CN205150258U - Modified unmanned aerial vehicle retrieves launching appliance - Google Patents
Modified unmanned aerial vehicle retrieves launching appliance Download PDFInfo
- Publication number
- CN205150258U CN205150258U CN201520644131.3U CN201520644131U CN205150258U CN 205150258 U CN205150258 U CN 205150258U CN 201520644131 U CN201520644131 U CN 201520644131U CN 205150258 U CN205150258 U CN 205150258U
- Authority
- CN
- China
- Prior art keywords
- shifting block
- unmanned plane
- collecting unit
- wind collecting
- reclaims
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses an unmanned aerial vehicle retrieves launching appliance, including organism and rotor, the top of rotor is equipped with the umbrella cabin, the umbrella under -deck is equipped with catapult and pack, the inside control switch that is equipped with of organism, control switch is connected with the catapult, organism inside is gone back the horizontally and is seted up a wind pressure chamber, the wind pressure chamber is equipped with an air intake and an air outlet, the air intake is connected with one album of wind ware, and the wind pressure intracavity still is equipped with shifting block and a plurality of spring, the position of shifting block is corresponding with the exit position of collection wind ware, a plurality of spring settings are between the last lateral wall and shifting block in wind pressure chamber, and the upper end of shifting block is still corresponding with control switch's position. The utility model discloses realize steady recovery in time to it mainly adopts the mechanical system to trigger control switch, its good reliability, security height.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, and the unmanned plane particularly relating to a kind of improvement reclaims launching appliance.
Background technology
Existing unmanned plane recovery method mainly contains parachuting and hits two kinds, net.Hit the assigned spot recovery that net recovery method is applicable to unmanned plane, recovery during inapplicable unmanned plane catastrophic failure.At present conventional parachuting mode to be launched by explosion or parachute is opened by lower throwing method, demolition bomb shooting method easily causes the secondary damage of aircraft, lower throwing method is comparatively strong to the dependence of wind-force and aircraft speed, and parachute occurs when catastrophic failure unmanned plane, and to open the probability of failure higher.
Utility model content
The utility model mainly to solve in prior art existing technical matters, thus provide a kind of and can steadily reclaim in time, the unmanned plane of improvement that safety is high reclaims launching appliance.
Above-mentioned technical matters of the present utility model is mainly solved by following technical proposals:
The unmanned plane of the improvement that the utility model provides reclaims launching appliance, comprise body and rotor, the top of described rotor is provided with umbrella cabin, ejector and pack is provided with in described umbrella cabin, described internal body is provided with master cock, described master cock is connected with described ejector, described internal body also level offer a blast chamber, described blast chamber is provided with a ventilation inlet and an air outlet, described ventilation inlet is connected with a wind collecting unit, and be also provided with shifting block and multiple spring in described blast chamber, the position of described shifting block is corresponding with the exit position of described wind collecting unit, between the upper side wall that multiple described spring is arranged on described blast chamber and described shifting block, and the upper end of described shifting block is also corresponding with the position of described master cock.
Further, the shape of described wind collecting unit is tubaeform, and the size of described shifting block and the end diameter of described wind collecting unit adapt.
Further, the shape of described shifting block is T-shaped, and multiple described springs are symmetricly set on the both sides of described shifting block.
Further, described wind collecting unit is threaded with described body.
Further, described air outlet place is also provided with a buzzer phone.
The beneficial effects of the utility model are: in the process that unmanned plane catastrophic failure falls rapidly, air-flow is at a high speed collected by wind collecting unit, shifting block in impact wind pressure chamber, shifting block under the effect of impulsive force on move trigging control switch, and then open ejector ejection pack, realize timely pulsation-free to reclaim, and it mainly adopts mechanical system trigging control switch, and its good reliability, safety are high.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of the unmanned plane recovery launching appliance of improvement of the present utility model,
Fig. 2 is the I place partial enlarged drawing of Fig. 1.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, to make advantage of the present utility model and feature can be easier to be readily appreciated by one skilled in the art, thus more explicit defining is made to protection domain of the present utility model.
Consult shown in Fig. 1-2, the unmanned plane of improvement of the present utility model reclaims launching appliance, comprise body 1 and rotor 2, the top of rotor 2 is provided with umbrella cabin 3, ejector 4 and pack 5 is provided with in umbrella cabin 3, body 1 inside is provided with master cock 6, master cock 6 is connected with ejector 4, body 1 inside also level offer a blast chamber 7, blast chamber 7 is provided with ventilation inlet 8 and an air outlet 9, ventilation inlet 8 is connected with a wind collecting unit 10, and in blast chamber 7, be also provided with shifting block 11 and multiple spring 12, the position of shifting block 11 is corresponding with the exit position of wind collecting unit 10, multiple spring 12 is arranged between the upper side wall in blast chamber 7 and shifting block 11, and the upper end of shifting block 11 is also corresponding with the position of master cock 6.In the process that the utility model falls rapidly at unmanned plane catastrophic failure, air-flow is at a high speed collected by wind collecting unit 10, shifting block 11 in impact wind pressure chamber 7, shifting block 11 under the effect of impulsive force on move trigging control switch 6, and then open ejector 4 and eject pack 5, realize timely pulsation-free to reclaim, and it mainly adopts mechanical system trigging control switch, and its good reliability, safety are high.
Concrete, conveniently gather air-flow, the shape of wind collecting unit 10 is tubaeform.The size of shifting block 11 and the end diameter of wind collecting unit 10 adapt, and add the impulsive force of air-flow to shifting block 11.And the shape of shifting block 11 is T-shaped, T-shaped jag is used for trigging control switch 6 and opens, and multiple springs 12 are symmetricly set on the both sides of shifting block 11, make the stress equalization of shifting block 11, avoid false triggering.
Preferably, conveniently Assembly &Disassembly, wind collecting unit 10 is threaded with body 1.Preferably, air outlet 9 place is also provided with a buzzer phone 13, impels buzzer phone 13 to report to the police by the air-flow collected in unmanned plane rapidly falling process, reminds ground controller to note reclaiming.
Above, be only detailed description of the invention of the present utility model, but protection domain of the present utility model is not limited thereto, any change of expecting without creative work or replacement, all should be encompassed within protection domain of the present utility model.Therefore, the protection domain that protection domain of the present utility model should limit with claims is as the criterion.
Claims (5)
1. the unmanned plane improved reclaims launching appliance, comprise body (1) and rotor (2), the top of described rotor (2) is provided with umbrella cabin (3), ejector (4) and pack (5) is provided with in described umbrella cabin (3), described body (1) inside is provided with master cock (6), described master cock (6) is connected with described ejector (4), it is characterized in that: described body (1) inside also level offer a blast chamber (7), described blast chamber (7) is provided with a ventilation inlet (8) and an air outlet (9), described ventilation inlet (8) is connected with a wind collecting unit (10), and be also provided with shifting block (11) and multiple spring (12) in described blast chamber (7), the position of described shifting block (11) is corresponding with the exit position of described wind collecting unit (10), between the upper side wall that multiple described spring (12) is arranged on described blast chamber (7) and described shifting block (11), and the upper end of described shifting block (11) is also corresponding with the position of described master cock (6).
2. the unmanned plane improved as claimed in claim 1 reclaims launching appliance, it is characterized in that: the shape of described wind collecting unit (10) is tubaeform, the size of described shifting block (11) and the end diameter of described wind collecting unit (10) adapt.
3. the unmanned plane improved as claimed in claim 2 reclaims launching appliance, it is characterized in that: the shape of described shifting block (11) is T-shaped, and multiple described springs (12) are symmetricly set on the both sides of described shifting block (11).
4. the unmanned plane improved as claimed in claim 3 reclaims launching appliance, it is characterized in that: described wind collecting unit (10) is threaded with described body (1).
5. the unmanned plane improved as claimed in claim 4 reclaims launching appliance, it is characterized in that: described air outlet (9) place is also provided with a buzzer phone (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520644131.3U CN205150258U (en) | 2015-08-24 | 2015-08-24 | Modified unmanned aerial vehicle retrieves launching appliance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520644131.3U CN205150258U (en) | 2015-08-24 | 2015-08-24 | Modified unmanned aerial vehicle retrieves launching appliance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205150258U true CN205150258U (en) | 2016-04-13 |
Family
ID=55685976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520644131.3U Expired - Fee Related CN205150258U (en) | 2015-08-24 | 2015-08-24 | Modified unmanned aerial vehicle retrieves launching appliance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205150258U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945477A (en) * | 2018-05-31 | 2018-12-07 | 智飞智能装备科技东台有限公司 | A kind of landing system for unmanned plane recycling |
-
2015
- 2015-08-24 CN CN201520644131.3U patent/CN205150258U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945477A (en) * | 2018-05-31 | 2018-12-07 | 智飞智能装备科技东台有限公司 | A kind of landing system for unmanned plane recycling |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20160413 Termination date: 20160824 |