CN2317172Y - Aircraft - Google Patents
Aircraft Download PDFInfo
- Publication number
- CN2317172Y CN2317172Y CN 98236688 CN98236688U CN2317172Y CN 2317172 Y CN2317172 Y CN 2317172Y CN 98236688 CN98236688 CN 98236688 CN 98236688 U CN98236688 U CN 98236688U CN 2317172 Y CN2317172 Y CN 2317172Y
- Authority
- CN
- China
- Prior art keywords
- air chamber
- delivering pipeline
- air
- main air
- utility
- 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 relates to an aircraft. A layer of thin aluminium sheet, an outer layer of which is cover on a rigidity framework, is divided into an air chamber and a loading chamber by partition boards; the inner part of the air chamber is provided with one layer of vacuum cotton and thin film sealing layers along the rigidity framework; the lower part of the partition boards is provided with main gas transmitting pipes; the main gas transmitting pipes are respectively communicated with the air chamber and a plurality of balloons which are arranged inside the air chamber. The utility model has the advantages of simple structure, flexible operation, safety, low cost, etc. and is suitable for aerial transit.
Description
The utility model relates to a kind of aircraft.
At present, airborne aircraft such as fire balloon, dirigible, awing owing to be subjected to technical limitation, awing can't widespread use, fire balloon is by the gas combustion apparatus burning heat air that is provided with on the gondola airbag aeration to be risen.The driving and the energy resource consumption of fire balloon are undesirable, and have the danger of fire.Airship, current airship, small-sized manufacturing value of service is not high, only limits to market such as airship advertisement and uses, and is used for transportation, rescue and relief work etc. and is air dreadnought and have to be worth than large-scale commerce, and air dreadnought is bulky, the construction costs height, and mostly be cases of otherwise standard design.
It is a kind of simple in structure that the purpose of this utility model is to provide, and cost is low, safe and reliable airborne aircraft.
In order to achieve the above object, the utility model is by dividing plate skin to be covered one deck thin aluminum sheet that covers on the rigid backbone to be divided into air chamber and to carry storehouse two parts, in air chamber, be provided with one deck vacuum cotton and thin film encapsulation layers along rigid backbone, be provided with main air delivering pipeline at the lower partition, main air delivering pipeline is connected with a plurality of balloons of air chamber and interior setting thereof respectively.
The utility model has the advantages that:
(1) simple in structure, cost is low, and is safe and reliable;
(2) this product operation is flexible, can be used for transportation.
Description of drawings:
Fig. 1 is a structural representation of the present utility model.
Below in conjunction with accompanying drawing embodiment of the present utility model is described in further detail.
As shown in Figure 1, the utility model is by dividing plate 8 skin to be covered one deck thin aluminum sheet 2 that covers on the rigid backbone 1 to be divided into air chamber 5 and to carry storehouse 9 two parts, in air chamber 5, be provided with one deck vacuum cotton 3 and thin film encapsulation layers 4 along rigid backbone 1, be provided with main air delivering pipeline 12 in dividing plate 8 bottoms, main air delivering pipeline 12 is connected with a plurality of balloons 6 of air chamber 5 and interior setting thereof respectively.
Described rigid backbone 1 lower end is provided with runner 10.
Described main air delivering pipeline 12 1 ends are provided with by-pass valve control 13.
Described air chamber 5 and balloon 6 admission ports and main air delivering pipeline 12 joints are provided with valve 7 and air-pressure gauge 11.
Described air chamber and main air delivering pipeline joint also are provided with by-pass valve control and air-pressure gauge.
The utility model be with a plurality of balloons and air chamber behind main air delivering pipeline input hydrogen, closing control valve starts to be located at the air generation plants of wing both sides simultaneously, this aircraft in transit will safety and reliability.
Claims (4)
1, a kind of airborne aircraft, form by balloon, air delivering pipeline, it is characterized in that: by dividing plate (8) skin is covered one deck thin aluminum sheet (2) that covers on the rigid backbone (1) and be divided into air chamber (5) and carry storehouse (9) two parts, in air chamber (5), be provided with one deck vacuum cotton (3) and thin film encapsulation layers (4) along rigid backbone (1), be provided with main air delivering pipeline (12) in dividing plate (8) bottom, main air delivering pipeline (12) is connected with a plurality of balloons (6) of air chamber (5) and interior setting thereof respectively.
2, according to the described airborne aircraft of claim 1, it is characterized in that: rigid backbone (1) lower end is provided with runner (10).
3, according to the described airborne aircraft of claim 1, it is characterized in that: main air delivering pipeline (12) one ends are provided with by-pass valve control (13).
4, according to the described airborne aircraft of claim 1, its feature is being done: air chamber (5) and balloon (6) admission port and main air delivering pipeline (12) joint are provided with valve (7) and air-pressure gauge (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 98236688 CN2317172Y (en) | 1998-02-18 | 1998-02-18 | Aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 98236688 CN2317172Y (en) | 1998-02-18 | 1998-02-18 | Aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2317172Y true CN2317172Y (en) | 1999-05-05 |
Family
ID=33984673
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 98236688 Expired - Fee Related CN2317172Y (en) | 1998-02-18 | 1998-02-18 | Aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2317172Y (en) |
-
1998
- 1998-02-18 CN CN 98236688 patent/CN2317172Y/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |