CN107140174A - Extreme low-altitude floatoblast - Google Patents
Extreme low-altitude floatoblast Download PDFInfo
- Publication number
- CN107140174A CN107140174A CN201610141480.2A CN201610141480A CN107140174A CN 107140174 A CN107140174 A CN 107140174A CN 201610141480 A CN201610141480 A CN 201610141480A CN 107140174 A CN107140174 A CN 107140174A
- Authority
- CN
- China
- Prior art keywords
- lift
- statocyst
- capsule
- gas bottle
- cockpit
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/60—Gas-bags surrounded by separate containers of inert gas
Abstract
A kind of extreme low-altitude floatoblast.It is made up of cockpit and statocyst and lift capsule, is set in cockpit and is provided with air inlet pipe and exhaust tube on the helium that appropriate pressure is filled in a gas bottle, gas bottle, gas bottle, and connected with the lift capsule being arranged at the top of cockpit；One catch net is set, statocyst is constrained in catch net, catch net rope is connected with cockpit；The volume of statocyst is fixed, and its lift produced is certain, and helium is filled with after statocyst, and the lift that statocyst is produced is slightly less than the gravity produced by whole device；Open the valve for the air inlet pipe being arranged on gas bottle, helium appropriate in gas bottle is slowly filled with lift capsule through air inlet pipe, with the increase of lift capsule volume, the volume that lift capsule arranges air also increases therewith, the lift that statocyst and lift capsule are produced jointly will be increased progressively, and whole device will be moved upwards；Conversely, whole device will be moved downward.And the lift that statocyst and lift capsule are produced jointly, when reaching balance, whole device will hover in aerial.
Description
Technical field
The present invention relates to a kind of helium air bag for being freely lifted or hovering in extreme low-altitude scope, belong to aircraft field.
Background technology
The helium that the lift-off principle of existing dirigible mainly uses the ratio atmospheric density being filled with airship envelope small arranges air and obtained
Lift so that dirigible goes up to the air.After dirigible lift-off, due to being limited by the buoyancy for the helium being filled with air bag, when the weight of dirigible
Amount is when changing, the consumption of such as fuel oil and when causing dirigible weight saving, to keep balance, it has to by the helium in air bag
Drain a part, and the resource of helium is more rare, price costly, therefore, can greatly increase cost.
The content of the invention
In order to solve the above problems, the present invention provides a kind of extreme low-altitude floatoblast, and it can not only keep floatoblast at any time in extreme low-altitude model
Interior balance is enclosed, and the helium being also possible that in air bag will not lose, and greatly reduce the cost of flight.
The technical solution adopted for the present invention to solve the technical problems is：Extreme low-altitude floatoblast is made up of cockpit and statocyst and lift capsule,
Set in cockpit and be provided with air inlet pipe and exhaust tube on the helium that appropriate pressure is filled in a gas bottle, gas bottle, gas bottle,
Be connected in air inlet pipe and exhaust tube on valve, exhaust tube and be also associated with light duty compressor, and by air inlet pipe and exhaust tube with
It is arranged on the lift capsule connection at the top of cockpit；To improve security, a catch net is set, statocyst is constrained in catch net,
Catch net rope is connected with cockpit；The volume of statocyst is fixed, and its lift produced is certain, and helium is filled with after statocyst,
The lift that statocyst is produced is slightly less than the gravity produced by whole device；The valve for the air inlet pipe being arranged on gas bottle is opened, will
Appropriate helium is slowly filled with lift capsule through air inlet pipe in gas bottle, with the increase of lift capsule volume, and lift capsule arranges air
Volume also increases therewith, according to Archimedes' principle, and the lift that statocyst and lift capsule are produced jointly will be increased progressively, whole dress
Put to move upwards；Conversely, when the helium in lift capsule is withdrawn into gas bottle, the lift that statocyst and lift capsule are produced jointly
To progressively it reduce, whole device will be moved downward.And the lift that statocyst and lift capsule are produced jointly is when reaching balance, whole dress
Putting will hover in aerial.
The beneficial effects of the invention are as follows lift capsule is when controlling whole device to rise, decline and hovering, it is not necessary to consume fuel.
Brief description of the drawings
The present invention is further described below in conjunction with the accompanying drawings.
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the structural representation of cockpit of the present invention.
1. catch net in figure, 2. statocysts, 3. lift capsules, 4. cockpits, 5. gas bottles, 6. air inlet pipe, 7. exhaust tubes.
Embodiment
Extreme low-altitude floatoblast is made up of cockpit (4) and statocyst (2) and lift capsule (3), and a gas bottle is set in cockpit (4)
(5), filled in gas bottle (5) and be provided with air inlet pipe (6) and exhaust tube (7) on the helium of appropriate pressure, gas bottle (5),
Valve is connected in air inlet pipe (6) and exhaust tube (7), and air inlet pipe (6) and exhaust tube (7) is present with setting
Lift capsule (3) connection at the top of cabin (4)；To improve security, a catch net (1) is set, statocyst (2) is constrained
In catch net (1), catch net (1) is connected with rope with cockpit (4)；The volume of statocyst (2) is fixed, and it is produced
Lift it is certain, helium is filled with after statocyst (2), the lift that statocyst (2) is produced is slightly less than produced by whole device
Gravity；Opening is arranged on the valve of the air inlet pipe (6) on gas bottle (5), by helium appropriate in gas bottle (5) through air inlet
Pipe (6) is slowly filled with lift capsule (3), and with the increase of lift capsule (3) volume, lift capsule (3) arranges the volume of air
Also increase therewith, according to Archimedes' principle, the lift that statocyst (2) and lift capsule (3) are produced jointly will be increased progressively,
Whole device will be moved upwards；Conversely, when the helium in lift capsule (3) is withdrawn into gas bottle (5), statocyst (2) and
The lift that lift capsule (3) is produced jointly will progressively reduce, and whole device will be moved downward；And statocyst (2) and lift capsule (3)
When the lift produced jointly reaches balance, whole device will hover in aerial.
Claims (5)
1. a kind of extreme low-altitude floatoblast, it is characterized in that；It constitutes by cockpit and statocyst and lift capsule.
2. extreme low-altitude floatoblast according to claim 1, it is characterized in that：The helium that appropriate pressure is filled in one gas bottle, gas bottle is set in cockpit.
3. extreme low-altitude floatoblast according to claim 1, it is characterized in that；Lift capsule is arranged at the top of cockpit.
4. extreme low-altitude floatoblast according to claim 1, it is characterized in that；Statocyst is constrained in catch net.
5. extreme low-altitude floatoblast according to claim 1, it is characterized in that；The volume of statocyst is fixed, and its lift produced is slightly less than the gravity produced by whole device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610141480.2A CN107140174A (en) | 2016-03-01 | 2016-03-01 | Extreme low-altitude floatoblast |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610141480.2A CN107140174A (en) | 2016-03-01 | 2016-03-01 | Extreme low-altitude floatoblast |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107140174A true CN107140174A (en) | 2017-09-08 |
Family
ID=59783446
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610141480.2A Pending CN107140174A (en) | 2016-03-01 | 2016-03-01 | Extreme low-altitude floatoblast |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107140174A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19904278A1 (en) * | 1999-02-03 | 2000-08-10 | Franz Hegele | Dirigible of penguin shape lifted by hydrogen gas has an outer zone filled with non combustible helium gas |
| CN1378949A (en) * | 2001-04-06 | 2002-11-13 | 刘春桥 | Lifting airship |
| CN101723092A (en) * | 2008-10-24 | 2010-06-09 | 刘永强 | Man-powered aircraft |
| CN102275634A (en) * | 2010-06-10 | 2011-12-14 | 渠仁书 | High-altitude entertainment device |
| CN104859834A (en) * | 2015-05-20 | 2015-08-26 | 王树强 | Low-energy-consumption fast controllable-change static ascending and descending device |
| CN205010464U (en) * | 2015-09-28 | 2016-02-03 | 东莞前沿技术研究院 | Aerostatics and utricule structure thereof |
-
2016
- 2016-03-01 CN CN201610141480.2A patent/CN107140174A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19904278A1 (en) * | 1999-02-03 | 2000-08-10 | Franz Hegele | Dirigible of penguin shape lifted by hydrogen gas has an outer zone filled with non combustible helium gas |
| CN1378949A (en) * | 2001-04-06 | 2002-11-13 | 刘春桥 | Lifting airship |
| CN101723092A (en) * | 2008-10-24 | 2010-06-09 | 刘永强 | Man-powered aircraft |
| CN102275634A (en) * | 2010-06-10 | 2011-12-14 | 渠仁书 | High-altitude entertainment device |
| CN104859834A (en) * | 2015-05-20 | 2015-08-26 | 王树强 | Low-energy-consumption fast controllable-change static ascending and descending device |
| CN205010464U (en) * | 2015-09-28 | 2016-02-03 | 东莞前沿技术研究院 | Aerostatics and utricule structure thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11124282B2 (en) | Bionic stratospheric airships | |
| CN201385779Y (en) | Inflatable rigid airship with rigid structure | |
| CN104417743A (en) | Bag body telescopic stratospheric airship | |
| CN102673771B (en) | Air floating aircraft with variable configuration | |
| CN105836096B (en) | Aerostatics platform and its assembly method based on Euler's body | |
| CN107150788A (en) | A kind of Fixed Wing AirVehicle for producing greater lift | |
| GB2483993A (en) | Membrane of gas envelopes of airships and balloons | |
| CN107140174A (en) | Extreme low-altitude floatoblast | |
| CN203975214U (en) | A kind of system of wafing that flies of utilizing natural wind motion | |
| CN205387191U (en) | Empty aircraft annular ballonet floats | |
| Voloshin et al. | Aerodynamic characteristics study and possible improvements of MAAT feeder airships | |
| CN105015754A (en) | Flying system moving by natural wind | |
| CN205770141U (en) | Many rotor wing unmanned aerial vehicles are used in a kind of wide water surface water sampling sky land and water three | |
| CN103950533A (en) | Thermal insulation airship | |
| CN201793013U (en) | Automatic inflatable balloon and hot balloon parachute | |
| CN204137318U (en) | A kind of dirigible utilizing the lifting of two gas cabins | |
| CN203601557U (en) | Aerostat pressure regulator allowing aerostat to be deflated through manual intervention | |
| CN106167091A (en) | Inflation rotor wing unmanned aerial vehicle | |
| CN109319083A (en) | A kind of axis change soft lighter-than-air flight device of buoyancy | |
| CN102514706B (en) | Aerostat descending with opening facing wind | |
| CN207173980U (en) | A kind of parachute | |
| CN202783781U (en) | Water-land takeoff and landing amphibious aircraft with inflatable cushion and paraglider | |
| CN205239888U (en) | Multipurpose dirigible of helium for promoting power is used to environment -friendly | |
| CN101885379A (en) | Automatically inflatable balloon and hot air balloon parachute | |
| CN202464117U (en) | Aerostat with windward opening to descend |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | 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 |
Application publication date: 20170908 |
|
| WD01 | Invention patent application deemed withdrawn after publication |