CN205098489U - Be used for pipe to penetrate high pressurized air source of unmanned aerial vehicle transmission separator - Google Patents
Be used for pipe to penetrate high pressurized air source of unmanned aerial vehicle transmission separator Download PDFInfo
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- CN205098489U CN205098489U CN201520921519.3U CN201520921519U CN205098489U CN 205098489 U CN205098489 U CN 205098489U CN 201520921519 U CN201520921519 U CN 201520921519U CN 205098489 U CN205098489 U CN 205098489U
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- pipe
- air source
- aerial vehicle
- unmanned aerial
- launching tube
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Abstract
The utility model discloses a be used for pipe to penetrate high pressurized air source of unmanned aerial vehicle transmission separator, including launching tube, protecgulum and support frame, the protecgulum is installed to the left end of launching tube, install the support frame on the lateral wall of launching tube, the inner chamber mid -mounting of launching tube has the piston, and the top of piston installs unmanned aerial vehicle, gas holder group is installed to the inner chamber of launching tube bottom, and the gas holder inter block is equipped with the gaseous matter, rotating base is installed to the bottom of gas holder group, the fixed bolster is installed to rotating base's right -hand member. This be used for pipe to penetrate high pressurized air source of unmanned aerial vehicle transmission separator through gas holder group, piston and launching tube structure, can use compressed air in the emission process, avoided appearing in the emission process light, and the circumstances of smog and sound takes place, increases and conceals the effect, and the cost price is cheap, and adaptability is good, and the transmission that is fit for medium and small unmanned aerial vehicle is more taken off.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, is specially one and penetrates unmanned plane high-pressure air source transmitting disengagement gear for pipe.
Background technology
Current existing unmanned plane feedway is generally the mode of rato, but the mode of rocket assist there will be light, smog and sound, property safe and out of sight is poor, and price is high simultaneously, bad adaptability, we need to design a kind of unmanned plane feedway for this reason.
Utility model content
The purpose of this utility model is that providing a kind of penetrates unmanned plane high-pressure air source transmitting disengagement gear, to solve the problem proposed in above-mentioned background technology for pipe.
For achieving the above object, the utility model provides following technical scheme: unmanned plane high-pressure air source transmitting disengagement gear penetrated by a kind of pipe that is used for, comprise canister launcher, protecgulum and bracing frame, the left end of described canister launcher is provided with protecgulum, the sidewall of described canister launcher is provided with bracing frame, the inner chamber of described canister launcher is provided with piston, and the top of piston is provided with unmanned plane, the intracavity bottom of described canister launcher is provided with storage tank group, and be provided with gaseous matter in storage tank group, the bottom of described storage tank group is provided with rotating base, the right-hand member of described rotating base is provided with fixed support.
Preferably, described storage tank group is formed by being no less than 3 storage tanks, and storage tank rounded arrangement in canister launcher.
Preferably, being provided with gaseous matter in described storage tank group is pressurized air.
Preferably, the bottom of support frame as described above is provided with the rubber pad of increasing friction force.
Compared with prior art, the beneficial effects of the utility model are: this is used for pipe and penetrates unmanned plane high-pressure air source transmitting disengagement gear, by storage tank group, piston and canister launcher structure, can use pressurized air in emission process, avoid and occur light in emission process, the situation of smog and sound occurs, increase hidden effect, cost of price is cheap, and comformability is good, is more applicable to the launch of medium and small unmanned plane.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation.
In figure: 1, protecgulum, 2, bracing frame, 3, canister launcher, 4, piston, 5, storage tank group, 6, rotating base, 7, fixed support.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Refer to Fig. 1, the utility model provides a kind of technical scheme: unmanned plane high-pressure air source transmitting disengagement gear penetrated by a kind of pipe that is used for, comprise canister launcher 3, protecgulum 1 and bracing frame 2, the left end of described canister launcher 3 is provided with protecgulum 1, the sidewall of described canister launcher 3 is provided with bracing frame 2, for supporting canister launcher 3, the inner chamber of described canister launcher 3 is provided with piston 4, and the top of piston 4 is provided with unmanned plane, launch for unmanned plane and power is provided, the intracavity bottom of described canister launcher 3 is provided with storage tank group 5, described storage tank group 5 is made up of 3 storage tanks, for unmanned plane provides power, and storage tank rounded arrangement in canister launcher 3, make the pressurized air that ejects more even, gaseous matter is provided with in storage tank group 5, gaseous matter is pressurized air, reach unglazed, smokelessly, noiseless advantage, the bottom of described storage tank group 5 is provided with rotating base 6, the right-hand member of described rotating base 6 is provided with fixed support 7, the bottom of support frame as described above 2 is provided with the rubber pad of increasing friction force, prevent having friction force little when transmitting, ground and bracing frame 2 skid, make unmanned plane standoff.
Principle of work: by triggering storage tank group 5 valve and opening it, instantaneous generation high pressure gas, produce thrust to piston 4, and piston 4 and unmanned plane are transmitted into takeoff speed and height, piston 1 comes off, and unmanned plane can rely on power to continue flight.
Although illustrate and described embodiment of the present utility model, for the ordinary skill in the art, be appreciated that and can carry out multiple change, amendment, replacement and modification to these embodiments when not departing from principle of the present utility model and spirit, scope of the present utility model is by claims and equivalents thereof.
Claims (4)
1. penetrate unmanned plane high-pressure air source transmitting disengagement gear for pipe for one kind, it is characterized in that: comprise canister launcher, protecgulum and bracing frame, the left end of described canister launcher is provided with protecgulum, the sidewall of described canister launcher is provided with bracing frame, the inner chamber of described canister launcher is provided with piston, and the top of piston is provided with unmanned plane, the intracavity bottom of described canister launcher is provided with storage tank group, and be provided with gaseous matter in storage tank group, the bottom of described storage tank group is provided with rotating base, and the right-hand member of described rotating base is provided with fixed support.
2. one according to claim 1 penetrates unmanned plane high-pressure air source transmitting disengagement gear for pipe, it is characterized in that: described storage tank group is formed by being no less than 3 storage tanks, and storage tank rounded arrangement in canister launcher.
3. one according to claim 1 penetrates unmanned plane high-pressure air source transmitting disengagement gear for pipe, it is characterized in that: being provided with gaseous matter in described storage tank group is pressurized air.
4. one according to claim 1 penetrates unmanned plane high-pressure air source transmitting disengagement gear for pipe, it is characterized in that: the bottom of support frame as described above is provided with the rubber pad of increasing friction force.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520921519.3U CN205098489U (en) | 2015-11-18 | 2015-11-18 | Be used for pipe to penetrate high pressurized air source of unmanned aerial vehicle transmission separator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520921519.3U CN205098489U (en) | 2015-11-18 | 2015-11-18 | Be used for pipe to penetrate high pressurized air source of unmanned aerial vehicle transmission separator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205098489U true CN205098489U (en) | 2016-03-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201520921519.3U Active CN205098489U (en) | 2015-11-18 | 2015-11-18 | Be used for pipe to penetrate high pressurized air source of unmanned aerial vehicle transmission separator |
Country Status (1)
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| CN (1) | CN205098489U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107458579A (en) * | 2017-08-01 | 2017-12-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of unmanned plane device |
| CN108609195A (en) * | 2018-05-30 | 2018-10-02 | 深圳市易飞方达科技有限公司 | A kind of folding wings unmanned plane emitter |
| CN109229413A (en) * | 2018-10-08 | 2019-01-18 | 湖南航天机电设备与特种材料研究所 | For the cold air emitter of flight test and the cold air launching technique of aircraft |
| CN109780445A (en) * | 2018-12-20 | 2019-05-21 | 兰州空间技术物理研究所 | A kind of high-pressure air source device |
| CN110065634A (en) * | 2019-04-23 | 2019-07-30 | 北京理工伺服科技有限公司 | Unmanned flight robot based on the cold power-assisted transmitting of compressed gas |
| CN110667873A (en) * | 2019-11-05 | 2020-01-10 | 贵州华图科技有限公司 | Unmanned aerial vehicle and method for catapulting unmanned aerial vehicle by utilizing compressed air |
| CN113525708A (en) * | 2021-09-06 | 2021-10-22 | 中国人民解放军战略支援部队航天工程大学 | Unmanned aerial vehicle launching device and using method |
-
2015
- 2015-11-18 CN CN201520921519.3U patent/CN205098489U/en active Active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107458579A (en) * | 2017-08-01 | 2017-12-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of unmanned plane device |
| CN108609195A (en) * | 2018-05-30 | 2018-10-02 | 深圳市易飞方达科技有限公司 | A kind of folding wings unmanned plane emitter |
| CN109229413A (en) * | 2018-10-08 | 2019-01-18 | 湖南航天机电设备与特种材料研究所 | For the cold air emitter of flight test and the cold air launching technique of aircraft |
| CN109780445A (en) * | 2018-12-20 | 2019-05-21 | 兰州空间技术物理研究所 | A kind of high-pressure air source device |
| CN110065634A (en) * | 2019-04-23 | 2019-07-30 | 北京理工伺服科技有限公司 | Unmanned flight robot based on the cold power-assisted transmitting of compressed gas |
| CN110065634B (en) * | 2019-04-23 | 2021-05-14 | 北京理工伺服科技有限公司 | Unmanned flying robot based on compressed gas cold-assisted launching |
| CN110667873A (en) * | 2019-11-05 | 2020-01-10 | 贵州华图科技有限公司 | Unmanned aerial vehicle and method for catapulting unmanned aerial vehicle by utilizing compressed air |
| CN113525708A (en) * | 2021-09-06 | 2021-10-22 | 中国人民解放军战略支援部队航天工程大学 | Unmanned aerial vehicle launching device and using method |
| CN113525708B (en) * | 2021-09-06 | 2023-09-26 | 中国人民解放军战略支援部队航天工程大学 | Unmanned aerial vehicle transmitting device and using method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |