - Fee Related CN206141831U (en) | 2016-08-09 | 2016-08-09 | Unmanned aerial vehicle buffering protection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206141831U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216644A (en) * | 2018-01-05 | 2018-06-29 | 安徽樵森电气科技股份有限公司 | A kind of rotor wing unmanned aerial vehicle and its fall-preventing protection device |
-
2016
- 2016-08-09 CN CN201620859058.6U patent/CN206141831U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216644A (en) * | 2018-01-05 | 2018-06-29 | 安徽樵森电气科技股份有限公司 | A kind of rotor wing unmanned aerial vehicle and its fall-preventing protection device |
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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: 20170503 Termination date: 20200809 |