CN1254054A - Fuel supplying device for airship - Google Patents
Fuel supplying device for airship Download PDFInfo
- Publication number
- CN1254054A CN1254054A CN 98114452 CN98114452A CN1254054A CN 1254054 A CN1254054 A CN 1254054A CN 98114452 CN98114452 CN 98114452 CN 98114452 A CN98114452 A CN 98114452A CN 1254054 A CN1254054 A CN 1254054A
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- CN
- China
- Prior art keywords
- gas
- air bag
- pump
- fuel
- airship
- 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
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- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
The present invention discloses a fuel supply device for airship, including gas bag, fuel gas which is charged into said air bag, sucking pump and pipeline for conveying gas, and is characterized by that the above-mentioned fuel gas is charged into the internal gas bag of the airship which possesses internal and external two layers of gas bags, the gas-conveying pipe is led out from the internal gas bag, passed through the external gas bag and connected with pump, and the pump is connected with engine by means of gas-conveying pipe. In the course of flying, when the airship has need of fuel gas, the pump can pump the fuel gas, through the pipeline, feed the fuel gas into the engine so as to implement fuel supply.
Description
The present invention relates to the air transportation field, exactly is a kind of fuel supply device of dirigible.
At present, the dirigible of using is to rely on the liquid fuel that stores in the fuel tank, offers engine combustion, makes it send power and promotes that dirigible advances.But this device also has significant disadvantages, that is exactly that the weight that has of liquid fuel self will take dirigible, this dependence aerostatic buoyancy, the means of transportation that could aloft fly can produce extremely limited lifting capacity, thereby has limited the raising of the usability of dirigible.
The purpose of this invention is to provide a kind of fuel supply device that does not take the limited lifting capacity of dirigible.
Technological scheme of the present invention is such: it comprises air bag and charges into the pipeline of inflammable gas, the pump that is used to bleed and gas transmission in this air bag, it is characterized in that: described inflammable gas charges in the interior air bag with inside and outside double-layer air bag of dirigible, draw pneumatic tube from interior air bag, pass outer air bag and link to each other with pump, pump links to each other with motor by pneumatic tube.
During use, inflammable gas is extracted out, by pipeline, be sent in the motor, for its use with pump.
After the present invention realized, the inflammable gas that charges in its air bag was as hydrogen, its density is littler than air, not only can produce certain buoyancy, but also can be used as fuel, so just can carry liquid fuel less, and burn the pollutant of gaseous fuel generation and lack than burning liquid fuel.
The present invention compared with prior art has practicability more widely after realizing, and reduces the consumption of oil and the environmental pollution of complying with.
Face is done explanation in further detail in conjunction with Figure of description to the embodiment of the invention:
Fig. 1 is a structural representation of the present invention.
As shown in Figure 1, the framework 13 that is connected to a fixed by the scalable air bag 12 of drum shape of the pipeline 10 of supporting post 1, hydrogen 2, interior air bag 3, helium 4, outer air bag 5, the pipeline 6 of discharging ballast, the container 7 that stores ballast, the pump 8 of bleeding, motor 9, gas transmission, ballast 11, the setting of outer air bag upper surface, with supporting post of the present invention is formed.
The present invention is provided support by the dirigible of the double-layer air bag in the prior art, the concrete practice is: in existing having, on the dirigible of outer air bag hydrogen charged in the interior air bag among the framework that is connected to a fixed with supporting post, in helium charged into, in the space that outer air bag forms, in use, along with hydrogen is drawn out of, the volume of interior air bag will constantly reduce, utricule will shrink and become flat, outer air bag upper surface should be provided with outer air bag and communicate, the capsule skin is corrugated, profile be drum shape with the telescopic air bag of gasbag pressure size, be beneficial to correspondingly the reduced volume use of being convenient to match with interior air bag.
The inflammable gas of being mentioned in the technical solution of the present invention is methane or can be rock gas also;
When bleeding, should discharge ballast with the corresponding weight of institute's gas bleeding generation buoyancy value itself;
The motor of mentioning among the present invention can be an internal-combustion engine, also can be fuel cell and motor combination.
Claims (1)
- A kind of fuel supply device of dirigible: it comprises air bag and charges into the inflammable gas of this air bag, the pump that is used to bleed and the pipeline of gas transmission, it is characterized in that: described inflammable gas charges in the interior air bag with inside and outside double-layer air bag of dirigible, draw pneumatic tube from interior air bag, pass outer air bag and link to each other with pump, pump links to each other with motor by pneumatic tube.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 98114452 CN1254054A (en) | 1998-11-12 | 1998-11-12 | Fuel supplying device for airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 98114452 CN1254054A (en) | 1998-11-12 | 1998-11-12 | Fuel supplying device for airship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1254054A true CN1254054A (en) | 2000-05-24 |
Family
ID=5224113
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 98114452 Pending CN1254054A (en) | 1998-11-12 | 1998-11-12 | Fuel supplying device for airship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1254054A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103094591A (en) * | 2013-01-25 | 2013-05-08 | 北京航空航天大学 | High-efficiency gas storage system applied to regenerative fuel cell of aerostat |
| CN104943845A (en) * | 2015-07-21 | 2015-09-30 | 中国科学院光电研究院 | Hydrogen energy source airship |
| CN105836096A (en) * | 2016-02-29 | 2016-08-10 | 上海交通大学 | Euler-body-based aerostat platform and assembly method thereof |
| CN106553746A (en) * | 2015-09-28 | 2017-04-05 | 东莞前沿技术研究院 | Aerostatics and its utricule structure |
| CN107031810A (en) * | 2017-01-13 | 2017-08-11 | 李宝军 | Gasbag-type hovering flight device |
| CN110550178A (en) * | 2019-08-13 | 2019-12-10 | 中国地质大学（武汉） | Mixed gas aerostat |
| CN113148101A (en) * | 2021-03-04 | 2021-07-23 | 邵明杰 | Small unmanned airship using hydrogen-helium hybrid energy |
-
1998
- 1998-11-12 CN CN 98114452 patent/CN1254054A/en active Pending
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103094591A (en) * | 2013-01-25 | 2013-05-08 | 北京航空航天大学 | High-efficiency gas storage system applied to regenerative fuel cell of aerostat |
| CN103094591B (en) * | 2013-01-25 | 2015-07-29 | 北京航空航天大学 | Be applied to the efficient gas storage system of the regeneratable fuel cell of aerostatics |
| CN104943845A (en) * | 2015-07-21 | 2015-09-30 | 中国科学院光电研究院 | Hydrogen energy source airship |
| CN106553746A (en) * | 2015-09-28 | 2017-04-05 | 东莞前沿技术研究院 | Aerostatics and its utricule structure |
| CN105836096A (en) * | 2016-02-29 | 2016-08-10 | 上海交通大学 | Euler-body-based aerostat platform and assembly method thereof |
| CN107031810A (en) * | 2017-01-13 | 2017-08-11 | 李宝军 | Gasbag-type hovering flight device |
| CN110550178A (en) * | 2019-08-13 | 2019-12-10 | 中国地质大学（武汉） | Mixed gas aerostat |
| CN113148101A (en) * | 2021-03-04 | 2021-07-23 | 邵明杰 | Small unmanned airship using hydrogen-helium hybrid energy |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |