CN106143894A - A kind of unmanned plane of helium (hydrogen) gas - Google Patents
A kind of unmanned plane of helium (hydrogen) gas Download PDFInfo
- Publication number
- CN106143894A CN106143894A CN201510211684.4A CN201510211684A CN106143894A CN 106143894 A CN106143894 A CN 106143894A CN 201510211684 A CN201510211684 A CN 201510211684A CN 106143894 A CN106143894 A CN 106143894A
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- annular balloon
- gas
- unmanned plane
- helium
- hydrogen
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Abstract
A kind of helium (hydrogen) gas unmanned plane, including machine support, support is provided with propeller, and frame central has air pressure observing and controlling element, pcb board and battery.Body rack outer end connects annular balloon by nylon wire button；Miniature electromagnetic valve on the Mini compressed air bag at body rack center connects annular balloon by gas tube；Equipped with miniature gas bleeder valve at the leakage port of annular balloon；The circuit of miniature electromagnetic valve and miniature gas bleeder valve electrically connects with air pressure measurement and control unit, is full of helium or hydrogen in annular balloon.The present invention lifts by annular balloon pressure regulation is automatically adjusted unmanned plane, reduces propeller power consumption, extends the flight time exponentially, and safety is high, lands steadily.
Description
Technical field:
The present invention relates to a kind of unmanned plane, the unmanned plane of particularly a kind of helium (hydrogen) gas.
Background technology:
Currently, unmanned plane has been existing mature technology, particularly four axle propeller
Unmanned plane application is the most extensive, but because being affected by energy-storage battery heavily quantitative limitation
Its flight cruising time can only be within half an hour, owing to flight limits cruising time
Unmanned plane uses service continuously some fixing spatial domains, and interim such as earthquake disaster is led to
News relaying and monitoring commander, the monitoring of forest fire protection, the dispatching and monitoring of traffic congestion with
And spraying is except haze etc..The most existing unmanned plane once accident is out of control, will drop down
Come, break machine and cause casualty accident, without safety guarantee.
Summary of the invention:
It is an object of the invention to provide a kind of unmanned plane extending the flight time at double,
Flight landing grease it in, eliminates air crash accident, improves safety coefficient.
Technical scheme: a kind of helium (hydrogen) gas unmanned plane, props up including body
Frame, support is provided with propeller, frame central organic core equipment cover, has in equipment cover
Air pressure measurement and control unit pcb board and battery.Body rack outer end is by nylon wire button even
T-Ring spheric balloon；Miniature electromagnetic valve on the Mini compressed air bag at body rack center leads to
Overcharge trachea and connect annular balloon；Lose heart equipped with miniature at the leakage port of annular balloon
Valve；The circuit of miniature electromagnetic valve and miniature gas bleeder valve electrically connects with air pressure measurement and control unit.
There is provided manipulation foundation by air pressure measurement and control unit to automatic-balancing system, control micro electric
Magnet valve works with miniature gas bleeder valve, to annular balloon inflation or disappointing, makes unmanned plane dish
Rotation continuation of the journey or stable landing.
Beneficial effects of the present invention: float by the pressure regulation of annular balloon is changed it
Power, the lifting of automodulation unmanned plane, decrease unmanned plane and originally rely on propeller to go up to the air
Power consumption, extend the continuation of the journey working time exponentially, when navigation is to predetermined work
Point is when spiraling, and propeller can reduce and rotates even stall, and unmanned plane still can be suspended in
Work on operating point, make the continuation of the journey working time extend exponentially, so unmanned plane
Be provided that service continuously in some fixing spatial domains, the temporary communications such as earthquake disaster relays
And monitoring commander, the monitoring of forest fire protection, traffic congestion and spraying except haze etc..
Because annular balloon is distributed on around propeller, effect protected to propeller.Rely on
The buoyancy of its helium (hydrogen) gas declines, it is achieved steadily soft landing, will not break unmanned plane,
Do not result in casualty accident, drastically increase safety coefficient yet.
Accompanying drawing illustrates:
The present invention is further described below in conjunction with the accompanying drawings
Fig. 1, top view of the present invention；
Fig. 2, the A-A sectional view of figure 2 above；
Fig. 3, upward view of the present invention；
Fig. 4, annular balloon pressure of the present invention regulation electrical principle block diagram.
In figure: 1. body rack, 2. propeller, 3. movement equipment cover, 4. air pressure observing and controlling
Unit, 5. Mini compressed air bag, 6. miniature electromagnetic valve, the most miniature gas bleeder valve, 8. annular
Balloon, 9. nylon wire button, 10. gas tube, 11.PCB plate, 12. batteries.
Detailed description of the invention:
In Fig. 1, Fig. 2, four propeller (2) are separately mounted to body rack
(1), on four axles, annular balloon (8) is arranged on four spiral shells as protection ring
Around, annular balloon (8) is fixed on machine to rotating plasma (2) by nylon wire button (9)
On body support frame (1), in the centre of body rack (1) equipped with movement equipment cover
(3), in machine core equipment cover (3), Mini compressed air bag (5), air pressure are installed
Measurement and control unit (4), miniature electromagnetic valve (6), pcb board (11), battery (12).
Gas tube (10) be connected to annular balloon (8) with miniature electromagnetic valve (6) it
Between, miniature gas bleeder valve (7) is also connected in annular balloon (8) with sebific duct.Pass through
Air pressure measurement and control unit (4) provides manipulation foundation to automatic-balancing system, and controls micro-
Type electromagnetic valve (6) and miniature gas bleeder valve (7) are turned on and off, and implement annular gas
The inflation/deflation of ball (8), makes unmanned plane extend cruising time or stable landing.
Claims (3)
1. helium (hydrogen) gas unmanned plane, including body rack (1), on support
Being provided with propeller (2), frame central has air pressure measurement and control unit (4), pcb board (11)
With battery (12), it is characterised in that: nylon wire button is passed through in body rack (1) outer end
(9) annular balloon (8) is connected；The Mini compressed air bag at body rack (1) center
(5) miniature electromagnetic valve (6) on connects annular balloon (8) by gas tube (10)；
Equipped with miniature gas bleeder valve (7) at the leakage port of annular balloon (8)；Miniature electromagnetic valve
And the circuit of miniature gas bleeder valve (7) electrically connects with air pressure measurement and control unit (4) (6).
A kind of helium (hydrogen) gas unmanned plane the most according to claim 1, it is special
Levy and be: the annular external diameter of annular balloon is 0.5～20m, and its tubulose latus rectum is
5～500cm.
A kind of helium (hydrogen) gas unmanned plane the most according to claim 1, it is special
Levy and be: in annular balloon, be full of helium or hydrogen.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510211684.4A CN106143894A (en) | 2015-04-21 | 2015-04-21 | A kind of unmanned plane of helium (hydrogen) gas |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510211684.4A CN106143894A (en) | 2015-04-21 | 2015-04-21 | A kind of unmanned plane of helium (hydrogen) gas |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106143894A true CN106143894A (en) | 2016-11-23 |
Family
ID=57347008
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510211684.4A Pending CN106143894A (en) | 2015-04-21 | 2015-04-21 | A kind of unmanned plane of helium (hydrogen) gas |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106143894A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107628246A (en) * | 2017-07-26 | 2018-01-26 | 青岛万祥如光机械技术研究有限公司 | A kind of unmanned plane line walking device |
| CN107697288A (en) * | 2017-07-26 | 2018-02-16 | 青岛万祥如光机械技术研究有限公司 | A kind of energy-saving unmanned plane |
| CN109110139A (en) * | 2018-09-07 | 2019-01-01 | 佛山皖和新能源科技有限公司 | A kind of novel unmanned plane auxiliary lifting device |
| CN111645854A (en) * | 2020-03-30 | 2020-09-11 | 上海交通大学医学院附属瑞金医院 | Unmanned aerial vehicle monitoring and sampling system for high-infectivity environment medical treatment |
| CN111717405A (en) * | 2020-06-23 | 2020-09-29 | 长沙航华电子科技有限公司 | Buoyancy auxiliary lifting device for unmanned aerial vehicle |
| CN113044226A (en) * | 2021-05-10 | 2021-06-29 | 浙江采盛环保有限公司 | Unmanned aerial vehicle that can be used to jungle and shoot |
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Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN2210150Y (en) * | 1994-09-06 | 1995-10-18 | 曾宪东 | Aircraft for advertisement |
| GB2297532A (en) * | 1995-02-06 | 1996-08-07 | Peter John Mckay | Hot air balloon |
| DE29722783U1 (en) * | 1997-12-23 | 1998-04-09 | Belovári, Ferenc, 80339 München | Hemispherical airship equipped with a rotating cabin, with its own propulsion |
| CN102050222A (en) * | 2009-11-05 | 2011-05-11 | 刘灵通 | Flying advertising device |
| DE202011050944U1 (en) * | 2011-08-09 | 2011-10-12 | Georg Riha | Floating camera mount for aerial photography |
| CN102542954A (en) * | 2012-02-09 | 2012-07-04 | 北京机械设备研究所 | Fully-automatic aerial display equipment |
| CN102897310A (en) * | 2012-10-26 | 2013-01-30 | 安徽神剑鹏升科技有限公司 | Unmanned small-size floating device |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107628246A (en) * | 2017-07-26 | 2018-01-26 | 青岛万祥如光机械技术研究有限公司 | A kind of unmanned plane line walking device |
| CN107697288A (en) * | 2017-07-26 | 2018-02-16 | 青岛万祥如光机械技术研究有限公司 | A kind of energy-saving unmanned plane |
| CN109110139A (en) * | 2018-09-07 | 2019-01-01 | 佛山皖和新能源科技有限公司 | A kind of novel unmanned plane auxiliary lifting device |
| CN111645854A (en) * | 2020-03-30 | 2020-09-11 | 上海交通大学医学院附属瑞金医院 | Unmanned aerial vehicle monitoring and sampling system for high-infectivity environment medical treatment |
| CN111645854B (en) * | 2020-03-30 | 2022-04-15 | 上海交通大学医学院附属瑞金医院 | Unmanned aerial vehicle monitoring and sampling system for high-infectivity environment medical treatment |
| CN111717405A (en) * | 2020-06-23 | 2020-09-29 | 长沙航华电子科技有限公司 | Buoyancy auxiliary lifting device for unmanned aerial vehicle |
| CN113044226A (en) * | 2021-05-10 | 2021-06-29 | 浙江采盛环保有限公司 | Unmanned aerial vehicle that can be used to jungle and shoot |
| CN113044226B (en) * | 2021-05-10 | 2022-05-13 | 陕西星汉智维科技有限公司 | Unmanned aerial vehicle that can be used to jungle and shoot |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161123 |