CN206664944U - A kind of new UAV Intelligent parachute - Google Patents
A kind of new UAV Intelligent parachute Download PDFInfo
- Publication number
- CN206664944U CN206664944U CN201720483228.XU CN201720483228U CN206664944U CN 206664944 U CN206664944 U CN 206664944U CN 201720483228 U CN201720483228 U CN 201720483228U CN 206664944 U CN206664944 U CN 206664944U
- Authority
- CN
- China
- Prior art keywords
- top closure
- parachute
- launching tube
- bottom cover
- unmanned plane
- Prior art date
- 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.)
- Active
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The utility model discloses a kind of new UAV Intelligent parachute, including top closure, the side of the top closure is provided with launching tube, the side of top closure is additionally provided with switch connecting pole, the side of the launching tube is provided with bottom cover, compression spring is provided between the top closure and bottom cover, the bottom cover obtains side and is provided with control circuit.The utility model UAV Intelligent parachute, succinct highly effective and safe, optimize device, system built-in angular sensor, control circuit only need to be to system power supply, it can be gone wrong in each system of unmanned plane still interference-free, normal work ensures unmanned plane air crash safety, the system can detect the attitude angle and acceleration of unmanned plane when working, only a condition is needed to meet, the extraction parachute that system will be deployed at first in very first time ejection parachute, it will further assist in the expansion of main chute, ensure the UAS and third-party personnel and property safety of high value, greatly reduce loss and support personnel's safety.
Description
Technical field
Unmanned plane field is the utility model is related to, specifically a kind of new UAV Intelligent parachute.
Background technology
The similar matured product of domestic and international market neither one at present, some existing products are all some users on the market
DIY equipment, do not possess use value, leading unmanned plane enterprise also only produced the similar production of very few several moneys in the industry
Product, and the unmanned machine equipment of incompatible third party and flight control system, it is completely dependent on to flying control and flying the sensor that carries of control, using rising
Come and its cumbersome, it is dangerous, it is desirable to it is high, and parachute-opening efficiency be present and success rate is low, parachute system on the market is generally tied
Structure is cumbersome, preponderance, the gentle dynamic profile of this body structure of unmanned plane is influenceed greatly, and other systems use cost is very high.
Utility model content
The purpose of this utility model is to provide a kind of new UAV Intelligent parachute that there is simple in construction, parachute-opening to imitate
The advantages of rate is high and safe to use, to solve the problems mentioned in the above background technology.
To achieve the above object, the utility model provides following technical scheme：A kind of new UAV Intelligent parachute, bag
Top closure is included, the side of the top closure is provided with launching tube, and top closure is connected with launching tube, the top closure
Side is additionally provided with switch connecting pole, switchs one end of connecting pole and the bottom of top closure and connects, switchs the other end of connecting pole
The inside of launching tube is extended to, the side of the launching tube is provided with bottom cover, and bottom cover is connected with launching tube, the top
Portion covers is provided with compression spring between bottom cover, and compression spring is located at the inside of launching tube, and the bottom cover obtains one
Side is provided with control circuit, and control circuit is connected with bottom cover, and control circuit is located at the inside of launching tube.
As further program of the utility model：The launching tube is columnar structured.
As further program of the utility model：The switch connecting pole is four size identical connecting poles, connection
Post is evenly distributed on the bottom of top closure.
Compared with prior art, the utility model beneficial effect：
The utility model UAV Intelligent parachute, succinct highly effective and safe, optimization device, system built-in angular sensor,
Control circuit outside the system is independently of unmanned plane other systems, can need to only go out to system power supply in each system of unmanned plane
Problem is still interference-free, and normal work ensures unmanned plane air crash safety, and the system can detect the attitude angle of unmanned plane when working
And acceleration, only need a condition to meet, the extraction parachute that system will be deployed at first in very first time ejection parachute will be further
The expansion of main chute is helped, the UAS and third-party personnel and property safety of high value is ensured, greatly reduces loss
And support personnel's safety.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model；
Fig. 2 is control circuit schematic diagram of the present utility model.
In figure：1- top closures；2- launching tubes；3- switchs connecting pole；31- connecting poles；4- bottom covers；5- compresses bullet
Spring；6- control circuits.
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.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Refer to Fig. 1-2, in the utility model embodiment, a kind of new UAV Intelligent parachute, including top closure
1, the side of top closure 1 is provided with launching tube 2, and top closure 1 is connected with launching tube 2, and launching tube 2 is whole to be columnar structured
Body structure uses the launching tube 2 of cylinder moulding, is fixed using 4 points, power switch indicator lamp power supply port is provided only with, to make device
Can be independent safely, attitude detection and parachute-opening circuit are integrated in inside device, outside only power taking, user opens using after energization
Pass, the side of top closure 1 are additionally provided with switch connecting pole 3, switch one end of connecting pole 3 and connect with the bottom of top closure 1
Connect, the other end of switch connecting pole 3 extends to the inside of launching tube 2, and switch connecting pole 3 is four size identical connecting poles
31, connecting pole 31 is evenly distributed on the bottom of top closure 1, is fixed using 4 points, and the side of launching tube 2 is provided with bottom cover
4, bottom cover 4 is connected with launching tube 2, and compression spring 5, compression spring 5 are provided between top closure 1 and bottom cover 4
In the inside of launching tube 2, bottom cover 4 obtains side and is provided with control circuit 6, to make parachute eject and deploy in the very first time,
Special to form a whole set of ejection system using compression spring 5, ignition switch and a small amount of solid fuel, system detectio to aircraft is lost
Air crash electric signal is controlled, the very first time opens ignition switch, ejects extraction parachute and main chute by solid fuel triggering compression spring 5, leads
Main chute is helped to deploy to complete slow drop of slowing down rapidly after drawing umbrella expansion, control circuit 6 is connected with bottom cover 4, and control circuit 6 is located at
The inside of launching tube 2, the UAV Intelligent parachute system are an independent unmanned plane security systems, the system built-in angular
Sensor, control circuit 6 only need to be to system power supplies, unlike other products need its specific winged control to provide parachute-opening signal and carry
For various data, outside the system is independently of unmanned plane other systems, can be gone wrong in each system of unmanned plane still interference-free, just
Normal job security unmanned plane air crash safety, according to statistics and experiment, unmanned plane out of control 99% body can all occurs and topple, the system
The attitude angle and acceleration of unmanned plane can be detected during work, only needs a condition to meet, system will eject in the very first time to drop
Fall the extraction parachute that umbrella deploys at first, will further assist in the expansion of main chute, ensure the UAS of high value and third-party
Personnel and property safety, greatly reduce loss and support personnel's safety.
In summary：The utility model UAV Intelligent parachute, succinct highly effective and safe, optimize device, angle setting in system
Sensor is spent, control circuit 6 only need to be to system power supply, can be at nobody outside the system is independently of unmanned plane other systems
Each system of machine goes wrong still without interruption, and normal work ensures unmanned plane air crash safety, and the system can detect unmanned plane when working
Attitude angle and acceleration, only need condition to meet, system will eject the traction that parachute deploys at first in the very first time
Umbrella, the expansion of main chute is will further assist in, ensure the UAS and third-party personnel and property safety of high value, greatly
Reduction loss and support personnel safety.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (3)
1. a kind of new UAV Intelligent parachute, including top closure (1), it is characterised in that：The one of the top closure (1)
Side is provided with launching tube (2), and top closure (1) is connected with launching tube (2), and the side of the top closure (1) is additionally provided with switch
Connecting pole (3), one end of switch connecting pole (3) are connected with the bottom of top closure (1), and the other end of switch connecting pole (3) prolongs
The inside of launching tube (2) is reached, the side of the launching tube (2) is provided with bottom cover (4), bottom cover (4) and launching tube
(2) connect, compression spring (5) is provided between the top closure (1) and bottom cover (4), compression spring (5) is positioned at transmitting
The inside of cylinder (2), the bottom cover (4) obtain side and are provided with control circuit (6), and control circuit (6) connects with bottom cover (4)
Connect, control circuit (6) is located at the inside of launching tube (2).
A kind of 2. new UAV Intelligent parachute according to claim 1, it is characterised in that：The launching tube (2) is
It is columnar structured.
A kind of 3. new UAV Intelligent parachute according to claim 1, it is characterised in that：The switch connecting pole
(3) it is four size identical connecting poles (31), connecting pole (31) is evenly distributed on the bottom of top closure (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720483228.XU CN206664944U (en) | 2017-04-27 | 2017-04-27 | A kind of new UAV Intelligent parachute |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720483228.XU CN206664944U (en) | 2017-04-27 | 2017-04-27 | A kind of new UAV Intelligent parachute |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206664944U true CN206664944U (en) | 2017-11-24 |
Family
ID=60370846
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720483228.XU Active CN206664944U (en) | 2017-04-27 | 2017-04-27 | A kind of new UAV Intelligent parachute |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206664944U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774949A (en) * | 2019-02-13 | 2019-05-21 | 南京智慧基础设施技术研究院有限公司 | A kind of intelligence multi-rotor unmanned aerial vehicle emergency parachute landing system |
| CN110823497A (en) * | 2019-12-03 | 2020-02-21 | 中国空气动力研究与发展中心 | Vertical wind tunnel tail spin test model anti-tail spin parachute ejection mechanism |
-
2017
- 2017-04-27 CN CN201720483228.XU patent/CN206664944U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774949A (en) * | 2019-02-13 | 2019-05-21 | 南京智慧基础设施技术研究院有限公司 | A kind of intelligence multi-rotor unmanned aerial vehicle emergency parachute landing system |
| CN110823497A (en) * | 2019-12-03 | 2020-02-21 | 中国空气动力研究与发展中心 | Vertical wind tunnel tail spin test model anti-tail spin parachute ejection mechanism |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108715228B (en) | Unmanned aerial vehicle falling protection control system and control method | |
| CN104118564B (en) | A kind of multi-rotor aerocraft safety system | |
| CN206664944U (en) | A kind of new UAV Intelligent parachute | |
| CN207257995U (en) | The unmanned plane that fail-safe is crashed | |
| CN206423599U (en) | Intelligent air bag protecting against shock clothes | |
| CN104443398B (en) | A kind of agricultural unmanned plane automatic deployment fender guard and method | |
| CN207580177U (en) | A kind of unmanned plane with buffer gear | |
| CN202609086U (en) | Downwards-throwing popup type parachute opening device of unmanned plane | |
| CN203946278U (en) | The parachuting umbrella cabin of unmanned plane | |
| CN106628150A (en) | Capture device for unmanned aerial vehicle | |
| CN204967904U (en) | Mobile phone protection device | |
| CN109677621A (en) | A kind of unmanned plane parachute and unmanned plane parachute control system | |
| CN209581882U (en) | A kind of plant protection drone with shatter-resistant air bag | |
| CN206020975U (en) | A kind of device that plunges for being applied to multi-rotor unmanned aerial vehicle | |
| CN108860633B (en) | Unmanned aerial vehicle capable of automatically opening air bag when falling after power consumption | |
| CN206345016U (en) | Delay to fall protection device and unmanned plane in the air | |
| CN203975233U (en) | A kind of multi-rotor aerocraft safety system | |
| CN215043750U (en) | Rotor unmanned aerial vehicle air crash protection device | |
| CN207274515U (en) | A kind of uav water emergency rescue device | |
| CN106477059A (en) | A kind of portable simple airplane parking area for rotor wing unmanned aerial vehicle | |
| CN206282915U (en) | A kind of outer penetration type side exhaust battery explosion-proof cap | |
| CN205212004U (en) | Insurance of intelligence power connects | |
| CN207000826U (en) | A kind of unmanned plane | |
| CN206367613U (en) | Multiaxis unmanned plane air bag device | |
| CN207773489U (en) | A kind of umbrella cabin device of unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |